Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 1(195)

Enclosure 2 – Description of GFE Aircrafts

1 GFE Aircraft Learjet LR35A ...... 4 1.1 Learjet LR35A Aircraft Maintenance Program ...... 4 1.1.1 Comprehensive description of Learjet Maintenance Program (MM-99) ...... 4 1.1.2 Modifications that affects the maintenance program ...... 5 1.1.3 Airframe Maintenance Documentation ...... 5 1.1.4 Engine Maintenance Documentation ...... 5 1.1.5 Maintenance Tasks related to changes ...... 6 1.1.6 Guiding documents issued by the Agency and Aviation Authority for both Airframe and Engines: ...... 6 1.2 GFE Aircraft Learjet 35A SE-DHO...... 7 1.2.1 Aircraft Specification ...... 7 1.2.2 Engines ...... 7 1.2.3 Avionics ...... 7 1.2.4 Mission System ...... 8 1.2.5 Mission Cable Harness to Hard Points ...... 9 1.2.6 Antenna layout ...... 10 1.2.7 Inspection due times and dates ...... 11 1.2.8 Implemented Changes ...... 12 1.3 GFE Aircraft Learjet 35A SE-DHP ...... 28 1.3.1 Aircraft Specification ...... 28 1.3.2 Engines ...... 28 1.3.3 Avionics ...... 28 1.3.4 Mission System ...... 29 1.3.5 Mission Cable Harness to Hard Points ...... 30 1.3.6 Antenna layout ...... 30 1.3.7 Inspektion due times and dates ...... 31 1.3.8 Implemented Changes ...... 32 2 GFE Aircraft Mitsubishi MU-2 ...... 47 2.1 Mitsubishi MU-2 Aircraft Maintenance Program ...... 47 2.1.1 Comprehensive description of Mitsubishi Maintenance Requirements Manual (MR-0178-2): ...... 47 2.1.2 Modifications that affects the maintenance program ...... 47 2.1.3 Maintenance Documentation ...... 48 2.1.4 Guiding documents to be used during maintenance: ...... 48 2.1.5 Maintenance Tasks related to changes ...... 48 2.1.6 Guiding documents issued by the Agency and Aviation Authority for both Airframe and Engines: ...... 49 2.2 GFE Aircraft Mitsubishi MU-2 SE-GHA ...... 50 2.2.1 Aircraft Specification ...... 50 2.2.2 Engines ...... 50 2.2.3 Propeller ...... 50 2.2.4 Avionics ...... 50

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 2(195) 2.2.5 Mission System ...... 51 2.2.6 Mission Cable Harness to Hard Points ...... 51 2.2.7 Antenna Layout ...... 52 2.2.8 Inspection due times and dates ...... 53 2.2.9 Implemented Changes ...... 54 2.3 GFE Aircraft Mitsubishi MU-2 SE-GHB ...... 75 2.3.1 Aircraft Specification ...... 75 2.3.2 Engines ...... 75 2.3.3 Propeller ...... 75 2.3.4 Avionics ...... 75 2.3.5 Mission System ...... 76 2.3.6 Mission Cable Harness to Hard Points ...... 76 2.3.7 Antenna Layout ...... 77 2.3.8 Inspection due times and dates ...... 78 2.3.9 Implemented Changes ...... 79 2.4 GFE Aircraft Mitsubishi MU-2 SE-GHD ...... 99 2.4.1 Aircraft Specification ...... 99 2.4.2 Engines ...... 99 2.4.3 Propeller ...... 99 2.4.4 Avionics ...... 99 2.4.5 Mission System ...... 100 2.4.6 Mission Cable Harness to Hard Points ...... 100 2.4.7 Antenna Layout ...... 101 2.4.8 Inspection due times and dates ...... 102 2.4.9 Implemented Changes ...... 103 2.5 GFE Aircraft Mitsubishi MU-2 SE-GHF ...... 123 2.5.1 Aircraft Specification ...... 123 2.5.2 Engines ...... 123 2.5.3 Propeller ...... 123 2.5.4 Avionics ...... 123 2.5.5 Mission System ...... 124 2.5.6 Mission Cable Harness to Hard Points ...... 124 2.5.7 Antenna Layout ...... 125 2.5.8 Inspection due times and dates ...... 126 2.5.9 Implemented Changes ...... 127 2.6 GFE Aircraft Mitsubishi MU-2 SE-IOV ...... 147 2.6.1 Aircraft Specification ...... 147 2.6.2 Engines ...... 147 2.6.3 Propeller ...... 147 2.6.4 Avionics ...... 147 2.6.5 Mission System ...... 148 2.6.6 Mission Cable Harness to Hard Points ...... 148 2.6.7 Antenna Layout ...... 149 2.6.8 Inspection due times and dates ...... 150 2.6.9 Implemented Changes ...... 151 2.7 GFE Aircraft Mitsubishi MU-2 SE-IUA ...... 171

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 3(195) 2.7.1 Aircraft Specification ...... 171 2.7.2 Engines ...... 171 2.7.3 Propeller ...... 171 2.7.4 Avionics ...... 171 2.7.5 Mission System ...... 172 2.7.6 Mission Cable Harness to Hard Points ...... 172 2.7.7 Antenna Layout ...... 173 2.7.8 Inspection due times and dates ...... 174 2.7.9 Implemented Changes ...... 175

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 4(195)

1 GFE Aircraft Learjet LR35A

1.1 Learjet LR35A Aircraft Maintenance Program

1.1.1 Comprehensive description of Learjet Maintenance Program (MM-99) The maintenance is (according to Learjet Maintenance Manual MM-99) based on 24 Phase Inspections, accomplished one at a time, in groups or collectively, as scheduled by the aircraft operator and in accordance with allowable inspection tolerances. Estimated utilization is 500 Hrs per A/C and year. Each Phase Inspection is contained within one of four (1 of 4) hourly or calendar driven inspection intervals, the 300 hour or 12 month A-Phases, 600 hour or 24 month B-Phases, 1200 hour or 48 month C-Phases and 2400 hour or 96 month D-Phases. Each of the primary inspection intervals (A, B, C, and D) contains six (6) stand-alone Phase Inspections.

Inspection list according to Learjet maintenance Manual MM-99: • Phase A2 300 hrs Inspection / Checks. • Phase A3 300 hrs Inspection / Checks. • Phase A4 300 hrs Inspection / Checks. • Phase A5 300 hrs Inspection / Checks. • Phase A6 300 hrs Inspection / Checks • Phase B1 600 hrs Inspection / Checks • Phase B2 600 hrs Inspection / Checks. • Phase B3 600 hrs Inspection / Checks • Phase B4 600 hrs Inspection / Checks. • Phase B5 600 hrs Inspection / Checks. • Phase B6 600 hrs Inspection / Checks. • Phase C1 1200 hrs Inspection / Checks. • Phase C2 1200 hrs Inspection / Checks • Phase C3 1200 hrs Inspection / Checks • Phase C4 1200 hrs Inspection / Checks. • Phase C5 1200 hrs Inspection / Checks • Phase C6 1200 hrs Inspection / Checks. • Phase D1 2400 hrs Inspection / Checks. • Phase D2 2400 hrs Inspection / Checks • Phase D3 2400 hrs Inspection / Checks • Phase D4 2400 hrs Inspection / Checks • Phase D5 2400 hrs Inspection / Checks. • Phase D6 2400 hrs Inspection / Checks. • 3000 Landings Inspections. • Major Landing Inspections. • 12 Year Airframe Inspections

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 5(195) • 12000 Hours Airframe Inspections. • Other Interval Inspections. • Unscheduled Maintenance Checks. • MPI Engine Zone Inspection. • Engine Light Maintenance TFE731-2.

1.1.2 Modifications that affects the maintenance program • The wings have been modified with hard points to carry ECM pods and outboard winches. • The R/H wing tip tank has been modified with tip radome covering antennas for an inboard ECM system ASTOR. • To supply the ECM equipment with 3-phase AC, one 3kVA inverter system has been installed in the inboard aft baggage area. (FAA STC SA125NE). • Operator Stand is installed in the cabin with equipment to control winches and ECM units. Set of monitoring equipment as TV-camera, mirrors etc. • Aft Body Strakes in accordance with AVCON STC ST00432WI (EASA/LBA TA0112) have been installed. • Alteration between Dual / Single Mid Fuselage Camera Pods and Structural Plugs in accordance with AVCON STC SA2479CE (EASA.IM.A.S.01449).

1.1.3 Airframe Maintenance Documentation Maintenance of the airframe is conducted according to the following documentation: • Learjet Maintenance Manual. MM-99 • Learjet Wiring Manual. WM-99 • Learjet Illustrated Parts Catalogue. • Learjet Service Bulletins. • Learjet Airplane Accessory Kit. • Learjet Airplane Modification Kit. • Learjet Structural Repair Manual. • Learjet Non-Destructive Inspection Manual. • Keith TR-134 System Service Manual. TR-134. • Saab AB, Technical Directives-Modification, issued by DOA EASA 21J.108. Continued Airworthiness.

1.1.4 Engine Maintenance Documentation Maintenance of the engines is conducted according to the following documentation: • Honeywell TFE731 Light Maintenance Manual. 72-02-01 • Honeywell TFE731 Illustrated Pars Catalogue. 72-00-71. • Honeywell TFE731 Service Bulletin for Service Life Limits of Critical Life Limited Components. SB TFE731-72-3001. • Honeywell TFE731 Service Bulletins. • Honeywell TFE731 Service Information Letters.

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 6(195)

1.1.5 Maintenance Tasks related to changes The following maintenance tasks are not included in the aircraft manufactures’ maintenance manual. The tasks are included in the operators AMP: • Structural Plugs in Cabin Annual/300 hrs Inspection/Checks • Operator’s Consol. Annual/300 hrs Inspection/Checks • Mission Power Annual/300 hrs Inspection/Checks • Mission Power 600 hrs Inspection/Checks • Mission Power 1200 hrs Inspection/Checks • ACAS II. 24 Months Inspection/Checks • Special Operational Fatigue Inspection 1200 hrs Inspection/Checks • Hard Points and ejection unit 300 Hrs Inspection

1.1.6 Guiding documents issued by the Agency and Aviation Authority for both Airframe and Engines: • FAA Airworthiness Directives. • Swedish NAA LVD. • EASA AD. • EC 2042/2003 Annex II Part-145- AMC. & Guidance Material. • BCL - C, -D, -M if operating under Swedish regulations • EASA Series-OPS

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 7(195)

1.2 GFE Aircraft Learjet 35A SE-DHO

1.2.1 Aircraft Specification Type: Serial Registration : Airframe Total Date Number: total Hours: Landing Reference: Cycles: Learjet 195 SE-DHO 13320 8780 2012-11-23 35A

1.2.2 Engines Type: TFE731 -2-2B Serial Total Hours Total Hours Hours Number: Since New: Cycles remaining to remaining to Since New: MPI: CZI: Left Engine P-74278 11122 7392 928 922 Right Engine P-74583 10648 7406 179 170

1.2.3 Avionics System: Type / Part Number: Note: Autopilot JET FC 200 Dual VHF-COM Collins VHF-22C HF-COM Collins 718U-5 ICS & Audio System DB System Dual VHF -NAV Collins VIR -30A GPS Garmin GPS 165 TSO Dual DME Collins DME40 ADF 1 Bendix/King KDF-805 XPDR 1 & 2 Collins TDR94D Mode S EHS TCAS II Collins TCAS-4000 Dual TCAS II VSI/RA/TA Indicator Collins TVI-920 TAWS / EGPWS Honeywell MK VI II RDR ALT Collins ALT -55B Weather Radar Honeywell Primus 400 MFD Display Honeywell MFRD ELT Kanad ELT 406-AF-H Dual Mach Airspeed indicator IDC 2680003-2 Altimeter incl. encoder LH IDC 518-16007-187 Altimeter RH IDC 23932 -053 Altitude Report & Alerting System IDC 23989 -011 Air Data Display Unit 9D-80130-32 Dual Flight Director Indicator Collins 329B-7R-2

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 8(195) Dual VG-Gyro JET VG-206(XX) Standby Altitude Gyro JET AI 804 Dual Horizontal Situation Indicator Collins 331A-6R Dual RMI Collins 332C-10 Dual DG -Gyro JET DN -101D RVSM FDR Sundstrand 980-4100-FWUS CVR Fairchild 93-A100-83

1.2.4 Mission System System: Description: Fixed general installations FR31 VHF/UHF COM Radio AN/ARC 182 VHF/UHF COM Radio GPS MAP System JET SI -3003B Inverter 115/200VAC 400Hz 3 phase KGS SPS -3052B Inverter 230VAC 50Hz Laser Prism Wing Pylon NATO 14” Alcon Ejector Unit LH and RH Wing Pylon EW system ASTOR Fixed installed system ADRIAN C & S Pod mounted system U95 -N Pod mounted system U95-D2 Pod mounted system U95 Sorc Pod mounted system A100 Pod mounted system Missile Threat Simulator DARTS Pod mounted system GMS Pod mounted system Chaff Dispenser BOX 3 Pod mounted system Target Towing MTR 101 Outboard pod mounted winch AS200 MDI (Miss Distance Indicator) TLX Height keeping target Precisions GPS Pos System TAPS

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 9(195)

1.2.5 Mission Cable Harness to Hard Points Used for Mission LH NATO Hard point: RH NATO Hard point: Note: System: Adrian C & S, U95-N, General Signal Harness General Signal Harness Two pair shielded U95-D2, U95 Sorc, AWG 20 x 25 A100, DARTS, GMS, BOX 3 and MTR 101 MTR 101 MTR 101 Harness MTR 101 Harness Two pair shielded AWG 20 x 3 AWG 16 x 4 + shield U95-N, U95-D2, U95 MIL-STD-1553B Data MIL-STD-1553B Data Twinax x 8 Sorc, A100 and GMS Bus Bus U95-N, U95-D2, U95 AC Power AC Power 115/200VAC AWG 12 x 10 + Sorc, A100, DARTS, 115/200VAC 400 Hz 3- 400 Hz 3-Phase 3 x 10 A shield GMS and BOX 3 Phase 3 x 10 A Adrian C & S, GMS DC Power 28 VDC 150 DC Power 28 VDC 150 AWG 4 x 4 and BOX 3 A A MTR 101 Coaxial 2 x 75 Ω Coaxial 2 x 75 Ω Adrian C & S Coaxial 3 x 50 Ω Coaxial 3 x 50 Ω Recognition Light Recognition Light Recognition Light Cable AWG 16 x 4 + Cable shield

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 10(195)

1.2.6 Antenna layout

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 11(195)

1.2.7 Inspection due times and dates Status date November 23 rd 2012.

Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date Due Landings Aircraft SE-DHO Phase A 300 hour insp. AMP 2012-07-16 13290 13590,3 2013-09-10 Phase B 600 hour insp. AMP 2011-03-05 13043 13643,3 2013-04-05 Phase C 1200 hour insp. AMP 2009-11-01 12849 14049,1 2013-10-31 Phase D 2400 hour insp. AMP 2009-08-18 12789 15189,6 2017-08-16 Special operational fatigue inspect AMP 2009-01-23 12620 13820,8 12000 Hrs Inspection AMP 2001-08-29 11269 17269,1 45 days insp. AMP 2012-10-19 13303 2012-12-03 6 Month Inspection AMP 2012-07-17 13290 2013-03-11 2 Year Inspection AMP 2011-06-17 13129 2013-07-20 12 Year Airframe inspection AMP 2001-08-28 2013-08-25 13503 MPI engine zone inspecition LH AMP 2009-10-22 12849 14249,1 MPI engine zone inspecition RH AMP 2005-04-12 12053 13453,6 300 Hrs Inspection AMP 2011-10-11 13182 13500 1200 Hrs Inspection AMP 2007-05-15 12440 13640 3000 Landing Inspection AMP 1996-01-24 9000 6000 Major Landing Gear Inspection AMP 1988-10-11 10745 Operator's Console 300h/1y insp. AMP 2012-04-23 13248 13548,8 2013-04-23 ACAS 2 (TCAS) 24month insp. AMP 2011-06-29 13129 2013-07-13 Mission equipment 300 hour insp. AMP 2012-07-19 13290 13590,3 Engine S/N P-74278 Remaining Engine 150 hrs insp. AMP 13431,82 111,34 Engine 300 hrs insp. AMP 13449,1 128,62 Engine 800 hrs insp. AMP 13649,1 328,62 Engine Compressor Zone Insp. AMP 14243,3 922,82 Engine Major Periodic Inspection AMP 14249,1 928,62 Engine S/N P-74583 Remaining Engine 150 hrs insp. AMP 13440,3 119,82 Engine 300 hrs insp. AMP 13471,8 151,32 Engine 800 hrs insp. AMP 13696 375,52 Engine Compressor Zone Insp. AMP 13490,8 170,32 Engine Major Periodic Inspection AMP 13499,9 179,42

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 12(195)

1.2.8 Implemented Changes

Abbreviations: Abbr. Issued by Explanation AAK Learjet Aircraft Accessory Kit AD EASA, FAA Airwortness Directive AMK Learjet Aircraft Mod Kit AW Learjet Accessory Wire LVA LFV Luftvärdighetsanvisning LVD LFV Luftvärdighetsdirektiv SB Keith, Learjet, Nyge Service Bullentin SIL Rockwell Service information letter SSB Nyge and Garmin Sofware SB SSK Learjet Special Spares K it STC Avcon, Flight Int., Keith, Supplement Type Certificate EASA TDM Nyge Tekniskt Direktiv Materiel

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type

2012-12-06

Document number Page 13(195) Status date November 23 rd 2012.

SB/AD etc Rev Subject Document reference Eff. date Rev Compliance Status Remarks Reference

AVCON, Avcon Industries, Inc. AVCON STC R Install. Avcon Fins 31-Mar-2005 R 01-Jul-2005 SA00432WI AVCON STC A Install. Plug of Dual Hatches 30-Jun-2005 A 01-Jul-2005 SA2479CE AVCON STC AFM suppl. increase T/O weight...... 25-Aug-1997 29-Jun-2005 ST00564WI AVCON STC C Increase Takeoff Weight to 19600 11-Mar-2005 C 01-Jul-2005 ST00611WI pounds AVCON STC B Increase Wing/Tip Zero Fuel Weight 28-Nov-1997 B 01-Jul-2005 ST00612WI AVCON STC C Increase Landing Weight to 16000 11-Mar-2005 C 01-Jul-2005 ST00613WI pounds

EASA, European Aviation Safety Agency EASA AD Incorrect transponder altitude 30-Aug-2006 18-Aug-2009 2006-0265 EASA AD Improve EHS Operation HONEYWELL SB MST 25-Aug-2008 01-Dec-2010 N/A N/A by transponder P/N installed 2008-0159 67A-34-56 HONEYWELL SSBMST 67A-SW5 Rev 1 EASA AD IR Mode S Transponder - DHC SB 8-34-243 Rev A 29-Apr-2009 IR 18-Aug-2009 PCW Are in compliance with EASA 2009-0097 Check/Modification EASA AD 2010-0067 AD2009-0097 Ref TDM03-17 DWG ROCKWELL SIL07-1 MF1030064-1 Rev.C EASA AD 1 Mode S Transponder Mod/Repl 30-Sep-2010 1 08-Dec-2010 N/A due to ADC p/n 2009-0173 EASA AD Portable Fire Extinguishers- 25-Nov-2009 07-May-2010 N/A N/A by current P/N installed 2009-0251-E Ident/Repl EASA AD Halon 1211 Fire Extinguishers EASA AD 2009-0278 FFE 15-Dec-2009 07-May-2010 N/A N/A by current P/N installed 2009-0262 Id/Repl ASB26-115 Rev C EASA AD Halon 1211 Fire Extinguishers EASA AD 2009-0262 22-Dec-2009 07-May-2010 N/A N/A by current P/N installed 2009-0278 Id/Repl

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 14(195) EASA AD R1 Mode S Transponder - 11-Jan-2010 R1 10-Mar-2010 N/A due to p/n 2010-0003 Check/Modification EASA AD IR Mode S Transponder -Mod/Repl 06-Oct-2010 IR 08-Dec-2010 N/A by ADC p/n installed 2010-0204 EASA AD KIDDE GRAVINER HAND 10-Sep-2012 2012-0037 OPERATTED FIRE EXTINGUISHER

FAA, U.S, Federal Aviation Administration FAA, U.S AD Donning oxygen masks 22-Nov-2000 20-Feb-2003 Complied with by insert of AFM 2000-24-19 Change 12 FAA, U.S AD Goodyear Flight Eagle Tire Tread LEARJET AW 32-021 01-May-2001 17-May-2001 N/A by s/n on tire 2001-07-11 Separat FAA, U.S AD Prevent erroneous altitude 20-Aug-2001 12-Feb-2009 N/A due to p/n 2001-15-17 interpretatio FAA, U.S AD To prev. structural damage to LEARJET SB 51-03 08-Mar-2004 09-Mar-2004 SB 51-04 previous carried out. 2004-03-08 eng.pylons LEARJET SB 51-04 Rev 5 FAA, U.S AD Detailed inspection of aileron cable. 09-Aug-2005 01-Nov-2005 2005-13-36 FAA, U.S AD Inspection of Tip Tank Flapper LEARJET SB 28-10 13-Sep-2005 14-Sep-2005 Flapper p/n 2323006-802 previously 2005-16-09 Valves Supersedes AD 95-25-03 installed. No further action req. FAA, U.S AD Modify Standby Fuel Pump switches LEARJET SB 28-11 Rev 23-Mar-2007 15-Mar-2007 Previusly complied with. Ref. 2007-04-18 5 Learjet SB 28-11 FAA, U.S AD Unsealed gaps in engine firewall 02-Oct-2007 11-Sep-2007 Previously carried out, ref. SB 54-03 2007-17-17 FAA, U.S AD HP-Turbine Disc replacement. 19-Feb-2008 06-Feb-2008 N/A due to engine model. 2008-02-19 FAA, U.S AD Remove from service ITT Duct 08-Aug-2012 2008-19-12 FAA US AD 74- 3 Transport category airplanes 11-May-2012 08-09 equipped with lavatories FAA, U.S AD To precl. a fail. of the Refr. Cond. Fan LEARJET SB 21-03 11-Dec-2000 20-Jan-1984 78-16-03 Issued 1978-08-17 FAA, U.S AD 1 Aeronca thrust Reversers Suppl to 19-Apr-1982 1 13-Feb-2009 N/A Aeronca Thrust Reversers not 79-08-01 AFM installed FAA, U.S AD Starter assisted airstart 24-Mar-1980 03-Dec-1993 80-06-02 FAA, U.S AD Cabin Main Entrance Upper Door LEARJET AMK79-09 01-May-1980 25-Jun-1980 80-07-09 FAA, U.S AD Airspeed Limitation Placard LEARJET SB 11-03 Rev 28-Aug-1980 19-Aug-1987 80-17-11 A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 15(195) FAA, U.S AD To Prevent loss of Emergency 28-Aug-1980 01-Jan-2003 N/A N/A due to Component p/n 80-18-08 electrical Power...... FAA, U.S AD 1 Motive Flow Valve LEARJET AMK80-07 11-Dec-1980 1 05-Nov-1980 80-19-09 FAA, U.S AD 1 AFM insert LFV LVD1635 Rev A 20-May-1985 1 09-Feb-2006 Checked. Previously complied with. 80-19-11 FAA, U.S AD Cockpit Voice Recorder A100 series 01-Apr-1981 12-Feb-2009 N/A due to model & s/n 81-04-06 FAA, U.S AD To ensure oper. without fuel LFV LVA1748 25-Jun-1981 10-Aug-1981 81-13-07 starvation FAA, U.S AD 2 Stall Warning Accelerometer Check LEARJET SB 27-12 Rev 10-Apr-1986 2 30-May-2007 Överförd till A1 phase insp. Ref. 82-01-05 B LFV LVA1912 Learjet Chpt.5 rev.74 och FAA AMOC från 2005-03-24 FAA, U.S AD Insp.RH Engine Hydraulic Pressure LEARJET SB 29-01 Rev 03-May-1983 12-Apr-1983 83-08-03 Line for Interference. 1 FAA, U.S AD To prevent Aileron/Trim 22-Oct-1984 01-Oct-2009 PCW 84-19-06 Tab Flutter due to failure of the trim tab ctrl system FAA, U.S AD Inspect LH Hydraulic Lines for LEARJET SB 29-02 20-Feb-1987 84-20-06 Interfere superseded by 86-22-05 FAA, U.S AD Airplane Lateral Control FAA, U.S AD 96-19-13 06-Sep-1985 06-Feb-2002 N/A due to config. (STC SA766NW 85-16-04 Characteristics LEARJET AMK83-05 LFV never been installed). LVD2034 FAA, U.S AD Collins HSI & FD indicators 31-Dec-1985 15-Jun-2009 N/A by p/n & s/n 85-22-10 FAA, U.S AD 1 Relocation of Battery Vent Inlet LEARJET SB 24-10 LFV 19-Jan-1988 1 10-Dec-1985 86-05-05 Fitting LVD2046 FAA, U.S AD To prevent of flap operation...... LEARJET AMK86-04 10-Nov-1986 20-Feb-1987 86-22-05 FAA, U.S AD Insp. of Fwd. Eng.Mounts for Cracks LEARJET SB 71-03 Rev 06-Feb-1987 17-Jan-2005 Para.A: see Phase A3 300 hour 87-02-06 1 insp. Para.B: see A/C status RAL FAA, U.S AD Autopilot FC-530 Limitations 09-Mar-1987 12-Feb-2009 N/A due to A/P model 87-04-06 FAA, U.S AD Inspection of Mechanical Prod. C/B's 27-Apr-1987 01-Oct-2009 PCW Ref. Jet East Inc. 25 july 1988 87-06-09 (gammal aircraft logbook) FAA, U.S AD Inspection of Drag Chute Riser LEARJET SB 25-07 Rev 03-Jul-1989 01-Oct-2009 89-12-01 A FAA, U.S AD Replace Texas Instr. Circuit Breakers 30-May-1990 01-Oct-2009 N/A due to type of C/B not installed in 90-09-10 aircraft Ref. Learjet PC. FAA, U.S AD Deactivation of Forward Cabinet and LEARJET SB 33-05 Rev 12-Feb-1991 22-Sep-2009 Post mod SB 33-06A 91-03-08 Overhead Fluoriscent Light Circuits A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 16(195) FAA, U.S AD SYSTEM TUBE (W-IN 30D) LEARJET AMK90-05 17-Nov-1992 17-Jun-1993 92-19-12 FAA, U.S AD Safety belt LFV LVD2588 25-Nov-1994 01-Oct-2009 N/A due to p/n 94-21-06 FAA, U.S AD 1 Omega Navigation System 27-Mar-2000 1 03-Dec-2010 AD note cancelled 95-19-04 FAA, U.S AD Insp.of Cabin Pressurization LEARJET SB 21-19 02-Nov-1995 24-Jan-1996 95-20-03 Outflow.... FAA, U.S AD IR ALC Series 66 fluorescent lamps 07-Aug-2012 95-22-01 FAA, U.S AD Inspection of Tip Tank Flapper LEARJET SB 28-10 27-Dec-1995 24-Jan-1996 95-25-03 Valves FAA, U.S AD Raisbeck Group STC SA766NW FAA, U.S AD 85-16-04 22-Oct-1996 09-Feb-2006 N/A due to config. (STC SA766NW 96-19-13 LEARJET AMK83-05 never been installed). FAA US AD 97- 1 GNS XLS and GNS XL system 01-Nov-2011 05-03 FAA, U.S AD Electrical Arcing and Fire Hazard LEARJET SB 21-24 Rev 24-Apr-1998 15-Sep-2009 N/A due to s/n 98-06-28 1 FAA, U.S AD 1 Inspection of seat restraint system LFV LVD2929 Rev 2 14-Jan-2000 1 01-Oct-2009 N/A due to manufacturing year 98-25-10 FAA, U.S AD Oxygens Masks 02-Jun-1999 30-Sep-2009 N/A due to different cure date 99-08-21 FAA, U.S AD Replacement or Spoiler Actuator LEARJET SB 27-36 28-Oct-1999 12-Feb-2009 N/A due to s/n 99-23-19

FLIGHT INT, Flight international inc. FLIGHT INT Hard points 26-nov-99 17-nov-88 STC SA1604SO

KEITH, Keith Products, Inc. KEITH SB 163 B Load Shed Installation 19-Nov-1999 15-May-2007 KEITH SB 166 A Belt Guard Installation 08-Oct-2001 15-May-2007 KEITH STC Install. of Electric-Driven Vapor A/C 12-Aug-1997 21-Jul-1999 ST09366SC

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 17(195) LEARJET, Bombardier, LEARJET LEARJET AAK WING ICE L. 30-Jun-1976 10-Nov-1988 76-03 LEARJET AAK A MLG OLEO ST PISTON 30-Jun-1978 A 10-Dec-1985 78-03 LEARJET AAK PITOT HEAT IND. 30-Jun-1979 25-Jul-1988 79-02 LEARJET AAK CONICAL FAN SPINNER 30-Jun-1979 10-Nov-1988 79-04 LEARJET AAK INCREASE T.O. WEIGHT 30-Jun-1980 10-Dec-1985 80-02 LEARJET AAK INCREASE LAND.WEIGHT 30-Jun-1980 10-Dec-1985 80-03 LEARJET AAK 1 Starter Contactor 30-Jun-2008 1 16-Sep-2008 PCW 81-01 LEARJET AAK 1 Install. Cabin Temp.Contr.Syst.filters 01-Oct-1982 1 22-Jan-2003 Final complied w/o C04708 82-02 LEARJET AAK GS ANTENNA 30-Jun-1985 10-Dec-1985 85-08 LEARJET AAK 1 Inst. of LDG Actuator Down Lock 22-Sep-2008 1 04-Nov-2008 Checked PCW. 86-02 Switch LEARJET AAK Installation of Doublers at Frame 6. 08-Jan-1990 29-Aug-2001 Installation doubler at frame #6 on 89-03 R/H side LEARJET AAK D Inst. of Doublers at Frame 7 11-Aug-1995 D 29-Aug-2001 89-04 LEARJET AAK 25 DG.FLAP LIMIT SWITCH 30-Jun-1989 02-May-1990 89-14 LEARJET AAK 1 Inst. of Batting at Wing Spar 1 Splice 22-Sep-2008 1 04-Nov-2008 Checked PCW. 90-12 LEARJET AAK IR Overhead Fluorescent Light. Wiring 30-Jan-1991 IR 22-Sep-2009 90-16 Prov. LEARJET AAK 1 Inst of Defog Temperature Sensors 16-Feb-2009 1 05-Jun-2009 N/A Due to Electric Windshield not 91-05 installed LEARJET 2 DOOR HANDLE 30-Jun-1978 06-Feb-1991 N/A due to s/n of aircraft. AMK 78-02 LEARJET A GENERATOR DRIVE SPLINES 30-Jun-1978 A 25-Jun-1980 AMK 78-08 DRIVE SHAFT LEARJET A ENGINE BLEED AIR PLUMBING 30-Jun-1978 A 26-Jun-1979 AMK 78-12

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 18(195) LEARJET A ESS.BUS 04-Jun-2007 A 11-Sep-2007 Previously carried out, ref. AMK 78- AMK 78-13 13 LEARJET EMERG.PRES. VALVE 30-Jun-1979 22-Oct-1979 AMK 79-06 LEARJET GENERATOR DRIVE SPLINES 30-Jun-1979 25-Jun-1980 AMK 79-07 LEARJET CAB.DOOR MECHANISM FAA, U.S AD 80-07-09 30-Jun-1979 25-Jun-1980 AMK 79-09 (AD800709) (AD800709) LFV LVA1613 LEARJET ENGINE FUEL TUBE 30-Jun-1979 25-Jun-1980 AMK 79-10 LEARJET A ENG.MOUNT (AD801711) 30-Jun-1980 A 27-Feb-1981 AMK 80-06 (AD801711) LEARJET MOTIVE FLOW VALVE (AD801909) FAA, U.S AD 80-19-09 30-Jun-1980 05-Nov-1980 AMK 80-07 (AD801909) Rev 1 LFV LVA1625 Rev A LEARJET 1 Installation of Current Limiter 28-Jun-2010 A 23-Jan-2009 Starter engage lamps, moved to AMK 80-17 Warning opt. position LEARJET HOR.STAB. HINGE PIN 30-Jun-1981 22-Jun-1982 AMK 81-17 LEARJET AILERON TRIM TAB BALANCE 30-Jun-1983 01-Oct-2009 PCW AMK 83-03 WEIGHT (AD84190 (AD84190 LEARJET WING STALL STRIP (AD851604) FAA, U.S AD 85-16-04 30-Jun-1983 20-Feb-1987 N/A due to config. (STC SA766NW AMK 83-05 (AD851604) FAA, U.S AD 96-19-13 never been installed). LEARJET A POWER DIST. 30-Jun-1985 A 24-Jan-1996 AMK 85-01 LEARJET WING FLAP SECTOR (AD862205) FAA, U.S AD 86-22-05 30-Jun-1986 20-Feb-1987 AMK 86-04 (AD862205) LEARJET A Replacement of Parallelling Control 01-Aug-1992 26-Jan-1993 AMK 90-04 Box LEARJET SYSTEM TUBE (AD921912) FAA, U.S AD 92-19-12 09-Oct-1991 05-Feb-1993 AMK 90-05 (AD921912) LEARJET Windshield Anti-Ice Thermostat 12-Aug-1998 15-Nov-1999 AMK 91-2A Replacem. Learjet SIL 30-005 LEARJET AW Goodyear Flight Eagle Tire Tread FAA, U.S AD 2001-07-11 05-Feb-2001 17-May-2001 N/A by s/n on tire. 32-021 Separat LEARJET SB Inspection/Replacement of cables 27-Feb-2001 10-Apr-2001 Kontr.i status 00-01 LEARJET SB FIRE EXT. BOTTLE (HYDROST.) 18-Nov-1992 21-Jun-1993 05-01 LEARJET SB A AIRSPEED LIMIT PLACARDS FAA, U.S AD 80-17-11 18-Sep-1980 A 19-Aug-1987 11-03 AD841906

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 19(195) LEARJET SB WASTE DISP.REC. PLACARDS 18-Dec-1981 23-Apr-1982 N/A due to model and s/n. 11-04 AD740809 LEARJET SB CREW SEAT BELT PLACARDS 31-Aug-1983 20-Oct-1980 11-05 LEARJET SB BATTERY PLACARDS 21-Jul-1987 19-Aug-1987 N/A due to SB32-04 is carried out. 11-06 LEARJET SB ID PLATE (O) 06-Nov-1992 01-Jan-1994 11-07 LEARJET SB Repl.of Fuel Servicing Placards 17-Dec-2001 10-Dec-2003 11-10 LEARJET SB CONDENSER FAN ASSY. FAA, U.S AD 78-16-03 12-Jul-1978 20-Jan-1984 21-03 AD781603 LEARJET SB Inst. of Refrigeration 22-Feb-1979 09-Feb-1979 21-04 Syst.Warn.Placard LEARJET SB CABIN PRES. SAFETY VALVE 18-Dec-1979 25-Feb-1980 21-05 LEARJET SB Insp.of Air Distr.Sleeves & Clamps- 23-Sep-1980 27-Feb-1981 21-06 Tailc LEARJET SB CABIN PRES. SAFETY VALVE 28-Oct-1980 12-Apr-1991 21-07 (CHANGED) Garrett SB 5-2290 LEARJET SB Insp.Cabin Press. Control Module for 12-Sep-1983 20-Jan-1984 21-09 PN LEARJET SB Insp. of Pneumatic Duct Temp. 26-Sep-1989 10-Nov-1990 21-12 Limiter LEARJET SB 1 OUTFLOW VALVE SAFETY VALVE 03-Jan-1995 1 24-Jan-1996 Superseded by SB 21-19. 21-14 (R) LEARJET SB 2 Repl. of Refrig.Syst. Press Switch 22-Jul-2005 2 11-Oct-2005 N/A to Keith R34. 21-15 LEARJET SB Mod. of Aux Cabin Heater Relay 16-May-1994 13-Apr-2006 21-16 Assy LEARJET SB 3 Imp.W-shield Aux.Defog & Aux.Crew 11-Aug-2008 3 04-Nov-2008 N/A N/A due to AAK86-1 not 21-18 Heat incorporated LEARJET SB Insp.of Cabin Press.Outflow & Safety FAA, U.S AD 95-20-03 03-Jan-1995 24-Jan-1996 21-19 Vlv 130406-21-A4011 R2,102850-21- A4021 R2 LEARJET SB Repl. Cabin Press. Outflow valve 14-Jul-1995 16-Sep-1999 21-20 Assy LEARJET SB 1 Inst.of Cabin Air Syst. 15-Aug-2003 1 03-Nov-2003 N/A due to s/n of aircraft. 21-22 Electr.Connector LEARJET SB 1 Repl.of Aux.Cabin Heater Wiring FAA, U.S AD 98-06-28 13-Aug-1996 1 15-Sep-2009 N/A due to s/n 21-24

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 20(195) LEARJET SB 3 Inst.of Improved Refrigeration 12-Nov-2007 2 06-Feb-2008 N/A Due to Keith Aircondition System 21-25 Comp.Asse TR-134 Installed LEARJET SB 5 Mod.of Auxiliary Cabin Heather 16-May-2007 5 05-Mar-2012 21-26 LEARJET SB Repl.of Yaw Damper Servo Sector 02-Feb-1979 03-Feb-1979 22-03 Bolts LEARJET SB C Mod. of Mach Trim Computer J.E.T 25-Mar-1980 C 20-Feb-1980 22-04 SB 501-1132-9E, -10B, -11 LEARJET SB Mod.of FC-530/-535 Autopilot 05-Jan-1987 12-Apr-1991 N/A N/A due to A/P model 22-05 Computer LEARJET SB 3 Inst.of Autopilot Accelerometer 11-Jun-2007 2 29-May-2007 N/A AAK 83-2 not complied with. 22-07 Monitor LEARJET SB 2 Increased FOD Protection-Installation 09-Jul-2001 2 11-Jan-2006 Previous revision carried out. 23-03 of Antenna Protection. LEARJET SB Insp.of Battery Vents for Obstruction 29-Sep-1980 21-Oct-1980 24-06 LEARJET SB Current Limiter Box Moisture Proofing 15-Jan-1981 12-Apr-1991 24-07 LEARJET SB Insp.of No.4 Gauge Electrical Cables 11-May-1982 26-Jan-1983 24-08 LEARJET SB Insp.Fuses for Proper Prot.Covering 19-Apr-1983 22-Jul-1983 24-09 & PN LEARJET SB Reloc.of Battery Vent Inlet Fitting FAA, U.S AD 86-05-05 18-jul-85 10-Dec-1985 24-10 AD860505 Rev 1 LEARJET SB Add.of Ret.for Gen.Warn.Ctrl 01-Nov-1990 12-Apr-1991 24-11 Box.Connect LEARJET SB 1 Inst.of Concorde Sealed Lead-Acid 24-Mar-2008 1 04-Sep-2008 24-15 Batt. LEARJET SB Insp.of Drag Chute Mechanism Bolt 10-Nov-1980 15-Jan-1981 25-03 LEARJET SB A Insp.of Drag Chute Mech.for Proper 11-Nov-1981 A 23-Nov-1986 25-04 Clear LEARJET SB Insp.Drag Chute Canister Lid Latch 19-Feb-1987 12-Feb-1987 25-06 Screw LEARJET SB A Insp.of Drag Chute Riser FAA, U.S AD 89-12-01 22-Mar-1989 A 01-Oct-2009 25-07 LEARJET SB A Verif.& Ident.of Eng.Fire 30-Apr-1991 A 17-Jun-1991 26-02 Ext.Bottl.Wire LEARJET SB 1 Engine Fire Element Insp./repl. 11-Aug-2008 1 04-Nov-2008 N/A N/A by s/n on elements 26-04 LEARJET SB A Repl.of Primary Control Syst.Stop 12-Sep-1975 A 19-Aug-1997 Checked. Previously complied with. 27-03 Bolts

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 21(195) LEARJET SB Insp.of Wing Flap Actuators 19-Dec-1978 20-May-1975 27-09 LEARJET SB Rework of Pilot/Copil.Ctrl Wheel Trim 19-Apr-1979 17-Aug-1979 27-10 .. LEARJET SB Insp.of Aileron for Drain Holes 06-Nov-1979 01-Mar-1980 27-11 LEARJET SB B Stall Warn.Accelerometer Op.Check FAA, U.S AD 82-01-05 25-Sep-1981 B 30-May-2007 Överförd till A1 phase insp. Ref. 27-12 Rev 2 LFV LVA1912 Learjet Chpt.5 rev.74 och FAA AMOC från 2005-03-24 LEARJET SB Insp.of Welds on Rudder Pedal 08-Sep-1983 20-Jan-1984 27-14 Supp.Assy LEARJET SB Insp.Flap Attach.Fittings for Cracks 27-May-1986 05-Sep-1986 27-16 LEARJET SB Insp.of Ail.& Rudder Ctrl Cable Assy 08-Nov-1993 01-Jan-1994 27-24 LEARJET SB Removal of Sealant from Aileron Rib 27-May-1997 19-Aug-1997 27-33 LEARJET SB 4 Inst.of Secondary Locking Feature 15-Aug-2003 4 03-Nov-2003 Previous rev. carried out. 27-35 LEARJET SB Replacement of Spolier Actuator FAA, U.S AD 99-23-19 14-Dec-1998 12-Feb-2009 N/A due to s/n 27-36 LEARJET SB 6 Insp/Inst. of Flap Structure 16-Aug-2010 6 10-Nov-2011 PCW Previous revision carried out 27-40 Components LEARJET SB Recalibration rosemount 19-Jan-2005 17-Mar-2005 N/A due to STC ST00321WI-D not 27-43 complied with. LEARJET SB 1 Insp. Spoiler panels 02-Apr-2012 27-45 LEARJET SB Insp.of Tip Tank Elect.Conduit for 20-Feb-1976 12-Apr-1991 28-02 INAKTIV Damag LEARJET SB Op.check of Fuel Jettison Valves 14-Feb-1980 23-Apr-1980 28-05 INAKTIV LEARJET SB Insp.of Rec.for Field Rep.of Mot.Flow 21-Aug-1980 09-Dec-1980 28-06 Vl LEARJET SB Insp.of Motive Flow Vlv Shroud Cover 27-Aug-1990 02-Nov-1990 28-08 LEARJET SB Inspection of Tip Tank Flapper FAA, U.S AD 2005-16-09 06-Oct-1995 14-Sep-2005 Flapper p/n 2323006-802 previously 28-10 Valves FAA, U.S AD 95-25-03 installed. No further action req. LEARJET SB 5 Inst.of Standby Fuel Pump FAA, U.S AD 2007-04-18 28-Sep-2009 5 26-Feb-2010 Rev. 1-4 PCW. AFM cheched for 28-11 Annunciators Change 14 LEARJET SB 2 Repl.of Tip Tank Flapper Valves 09-May-2001 2 29-Aug-2001 28-14

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 22(195) LEARJET SB 1 Inst.of Fuel Panel Overlay Blank. 14-Jan-2004 1 30-Aug-2007 Cover installed 28-17 Plate LEARJET SB Insp./Repl. of Fuel Filter Elements 24-Aug-2009 30-Oct-2009 N/A due to filter p/n 28-18 LEARJET SB 1 Insp.RH Eng.Hydr.Press.Line for FAA, U.S AD 83-08-03 10-Sep-1996 1 01-Nov-2005 N/A due to installation of reducingvalve 29-01 Interfer 3000-1500 psi LEARJET SB Insp.LH Eng.Hydr.Lines for FAA, U.S AD 84-20-06 15-Jun-1983 23-Aug-1983 29-02 Interference LEARJET SB Insp.Hydr.Tube Assy & Wiring for 14-Jan-1985 18-Apr-1985 29-03 Interf. LEARJET SB Repl.of Hydr.Reservoir Sight Glass 07-Oct-1992 01-Jan-1994 29-05 Assy LEARJET SB Windshield Anti-Ice Timer Op. Check 19-Jan-1983 28-Feb-1983 30-01 LEARJET SB 1 Repl. of Wing Anti-Ice Transverse 12-Feb-1999 1 04-Aug-2000 30-10 Duct LEARJET SB 3 Inst.of High Current Capacity Wire 05-May-2008 3 04-Sep-2008 PCW 30-11 LEARJET SB Repl.of Oil Press.Annunciator Cap 26-Oct-1992 01-Jan-1994 31-01 Assy LEARJET SB Insp.of LG Brake & Torque Link for 25-Aug-1981 12-Apr-1991 32-03 Inter LEARJET SB Repl.of LG Hydraulic Selector Valve 23-Jan-1989 06-Nov-1990 32-04 LEARJET SB 1 Inst.of MLG Lower Torque Arms 10-Nov-1995 1 13-Jan-2004 32-07 LEARJET SB Inst.of Main Landing Gear Wheel 19-Jan-1999 15-Mar-1999 N/A. Affected Wheel Assy not installed. 32-18 Screens LEARJET SB Repl.of Landing Gear Shuttle Valve 09-Mar-2000 30-Jun-2000 Found N/A to Part Number. 32-20 Bolt LEARJET SB Repl.of Brake Valve Adjustment 01-May-2000 29-Aug-2001 32-21 Screw LEARJET SB 1 Mod landing gear squat switch wiring 09-Apr-2007 1 29-May-2007 Previously carried out 32-23 LEARJET SB Insp/Repl of the Nose Gear Wheel 18-Jan-2010 10-May-2010 N/A by s/n 32-26 Assy LEARJET SB Insp.& Mod. of LH Fwd Cabinet Light 24-Apr-1985 12-Apr-1991 N/A N/A due to interior config. 33-03 Assy LEARJET SB A Deactiv.of Fwd Cabinet & Overhead FAA, U.S AD 91-03-08 / 21-Dec-1990 A 12-Aug-1991 33-05 Light. AD901406 LEARJET SB A Activ.of Fwd Cabinet & Overhead 12-Apr-1991 A 22-Sep-2009 33-06 Fluore..

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 23(195) LEARJET SB Insp.of Static Ports 11-Jun-1982 21-Oct-1982 34-04 LEARJET SB Replacarding Oxygen Bottle Shutoff 27-Feb-2004 20-Sep-2004 N/A N/A by p/n on oxygen regulator 35-04 Valve LEARJET SB A Insp.& Repl.of Eng.Bleed Air Flex 25-May-1978 A 12-Apr-1991 N/A N/A by s/n on aircraft 36-02 Tube.. LEARJET SB Repl Air Bottle & Weight-Balance 14-Dec-2009 11-Mar-2010 Due to weighing after installation of 36-03 Change bottle p/n 6600194-6 LEARJET SB Insp.Baggage Comp.Struct. for 18-Jul-1985 10-Dec-1985 51-01 Corrosion AD 84-12-03 LEARJET SB Insp.of Forward Engine Beam Shear FAA, U.S AD 2004-03-08 01-Feb-2001 06-Sep-2001 N/A N/A due to SB 51-04 performed. 51-03 Web. LEARJET SB 5 Rep.of Forward Engine Beam Shear FAA, U.S AD 2004-03-08 12-Oct-2009 5 11-Mar-2010 No rework required 51-04 Web LEARJET SB 3 20-Jan-2005 No rework req. 51-4 LEARJET SB Mod.of Access Door Lock 16-Apr-1979 12-Apr-1991 Found N/A. No locks installed. 52-04 Assemblies LEARJET SB Insp.of Cabin Int.Liner-Areas Of 04-Nov-1980 12-Apr-1991 52-05 Emerg.. LEARJET SB Mod.of Lwr Cabin Door Hook 18-Dec-1992 01-Jan-1994 52-06 Mechanism LEARJET SB Repl.of Lwr Cabin Door Cable & 15-Sep-1993 06-Feb-1995 52-07 Handle As LEARJET SB 1 Repl.of Upper Cabin Door Torsion 03-Jun-1999 1 20-Sep-1999 N/A. 24 inch door not installed. 52-10 Bar Arm LEARJET SB Inspect for Tailcone Drains 18-Dec-1992 01-Jan-1994 53-07 LEARJET SB Inst.of Nutplates on Circ.Br.Panel 14-Feb-1994 06-Feb-1995 53-08 Suppo LEARJET SB 1 Repl.of LowerStinger & Ventral Fin 17-Mar-2008 1 14-May-2008 N/A Due to Avcon Fins STC ST00432WI 53-10 Skin LEARJET SB 3 Mod.of Tailcone Ballast Weight 01-Jun-2009 3 28-Jan-2010 N/A Not incorporated. 53-11 Installat LEARJET SB Insp. Intern. baggage comp. floor 16-Jan-2006 08-Mar-2006 N/A Due to S/N 53-13 splice LEARJET SB Insp.for Silicon Firesleeve-Start&Gen 11-Jun-1982 06-Oct-1982 54-01 Ca LEARJET SB Insp/Firewall Sealing Modification 16-Mar-2001 02-Nov-2005 R/H side carried out 54-03 LEARJET SB Insp/Repl.of Upper and Lower Pylon 08-Aug-2001 22-Mar-2002 N/A by s/n on aircraft. 54-04 Skins

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 24(195) LEARJET SB Insp.Horiz.Stab.Hinge Assy for 16-Aug-1991 16-Aug-1991 N/A No Thrust Reversers installed. 55-01 Cracks LEARJET SB 2 Inst.of Doublers on Horiz.Stabili.Skin 23-Feb-2009 2 10-Jun-2009 PCW 55-04 LEARJET SB Imp.of Horiz.Stabilizer Actuator 16-Jan-1998 30-Sep-1998 55-05 Access LEARJET SB Mod.of Navigation Light Wiring 30-Aug-2004 13-May-2005 55-06 Conduit LEARJET SB Eng.Firewall Sealing at Feed-Thru 13-May-1982 15-Jul-1982 71-02 Condui LEARJET SB B Insp.of Eng. I.T.T. Cable Connectors 07-Nov-1983 B 22-Jul-1983 76-01 LEARJET SB Insp/Repl.of Aileron Ctrl Cables 23-Dec-2002 12-Dec-2002 Cables N/A by cal.time. A27-42 LEARJET SB ALCOHOL ANTI-ICE SYSTEM (W-IN 18-Dec-1992 26-Jan-1993 A30-03 10H) LEARJET SB 1 Insp.of Landing Gear Actuator 21-Apr-1997 1 17-Apr-1998 A32-15 Pistons LEARJET SSK Evaporator Assy. 10-Feb-1989 20-Jul-1994 980 LEARJET SSK Repl. of Spoiler Act. Support Bracket 19-Dec-1986 04-Aug-2000 Carried out on R/H side, kit 981 2692006-4. LEARJET SSK 2 Repl. of Landing Gear Wheel 21-Jan-1991 2 14-Oct-1997 see w/o C00671 for 2 wheels 993 Bearings

LFV, Luftfartsverket LFV LVA 1613 Modifiering av övre kabindörr LEARJET AMK79-09 27-May-1980 25-Jun-1980 LFV LVA 1625 A Till,gg i flyghandbok. T,thetskontroll FAA, U.S AD 80-19-09 23-Jun-1980 A 05-Nov-1980 Rev 1 LEARJET AMK80- 07 LFV LVA 1748 Revision av Flyghandbok. FAA, U.S AD 81-13-07 24-Aug-1981 10-Aug-1981 Br,nslem,ngd LFV LVA 1912 Periodisk kontroll av Stallvarning. FAA, U.S AD 82-01-05 10-Nov-1983 30-May-2007 Överförd till A1 phase insp. Ref. Rev 2 LEARJET SB 27-12 Learjet Chpt.5 rev.74 och FAA Rev B AMOC från 2005-03-24 LFV LVD 1635 A Revision Flyghandbok/kontr. A/P & FAA, U.S AD 80-19-11 15-Jul-1985 A 28-Sep-2009 PCW Ref. FAA AD 80-19-11 R1 mod. Rev 1 LFV LVD 2034 Reducering av MMO FAA, U.S AD 85-16-04 30-Aug-1985 06-Feb-2002 N/A due to config. (STC SA766NW never been installed).

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 25(195) LFV LVD 2046 Kontroll av batterihållare FAA, U.S AD 86-05-05 25-nov-85 10-Dec-1985 Rev 1 LFV LVD 2352 Shoulder Harness Inst. FAA AC 43-13 CHPT 9 23-May-1991 17-Jun-1991 checked OK. LFV LVD 2588 Byte av säkerhetsbälten FAA AD 94- FAA, U.S AD 94-21-06 05-Jan-1995 01-Oct-2009 N/A due to p/n 21-06 LFV LVD 2853 Periodisk funktionskontroll av 23-Mar-1998 13-Aug-2010 nödutgång LFV LVD 2929 2 Kontroll av bältens låsfunktion AD 98- FAA, U.S AD 98-25-10 13-Jan-2000 2 01-Oct-2009 N/A due to manufacturing year 25-10 Rev 1 LFV LVD 3148 Modif. Transponder kontrollpanel 17-Aug-2001 12-Feb-2009 N/A due to p/n

NYGE, Saab Aerotech Aircraft Services NYGE SB 08- EGPWS System Provision for Inhibit 30-Nov-2009 A 08-Feb-2010 06-34-03 A Unit) NYGE SSB A 29-Nov-2006 DR-MGPC- YELL NYGE TDM 12- A L35A Move mission inverter A 10-Sep-2012 22 NYGE TDM Installation laser prismor L35 A 10-Sep-2012 12.23 NYGE TDM Installation Underving-kanaler 16-Oct-2002 12-Dec-2003 LFV app.No: M21/02 revision 1. 02-25 NYGE TDM Box 3 Installation 01-Nov-2002 03-Dec-2003 Approved in accordance with EASA 02-26 2004-11267 and with LFV AFMS S04/89 R2. NYGE TDM Utv. Framtagning mod.balkar LR-35 18-Nov-2002 12-Dec-2003 02-28 NYGE TDM B Operators Console L35A 02-Apr-2007 B 26-Feb-2008 only updated to rev.B 03-03 NYGE TDM Alkan Fairings (mod.) 27-Feb-2003 12-Dec-2003 Approved by EASA no. 235 in 03-07 accordance with LFV Mod. Cert. No. M29/03. NYGE TDM ACAS Installation 06-May-2003 28-Oct-2004 Approved i.a.w. EASA Doc. No: 03-17 STC S.A.00255 NYGE TDM Mission Inverter Modif. 20-Nov-2003 05-Dec-2003 Approved in accordance with LFV 03-19 M37/03 and EASA 1985. NYGE TDM U95 Installation L35A 10-Sep-2003 D 08-Nov-2005 Rev.D updated 03-23

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 26(195) NYGE TDM D Astor L35A 16-Jan-2004 D 21-Nov-2012 Effektindikering/Ground test 04-03 NYGE TDM C Darts System L35A 05-Dec-2006 01-Jan-2006 Approved in accordance with DOA 04-06 21J.108,04-06. NYGE TDM Removal of Reflector System 30-May-2005 11-Nov-2005 Approved i.a.w. DOA 21J.108,05-06 05-06 NYGE TDM Install. Jumpseat Intercom 18-Jul-2005 08-Dec-2005 Approved in accordance with DOA 05-15 21J.108,05-15. NYGE TDM GMS anpassning i nya OP-racken 26-Aug-2005 08-Dec-2005 Approved in accordance with DOA 05-17 21J.108,05-17. NYGE TDM Install. GPS Map and GP&C 08-Sep-2005 11-Nov-2005 Approved in accordance with DOA 05-19 Transponder 21J.108,05-19. NYGE TDM Install. Mission Equip. new OP- 13-Sep-2005 11-Nov-2005 Approved in accordance with DOA 05-20 Console 21J.108,05-20. NYGE TDM Install. Cabin Side Wall Cable 20-Oct-2005 11-Nov-2005 Approved in accordance with DOA 05-26 Channel 21J.108,05-26. NYGE TDM Install. Structural Plug FAA STC 11-Nov-2005 11-Nov-2005 Approved in accordance with DOA 05-34 SA2479CE 21J.108,05-34. NYGE TDM Re-mod. Hydraulic system 05-May-2006 15-May-2007 06-22 NYGE TDM Robot 15 Radar Altimeter (Nav Demo 05-Jul-2006 26-Oct-2006 06-33 Pod) NYGE TDM Meteor Proximity Fuse 05-Jul-2006 26-Oct-2006 06-34 NYGE TDM A A100 (to carry on L35A) 23-Apr-2007 A 25-Feb-2008 06-36 NYGE TDM C Enhanced Surveillance L35A 09-Mar-2010 C 18-Aug-2009 Original compliance to rev A of 08-02 TDM. TDM rev B and C does not affect previous compliance. NYGE TDM C EGPWS MK.8 & Mission Inhibit 05-Mar-2010 C 30-Oct-2008 Original compliance with rev A. Rev 08-06 System B and C does not affect previous compliance. NYGE TDM E LR35A GPS-Map Display 12-Apr-2010 E 10-Sep-2012 Compliance was IAW TDM rev B. 08-07 Previous compliance not affected by rev D. NYGE TDM C Install termination resistors D 01-Sep-2012 08-09 NYGE TDM A Barlast DARTS L35A 10-Mar-2008 A 10-Mar-2008 08-13 NYGE TDM C ELT 406 L35A 04-Jul-2008 C 03-May-2010 Original compliance with TDM rev 08-17 A. Rev B and C does not affect previous complaiance.

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 27(195) NYGE TDM A Mission Antenna Adapter 28-Oct-2008 A 15-Dec-2008 08-26 NYGE TDM C LR35A U-95 SORC Lite 24-Sep-2009 C 30-Sep-2009 Original compliance i.a.w rev B 09-01 NYGE TDM E LR35A Removable Hard Disk Drives 30-Apr-2010 E 04-July-2012 09-30 NYGE TDM A Overload Sensing Control 02-Jun-2010 A 14-Oct-2010 Initial complaiance was I.A.W TDM 10-04 rev 2 NYGE TDM A LR35A U95-D2 22-Apr-2010 A 15-Jun-2010 10-27 NYGE TDM Installation Intercom 10-Jan-1995 24-Jan-1995 95-01 NYGE TDM Modifiering Transponder-system 10-Jan-1995 24-Jan-1995 95-02 NYGE TDM Miss-rack,GPS-antenn,CVR,inverter 12-Feb-1996 15-Mar-1996 96-01 m.m. NYGE TDM TAPS 20-Feb-1997 01-Jan-1998 97-01 NYGE TDM Kontrollprogram SE-DHO 26-Nov-1997 01-Jan-1998 97-09 NYGE TDM Astor L35A 09-Mar-1998 10-Feb-1998 Approved in accordance with LFV 98-06 M20/99. NYGE TDM Installation BRNAV L35A 26-Jun-1998 16-Apr-1998 Approved in accordance with S- 98-12 CAA Approval reference LS 2005- 7326.

ROCKWELL, Rockwell Collins U.K.Ltd ROCKWELL Reply Inhibition On The Ground EASA AD 2009-0097 Rev 25-May-2007 18-Aug-2009 PCW Are in compliance with EASA SIL 07-1 IR AD2009-0097 Ref TDM03-17 DWG MF1030064-1 Rev.C

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 28(195) 1.3 GFE Aircraft Learjet 35A SE-DHP

1.3.1 Aircraft Specification Type: Serial Registration: Airframe Total Date Number: total Hours: Landing Reference: Cycles: Learjet 075 SE-DHP 12549 8437 2012-11-23 35A

1.3.2 Engines Type: TFE731-2-2B Serial Total Hours Total Hours Hours Number: Since New: Cycles remaining remaining Since New: to MPI: to CZI: Left Engine P-74542 14889 11860 549 561 Right Engine P-74277 10913 7322 1051 3851

1.3.3 Avionics System: Type / Part Number: Note: Autopilot JET FC 200 Dual VHF-COM Collins VHF-22C HF-COM Collins 718U-5 ICS & Audio System DB System Dual VHF -NAV Collins VIR -30A GPS Garmin GPS 165 TSO Dual DME Collins DME40 ADF 1 & 2 Bendix/King KDF-806 XPDR 1 & 2 Collins TDR94D Mode S EHS TCAS II Collins TCAS-4000 TCAS II VSI/RA/TA Indicator LH / Collins TVI -920 RH TAWS / EGPWS Honeywell MK VI RDR ALT Collins ALT -55B Weather Radar Honeywell Primus 400 MFD Display Honeywell MFRD ELT Kanad ELT 406-AF-H Dual Mach Airspeed indicator IDC 2680003-2 Altimeter incl. encoder LH IDC 28007-017 Altimeter RH IDC 23932 -053 Altitude Report & Alerting System IDC 23989 -011 Air Data Display Unit 9D-80130-32 Flight Director Indicator LH Collins 329B-7R-2 Vertial Gyro Indicator RH JET 5-4000-08

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 29(195) Dual VG-Gyro JET VG-206EL Standby Altitude Gyro JET AI 804 Horizontal Situation Indicator LH Collins 331A-6R Horizontal Situation Indicator RH Collins 331A-3G Dual RMI Collins 332C -10 Dual DG -Gyro JET DN -101D RVSM FDR Sundstrand 980-4100-FWUS CVR Fairchild 93-A100-83

1.3.4 Mission System System: Description: Fixed general installations FR31 VHF/UHF COM Radio AN/ARC 182 VHF/UHF COM Radio GPS MAP System JET SI -3003B Inverter 115/200VAC 400Hz 3 phase KGS SPS-3052B Inverter 230VAC 50Hz Laser Prism Wing Pylon NATO 14” Alcon Ejector Unit LH and RH Wing Pylon EW system ASTOR Fixed installed system ADRIAN C & S Pod mounted system U95-N Pod mounted system U95-D2 Pod mounted system U95 Sorc Pod mounted system A100 Pod mounted system Missile Threat Simulator DARTS Pod mounted system GMS Pod mounted system Chaff Dispenser BOX 3 Pod mounted system Target Towing MTR 101 Outboard pod mounted winch AS200 MDI (Miss Distance Indicator) TLX Height keeping target Precisions GPS Pos System TAPS

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 30(195)

1.3.5 Mission Cable Harness to Hard Points Used for Mission LH NATO Hard point: RH NATO Hard point: Note: System: Adrian C & S, U95-N, U95- General Signal Harness General Signal Harness Two pair shielded D2, U95 Sorc, A100, DARTS, GMS, BOX 3 and MTR 101 AWG 20 x 25 MTR 101 MTR 101 Harness MTR 101 Harness Two pair shielded AWG 20 x 3 AWG 16 x 4 + shield U95-N, U95-D2, U95 MIL-STD-1553B Data MIL-STD-1553B Data Twinax x 8 Sorc, A100 and GMS Bus Bus U95-N, U95-D2, U95 Sorc, AC Power AC Power 115/200VAC AWG 12 x 10 + A100, DARTS and GMS 115/200VAC 400 Hz 3- 400 Hz 3-Phase 3 x 10 A shield Phase 3 x 10 A Adrian C & S, GMS and BOX DC Power 28 VDC 150 DC Power 28 VDC 150 AWG 4 x 4 3 A A MTR 101 Coaxial 2 x 75 Ω Coaxial 2 x 75 Ω Adrian C & S Coaxial 3 x 50 Ω Coaxial 3 x 50 Ω Recognition Light Recognition Light Recognition Light Cable AWG 16 x 4 + Cable shield

1.3.6 Antenna layout

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 31(195)

1.3.7 Inspektion due times and dates Status date November 23 rd 2012.

Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date Due Landings Aircraft SE-DHP Phase A 300 hour insp. AMP 2012-01-09 12407 12707 2013-02-09 Phase B 600 hour insp. AMP 2012-01-09 12407 13007 2014-02-09 Phase C 1200 hour insp. AMP 2010-11-05 12288 13488 2014-11-04 Phase D 2400 hour insp. AMP 2010-12-01 12288 14688 2018-11-29 Special operational fatigue inspect AMP 2009-02-26 11911 13111,3 12000 Hrs Inspection AMP 2001-03-26 10287,00 16287 45 days insp. AMP 2012-11-16 12547 2012-12-31 6 Month Inspection AMP 2012-08-06 12509 2013-02-06 2 Year Inspection AMP 2010-12-01 12288 2012-11-30 12 Year Airframe inspection AMP 2001-03-25 2013-03-22 13042 MPI engine zone inspecition LH AMP 2007-04-17 11653 13053,5 MPI engine zone inspecition RH AMP 2010-03-04 12186 13586,7 300 Hrs Inspection AMP 2012-01-12 12407 12707,8 1200 Hrs Inspection AMP 2008-01-15 11781 12981,9 3000 Landing Inspection AMP 6000 Major Landing Gear Inspection AMP 1998-08-19 12000 Operator's Console 300h/1y insp. AMP 2011-11-24 12400 12707 2013-02-09 ACAS 2 (TCAS) 24month insp. AMP 2011-11-24 12400 2013-11-23 Mission equipment 300 hour insp. AMP 2012-01-17 12407 12707,8 Engine S/N P-74542 Remaining Engine 150 hrs insp. AMP 12557,8 8,3 Engine 300 hrs insp. AMP 12588,7 39,2 Engine 800 hrs insp. AMP 13299,1 749,6 Engine Compressor Zone Insp. AMP 13111,1 561,6 Engine Major Periodic Inspection AMP 13099,1 549,6 Engine S/N P-74277 Remaining Engine 150 hrs insp. AMP 12557,8 8,3 Engine 300 hrs insp. AMP 12800,9 251,4 Engine 800 hrs insp. AMP 13000,9 451,4 Engine Compressor Zone Insp. AMP 16400,9 3851,4 Engine Major Periodic Inspection AMP 13600,9 1051,4

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 32(195)

1.3.8 Implemented Changes Status date November 23rd 2012. For abbreversions see chapter 1.2.8

SB/AD etc Rev Subject Document reference Eff. date Rev Compliance Status Remarks Reference

AVCON, Avcon Industries, Inc AVCON STC R Install. Avcon Fins 31 -mar -05 R 12 -jul -06 SA00432WI AVCON STC A Install. Plug of Dual Hatches 30 -jun -05 A 12 -jul -06 SA2479CE AVCON STC AFM suppl. increase T/O weight...... 25 -aug -97 13 -jul -06 ST00564WI AVCON STC C Increase Takeoff Weight to 19600 11 -mar -05 C 12 -jul -06 ST00611WI pounds AVCON STC B Increase Wing/Tip Zero Fuel Weight 28 -nov -97 B 12 -jul -06 ST00612WI AVCON STC C Increase Landing Weight to 16000 11 -mar -05 C 12 -jul -06 ST00613WI pounds

EASA, European Aviation Safety Agency EASA AD 2006 - Incorrect transponder altitude 30 -Aug - 13 -Nov - 0265 2006 2009 EASA AD 2008 - Improve EHS Operation HONEYWELL SB MST 67A -34 -56 25 -Aug - 01 -Dec -2010 N/A transponder P/N installed 0159 HONEYWELL SSBMST 67A-SW5 Rev 2008 1 EASA AD 2009 - IR Mode S Transponder - DHC SB 8 -34 -243 Rev A EASA AD 29 -Apr - IR 28 -Jul -2009 0097 Check/Modification 2010-0067 ROCKWELL SIL07-1 2009 EASA AD 2009 - 1 Mode S Transponder Mod/Repl 30 -Sep - 1 08 -Dec -2010 N/A due to ADC p/n 0173 2010

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 33(195) EASA AD 2009- Portable Fire Extinguishers- 25-Nov- 07-May- N/A N/A by current P/N installed 0251-E Ident/Repl 2009 2010 EASA AD 2009- Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0278 FFE ASB26- 15-Dec- 07-May- N/A N/A by current P/N installed 0262 115 Rev C 2009 2010 EASA AD 2009- Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009-0262 22-Dec- 07-May- N/A N/A by current P/N installed 0278 2009 2010 EASA AD 2010- R1 Mode S Transponder - 11-Jan- R1 10-Mar- N/A due to p/n 0003 Check/Modification 2010 2010 EASA AD 2010 - IR Mode S Transponder -Mod/Repl 06 -Oct - IR 08 -Dec -2010 N/A by ADC p/n installed 0204 2010 EASA AD 2012 - KIDDE GRAVINER HAND OPERATTED 06 -sep -2012 0237 FIRE EXTINGUISHER EASA STC Install. of Dual Openable Hatches 20 -feb -06 23 -nov -06 EASA.IM.A.S.0144 9

FAA, U.S, Federal Aviation Administration FAA, U.S AD 2000 - Donning oxygen masks 22 -nov -00 26 -feb -03 Complied with by insert of AFM change 12 24-19 FAA, U.S AD 2001 - Goodyear Flight Eagle Tire Tread LEARJET AW 32 -021 01 -May - 17 -May -2001 N/A by s/n on tire 07-11 Separat 2001 FAA, U.S AD 2001 - Prevent erroneous altitude 20 -aug -01 12 -feb -09 N/A due to p/n 15-17 interpretatio FAA, U.S AD 2004 - To prev. structural damage to LEARJET SB 51 -03 LEARJET SB 51 -04 08 -mar -04 09 -mar -04 SB 51 -04 previous carried out. 03-08 eng.pylons Rev 5 FAA, U.S AD 2005 - Detailed inspection of aileron cable. 09 -aug -05 19 -sep -05 Checked OK. 13-36 FAA, U.S AD 2005 - Inspection of Tip Tank Flapper Valves LEARJET SB 28 -10 13 -sep -05 14 -sep -05 Flapper p/n 2323006 -802 previously installed. No 16-09 Supersedes AD 95-25-03 further action req. FAA, U.S AD 2007 - Modify Standby Fuel Pump "switches" LEARJET SB 28 -11 Rev 5 23 -mar -07 15 -mar -07 Previusly complied with. Ref. Learjet SB 28 -11 04-18 FAA, U.S AD 2007 - Unsealed gaps in engine firewall 02 -Oct - 11 -sep -07 Previously carried out, ref. SB 54 -03 17-17 2007 FAA, U.S AD 2008 - HP -Turbine Disc replacement. 19 -feb -08 06 -feb -08 N/A due to engine model. 02-19 FAA US AD 74 -08 - 3 Transport categoryairplanes equipped 11 -May -2012 09 with lavatories

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 34(195) FAA, U.S AD 76-18- Connection of Inverter to correct Bus LEARJET SB 24-03 11-dec-00 11-dec-00 This AD is carried out 1976-09-29 07 FAA, U.S AD 78-16- To precl. a fail. of the Refr. Cond. Fan LEARJET SB 21-03 11-dec-00 11-dec-00 This AD is carried out 1978-07-30 03 Issued 1978-08-17 FAA, U.S AD 79-08- 1 Aeronca thrust Reversers Suppl to 19-apr-82 1 13-feb-09 N/A Aeronca Thrust Reversers not installed 01 AFM FAA, U.S AD 80-06- Starter assisted airstart 24-mar-80 03-dec-93 02 FAA, U.S AD 80 -07 - Cabin Main Entrance Upper Door LEARJET AMK79 -09 01 -May - 17 -nov -80 09 1980 FAA, U.S AD 80 -17 - Airspeed Limitation Placard LEARJET SB 11 -03 Rev A 28 -aug -80 23 -sep -80 11 FAA, U.S AD 80 -18 - To Prevent loss of Emergency 28 -aug -80 01 -jan -03 N/A due to Component p/n 08 electrical Power...... FAA, U.S AD 80 -19 - 1 Motive Flow Valve LEARJET AMK80 -07 LFV LVA1625 11 -dec -80 1 24 -dec -80 09 Rev A FAA, U.S AD 80 -19 - 1 AFM insert LFV LVD1635 Rev A 20 -May - 1 09 -feb -06 Checked. Previously complied with. 11 1985 FAA, U.S AD 81 -04 - Cockpit Voice Recorder A100 series 01 -apr -81 12 -feb -09 N/A due to model & s/n 06 FAA, U.S AD 81 -13 - To ensure oper. without fuel LFV LVA1748 25 -jun -81 10 -aug -81 07 starvation FAA, U.S AD 82 -01 - 2 Stall Warning Accelerometer Check LEARJET SB 27 -12 Rev B LFV 10 -apr -86 2 12 -jun -06 Överförd till A1 phase insp. Ref. Learjet Chpt.5 05 LVA1912 rev.74 och FAA AMOC från 2005-03-24 FAA, U.S AD 83 -08 - Insp.RH Engine Hydraulic Pressure LEARJET SB 29 -01 Rev 1 03 -May - 19 -dec -08 03 Line for Interference. 1983 FAA, U.S AD 84 -19 - To prevent Aileron/Trim Tab Flutter 22 -Oct - 14 -jun -85 06 due to failure of the trim tab ctrl 1984 system FAA, U.S AD 84 -20 - Inspect LH Hydraulic Lines for LEARJET SB 29 -02 03 -nov -86 06 Interfere superseded by 86 -22 -05 FAA, U.S AD 85 -16 - Airplane Lateral Control FAA, U.S AD 96 -19 -13 LEARJET 06 -sep -85 22 -jan -86 N/A due to config. (STC SA766NW never been installed). 04 Characteristics AMK83 -05 LFV LVD2034 FAA, U.S AD 85 -22 - Collins HSI & FD indicators 31 -dec -85 15 -jun -09 N/A by p/n & s/n 10 FAA, U.S AD 86 -05 - 1 Relocation of Battery Vent Inlet Fitting LEARJET SB 24 -10 LFV LVD2046 19 -jan -88 1 18 -jun -86 05 FAA, U.S AD 86 -22 - To prevent of flap operation...... LEARJET AMK86 -04 10 -nov -86 03 -nov -86 05

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 35(195) FAA, U.S AD 87-02- Insp. of Fwd. Eng.Mounts for Cracks LEARJET SB 71-03 Rev 1 06-feb-87 17-jan-05 Para.A: see Phase A3 300 hour insp. Para.B: see A/C 06 status RAL FAA, U.S AD 87-04- Autopilot FC-530 Limitations 09-mar-87 12-feb-09 N/A due to A/P model 06 FAA, U.S AD 89-12- Inspection of Drag Chute Riser LEARJET SB 25-07 Rev A 03-jul-89 07-dec-10 N/A N/A by Riser P/N installed 01 FAA, U.S AD 91-03- Deactivation of Forward Cabinet and LEARJET SB 33-05 Rev A 12-feb-91 19-dec-08 08 Overhead Fluoriscent Light Circuits FAA, U.S AD 92 -19 - SYSTEM TUBE (W -IN 30D) LEARJET AMK90 -05 17 -nov -92 15 -feb -93 12 FAA, U.S AD 95 -19 - 1 Omega Navigation System 27 -mar -00 1 03 -dec -10 N/A AD note cancelled 04 FAA, U.S AD 95 -20 - Insp.of Cabin Pressurization LEARJET SB 21 -19 02 -nov -95 02 -dec -95 03 Outflow.... FAA, U.S AD 95 -22 - ALC Series 66 fluorescent lamps 07 -Aug -2012 01 FAA, U.S AD 95 -25 - Inspection of Tip Tank Flapper Valves LEARJET SB 28 -10 27 -dec -95 14 -feb -96 03 FAA, U.S AD 96 -19 - Raisbeck Group STC SA766NW FAA, U.S AD 85 -16 -04 LEARJET 22 -Oct - 22 -jan -86 N/A due to config. (STC SA766NW never been installed). 13 AMK83 -05 1996 FAA US AD 97 -05 - 1 GNS XLS and GNS XL system 1-Nov -2011 03 FAA, U.S AD 98 -06 - Electrical Arcing and Fire Hazard LEARJET SB 21 -24 Rev 1 24 -apr -98 09 -dec -08 N/A due to s/n 28 FAA, U.S AD 98 -25 - 1 Inspection of seat restraint system LFV LVD2929 Rev 2 14 -jan -00 1 03 -dec -10 N/A Affected seat belts not installed 10 FAA, U.S AD 99 -08 - Oxygens Masks 02 -jun -99 19 -dec -08 N/A due to different cure date 21 FAA, U.S AD 99 -23 - Replacement or Spoiler Actuator LEARJET SB 27 -36 28 -Oct - 09 -dec -08 N/A due to s/n 19 1999

FLIGHT INT, Flight international inc FLIGHT INT STC Hard points 26-nov-99 22-May-1989 SA1604SO

KEITH, Keith Products, Inc

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 36(195) KEITH SB 163 B Load Shed Installation 19-nov-99 B 17-apr-07 KEITH SB 166 A Belt Guard Installation 08 -Oct - A 17 -apr -07 2001 KEITH STC Install. of Electric -Driven Vapor A/C 12 -aug -97 06 -aug -99 ST09366SC

LEARJET, Bombardier, LEARJET LEARJET AAK 71 -13 F Gravel Runway Operations Kit 10 -sep -99 F 27 -mar -01 LEARJET AAK 76 -03 WING ICE L. 30 -jun -76 11 -May -1989 LEARJET AAK 79-02 PITOT HEAT IND. 30-jun-79 03-jul-81 LEARJET AAK 79 -04 CONICAL FAN SPINNER 30 -jun -79 22 -apr -89 LEARJET AAK 80 -02 INCREASE T.O. WEIGHT 30 -jun -80 15 -nov -84 LEARJET AAK 80 -03 INCREASE LAND.WEIGHT 30 -jun -80 02 -dec -88 LEARJET AAK 81-01 1 Starter Contactor 30-jun-08 1 16-sep-08 PCW LEARJET AAK 82 -02 1 Install. Cabin Temp.Contr.Syst.filters 01 -Oct - 1 08 -mar -06 N/A N/A by s/n 1982 LEARJET AAK 83 -06 VERT.STAB. ACCESS 30 -jun -83 29 -jul -84 LEARJET AAK 83 -08 Inst.of Comp.to allow variable Pitch 08 -mar -85 28 -nov -01 Checked. Previously complied with. Trim Settings at takeoff LEARJET AAK 84 -03 A WINDSHIELD HEAT 30 -jun -84 A 12 -mar -85 LEARJET AAK 86 -02 1 Inst. of LDG Actuator Down Lock 22 -sep -08 1 04 -nov -08 Checked PCW. Switch LEARJET AAK 89 -04 D Inst. of Doublers at Frame 7 11 -aug -95 D 27 -mar -01 LEARJET AAK 89-14 25 DG.FLAP LIMIT SWITCH 30-jun-89 02-May-1990 LEARJET AAK 90 -12 1 Inst. of Batting at Wing Spar 1 Splice 22 -sep -08 1 04 -nov -08 Checked PCW. LEARJET AAK 90 -16 IR Overhead Fluorescent Light. Wiring 30 -jan -91 IR 10 -mar -09 Prov. LEARJET AAK 91 -05 1 Inst of Defog Temperature Sensors 16 -feb -09 1 05 -jun -09 N/A Due to Electric Windshield not installed LEARJET AMK 76 - A WING SKIN FASTENERS 30 -jun -76 A 14 -dec -79

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 37(195) 02 LEARJET AMK 76 - 1 CABIN AIR CONTR.VALVE 30 -jun -76 24 -dec -77 07 LEARJET AMK 76 - A OIL PRES. TRANSM. 30 -jun -76 A 24 -dec -77 09 LEARJET AMK 77 - AIL.CABLE PULLEY 30 -jun -77 24 -dec -77 01 LEARJET AMK 77 - ENGINE BLEED AIR VALVE 30 -jun -77 24 -dec -77 03 LEARJET AMK 77 - A WING BOLTS 30 -jun -77 A 24 -dec -77 06 LEARJET AMK 77 - ESS.BUS C/B PANEL 30 -jun -77 24 -dec -77 08 LEARJET AMK 78- ENGINE BLEED AIR DUCT 30-jun-78 23-feb-86 04 LEARJET AMK 78- A ENGINE BLEED AIR TUBE 30-jun-78 A 08-nov-79 06 LEARJET AMK 78- A GENERATOR DRIVE SPLINES DRIVE 30-jun-78 A 19-jun-85 08 SHAFT LEARJET AMK 78- A ENGINE BLEED AIR PLUMBING 30-jun-78 A 15-jan-80 12 LEARJET AMK 78- A ESS.BUS 04-jun-07 A 11-sep-07 Previously carried out, ref. AMK 78-13 13 LEARJET AMK 79- CAB.DOOR MECHANISM (AD800709) FAA, U.S AD 80-07-09 LFV LVA1613 30-jun-79 17-nov-80 09 (AD800709) LEARJET AMK 79- ENGINE FUEL TUBE 30-jun-79 12-jul-80 10 LEARJET AMK 79- AILERON DRAIN 30-jun-79 17-nov-80 11 LEARJET AMK 80- B RUDDER PEDAL 30-jun-80 B 03-aug-81 01 LEARJET AMK 80- A ENG.MOUNT (AD801711) (AD801711) 30-jun-80 A 15-apr-81 06 LEARJET AMK 80- MOTIVE FLOW VALVE (AD801909) FAA, U.S AD 80-19-09 Rev 1 LFV 30-jun-80 24-dec-80 07 (AD801909) LVA1625 Rev A LEARJET AMK 80- 1 Installation of Current Limiter 28-jun-10 A 04-jul-08 Starter engage lamps, moved to opt. position 17 Warning LEARJET AMK 81- HOR.STAB. HINGE PIN 30-jun-81 23-mar-86 17

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 38(195) LEARJET AMK 83- AILERON TRIM TAB BALANCE WEIGHT 30-jun-83 14-jun-85 03 (AD84190 (AD84190 LEARJET AMK 83- WING STALL STRIP (AD851604) FAA, U.S AD 85-16-04 FAA, U.S AD 30-jun-83 22-jan-86 N/A due to config. (STC SA766NW never been installed). 05 (AD851604) 96-19-13 LEARJET AMK 84- SPOILER SYSTEM 30-jun-84 23-mar-86 08 LEARJET AMK 85- A POWER DIST. 30-jun-85 A 23-mar-86 01 LEARJET AMK 86 - WING FLAP SECTOR (AD862205) FAA, U.S AD 86 -22 -05 30 -jun -86 03 -nov -86 04 (AD862205) LEARJET AMK 90 - SYSTEM TUBE (AD921912) FAA, U.S AD 92 -19 -12 09 -Oct - 25 -jan -93 05 (AD921912) 1991 LEARJET AW 32 - Goodyear Flight Eagle Tire Tread FAA, U.S AD 2001 -07 -11 05 -feb -01 17 -May -2001 N/A by s/n on tire. 021 Separat LEARJET SB 00 -01 Inspection/Replacement of cables 27 -feb -01 26 -mar -01 LEARJET SB 05-01 FIRE EXT. BOTTLE (HYDROST.) 18-nov-92 18-nov-92 LEARJET SB 11 -02 AIRSPEED LIMIT PLACARDS 06 -dec -76 02 -jan -77 LEARJET SB 11 -03 A AIRSPEED LIMIT PLACARDS AD841906 FAA, U.S AD 80 -17 -11 18 -sep -80 A 23 -sep -80 LEARJET SB 11 -04 WASTE DISP.REC. PLACARDS 18 -dec -81 25 -jul -91 N/A due to model and s/n. AD740809 LEARJET SB 11 -05 CREW SEAT BELT PLACARDS 31 -aug -83 23 -Oct -1983 LEARJET SB 11-06 BATTERY PLACARDS 21-jul-87 25-jul-91 N/A due to SB32-04 is carried out. LEARJET SB 11 -07 ID PLATE (O) 06 -nov -92 23 -jul -93 LEARJET SB 11 -10 Repl.of Fuel Servicing Placards 17 -dec -01 06 -feb -04 LEARJET SB 21 -02 Cabin Air Distribution 02 -May - 25 -jul -91 N/A. Optional. 1977 LEARJET SB 21 -03 CONDENSER FAN ASSY. AD781603 FAA, U.S AD 78 -16 -03 12 -jul -78 30 -jul -78 LEARJET SB 21-04 Inst. of Refrigeration 22-feb-79 23-May-1979 Syst.Warn.Placard LEARJET SB 21-05 CABIN PRES. SAFETY VALVE 18-dec-79 05-May-1980 LEARJET SB 21 -06 Insp.of Air Distr.Sleeves & Clamps - 23 -sep -80 16 -nov -80 Tailc LEARJET SB 21 -07 CABIN PRES. SAFETY VALVE 28 -Oct - 29 -jan -81 (CHANGED) Garrett SB 5-2290 1980

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 39(195) LEARJET SB 21-14 1 OUTFLOW VALVE SAFETY VALVE (R) 03-jan-95 1 22-dec-95 Superseded by SB 21-19. LEARJET SB 21 -15 2 Repl. of Refrig.Syst. Press Switch 22 -jul -05 2 11 -Oct -2005 N/A to Keith R34. LEARJET SB 21 -18 3 Imp.W -shield Aux.Defog & Aux.Crew 11 -aug -08 3 04 -nov -08 N/A N/A due to AAK86 -1 not incorporated Heat LEARJET SB 21 -19 Insp.of Cabin Press.Outflow & Safety FAA, U.S AD 95 -20 -03 03 -jan -95 22 -dec -95 Vlv 130406-21-A4011 R2,102850-21- A4021 R2 LEARJET SB 21 -24 1 Repl.of Aux.Cabin Heater Wiring FAA, U.S AD 98 -06 -28 13 -aug -96 1 09 -dec -08 N/A due to s/n LEARJET SB 21 -25 3 Inst.of Improved Refrigeration 12 -nov -07 2 06 -feb -08 N/A Due to Keith Aircondition System TR -134 Installed Comp.Asse LEARJET SB 21 -26 5 Mod.of Auxiliary Cabin Heather 16 -May - 5 05 -Mar -2012 2007 LEARJET SB 22 -02 Sec.Yaw Damper Servo Cable Clamp 06 -sep -78 10 -mar -78 Bolt LEARJET SB 22 -03 Repl.of Yaw Damper Servo Sector 02 -feb -79 03 -jun -79 Bolts LEARJET SB 22 -04 C Mod. of Mach Trim Computer J.E.T SB 25 -mar -80 C 01 -sep -91 N/A 501-1132-9E, -10B, -11 LEARJET SB 22 -05 Mod.of FC -530/ -535 Autopilot 05 -jan -87 25 -jul -91 N/A N/A due to A/P model Computer LEARJET SB 22 -07 3 Inst.of Autopilot Accelerometer 11 -jun -07 2 29 -May -2007 N/A AAK 83 -2 not complied with. Monitor LEARJET SB 23 -03 2 Increased FOD Protection -Installation 09 -jul -01 2 11 -jan -06 Previous revision carried out. of Antenna Protection. LEARJET SB 24 -03 AC Inverter Excitation & Control FAA, U.S AD 76 -18 -07 09 -aug -76 29 -sep -76 Check LEARJET SB 24 -04 A Reloc.of AC 01 -jun -77 A 24 -dec -77 Second.Inv.Ground.Connection LEARJET SB 24 -05 Repl.of Generator Bearings Bendix SB 02 -May - 27 -jul -78 R-358 & Suppl No.1 1978 LEARJET SB 24 -06 Insp.of Battery Vents for Obstruction 29 -sep -80 25 -jul -91 N/A Found not applicable due to incorporation of SB 24 - 15. LEARJET SB 24 -07 Current Limiter Box Moisture Proofing 15 -jan -81 25 -jul -91 LEARJET SB 24 -08 Insp.of No.4 Gauge Electrical Cables 11 -May - 25 -jul -91 1982 LEARJET SB 24 -09 Insp.Fuses for Proper Prot.Covering & 19 -apr -83 25 -jul -91 PN

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 40(195) LEARJET SB 24-10 Reloc.of Battery Vent Inlet Fitting FAA, U.S AD 86-05-05 Rev 1 18-Jul- 18-jun-86 AD860505 1985 LEARJET SB 24-11 Add.of Ret.for Gen.Warn.Ctrl 01-nov-90 25-jul-91 Box.Connect LEARJET SB 24-15 1 Inst.of Concorde Sealed Lead-Acid 24-mar-08 1 04-sep-08 PCW Batt. LEARJET SB 25-03 Insp.of Drag Chute Mechanism Bolt 10-nov-80 09-jun-81 LEARJET SB 25 -04 A Insp.of Drag Chute Mech.for Proper 11 -nov -81 A 15 -aug -82 Clear LEARJET SB 25 -06 Insp.Drag Chute Canister Lid Latch 19 -feb -87 25 -jul -91 Screw LEARJET SB 26 -02 A Verif.& Ident.of Eng.Fire 30 -apr -91 A 25 -jul -91 Ext.Bottl.Wire LEARJET SB 26-03 2 Repl. of Fire extinguishing Bottle Ass. 20-aug-07 2 21-jan-08 Carried out at L/H side LEARJET SB 26 -04 1 Engine Fire Element Insp./repl. 11 -aug -08 1 04 -nov -08 N/A N/A by s/n on elements LEARJET SB 27 -05 Stall Warn.Computer Plug & 13 -sep -76 31 -dec -76 Receptacle ID LEARJET SB 27 -06 Insp.of Alt.Pressure Switch Wiring 06 -May - 27 -dec -77 1977 LEARJET SB 27 -07 Mod.of Spoileron Computer Assembly 01 -Oct - 12 -mar -85 J.E.T SB 501-1133-4 1977 LEARJET SB 27 -08 Wiring of Pilot & Copilot Cntrl Wheel.. 24 -May - 13 -dec -81 1978 LEARJET SB 27 -09 Insp.of Wing Flap Actuators 19 -dec -78 25 -jul -91 LEARJET SB 27 -10 Rework of Pilot/Copil.Ctrl Wheel Trim 19 -apr -79 01 -jul -80 .. LEARJET SB 27 -11 Insp.of Aileron for Drain Holes 06 -nov -79 27 -dec -79 LEARJET SB 27-12 B Stall Warn.Accelerometer Op.Check FAA, U.S AD 82-01-05 Rev 2 LFV 25-sep-81 B 12-jun-06 Överförd till A1 phase insp. Ref. Learjet Chpt.5 LVA1912 rev.74 och FAA AMOC från 2005-03-24 LEARJET SB 27-14 Insp.of Welds on Rudder Pedal 08-sep-83 27-mar-84 Supp.Assy LEARJET SB 27-16 Insp.Flap Attach.Fittings for Cracks 27-May- 03-nov-86 1986 LEARJET SB 27-24 Insp.of Ail.& Rudder Ctrl Cable Assy 08-nov-93 01-dec-93 Ter LEARJET SB 27-33 Removal of Sealant from Aileron Rib 27-May- 19-feb-98 1997

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 41(195) LEARJET SB 27-35 4 Inst.of Secondary Locking Feature 15-aug-03 4 03-nov-03 Previous rev. carried out. LEARJET SB 27 -36 Replacement of Spolier Actuator FAA, U.S AD 99 -23 -19 14 -dec -98 09 -dec -08 N/A due to s/n LEARJET SB 27 -40 6 Insp/Inst. of Flap Structure 16 -aug -10 6 10 -Nov -2011 PCW Previous revision carried out Components LEARJET SB 27 -43 Recalibration rosemount 19 -jan -05 17 -mar -05 N/A due to STC ST00321WI -D not complied with. LEARJET SB 27 -45 1 Insp. Spoiler panels 29 -Mar -2012 LEARJET SB 28-02 Insp.of Tip Tank Elect.Conduit for 20-feb-76 03-jan-77 INAKTIV Damag LEARJET SB 28-04 Reloc.of Fuel Probes on Wing Tank 01-nov-77 20-sep-79 Access LEARJET SB 28 -05 Op.check of Fuel Jettison Valves 14 -feb -80 07 -sep -80 INAKTIV LEARJET SB 28 -06 Insp.of Rec.for Field Rep.of Mot.Flow 21 -aug -80 24 -sep -80 Vl LEARJET SB 28 -08 Insp.of Motive Flow Vlv Shroud Cover 27 -aug -90 09 -jan -91 LEARJET SB 28-10 Inspection of Tip Tank Flapper Valves FAA, U.S AD 2005-16-09 FAA, U.S 06-Oct- 14-sep-05 Flapper p/n 2323006-802 previously installed. No AD 95-25-03 1995 further action req. LEARJET SB 28-11 5 Inst.of Standby Fuel Pump FAA, U.S AD 2007-04-18 28-sep-09 5 26-feb-10 Rev. 1-4 PCW. AFM cheched for Change 14 Annunciators LEARJET SB 28-14 2 Repl.of Tip Tank Flapper Valves 09-May- 2 31-aug-01 SB previuos installed. 2001 LEARJET SB 28-18 Insp./Repl. of Fuel Filter Elements 24-aug-09 30-Oct-2009 N/A due to filter p/n LEARJET SB 29 -01 1 Insp.RH Eng.Hydr.Press.Line for FAA, U.S AD 83 -08 -03 10 -sep -96 1 19 -dec -08 due to remod. hyd.syst. Interfer LEARJET SB 29 -02 Insp.LH Eng.Hydr.Lines for FAA, U.S AD 84 -20 -06 15 -jun -83 14 -aug -83 Interference LEARJET SB 29 -05 Repl.of Hydr.Reservoir Sight Glass 07 -Oct - 23 -jul -93 N/A Assy 1992 LEARJET SB 30 -10 1 Repl. of Wing Anti -Ice Transverse Duct 12 -feb -99 1 08 -dec -99 LEARJET SB 30 -11 3 Inst.of High Current Capacity Wire 05 -May - 3 04 -sep -08 PCW 2008 LEARJET SB 31 -01 Repl.of Oil Press.Annunciator Cap 26 -Oct - 01 -dec -93 Assy 1992 LEARJET SB 32 -03 Insp.of LG Brake & Torque Link for 25 -aug -81 25 -jul -91 Inter

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 42(195) LEARJET SB 32-04 Repl.of LG Hydraulic Selector Valve 23-jan-89 09-jan-91 LEARJET SB 32 -07 1 Inst.of MLG Lower Torque Arms 10 -nov -95 1 31 -Oct -2003 LEARJET SB 32 -18 Inst.of Main Landing Gear Wheel 19 -jan -99 15 -mar -99 N/A. Affected Wheel Assy not installed. Screens LEARJET SB 32 -20 Repl.of Landing Gear Shuttle Valve 09 -mar -00 30 -jun -00 N/A Found N/A to Part Number. LEARJET SB 32 -21 Repl.of Brake Valve Adjustment Screw 01 -May - 26 -mar -01 2000 LEARJET SB 32 -23 1 Mod landing gear squat switch wiring 09 -apr -07 1 29 -May -2007 N/A Previously carried out LEARJET SB 32-26 Insp/Repl of the Nose Gear Wheel 18-jan-10 10-May-2010 N/A by s/n Assy LEARJET SB 32 -27 IR Sealant on Anti -Skid Solnoid 14 -Jun -2011 LEARJET SB 33 -01 Add.of Drain Holes in Tip Tank Nose 03 -jan -77 11 -feb -77 Cone LEARJET SB 33 -03 Insp.& Mod. of LH Fwd Cabinet Light 24 -apr -85 25 -jul -91 N/A N/A due to interior config. Assy LEARJET SB 33-05 A Deactiv.of Fwd Cabinet & Overhead FAA, U.S AD 91-03-08 21-dec-90 A 19-dec-08 Light. AD901406 LEARJET SB 33-06 A Activ.of Fwd Cabinet & Overhead 12-apr-91 A 26-feb-09 Fluore.. LEARJET SB 34-04 Insp.of Static Ports 11-jun-82 25-jul-91 LEARJET SB 35 -01 Insp.of Oxygen Mask Microphone Jack 09 -sep -77 25 -jul -91 Wiri LEARJET SB 35 -04 Replacarding Oxygen Bottle Shutoff 27 -feb -04 04 -aug -04 Placards installed. Valve LEARJET SB 36 -02 A Insp.& Repl.of Eng.Bleed Air Flex 25 -May - A 01 -sep -91 Tube.. 1978 LEARJET SB 36 -03 Repl Air Bottle & Weight -Balance 14 -dec -09 11 -mar -10 Due to weighing after installation of bottle p/n Change 6600194-6 LEARJET SB 51 -01 Insp.Baggage Comp.Struct. for 18 -jul -85 06 -sep -85 Corrosion AD 84-12-03 LEARJET SB 51 -03 Insp.of Forward Engine Beam Shear FAA, U.S AD 2004 -03 -08 01 -feb -01 1200H 06 -sep -01 N/A N/A due to SB 51 -04 performed. Web. LEARJET SB 51 -04 5 Rep.of Forward Engine Beam Shear FAA, U.S AD 2004 -03 -08 12 -Oct - 5 11 -mar -10 No rework required Web 2009 LEARJET SB 51 -4 3 20 -jan -05 No rework req.

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 43(195) LEARJET SB 52-02 Adj.of Lwr Cabin Door Hok Act.Toggle 09-aug-77 14-jun-85 Sw. LEARJET SB 52-04 Mod.of Access Door Lock Assemblies 16-apr-79 25-jul-91 N/A Found N/A. No locks installed. LEARJET SB 52 -05 Insp.of Cabin Int.Liner -Areas Of 04 -nov -80 25 -jul -91 Emerg.. LEARJET SB 52 -06 Mod.of Lwr Cabin Door Hook 18 -dec -92 01 -dec -93 Mechanism LEARJET SB 52 -10 1 Repl.of Upper Cabin Door Torsion Bar 03 -jun -99 1 20 -sep -99 N/A. 24 inch door not installed. Arm LEARJET SB 53 -01 Inst.of Rivets at Fwd Eng.Beam & 27 -apr -77 01 -sep -91 N/A Frame24 LEARJET SB 53 -07 Inspect for Tailcone Drains 18 -dec -92 01 -dec -93 LEARJET SB 53 -08 Inst.of Nutplates on Circ.Br.Panel 14 -feb -94 15 -dec -94 Suppo LEARJET SB 53 -10 1 Repl.of LowerStinger & Ventral Fin 17 -mar -08 1 14 -May -2008 N/A Due to Avcon Fins STC ST00432WI Skin LEARJET SB 53 -11 3 Mod.of Tailcone Ballast Weight 01 -jun -09 3 08 -jan -10 Ballast not/never installed Installat LEARJET SB 53 -13 Insp. Intern. baggage comp. floor 16 -jan -06 08 -mar -06 N/A Due to S/N splice LEARJET SB 54 -01 Insp.for Silicon Firesleeve -Start& Gen 11 -jun -82 25 -jul -91 Ca LEARJET SB 54 -03 Insp/Firewall Sealing Modification 16 -mar -01 17 -apr -07 L/H side carried out LEARJET SB 54 -04 Insp/Repl.of Upper and Lower Pylon 08 -aug -01 22 -mar -02 N/A by s/n on aircraft. Skins LEARJET SB 55 -01 Insp.Horiz.Stab.Hinge Assy for Cracks 16 -aug -91 16 -aug -91 N/A No Thrust Reversers installed. LEARJET SB 55 -04 2 Inst.of Doublers on Horiz.Stabili.Skin 23 -feb -09 2 10 -jun -09 PCW LEARJET SB 55-05 Imp.of Horiz.Stabilizer Actuator 16-jan-98 30-Oct-1998 Access LEARJET SB 55-06 Mod.of Navigation Light Wiring 30-aug-04 30-nov-04 Conduit LEARJET SB 71-01 Insp.for Interf.between LH Eng Starter 08-sep-76 02-jan-77 & LEARJET SB 71-02 Eng.Firewall Sealing at Feed-Thru 13-May- 25-jul-91 Condui 1982 LEARJET SB 71-03 1 Insp.of Fwd Eng.Mounts for Cracks FAA, U.S AD 87-02-06 10-feb-95 1 27-jan-97

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 44(195) LEARJET SB 71-05 2 Repl.of Fwd Eng.Mount Bolts 18-jun-93 2 10-jan-95 Bolt replaced L/H side w/o C00454 1997-01-21. LEARJET SB 76 -01 B Insp.of Eng. I.T.T. Cable Connectors 07 -nov -83 B 27 -sep -84 LEARJET SB 80 -02 A Repl.of Starter Rly Cover & Magnetic 04 -mar -77 A 18 -sep -79 Cor Bendix SB R-352A, R-355 LEARJET SB A27 -42 Insp/Repl.of Aileron Ctrl Cables 23 -dec -02 11 -jan -03 1ea: cable effective by cal.time, inspected OK. LEARJET SB A32 -15 1 Insp.of Landing Gear Actuator Pistons 21 -apr -97 1 19 -feb -98 LEARJET SSK 981 Repl. of Spoiler Act. Support Bracket 19-dec-86 27-mar-01 LEARJET SSK 993 2 Repl. of Landing Gear Wheel Bearings 21 -jan -91 2 08 -jan -98

LFV, Luftfartsverket LFV LVA 1613 Modifiering av övre kabindörr LEARJET AMK79 -09 27 -May - 17 -nov -80 1980 LFV LVA 1625 A Till,gg i flyghandbok. T,thetskontroll FAA, U.S AD 80 -19 -09 Rev 1 23 -jun -80 A 24 -dec -80 LEARJET AMK80-07 LFV LVA 1748 Revision av Flyghandbok. FAA, U.S AD 81 -13 -07 24 -aug -81 10 -aug -81 Br,nslem,ngd LFV LVA 1912 Periodisk kontroll av Stallvarning. FAA, U.S AD 82 -01 -05 Rev 2 10 -nov -83 12 -jun -06 Överförd till A1 phase insp. Ref. Learjet Chpt.5 LEARJET SB 27-12 Rev B rev.74 och FAA AMOC från 2005-03-24 LFV LVD 1635 A Revision Flyghandbok/kontr. A/P & FAA, U.S AD 80 -19 -11 Rev 1 15 -jul -85 A 28 -sep -09 PCW Ref. FAA AD 80 -19 -11 R1 mod. LFV LVD 2034 Reducering av MMO FAA, U.S AD 85 -16 -04 30 -aug -85 22 -jan -86 N/A due to config. (STC SA766NW never been installed). LFV LVD 2046 Kontroll av batterihållare FAA, U.S AD 86 -05 -05 Rev 1 25 - 18 -jun -86 Nov -1985 LFV LVD 2352 Shoulder Harness Inst. FAA AC 43 -13 23 -May - 25 -jul -91 checked OK. CHPT 9 1991 LFV LVD 2853 Periodisk funktionskontroll av 23 -mar -98 02 -dec -10 nödutgång LFV LVD 3148 Modif. Transponder kontrollpanel 17 -aug -01 12 -feb -09 N/A due to p/n

NYGE, Saab Aerotech Aircraft Services NYGE SB 08 -06 -34 - A EGPWS System Provision for Inhibit 30 -nov -09 A 04 -mar -10

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 45(195) 03 Unit) NYGE TDM 02 -20 GMS Prototyp 27 -aug -02 05 -jun -04 utf. i samband med Kapsel -mod. NYGE TDM 02 -25 Installation Underving -kanaler 16 -Oct - 10 -nov -03 LFV app.No: M21/02 revision 1. 2002 NYGE TDM 02 -26 Box 3 Installation 01 -nov -02 29 -sep -03 Approved in accordance with EASA 2004 -11267 and with LFV AFMS S04/89 R2. NYGE TDM 02 -28 Utv. Framtagning mod.balkar LR -35 18 -nov -02 10 -nov -03 NYGE TDM 03 -03 B Operators Console L35A 02 -apr -07 B 26 -feb -08 only updated to rev.B NYGE TDM 03-07 Alkan Fairings (mod.) 27-feb-03 10-nov-03 Approved by EASA no. 235 in accordance with LFV Mod. Cert. No. M29/03. NYGE TDM 03 -17 ACAS Installation 06 -May - 30 -nov -04 Approved i.a.w. EASA Doc. No: STC S.A.00255. 2003 NYGE TDM 03 -19 Mission Inverter Modif. 20 -nov -03 05 -nov -03 Approved in accordance with LFV M37/03 and EASA 1985. NYGE TDM 03 -23 U95 Installation L35A 10 -sep -03 D 10 -mar -06 Rev.D updated NYGE TDM 04-03 D Astor L35A 16-jan-04 D 21-Nov-2012 NYGE TDM 04 -06 C Darts System L35A 05 -dec -06 01 -jan -06 Approved in accordance with DOA 21J.108.04 -06. NYGE TDM 05 -06 Removal of Reflector System 30 -May - 02 -jun -06 Approved i.a.w. DOA 21J.108.05 -06 2005 NYGE TDM 05 -15 Install. Jumpseat Intercom 18 -jul -05 23 -nov -06 Approved in accordance with DOA 21J.108.05 -15A NYGE TDM 05 -19 Install. GPS Map and GP&C 08 -sep -05 23 -nov -06 Approved in accordance with DOA Transponder NYGE TDM 05 -20 Install. Mission Equip. new OP - 13 -sep -05 23 -nov -06 Approved in accordance with DOA 21J.108.05 -20A Console NYGE TDM 05 -26 Install. Cabin Side Wall Cable Channel 20 -Oct - 23 -nov -06 Approved in accordance with DOA 21J.108.05 -26A 2005 NYGE TDM 06 -22 Re -mod. Hydraulic system 05 -May - 07 -nov -06 2006 NYGE TDM 06 -36 A A100 (to carry on L35A) 23 -apr -07 A 25 -feb -08 NYGE TDM 08-02 C Enhanced Surveillance L35A 09-mar-10 C 28-jul-09 Original compliance to rev A of TDM. TDM rev B and C does not affect previous compliance. NYGE TDM 08-06 C EGPWS MK.8 & Mission Inhibit System 05-mar-10 C 04-jul-08 Original compliance with rev A. Rev B and C does not affect previous compliance. NYGE TDM 08-07 E LR35A GPS-Map Display 12-apr-10 E 28-Aug-2012 Compliance was IAW TDM rev A. Previous compliance not affected by rev D.

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 46(195) NYGE TDM 08-09 C Install Termination resistor C 01-09-2012 NYGE TDM 08 -13 A Barlast DARTS L35A 10 -mar -08 A 10 -mar -08 NYGE TDM 08 -17 C ELT 406 L35A 04 -jul -08 C 04 -jul -08 Original compliance with TDM rev A. Rev B and C does not affect previous complaiance. NYGE TDM 08 -26 A Mission Antenna Adapter 28 -Oct - A 22 -dec -08 2008 NYGE TDM 09 -30 E LR35A Removable Hard Disk Drives 30 -apr -10 E 04 -July -2012 Original compliance was i.a.w TDM rev A. Rev B does not affect previous installation. NYGE TDM 10 -04 B Overload Sensing Control 02 -jun -10 B 28 -Sep -2012 NYGE TDM 10 -27 A LR35A U95 -D2 22 -apr -10 A 15 -jun -10 NYGE TDM 10 -31 A Overload Sensing Control Provisions 01 -jul -10 A 06 -jul -10 NYGE TDM 12 -22 A L35A Move mission inverter A 28 -Sep -2012 NYGE TDM 12 -23 A Installation laser prismor L35 A 28 -Sep -2012 NYGE TDM 95 -01 Installation Intercom 10 -jan -95 16 -jan -95 NYGE TDM 95-03 Modifiering Transponder-system 06-feb-95 16-jan-95 NYGE TDM 96 -04 Miss -rack,GPS -antenn,CVR,inverter 12 -feb -96 15 -mar -96 m.m. NYGE TDM 97-01 TAPS 20-feb-97 01-jan-98 NYGE TDM 98 -06 Astor L35A 09 -mar -98 27 -apr -98 NYGE TDM 98 -12 Installation BRNAV L35A 26 -jun -98 31 -May -1998 NYGE TDM 98 -13 Kontrollprogram SE -DHP 26 -jun -98 15 -aug -98

ROCKWELL, Rockwell Collins U.K.Ltd ROCKWELL SIL 07 - Reply Inhibition On The Ground EASA AD 2009 -0097 Rev IR 25 -May - 28 -jul -09 1 2007

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 47(195) 2 GFE Aircraft Mitsubishi MU-2 2.1 Mitsubishi MU-2 Aircraft Maintenance Program

2.1.1 Comprehensive description of Mitsubishi Maintenance Requirements Manual (MR-0178-2):

The maintenance is (according to Mitsubishi Maintenance Requirements Manual MR-0178- 2.) divided into 100 hours intervals between each periodic inspection. Some inspections have both flight time and calendar time limitations; they must be complied with when the first limitation becomes due. For maintenance planning purpose, a "Window For Compliance" can be established for each inspection. An inspection accomplished within the window, will be considered as if it was completed at the flight time or calendar time due. It is not allowed to accumulate the time between inspections.

Inspection list according to Mitsubishi Maintenance Requirements manual MR-0178-2: • 100 Hrs/12 Month • 200 Hrs/12 Month • 600 Hrs/36 Month • 1000 Hrs • 1200 Hrs • 1800 Hrs • 2000 Hrs • 1 Year • 2 Year • 10 Year • Detailed and General Engine Inspection

2.1.2 Modifications that affects the maintenance program If no individual reg. numbers are mentioned, the information applies for all six individuals. • The fuselage is modified with a hatch, which enables deployment and changing Soft Sleeve Targets during the flight. • An inboard hydraulic driven winch - Air Target MBV-7 Mk II - is installed. (SE- GHD, SE-IOV and SE-IUA). • An aircraft hydraulic system, which consists of a hydraulic oil tank installed in the centre wing leading edge, an engine driven hydraulic pump installed on the left engine and a shut off valve installed in the left wing leading edge, has been installed in order to supply the inboard winch with necessary hydraulic power for operation. (SE-GHD, SE-IOV and SE-IUA). • One retractable launcher arm for sleeve targets is installed under the fuselage. (SE- GHD, SE-IOV and SE-IUA). • A set of Laser Reflector Prisms is installed on the fuselage. (SE-GHD, SE-IOV and SE-IUA)

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 48(195) • The wings have been modified with hard points to carry external under-wing stores • The nose radome and wing tip tanks have been modified with radome covering antennas for the inboard ECM-system ASTOR. (SE-GHA, SE-GHB and SE-GHF). • To supply the ECM equipment, a 3-face AC, 3kVA inverter system has been installed in the inboard aft baggage area. • An operator console is installed in the cabin with equipment to operate the winch and ECM units, including a set of surveillance equipment as TV-camera, mirrors etc. • On airplanes modified with ECM System, the R/H steering wheel is removed by installation of operator’s work station. (SE-GHA, SE-GHB, SE-GHD and SE-GHF). • AMOC Approval: EASA.A.AMOC.01276. Exemption from installation of Rosemount ice-detector in accordance with JCAB TCD4529-97 and MHI SB217.

2.1.3 Maintenance Documentation Maintenance of the aircraft is conducted according to the following documentation: • Mitsubishi Maintenance Requirement Manual MR-0178-2 • Honeywell MM 72-01-32 applicable to TPE331-6-252M • Honeywell SB TPE331-72-0404 applicable to TPE331-6-252M • Honeywell SB TPE331-72-0019 • Hartzell SL 61-61Y

2.1.4 Guiding documents to be used during maintenance: • Mitsubishi Maintenance Manual YET 68035 • Mitsubishi Maintenance Manual YET 71370 • Mitsubishi Maintenance Manual YET 74132 • Mitsubishi Illustrated Parts Catalogue YET 68036B • Mitsubishi Illustrated Parts Catalogue YET 72092A • Mitsubishi Illustrated Parts Catalogue YET 74134A • Mitsubishi Structural Repair Manual YET 72035A • Mitsubishi Airplane Flight Manual • Mitsubishi Pilot Operating Manual • Mitsubishi Service Bulletins, -Recommendations, -Letters • Honeywell TPE331 Service Bulletins. -Recommendations. –Letters • Saab AB TVO • Saab AB TDM

2.1.5 Maintenance Tasks related to changes The following maintenance tasks are not included in the aircraft manufactures’ maintenance manual. The tasks need to be included in the operators AMP: • Launcher Arm 3 months inspection • Launcher Arm 100 hours inspection • Provisions for Special Mission. 1 year inspection • Special Operational Fatigue Inspection 1000 hours

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 49(195)

2.1.6 Guiding documents issued by the Agency and Aviation Authority for both Airframe and Engines: • Requirements in BCL-M4.3 • FAA Airworthiness Directives • JCAB Airworthiness Directives • EASA Airworthiness Directives • LVD Swedish Airworthiness Directives.

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 50(195)

2.2 GFE Aircraft Mitsubishi MU-2 SE-GHA

2.2.1 Aircraft Specification Type: Serial Registration : Airframe Total Date Number: total Hours: Landing Reference: Cycles: MU-2B-20 283 SE-GHA 10586 5954 2012-11-23

2.2.2 Engines Type: Honeywell TPE331 -6-252M Serial Total Hours Total Hours remaining to Number: Since New: Cycles overhaul/HSI/GBl: Since New: Left Engine P27094 8140 10755 3330/923/2723 Right Engine P20322 3718 4975 1693/1073/2873

2.2.3 Propeller Type Number: Serial Number: Overhaul Due Date: Left Propeller HC-B3TN-5E BVA 6125 2014-12-16 Right Propeller HC-B3TN-5E BVA 6718 2015-11-15

2.2.4 Avionics System: Type / Part Number: Note: Autopilot & Flight Director Century IV COM/NAV/GPS 1 Garmin GNS 530 COM/NAV/GPS 2 Garmin GNS 430 Audiopanel Bendix/King KMA-24H-70 MKR Bendix/King KR -21 DME Bendix/King KDM -706 ADF Bendix/King KDF-806 XPDR 1 Garmin GTX 330D Mode S EHS XPDR 2 Garmin GTX 330 *) Mode S EHS RDR ALT Bendix/King KRA-10A ELT Kanad ELT 406-AF-H Airspeed I ndicator LH / RH Aerosonic 20040 -161 / 20040 - 0186 Altimeter LH United Instr. Inc. 5934 PAD -1 Altimeter incl. encoder RH United Instr. Inc. 5035P -P40 Altitude Reporter Narco AR 850 Altitude Alerter Aero Mechanism AM 275C Vertical Speed Indicator LH Aerosonic RC-60-MS-10-3 Attitude Gyro & Flight Director Ind. Century 52C77

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 51(195) LH Attitude Gyro Ind. RH AIM 504-0006-914 Turn & Bank Ind. LH R.C Allen A5930-02 Horizontal Situation Indicator LH Bendix/King KPI-553A DG -Gyro Sperry C -14A Directional Gyro RMI Ind. LH AIM 254 -1D CDI Indicator Garmin GI-106A *) XPDR 2 without diversity configuration

2.2.5 Mission System System : Description: Fixed general installations VHF/UHF COM 1 & 2 FR31 GPS MAP JET SI-3003B Inverter 115/200VAC 400Hz 3 phase Laser Prism MIL-STD-1553 Bus LH Wing Pylon Wing Pylon NATO 14” Alcon Ejector Unit LH and RH Wing Pylon EW system ASTOR Fixed installed system ADRIAN Pod mounted system LH and RH Wing Pylon U95 N Pod mounted system LH Wing Pylon A100 Pod mounted system LH Wing Pylon Missile Threat Simulator DARTS Pod mounted system LH Wing Pylon Chaff Dispenser BOX 3 Pod mounted system LH and RH Wing Pylon

2.2.6 Mission Cable Harness to Hard Points Used for Mission LH NATO Hard point: RH NATO Hard point: Note: System: Adrian C & S, U95-N, A100, General Signal Harness General Signal Harness DARTS and BOX 3 AWG22 shielded x 44 AWG22 shielded x 50 U95-N and A100 MIL-STD-1553B Data Triax Cable x 1 Bus U95-N, A100 and DARTS AC Power AWG 12 x 4 115/200VAC 400 Hz 3- twisted Phase 3 x 10 A AWG 16 x 2 AWG 20 x 2 Adrian C & S and BOX 3 DC Power 28 VDC 200 DC Power 28 VDC 200 AWG 2 x 2 A A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 52(195) Adrian C & S Coax Cable 1 x 50 Ω Coax Cable 1 x 50 Ω Prepared installation Ethernet LAN Cable

2.2.7 Antenna Layout

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 53(195)

2.2.8 Inspection due times and dates Status date November 23 rd 2012.

Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date Aircraft SE-GHA Vingstudie MU-2 AMP 2011-09-19 10470,92 11500 100 Hour Inspection AMP 2012-09-14 10568,72 10670,92 2013-09-14 200 Hour Inspection AMP 2012-09-14 10568,72 10768,72 2013-10-04 600 Hour Inspection AMP 2011-04-13 10424,42 11024,42 2014-04-12 1000 Hour Inspection AMP 2011-09-19 10470,92 11500 1200 Hour Inspection AMP 2012-09-25 10568,72 11768,72 1800 Hour Inspection AMP 2005-02-04 9700 11500 2000 Hour Inspection AMP 2005-02-03 9500 11500 1 Year Inspection AMP 2012-09-18 10568,72 2013-10-04 2 Year Inspection AMP 2012-09-20 10568,72 2014-10-04 10 Year Inspection AMP 2005-02-04 9700 2015-02-02 Engine S/N P-20322 Remaining Engine Assembly (Overhaul) AMP 12280,1 1693,72 Engine Hot Section Inspection AMP 11660,1 1073,72 Engine Gearbox Inspection AMP 13460,1 2873,72 Engine S/N P-27094 Engine Assembly (Overhaul) AMP 13916,9 3330,52 Engine Hot Section Inspection AMP 11509,8 923,42 Engine Gearbox Inspection AMP 13309,8 2723,42

Propeller L/H O/H AMP 2009-12-17 13394,52 2014-12-16 Propeller R/H O/H AMP 2010-11-16 13382,5 2015-11-15

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type

2012-12-06

Document number Page 54(195)

2.2.9 Implemented Changes Abbreviations: Abbr. Issued by Explanation AAK Learjet Aircraft Accessory Kit AD EASA, FAA, Finnish CA, Airwortness Directive JCAB AMK Learjet Aircraft Mod Kit AW Learjet Accessory Wire LVA LFV Luftvärdighetsanvisning LVD LFV Luftvärdighetsdirektiv MSB Mitsubishi Mitsubishi. SB MSR Mitsubishi Mitsubishi SR SA Hartzell Service advisory SB Keith, Learjet, Nyge , Service Bullentin Century, Garrett, MAI, Hartzell, Mitsubishi, Narco SI Hartzell Service information SIB EASA Service information bullentin SIL Rockwell Service information letter SL Mitsubishi Service Letter SN Mitsubishi Service news SR Mitsubishi Service recomendation SSB Nyge and Garmin Sofware SB SSK Learjet Special Spares K it STC Avcon, Flight Int., Keith, Supplement Type Certificate

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 55(195) Mitsubishi TDM Nyge Tekniskt Direktiv Materiel TVO Nyge Teknisk Verkstad Order

Status date November 23 rd 2012. SB/AD etc Rev Subject Document reference Eff. date Rev Compliance Status Remarks Reference

CENTURY, Century Flight Systems Inc. CENTURY SB CSB - Check for frayed Bridle Cable 21 -feb -05 16 -nov -10 2005-01

EASA, European Aviation Safety Agency EASA AD 2006 - Incorrect transponder altitude 30 -aug -06 27 -nov -09 0265 EASA AD 2009 - Portable Fire Extinguishers - 25 -nov -09 07 -May - N/A by current P/N installed 0251-E Ident/Repl 2010 EASA AD 2009 - Halon 1211 Fire Extinguishers EASA AD 2009 -0278 FFE ASB26 -115 Rev C 15 -dec -09 07 -May - N/A by current P/N installed 0262 Id/Repl 2010 EASA AD 2009 - Halon 1211 Fire Extinguishers EASA AD 2009 -0262 22 -dec -09 07 -May - N/A by current P/N installed 0278 Id/Repl 2010 EASA AD 2010 - R1 Mode S Transponder - 11 -jan -10 R1 10 -mar -10 N/A due to model 0003 Check/Modification EASA AD 2012 - KIDDE GRAVINER HAND OPERATTED 04 -Oct - 0037 FIRE EXTINGUISHER 2012 EASA SIB 2008 - Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN 17 -dec -08 21 -sep -10 N/A by SSB 0845 incorporated 58R1 SSB0845 Rev IR EASA SIB 2009 -14 Upgrade to main unit/GPS software 24 -jun -09 28 -sep -09 N/A due to model

FAA, U.S, Federal Aviation Administration FAA, U.S AD 2000 - 1 Flight in Icing Condition AFM De - FINNISH AD M 2435/97 FINNISH AD M 07 -jul -00 1 22 -nov -01 Action not required due to s/n. N/A Due to 09-15 FAA, U.S AD icing 2786/00 MAI SB 086/74-002 Rev A MAI paragraph b. 2000-02-25 SB 093/22-009 MAI SB 096/30-004

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 56(195) MITSUBISHI SB 226 Rev E MITSUBISHI SB 231 Rev B MITSUBISHI SB 232 Rev A FAA, U.S AD 2003- Windshield check FINNISH AD M 3076 LFV LVD2678 MAI SB 01-Oct- 16-nov-10 17-04 087/56-001 Rev B MITSUBISHI SB 224 Rev 2003 C FAA, U.S AD 2003- 1 Forecast Icing Conditions FINNISH AD T5007/03 JCAB AD TCD- 16-apr-04 1 17-May- inserted in AFM limitations 22-07 4753A-2004 MAI SN 071/00-006 Rev D 2004 MITSUBISHI SN 117 Rev D FAA, U.S AD 2005 - Prop. mounting bolt insp. HARTZELL SB 61 -279 ALERT Rev 4 29 -jul -05 14 -sep -05 Propellerbolts previously checked u/a 14-12 FAA, U.S AD 2005- Prop de-icer "FASTprop" 14-Oct- 12-Oct- N/A Due to boots p/n 18-20 2005 2005 FAA, U.S AD 2006- Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB 11-aug-06 18-mar-03 c/o in conjunction with vingstudie 13-15 241 Rev A FAA, U.S AD 2006- Safety evaluation (feathering MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06 24-aug-06 se Mitsubishi SB 229 15-07 linkage) FAA, U.S AD 2006- Detect & correct torque transducers MAI SB 095/77-002 MITSUBISHI SB 233 22-sep-06 21-sep-06 PCW see MSB 233A 17-01 Rev B FAA, U.S AD 2006- Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 16-nov-10 17-05 FAA, U.S AD 2007- Reduce max deflect elev nose-down MITSUBISHI SB 216 MITSUBISHI SB 228 25-sep-07 11-sep-07 Previously carried out i.a.w. mentioned SB's. 17-09 trim FAA, U.S AD 71- Fuel Tank Fungus Coating Peeling 01-May-1972 01-jan-96 N/A by s/n 14-01 FAA, U.S AD 74- Windshield Outer Panes LFV LVA829 Rev A MITSUBISHI SB 163 Rev 30-jan-78 05-May- 11-01 B 1974 FAA, U.S AD 75- Main Wing Flap JCAB AD TCD-1094A-76 LFV LVA1011 Rev 05-aug-75 18-jan-77 Revision C PCW by Swedair. 16-13 A MITSUBISHI SB 167 Rev D FAA, U.S AD 75- Propeller Pitch Control Lever JCAB AD TCD-1188-75 LFV LVA1012 12-aug-75 20-jan-88 16-20 MITSUBISHI SB 168 Rev A FAA, U.S AD 78- Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A 23-feb-78 18-jan-88 03-05 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A FAA, U.S AD 81- 1 Engine Aft Nacelles 01-apr-81 1 22-nov-97 Previously complied with 06-01 FAA, U.S AD 81- 1 Engine's Electrical wiring SB 036/71- 21-jan-82 1 02-dec-10 N/A N/A by model 25-04 003A, SB 043/71-005 FAA, U.S AD 82- Electrical Wiring Inspection 15-apr-82 18-mar-82 08-02

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 57(195) FAA, U.S AD 83- 2 To preclude prop. attach bolt FINNISH AD M 1168/83 Rev 1 FINNISH AD 28-apr-82 2 20-May- Ref. MU2B MM chap 13.4 when using bolts P/N B- 08-01 failures T5114/05 HARTZELL SI 140A Rev 9 2005 3339 only FAA US AD 83-09- Strobe Light Assemblies 16-Mar- 02 2012 FAA, U.S AD 84- Torque of Air Tube Coupling Nuts SB MAI SB 047/30-001 Rev A MITSUBISHI SB 28-jun-84 31-jul-84 12 -04 047/30 -001, SB 196A 196 Rev A FAA, U.S AD 84- Elevator TrimTab Bracket Insp/Repl. MAI SB 031/27-005 Rev 1 MITSUBISHI SB 18-dec-84 18-apr-85 25-02 SB 031/27-005 R1, SB 176E 176 Rev E FAA, U.S AD 86 - NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2 13 -aug -86 15 -jul -04 Found SB 181 part 2 PCW. 15-03 Rev B FAA, U.S AD 86 - To assure anti -ice capability of pitot LFV LVD2015 Rev B 06 -Oct - 07 -feb -00 20-01 SB 1986 FAA, U.S AD 86 - To prevent engine flameout in an GARRETT SB 74 -0003 Rev 6 MAI SR 31 -dec -87 09 -mar -09 see applicable engine for c/o 26-02 iceing SB 74-0003, SR 040/74-001 040/74-001 MITSUBISHI SB 226 Rev E MITSUBISHI SR 066 FAA, U.S AD 87- Addit. Seal and Flap Flexible Shaft MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 14-jun-85 04-03 Insp SB 051/27-007, SB 198 FAA, U.S AD 87- Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 17-May- 12-02 1990 FAA, U.S AD 88- Bendix Autopilot Disengagement SB LFV LVD2190 MAI SB 066/22-006 Rev A 11-jul-98 06-jun-89 N/A N/A due to Autopilot model 13-01 066/22-006 MITSUBISHI SB 206 FAA, U.S AD 88- 1 To minimize confusion in LFV LVD2206 MAI SB 066/22-006 Rev A 28-jan-89 1 25-Jan- 21-01 autopilot/manua SB 066/22-006 2012 FAA, U.S AD 88 - To prevent flap control failure SB LFV LVD2202 MAI SB 067/27 -008 Rev A 04 -dec -88 15 -feb -95 23-01 067/27-008, SB 189B FAA, U.S AD 93 - ELECTRIC TRIM SYSTEM SB 079/27 - LFV LVD2477 MAI SB 079/27 -010 01 -jun -93 27 -mar -09 N/A by s/n 07-11 010 FAA, U.S AD 94 - Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11 -apr -94 31 -mar -93 04 -16 FAA, U.S AD 94 - Change of Flight Idle Blade Angel SB LFV LVD2551 MAI SB 016/71 -001 10 -jun -94 27 -mar -09 N/A by s/n 11 -04 016/61 -001 FAA, U.S AD 96 - Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD - 27 -dec -96 13 -feb -02 25 -02 4552 -96 LFV LVD2749 FAA, U.S AD 97 - Vent Check Valve Assy LFV LVD2769 16 -apr -97 05 -May - N/A N/A due to s/n. 04 -13 1997 FAA, U.S AD 97 - Icing related incidents/accidents 17 -Oct - 02 -dec -98 20 -14 CNL 1997 FAA, U.S AD 97 - To prevent loss of airplane FINNISH AD M 2524/98 21 -jan -98 03 -dec -10 N/A AD superseeded by AD 2010 -10 -17 25-02 ctrl/overspe

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 58(195) FAA, U.S AD 98- Forward fitting bolt of wingtip tank LFV LVD2688 19-Oct- 29-nov-96 20-39 SB 1998

FINNISH, Finnish Civil Aviation Adm. FINNISH AD M Kontroll av rören till strobe -kablarna MITSUBISHI SB 174 PART 1 Rev C 07 -jul -83 16 -nov -10 1177/83 FINNISH AD M Justering av br,nslefl"de MHI SB JCAB AD TCD -4890 -98 MAI SB 097/73 -001 12 -nov -99 16 -nov -10 2609/98 097/73-001, TCD-4890-98 FINNISH AD M Kontroll av vindrutor och fönster FAA, U.S AD 2003 -17 -04 21 -aug -03 16 -nov -10 3076

GARMIN, Garmin GARMIN SSB 0844 Software Version 5.04 EASA SIB2008 -58R1 19 -May - A 14 -nov -08 2010 GARMIN SSB Software Version 6.04 EASA SIB2008 -58R1 19 -May - O 14 -nov -08 0845 2010

GARRETT, AlliedSignal Aerospace GARRETT SB 74 - 6 Replace Ignition Unit AD 74 -0003 FAA, U.S AD 86 -26 -02 25 -mar -94 6 09 -mar -09 see applicable engine for c/o 0003

HARTZELL, Hartzell Propeller Inc. HARTZELL SB 61 - Propeller mounting bolt inspection MITSUBISHI SL 053/72 -003 , MITSUBISHI 08 -feb -02 06 -jun -02 256 SL 080 HARTZELL SB 61 - 4 Prop. mounting bolt insp. FAA, U.S AD 2005 -14 -12 , MITSUBISHI SL 04 -Oct - 4 14 -nov -05 Propellerbolts previously checked u/a 279 ALERT 085 2005 HARTZELL SB A61- 3 Counterweight Slug Bolt Inspection EASA SIB2008-88 , FAA, U.S AD 2009-10- 15-jul-09 3 21-sep-10 N/A by SSB 0845 incorporated 313 14 HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2 , LFV 30-mar-05 9 13-mar-08 see previously revision LVA1424 Rev A

JCAB, Japan Civil Aviation

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 59(195) Bureau JCAB AD TCD -0642 -70 AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07 -feb -70 18 -jan -88 JCAB AD TCD-0518-68 Rivet holes elevator hinge fitting JCAB AD TCD - Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07 -feb -70 15 -Jul -2004 N/A N/A by s/n. by s/n 0643-70 26-Mar- 2009 JCAB AD TCD - Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25 -mar -70 26 -mar -09 N/A by model 0652-70 JCAB AD TCD - Engine Nacelle Tail Area - 25 -mar -70 26 -mar -09 N/A by model 0653-70 Modification of JCAB AD TCD - Replacement of bearing in LFV LVA457 MITSUBISHI SB 123 01 -May - 26 -mar -09 N/A by s/n 0660-70 nosegearstrut 1970 JCAB AD TCD - Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 Rev 25 -mar -72 14 -jul -04 N/A N/A by s/n. 0730-1-72 B JCAB AD TCD - Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10 -dec -86 26 -mar -09 N/A by s/n 0730-2-86 JCAB AD TCD - Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04 -sep -72 09 -Oct - N/A N/A due to s/n. 0859-72 1972 JCAB AD TCD - NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09 -Oct - 31 -dec -72 N/A N/A due to s/n. 0866-72 1972 JCAB AD TCD - Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 Rev 12 -nov -74 18 -jan -88 N/A N/A due to s/n. 0947A-74 A JCAB AD TCD - Inspection of Windshields MITSUBISHI SB 163 Rev B 22 -dec -78 26 -mar -09 0948A-1-78 JCAB AD TCD - Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 Rev 07 -Oct - 05 -May - 0948A-74 B 1974 1974 JCAB AD TCD - Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 Rev 06 -Oct - 18 -apr -85 1001A-76 E 1976 JCAB AD TCD- Replacement of Elevator Trim Tab FINNISH AD M 1080/82 LFV LVD1971 12-dec-84 18-apr-85 1001B-2-84 Bracket MITSUBISHI SB 176 Rev E JCAB AD TCD- Insp. of wingflap controlsystem FAA, U.S AD 75-16-13 LFV LVA1011 Rev A 06-sep-76 18-jan-77 Revision C PCW by Swedair. 1094A-76 MITSUBISHI SB 167 Rev D JCAB AD TCD- Insp. of propeller controllever inst. FAA, U.S AD 75-16-20 LFV LVA1012 06-May- 20-jan-88 1188-75 MITSUBISHI SB 168 Rev A 1975 JCAB AD TCD- Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev A 20-sep-75 15-jul-04 Found SB 171 and SB 180 PCW. 1202-75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A JCAB AD TCD - Insp/mod of NLG shimmydamper LFV LVA1013 MITSUBISHI SB 169 Rev B 16 -jun -75 10 -jul -75 1209-75 locking

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 60(195) JCAB AD TCD- Insp./repl. of MLG fwd door LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 18-jan-88 N/A N/A due to model. 1235-75 emerg.cables JCAB AD TCD- Supp.,MLG Forward D. Actuating MITSUBISHI SB 172 14-nov-75 26-mar-09 N/A by model 1272-75 Mech.-I&M JCAB AD TCD- Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76 24-nov-09 PCW Ref. SB 173 1284 -1-76 JCAB AD TCD- Fire hazard in rear baggage 01-jul-76 26-mar-09 N/A by s/n 1328-76 compartment JCAB AD TCD - Barrel Nut, Inner/Outer Wing Conn. - MITSUBISHI SB 175 16 -aug -76 01 -sep -09 N/A by s/n 1353-76 Repl. JCAB AD TCD - Inspect strobelight conduit in LFV LVA1196 18 -Oct - 18 -jan -88 Part.1 1370-76 Tiptank 1976 JCAB AD TCD - Inspect strobelight conduit in MITSUBISHI SB 174 PART 1 Rev C 05 -nov -81 16 -nov -10 1370A-81 Tiptank supersed TCD-1370-76 JCAB AD TCD - Insp. rear eng. cowling reg. LFV LVA1197 Rev A MITSUBISHI SB 177 06 -feb -02 22 -nov -77 Previously complied with 1379-1-80 heatdamage Rev B JCAB AD TCD - Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12 -dec -77 24 -mar -09 ref. SB 180 1520A -77 JCAB AD TCD - Fatigue failure of the NLG strut assy. LFV LVA1546 MITSUBISHI SB 181 PART 12 -jul -85 15 -jul -04 PCW Found SB 181 part 2 PCW. 1768 -1-85 JCAB AD TCD - Modification of LFV LVA1583 MITSUBISHI SB 182 05 -feb -02 11 -feb -80 N/A N/A due to s/n. 1817 -79 bagagecompartment JCAB AD TCD - Insp. firewarning & emerg.power LFV LVA1740 MITSUBISHI SB 187 Rev B 05 -feb -02 27 -May - N/A N/A due to s/n. 2048-81 circuit 1985 JCAB AD TCD - Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05 -feb -02 12 -Oct - 2070-81 1981 JCAB AD TCD - Insp./replace engine electrical LFV LVA1788 MITSUBISHI SB 191 06 -feb -02 18 -mar -82 2113-82 harness JCAB AD TCD - Flap system torquetubes supersed 01 -feb -89 24 -mar -09 PCW 2252-2-88 TCD-2252-1-87 JCAB AD TCD - Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04 -feb -83 15 -feb -95 2252-83 JCAB AD TCD - NLG. bracket attaching to drag strut 13 -aug -83 24 -mar -09 N/A by model 2263-83 JCAB AD TCD - Engine inlet anti -ice tubing. MITSUBISHI SB 196 Rev A 05 -jun -84 10 -mar -09 PCW 2342-1-84 Torq./lock JCAB AD TCD - Engine inlet anti -ice tubing. LFV LVA1942 MITSUBISHI SB 196 Rev A 06 -feb -02 31 -jul -84 2342-84 Torq./lock JCAB AD TCD - Pitot Tube Wiring LFV LVD2015 Rev B MITSUBISHI SR 053A 16 -jun -87 15 -jul -04 SB PCW. 2450A-87

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 61(195) JCAB AD TCD- Add. seal/Tq. insp of flap flex. shaft 01-May- 09-mar-09 PCW see TCD-2451-85 2451-1-87 1987 JCAB AD TCD- Add. seal/Tq. insp of flap flex. shaft LFV LVD2037 MITSUBISHI SB 198 30-sep-85 14-jun-85 2451-85 Superseeded by TCD-2451-1-87 JCAB AD TCD- Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 17-May- 2545 -1-88 1990 JCAB AD TCD- Auto-ignition System FINNISH AD M 2435/97 LFV LVD2761 01-feb-97 22-nov-01 2679A-97 MITSUBISHI SB 226 Rev E JCAB AD TCD - Bendix M4C Autopilot System MITSUBISHI SB 206 05 -nov -97 16 -nov -09 N/A due to Autopilot model 2856-1-97 JCAB AD TCD - Insp./mod. of rudder trimtab LFV LVD2338 MITSUBISHI SB 211 28 -mar -91 14 -jul -04 N/A N/A by s/n. 3378-90 leadingedge JCAB AD TCD - Anti ice/De -ice system FINNISH AD M 2364/96 LFV LVD2347 Rev 25 -May - 16 -nov -10 3393A-96 1 MITSUBISHI SB 212 Rev A 1996 JCAB AD TCD - Unintentional engagement of 17 -jun -91 24 -mar -09 N/A by model 3464-91 A/P...... JCAB AD TCD - Mod.of Autopilote pitchtrimsystem FINNISH AD M 2581/98 LFV LVD2450 LFV 17 -aug -98 27 -Oct - 3740A-98 MSB 216, 228 LVD 2898 LVD2898 MITSUBISHI SB 216 MITSUBISHI 1998 SB 228 JCAB AD TCD- Tiptank inst FINNISH AD M 2110/93 LFV LVD2512 10-sep-93 21-feb-94 3901-93 MITSUBISHI SB 221 JCAB AD TCD- Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592 28-nov-94 24-mar-95 3942-1-94 MITSUBISHI SB 219 Rev A JCAB AD TCD - Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01 -feb -94 08 -mar -95 3942-94 JCAB AD TCD - Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688 01 -apr -96 29 -nov -96 4310-96 MITSUBISHI SB 225 JCAB AD TCD - Windshield/window insp. FINNISH AD M 2331/96 LFV LVD2678 01 -nov -95 16 -nov -10 4311 -95 MITSUBISHI SB 224 Rev C JCAB AD TCD - Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689 01 -apr -96 30 -jul -96 4379 -96 MITSUBISHI SB 229 JCAB AD TCD - Icing Limitation FAA, U.S AD 96 -25 -02 LFV LVD2749 27 -dec -96 13 -feb -02 4552 -96 JCAB AD TCD - Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI SB 14 -jul -97 04 -Oct - 4625 -97 093/22 -009 2001 JCAB AD TCD - Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B 16 -mar -01 13 -mar -09 PCW Ref AMOC LFV Appr M15/01, TDM 01 -45 4625A -2001 NYGE TDM01 -45 JCAB AD TCD - De -ice system Modification FINNISH AD M 2461/97 LFV LVD2800 01 -May - 14 -jul -04 PCW 4626-97 MITSUBISHI SB 232 Rev A 1997

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 62(195) JCAB AD TCD- Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819 01-jun-97 25-mar-99 4684-97 MITSUBISHI SB 230 JCAB AD TCD- Ändring av flyghandbok LVD FINNISH AD M 2518/98 LFV LVD2922 18-feb-98 02-dec-98 FAA AD utförd. 4753-98 2922,FAA AD 97-20-14, MHI SN MITSUBISHI SN 117 Rev D 117A JCAB AD TCD- Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 17-May- inserted in AFM limitations 4753A-2004 2004 JCAB AD TCD- Inspection of landing gear power FINNISH AD M 2574/98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model 4838-98 train MITSUBISHI SB 235 JCAB AD TCD- Inappropriate calib. of eng. trq- MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A. 4889-2-2007 meter JCAB AD TCD- Insp. of Engine Torque Indication FINNISH AD M 2608/98 LFV LVD2924 05-nov-98 14-jul-04 PCW 4889-98 System LFV 2924, MU SB 233 MITSUBISHI SB 233 Rev B JCAB AD TCD- Check of flight idle FF LVD 2925, MU FINNISH AD M 2609/98 LFV LVD2925 04-nov-98 16-nov-10 4890-98 SB 234 MITSUBISHI SB 234 JCAB AD TCD- Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17-May- 24-mar-09 N/A by model 5030-99 1999 JCAB AD TCD- AFM revision LFV LVD3112 27-nov-00 12-feb-02 5432-2000 JCAB AD TCD- To prevent loss of airplane control LFV LVD3123 16-mar-01 12-feb-02 5547-2001 JCAB AD TCD- Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12-sep-01 04-Oct- 5747-2001 2001 JCAB AD TCD - Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27 -dec -01 17 -jan -02 5864-2001 JCAB AD TCD - Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17 -mar -03 04 -nov -03 6127-2003 JCAB AD TCD - Inspection of Wing Attachment MITSUBISHI SB 241 Rev A 27 -dec -06 17 -jan -07 c/o in conjunction with wingstudie 7030 -2006 Hardware

LFV, Luftfartsverket LFV LVA 1011 A Kontroll av vingklaffarnas FAA, U.S AD 75-16-13 JCAB AD TCD- 05-feb-02 A 18-jan-77 Revision C PCW by Swedair. manöversystem 1094A-76 MITSUBISHI SB 167 Rev D LFV LVA 1012 Kontroll av propellerreglagets FAA, U.S AD 75-16-20 JCAB AD TCD-1188- 05-feb-02 20-jan-88 montering 75 MITSUBISHI SB 168 Rev A LFV LVA 1013 Kontr. och mod. av låsning på JCAB AD TCD-1209-75 MITSUBISHI SB 169 05-feb-02 10-jul-75 nosställ Rev B

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 63(195) LFV LVA 1014 A Kontr. & byte av motorinkl. FAA, U.S AD 78-03-05 JCAB AD TCD-1202- 05-feb-02 A 18-jan-88 låsanordning 75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A LFV LVA 1083 Insp. & utbyte av lina för JCAB AD TCD-1235-75 MITSUBISHI SB 170 05-feb-02 18-jan-88 N/A N/A due to s/n. nödöppning Rev A LFV LVA 1196 Isolering av strobe light från bränsle JCAB AD TCD-1370-76 MITSUBISHI SB 174 06-feb-02 16-nov-10 PART 1 Rev C LFV LVA 1197 A Förhindr. av värmeskador på JCAB AD TCD-1379-1-80 MITSUBISHI SB 06-feb-02 A 22-nov-77 Previously complied with bak.motorpl. 177 Rev B LFV LVA 1238 Kontr. & byte av infästningsdet. 06-feb-02 21-apr-09 N/A by s/n trimrod LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86-15-03 JCAB AD TCD-1768- 06-feb-02 18-jan-88 1-85 MITSUBISHI SB 181 PART 2 Rev B LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD-1817-79 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n. LFV LVA 1740 Kontr.av brandvarnings -och JCAB AD TCD -2048 -81 MITSUBISHI SB 187 05 -feb -02 31 -aug -09 N/A by s/n n"dstr"mskret Rev B LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD -2070 -81 MITSUBISHI SB 188 05 -feb -02 12 -Oct - 1981 LFV LVA 1788 Kontroll/Utbyte av elledningar på JCAB AD TCD -2113 -82 MITSUBISHI SB 191 06 -feb -02 18 -mar -82 motor LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör JCAB AD TCD -2252 -83 MITSUBISHI SB 189 06 -feb -02 15 -feb -95 Rev C LFV LVA 1942 Momentdragning/låsn.av koppl.i JCAB AD TCD -2342 -84 MITSUBISHI SB 196 06 -feb -02 31 -jul -84 varmlufts Rev A LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD -0643 -70 MITSUBISHI SB 114 05 -feb -02 15 -jul -04 N/A N/A by s/n. LFV LVA 439 Rev. av flyghandbok betr. JCAB AD TCD -0642 -70 MITSUBISHI SB 112 05 -feb -02 18 -jan -88 bränslespec. Rev C LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD -0652 -70 MITSUBISHI SB 119 05 -feb -02 26 -mar -09 N/A by model LFV LVA 457 Utbyte av lager i nosst,llets JCAB AD TCD -0660 -70 MITSUBISHI SB 123 05 -feb -02 26 -mar -09 N/A by s/n st"td,mp. LFV LVA 543 B Insp. och målning av integraltankar JCAB AD TCD -0730 -1-72 05 -feb -02 B 14 -jul -04 N/A N/A by s/n. LFV LVA 645 Modifiering av el -system JCAB AD TCD -0859 -72 MITSUBISHI SB 156 05 -feb -02 16 -nov -09 N/A by s/n LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD-0866-72 05-feb-02 31-aug-09 N/A by s/n LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD -0947A -74 MITSUBISHI SB 05 -feb -02 A 18 -jan -88 N/A N/A due to s/n. 162 Rev A LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74 -11 -01 FAA, U.S AD 75 -03 - 05 -feb -02 A 05 -May -

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 64(195) 06 JCAB AD TCD-0948A-74 MITSUBISHI SB 1974 163 Rev B LFV LVA 886 A Kontroll/byte av JCAB AD TCD-1001A-76 05-feb-02 A 18-apr-85 höjdtrimroderarmar LFV LVD 1238 Kontr./byte infästn.det. 15-apr-77 31-aug-09 N/A by s/n höjdtrimroder LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD-1001B-2-84 MITSUBISHI SB 18-jan-85 18-apr-85 176 Rev E LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34 - FAA, U.S AD 86 -20 -01 JCAB AD TCD - 24 -May - B 06 -mar -86 005 Rev A, MHI SR 53 2450A-87 MAI SR 020/34-005 1985 MITSUBISHI SR 053A LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85 14-jun-85 LFV LVD 2069 Altimeter 25 -mar -86 18 -jan -88 N/A N/A by p/n & s/n LFV LVD 2113 Modif. & revision Handbook MHI SR 26 -jan -87 11 -sep -87 006B, MAI SR 040/74-001RA LFV LVD 2190 Autopilot Switch MU2 SB 066/22 - FAA, U.S AD 88 -13 -01 MAI SB 066/22 -006 19 -aug -88 17 -May - N/A Bendix A/P ej installerad 006 och SB 206 Rev A MITSUBISHI SB 206 1990 LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD -2545 -1-88 MITSUBISHI SB 19 -aug -88 25 -Oct - 201 Rev A 1988 LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88 -23 -01 JCAB AD TCD -2252 - 08 -dec -88 15 -feb -95 1-87 MAI SB 067/27-008 Rev A MITSUBISHI SB 189 Rev C LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88 -21 -01 Rev 1 08 -dec -88 12 -feb -02 LFV LVD 2338 Kont./Mod.av sidorodrets JCAB AD TCD -3378 -90 MITSUBISHI SB 211 28 -mar -91 14 -jul -04 N/A N/A by s/n. trimroderframka Mitsubishi MHI SB 211 LFV LVD 2347 1 Control Deice-system Mitsubishi SB JCAB AD TCD-3393A-96 MITSUBISHI SB 29-May- 1 16-nov-10 212A 212 Rev A 1996 LFV LVD 2352 Shoulder Harness Inst. FAA AC 43 -13 23 -May - 05 -jun -91 checked OK. CHPT 9 1991 LFV LVD 2450 Elevator Trim Tab Installation MU SB JCAB AD TCD -3740A -98 MITSUBISHI SB 03 -dec -92 31 -mar -93 216 216 LFV LVD 2477 Electric Trim System AD930711, MU FAA, U.S AD 93 -07 -11 MAI SB 079/27 -010 03 -jun -93 27 -mar -09 N/A by s/n SB 079/27-0-010 LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD -3901 -93 MITSUBISHI SB 221 02 -dec -93 21 -feb -94 LFV LVD 2537 Reducering av Höjdrodrets FAA, U.S AD 94-04-16 MITSUBISHI SB 216 07-apr-94 31-mar-93 trimområde. FAA AD 94-04-16, SB

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 65(195) 216 LFV LVD 2538 Byte Låspinne i landställets nödutf. JCAB AD TCD -3942 -94 MITSUBISHI SB 219 07 -apr -94 24 -mar -95 SB 219 Rev A LFV LVD 2551 Adj.of Ground Idle FAA AD 94 -11 -04 FAA, U.S AD 94 -11 -04 22 -jun -94 27 -mar -09 N/A by s/n LFV LVD 2592 Insp/Repl. of Lock -pin in L/G JCAB AD TCD -3942 -1-94 MITSUBISHI SB 09 -feb -95 24 -mar -95 gearbox TCD-3942-1-94, MSB 219A 219 Rev A LFV LVD 2678 Kontr. av vindrutor och fönster MHI FAA, U.S AD 2003 -17 -04 JCAB AD TCD - 12 -mar -96 16 -nov -10 SB 224 Rev A 4311-95 MITSUBISHI SB 224 Rev C LFV LVD 2688 Kontr/byte av infästn.bult för FAA, U.S AD 98 -20 -39 JCAB AD TCD -4310 - 09 -May - 29 -nov -96 tiptank MU-2 SB 225 96 MITSUBISHI SB 225 1996 LFV LVD 2689 Kontroll av linkage för prop.flöjning JCAB AD TCD -4379 -96 MITSUBISHI SB 229 09 -May - 30 -jul -96 MU-2 SB 229 1996 LFV LVD 2732 Inspection/ Replacement of Prop FAA, U.S AD 96 -18 -14 HARTZELL SB 61 - 27 -sep -96 09 -mar -98 Prop. utbytt mot BVA Hub. FAA AD 96-18-14, Hz SB 136H 261 Rev 1 LFV LVD 2749 Revision av flyghandbok AFM TCD - FAA, U.S AD 96 -25 -02 JCAB AD TCD -4552 - 21 -jan -97 13 -feb -02 4552-96 96 LFV LVD 2761 Installation av autoignition system JCAB AD TCD -2679A -97 MITSUBISHI SB 14 -feb -97 19 -mar -99 TCD-2679A-97 226 Rev E LFV LVD 2769 Demont.av backventil i FAA, U.S AD 97 -04 -13 MITSUBISHI SB 130 18 -mar -97 05 -May - N/A due to s/n. bränslesystemets MU-2 SB 130A Rev A 1997 LFV LVD 2800 Mod. av De -ice Monitoring System JCAB AD TCD -4626 -97 MITSUBISHI SB 232 28 -aug -97 08 -May - Mitsubishi SB 232, TCD-4626-97 Rev A 1998 LFV LVD 2819 Mod.av lagerboxar för JCAB AD TCD -4684 -97 MITSUBISHI SB 230 18 -nov -97 09 -mar -98 landställssystem Mitsubishi SB 230 LFV LVD 2853 Periodisk funktionskontroll av 23 -mar -98 16 -nov -10 nödutgång LFV LVD 2897 Kontroll av landst,llets drivsystem JCAB AD TCD -4838 -98 MITSUBISHI SB 235 02 -aug -98 24 -mar -09 N/A by model TCD-4838-98, SB 235 LFV LVD 2898 Mod. av autopilotens JCAB AD TCD -3740A -98 MITSUBISHI SB 27 -aug -98 27 -Oct - höjdtrimsystem TCD-3740A-98, SB 216 MITSUBISHI SB 228 1998 216, 228 LFV LVD 2922 Änd.av Flyghandbok -Extra krav på JCAB AD TCD -4753 -98 MITSUBISHI SN 117 12 -nov -98 02 -dec -98 FAA AD utförd. typutbi TCD-4753-98, MHI SN 117A Rev D LFV LVD 2924 Kontr/Just av motorernas Torque JCAB AD TCD -4889 -98 MITSUBISHI SB 233 01 -dec -98 19 -mar -99 indikeri MHI SB 233, TCD-4889-98 Rev B LFV LVD 2925 Kontr/just av mot bränsleflöde JCAB AD TCD -4890 -98 MITSUBISHI SB 234 01 -dec -98 08 -apr -10 Flight Id MHI SB 234 LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD -5030 -99 MITSUBISHI SB 209 18 -jun -99 24 -mar -09 N/A by model

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 66(195) Rev B LFV LVD 3112 Revision av flyghandbok JCAB AD TCD -5432 -2000 30 -jan -01 12 -feb -02 LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD -4625A -2001 MAI SB 02 -apr -01 04 -Oct - Ref AMOC LFV Appr M15/01, TDM 01 -45 093/22-009 MITSUBISHI SB 231 Rev B 2001 NYGE TDM01-45 LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD -5547 -2001 02 -apr -01 12 -feb -02 LFV LVD 3166 Sprickkontroll av infästning till ving - JCAB AD TCD -5747 -2001 MITSUBISHI SB 20 -sep -01 04 -Oct - spetstank 236 2001 LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD -5864 -2001 MAI SB 099/27 - 09 -jan -02 17 -jan -02 012 MITSUBISHI SB 237 LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD -6127 -2003 MITSUBISHI SB 21 -mar -03 04 -nov -03 239

MAI, Mitsubishi Aircraft International MAI SB 047/30- A Torque of Bleed Air Tube Coupling FAA, U.S AD 84-12-04 MITSUBISHI SB 196 19-jul-84 A 31-jul-84 001 Nuts AD 84-12-04,SB 196A Rev A MAI SB 051/27- Add.Seal and Flap Flexible Shaft FAA, U.S AD 87-04-03 01-feb-85 14-jun-85 007 Torque AD 87-04-03, SB 198 MAI SB 067/27- A Insp/Repl. of Flap Control System FAA, U.S AD 88-23-01 LFV LVD2202 29-mar-95 A 15-feb-95 008 Torque AD 88-23-01, SB 189B MAI SB 069/24- Split Radio Bus Inspection and MAI SB 066/22-006 Rev A 17-nov-88 06-jun-89 N/A N/A due to Aircraft s/n 006 Rework MAI SB 086/74- A Auto-Ignition System Installation FAA, U.S AD 2000-09-15 Rev 1 FINNISH 05-Oct- A 22-nov-01 Action not required due to s/n. 002 AD M 2435/97 MITSUBISHI SB 226 Rev E 2000 MAI SB 089/57 - A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98 -20 -39 05 -nov -96 A 29 -nov -96 N/A N/A due to s/n. 002 MAI SN 110/00 - Power Lever Position Warning 25 -feb -09 09 -nov -09 SB 240 considered 017A MAI SN 111/77- Torque Indicating System Shift 20-nov-08 11-mar-09 SB 233 considered 004 Potential MAI SR 020/34 - Anti Ice Capability AD 86 -20 -01, SR FAA, U.S AD 86 -20 -01 LFV LVD2015 Rev B 06 -Oct - 07 -feb -00 N/A N/A due to s/n. 005 053A MITSUBISHI SR 053A 1986

MITSUBISHI, Mitsubishi Heavy Industries Ltd MITSUBISHI MSR B **RECOVERED RECORD** 11 -sep -87

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 67(195) 066 MITSUBISHI SB Bendix M4D 18 -dec -87 17 -May - N/A 066 1990 MITSUBISHI SB M-4() Autop.Engage Switch Guard 11 -apr -91 12 -apr -95 N/A 076/22-008 Install. MITSUBISHI SB C Anti -Ice Additive in Fuel -Usage of JCAB AD TCD -0642 -70 LFV LVA439 09 -Oct - C 18 -jan -88 112 1971 MITSUBISHI SB Fuel Quantity Indicator JCAB AD TCD -0643 -70 LFV LVA438 01 -jan -70 15 -jul -04 N/A N/A by s/n. 114 Readjustmnet MITSUBISHI SB The Bolt and Bolt Hole Diam. of JCAB AD TCD -0652 -70 LFV LVA456 10 -mar -70 26 -mar -09 N/A by model 119 Nose L.G MITSUBISHI SB Bearing,Oleo Strut,Nose L.G. -Repl. JCAB AD TCD -0660 -70 LFV LVA457 01 -apr -70 26 -mar -09 N/A by s/n 123 of MITSUBISHI SB Scissors Switch,Nose L.G. -Install. of 31-aug-70 18-jan-88 N/A 124 MITSUBISHI SB B Tip Tank Air Pressure Modification 28-jun-94 B 05-nov-09 N/A by model & s/n 128 MITSUBISHI SB B Top Coating, Wing Integral Main JCAB AD TCD-0730-1-72 JCAB AD TCD- 05-jan-72 B 14-jul-04 N/A N/A by s/n. 143 F.T.-SIo 0730-2-86 MITSUBISHI SB A Flex. Shafts, Flap Control Sys.-Insp. JCAB AD TCD-0947A-74 LFV LVA828 Rev A 03-Oct- A 18-jan-88 N/A 162 of (AD750201) 1974 MITSUBISHI SB B Insp. of Outer Pane, Front Winds. & FAA, U.S AD 74-11-01 JCAB AD TCD- 16-nov-78 05-May- 163 Inst 0948A-1-78 JCAB AD TCD-0948A-74 LFV 1974 LVA829 Rev A MITSUBISHI SB A Lubr. Interval,Wheel Bearing,Main & 24 -jul -80 19 -jan -88 N/A 165 Nose MITSUBISHI SB Wing Flap 24 -jul -80 18 -jan -88 N/A 166 MITSUBISHI SB D Flap M.Jack Screw-Insp. of and/or FAA, U.S AD 75-16-13 JCAB AD TCD- 24-jul-80 D 18-jan-77 Revision C PCW by Swedair. 167 Main G 1094A-76 LFV LVA1011 Rev A MITSUBISHI SB A Propeller Pitch Control Lever-Insp. FAA, U.S AD 75-16-20 JCAB AD TCD-1188- 24-jul-80 A 20-jan-88 168 of (AD761620) 75 LFV LVA1012 MITSUBISHI SB B Shimmy Damper-Insp. and JCAB AD TCD-1209-75 LFV LVA1013 24-jul-80 B 05-nov-09 PCW 169 Modification of MITSUBISHI SB A MLG Forward Door Em.Op. Cable- JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77 A 18-jan-88 N/A N/A due to s/n 170 Insp. & Re (AD762204) MITSUBISHI SB B Latches,Eng. Nacelle Upper D.- FAA, U.S AD 78-03-05 JCAB AD TCD-1202- 17-nov-77 B 18-jan-88 171 Insp.& Mod (AD780305) 75 LFV LVA1014 Rev A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 68(195) MITSUBISHI SB A Drag Strut, Main L.G.-Modification JCAB AD TCD-1284-1-76 24-jul-80 12-feb-76 173 of MITSUBISHI SB C Tip Tank Conduit Tube-Insp.of,and FINNISH AD M 1177/83 JCAB AD TCD- 02-Oct- C 16-nov-10 174 PART 1 Rew.of (AD830902) 1370A-81 LFV LVA1196 1981 MITSUBISHI SB Barrel Nut, Inner/Outer Wing Conn.- JCAB AD TCD-1353-76 26-jun-76 01-sep-09 N/A 175 Repl. MITSUBISHI SB E Elevator Trim Tab Bracket-Repl. of FAA, U.S AD 84-25-02 FINNISH AD M 26-sep-84 E 18-apr-85 176 LVD1971, AD 84-25-02, SB 031/27- 1080/82 JCAB AD TCD-1001A-76 JCAB AD 005R1 TCD-1001B-2-84 LFV LVD1971 MITSUBISHI SB B Mod. of Engine Nacelle Tail Area JCAB AD TCD-1379-1-80 LFV LVA1197 Rev 11-sep-80 B 22-nov-77 Previously complied with 177 (AD810601) A MITSUBISHI SB Rodd Assem., Engine Nacelle Upper 27-May- 25-Oct- 179 D.-R&M 1977 1988 MITSUBISHI SB A Link, Engine Nacelle Upper D.-Repl. FAA, U.S AD 78-03-05 JCAB AD TCD-1202- 17-nov-77 A 20-apr-78 180 of (AD780305) 75 JCAB AD TCD-1520A-77 LFV LVA1014 Rev A MITSUBISHI SB B Insp. and Repl. of Nose L.G. Strut FAA, U.S AD 86-15-03 JCAB AD TCD-1768- 08-apr-85 B 18-jan-88 181 PART 2 Assem (AD801812) 1-85 LFV LVA1546 MITSUBISHI SB Add. of Ceiling Cover, Rear Bagg. JCAB AD TCD-1817-79 LFV LVA1583 16-nov-79 16-nov-79 N/A N/A due to s/n. 182 Comp. MITSUBISHI SB Turnbuckle, Control Cables -Repl. of 04-apr-80 05-feb-88 184 MITSUBISHI SB Down Lock Mech., Nose L.G.-Insp. of JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 12-Oct- 188 1981 MITSUBISHI SB C Flap Control Torque Tube AD 88-23- FINNISH AD M 2722/00 JCAB AD TCD- 28-jun-94 C 15-feb-95 189 01, SB 067/27-008 2252-1-87 JCAB AD TCD-2252-83 LFV LVA1873 LFV LVD2202 MITSUBISHI SB A Trav. Nut Repl. of L.G. Mech. Stop 28-jun-94 06-dec-83 190 Assem MITSUBISHI SB Engine El. Wire -Insp. and JCAB AD TCD -2113 -82 LFV LVA1788 21 -dec -81 18 -mar -82 191 Replacement of (AD820802) MITSUBISHI SB B Landing Gear Warning Horn 15-jun-94 B 04-dec-00 Rev A är utförd. 193 Syst.Modif. MITSUBISHI SB Master Cauting Light Visibility-Impr. 23-aug-82 23-mar-83 194 of MITSUBISHI SB A Ret. of coupling nut on the bleed air FAA, U.S AD 84-12-04 JCAB AD TCD-2342- 12-apr-84 A 31-jul-84 196 tu AD 84-12-04, SB 047/30-001 1-84 JCAB AD TCD-2342-84 LFV LVA1942 MAI SB 047/30-001 Rev A MITSUBISHI SB Add. Seal & Torque Insp. of Flap FAA, U.S AD 87 -04 -03 JCAB AD TCD -2451 - 13 -feb -85 14 -jun -85 198 Flex.Sh LVD2037, AD 87-04-03, SB 85 LFV LVD2037

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 69(195) 051/27-007 MITSUBISHI SB A Engine Lubricating Tubing Insp. & 24 -jun -94 A 06 -nov -09 PCW 199 Protec MITSUBISHI SB B Insp of Nose Ldg Gear Drag Strut 24 -jun -94 A 25 -Oct - 200 Link 1988 MITSUBISHI SB A Generator Circuit Wires Insp. and FAA, U.S AD 87 -12 -02 JCAB AD TCD -2545 - 02 -mar -88 A 17 -May - 201 Mod. 1-88 LFV LVD2191 1990 MITSUBISHI SB Speed Placard Change 03 -mar -87 05 -feb -88 204 MITSUBISHI SB Bendix Autop.Disengagement FAA, U.S AD 88 -13 -01 JCAB AD TCD -2856 - 13 -Oct - 31 -jan -89 N/A N/A due to Autopilot model 206 Method Stand. 1-97 LFV LVD2190 1987 MITSUBISHI SB Rudder T.T. & Elevator T.T. Insp. & 20 -May - 27 -nov -09 207 Rep. 1988 MITSUBISHI SB B Fuselage inspection JCAB AD TCD-5030-99 LFV LVD2988 19-apr-99 B 24-mar-09 N/A by model 209 MITSUBISHI SB A Engine Ignition Unit Replacement 12-nov-96 06-mar-98 210 MITSUBISHI SB Rudder Trim Tab Modification (LVD JCAB AD TCD-3378-90 LFV LVD2338 20-nov-90 14-jul-04 N/A 211 2338) MITSUBISHI SB A Insp of Anti-ice/Deice Systems (LVD JCAB AD TCD-3393A-96 LFV LVD2347 Rev 25-apr-96 A 16-nov-10 212 2347), 1 MITSUBISHI SB Engine Control Rod Inspection 06-dec-91 31-mar-93 214 MITSUBISHI SB Removel of Prop. Governor Speed 23-Oct- 31-jan-92 N/A N/A due to -1 engine 215 Signal 1991 MITSUBISHI SB Elevator Trim Tab Installation (LVD FAA, U.S AD 2007-17-09 FAA, U.S AD 94- 11-sep-92 31-mar-93 216 2450 04-16 JCAB AD TCD-3740A-98 LFV LVD2450 LFV LVD2537 LFV LVD2898 MITSUBISHI SB A Propeller Feathering Linkage 17-jan-94 A 21-feb-94 218 Inspection MITSUBISHI SB A Emergency Gear Down G.box Lower JCAB AD TCD-3942-1-94 JCAB AD TCD- 24-Oct- A 24-mar-95 219 Pin Repl 3942-94 LFV LVD2538 LFV LVD2592 1994 MITSUBISHI SB Tip Tank Conduit Tube Insp. and JCAB AD TCD-3901-93 LFV LVD2512 10-aug-93 21-feb-94 221 Rep. MITSUBISHI SB Fuselage Waterproof Modification 28-jun-94 19-mar-99 222 SR 019 MITSUBISHI SB Pitot/Static System Improvement SR MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 07-feb-00 223 064

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 70(195) MITSUBISHI SB C Acrylic Windsheild/Window glass FAA, U.S AD 2003-17-04 FINNISH AD M 30-apr-98 C 16-nov-10 224 Insp. UHB 3076 JCAB AD TCD-4311-95 LFV LVD2678 MITSUBISHI SB Forward fitting bult of wingtip tank FAA, U.S AD 98-20-39 FINNISH AD M 29-sep-95 29-nov-96 225 LVD 2688 2351/96 JCAB AD TCD-4310-96 LFV LVD2688 MITSUBISHI SB E Auto-Ignition System Installation FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S 18-sep-01 E 22-nov-01 PCW 226 LVD 2761 (2113), AD TCD-2679A-97 AD 86-26-02 FINNISH AD M 2435/97 FINNISH AD M 2786/00 JCAB AD TCD- 2679A-97 LFV LVD2761 MAI SB 086/74- 002 Rev A MITSUBISHI SB Rudder Torque Tube Modification 20 -dec -96 09 -mar -98 227 MITSUBISHI SB Elevator Trim Indicator Modification FAA, U.S AD 2007 -17 -09 FINNISH AD M 13 -jul -98 27 -Oct - 228 LFV 2898 2581/98 JCAB AD TCD-3740A-98 LFV 1998 LVD2898 MITSUBISHI SB Feathering Valve/Linkage Insp. FAA, U.S AD 2006 -15 -07 JCAB AD TCD - 20 -feb -96 30 -jul -96 229 4379-96 LFV LVD2689 MITSUBISHI SB Mod.of Bearing Box Ldg. Gear Act. JCAB AD TCD -4684 -97 LFV LVD2819 05 -mar -97 09 -mar -98 230 LVD 2819 MITSUBISHI SB B Inst.of Trim -In -Motion Alert System FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH 11 -dec -02 B 03 -mar -03 SL 079 allready performed. 231 AD M 2460/97 UPPHÄVD FINNISH AD M 2786/00 JCAB AD TCD-4625A-2001 LFV LVD3122 MAI SB 093/22-009 NYGE TDM01-45 MITSUBISHI SB A De -Ice System Modification LVD FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH 06 -jun -02 A 06 -jun -02 N/C due to previuosly complied with SB 232 rev 0. 232 2800, TCD-4626-97 AD M 2786/00 JCAB AD TCD-4626-97 LFV LVD2800 MAI SB 096/30 -004 MITSUBISHI SB B Insp.of Engine Torque Indication FAA, U.S AD 2006 -17 -01 FINNISH AD M 08 -mar -07 B 18 -apr -07 Checked, previously carried out 233 System. TCD-4889-98, LFV 2924 2608/98 JCAB AD TCD-4889-2-2007 JCAB AD TCD-4889-98 LFV LVD2924 MITSUBISHI SB Fl.Check of the Flight Idle Fuel Flow FAA, U.S AD 2006-17-05 JCAB AD TCD- 07-Oct- 16-nov-10 234 Se TCD-4890-98, LVD 2925 4890-98 LFV LVD2925 1998 MITSUBISHI SB Inspection of landing gear power JCAB AD TCD-4838-98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model 235 train MITSUBISHI SB Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-01 04-Oct- 236 2001 MITSUBISHI SB Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-01 17-jan-02 237 MITSUBISHI SB Main Landing Gear Door Safety Pin 05-dec-02 09-jan-03 Perf. at each 600 h. insp. 238

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 71(195) MITSUBISHI SB Pneumatic Line Insp. and JCAB AD TCD-6127-2003 LFV LVD3322 26-dec-02 04-nov-03 239 Modification MITSUBISHI SB Inst.of Trottle Quadrant Placard 26-feb-03 20-Oct- 240 2003 MITSUBISHI SB A Inspection of Wing Attachment FAA, U.S AD 2006-13-15 JCAB AD TCD- 21-nov-06 A 17-jan-07 c/o in conjunction with wingstudie 241 Hardware 7030 -2006 MITSUBISHI SL System 17-feb-89 28-jun-91 060 MITSUBISHI SL Automatic Autopilot Disconnect 28 -jan -02 16 -nov -10 078 System MITSUBISHI SL Diode inst.in Flap Position 28 -jan -02 04 -Oct - 079 Ind.Curcuit 2001 MITSUBISHI SL Hartzell Propeller Mounting Bolt HARTZELL SB 61 -256 05 -apr -02 26 -aug -02 Compliance in according to HC -SB -61 -256. 080 Insp. MITSUBISHI SL Pneumatic De -Ice Monitoring 14 -jun -04 16 -nov -10 084 System MITSUBISHI SL Hartzell prop. mount. bolt insp. HARTZELL SB 61 -279 ALERT Rev 4 17 -May - 14 -sep -05 Propellerbolts previously checked u/a 085 2005 MITSUBISHI SN B Rudder Torque Tube AD 86 -20 -01, 05 -nov -86 B 17 -jan -88 053 SB 020/34 -005 MITSUBISHI SN D Icing Awareness Training Video FAA, U.S AD 2003 -22 -07 Rev 1 JCAB AD 14 -jun -04 D 17 -May - 117 TCD -4753 -98 LFV LVD2922 2004 MITSUBISHI SN Water Ingress into Vertical Stabilizer 19 -dec -03 12 -mar -04 146 MITSUBISHI SN Reminders for safe operation 18 -nov -05 22 -mar -06 Genomförs enl. AMP MU -2 & DHB 148 MITSUBISHI SN Power Lever Position Warning 25 -feb -09 09 -nov -09 SB 240 considered 156A MITSUBISHI SN Torque Indicating System Shift 20 -nov -08 11 -mar -09 SB 233 considered 157 Potential MITSUBISHI SN Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09 -dec -09 11 -mar -10 Ref STC SA01913SE 161 MITSUBISHI SN IR Part 2, one time inspection of 04 -Oct - 164 mechanical stop bearing. 2012 MITSUBISHI SR Modifiering av pitotrör FAA, U.S AD 86 -20 -01 JCAB AD TCD - 23 -Oct - 06 -mar -86 053A 2450A-87 LFV LVD2015 Rev B MAI SR 1984 020/34 -005 MITSUBISHI SB 223 MITSUBISHI SR Pitot & Static System MITSUBISHI SB 223 30 -apr -85 27 -feb -00 064

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 72(195) MITSUBISHI SR Warning Horn 20-jan-86 18-jan-88 065 MITSUBISHI SR Emergency Exit Placard 17-sep-85 18-jan-88 067 MITSUBISHI SR Air Filter Replacement for Vacuum 25-apr-00 09-dec-05 072 Syst. MITSUBISHI SR Inst. tip tank placard 29-Oct- 01-jun-05 075 2004 MITSUBISHI STC Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10 -dec -09 11 -mar -10 See MU -2B AMP Chpt 3 100h/1y inspection SA01913SE

NARCO, Narco NARCO SB ELT10 - ELT ASSY 18 -apr -88 28 -jun -91 N/A 16

NYGE, Saab Aerotech Aircraft Services NYGE TDM 01 -45 Installation of Trim -In -Motion Alert JCAB AD TCD -4625A -2001 LFV LVD3122 07 -May - 04 -Oct - Syst. and Automatic A/P Disconnect MITSUBISHI SB 231 Rev B 2001 2001 syst. NYGE TDM 02-10 Installation of TPE331-6-252M 25-mar-02 04-Oct- Engines 2001 NYGE TDM 02-24 Installation Moving MAP 10-Oct- 28-Oct- 2002 2002 NYGE TDM 02-32 Installation EMI film 10-dec-02 10-jan-04 NYGE TDM 02 -33 Viktminskning MU -2B 24 -dec -02 01 -mar -04 NYGE TDM 03 -08 8 GNS430/530 & MODE S GTX330 04 -mar -03 8 31 -Oct - install. 2008 NYGE TDM 03 -11 C Astor 2 MU -2B 19 -mar -03 C 06 -Oct - Original compliance was as per TDM rev A.The A/C 2003 installation is IAW rev C as not affected by rev B and C.F01322, F01347, F01349 NYGE TDM 03 -15 A U95 with General Control System 24 -apr -03 A 25 -feb -08 NYGE TDM 03 -28 F Nav Demo Pod 19 -dec -03 F 27 -nov -09 Original compliance by Rev D. Not affected by rev F. NYGE TDM 05 -16 Viktor Counter Weight Pod 18 -nov -05 18 -nov -05 NYGE TDM 06-28 A Removable FR-31 29-jun-07 A 01-Oct-

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 73(195) 2007 NYGE TDM 06 -41 A Darts (to carry on MU -2B -20/26) 20 -nov -06 A 07 -feb -08 NYGE TDM 06 -42 A Barlast DARTS MU -2B 04 -dec -07 A 07 -feb -08 NYGE TDM 07 -30 A Install. of Emergency Axe 28 -feb -08 A 28 -feb -08 NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 27-nov-09 NYGE TDM 08 -28 B ELT 406 MU -2B 29 -sep -08 B 31 -Oct - Original compliance with TDM rev A. Rev B does 2008 not affect previous complaiance. NYGE TDM 09 -22 A Electrical Wiring Feed Through 08 -sep -09 A 27 -nov -09 NYGE TDM 09 -27 A GPS Splitter 12 -Oct - A 27 -nov -09 2009 NYGE TDM 09 -33 A MU -2B Loudspeaker in Cockpit 04 -dec -09 A 04 -May - C/W 2010 NYGE TDM 10 -25 A MU -2B Terminating Resistor 08 -apr -10 A 19 -May - C/W 2010 NYGE TDM 10 -46 A MU -2 Alternate lap top computers A 10 -Jun - 2011 NYGE TDM 11 -35 A Terminating resistor A 27 -Jan - 2012 NYGE TDM 12 -21 A Avinstallation IK 14 -Aug - 2012 NYGE TDM 12 -40 A MU -2B Relocation of MIC/Phone 04 -Oct - Jacks 2012 NYGE TDM 95 -04 4 Vingstudie 20 -sep -98 4 18 -mar -03 NYGE TDM 97 -03 Astor MU -2 25 -feb -97 04 -mar -98 NYGE TDM 98 -08 Torrluft ASTOR 27 -May - 17 -aug -98 1998 NYGE TDM 99 -03 Install. Auto Ignition 03 -mar -99 19 -mar -99 NYGE TVO 1/09 Inspektion av Stringers & struktur 25-feb-09 04-mar-09 Inspected with remarks vinge NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 31-mar-93 NYGE TVO 1/96 Slitage Flap Guide Rail 12 -apr -96 09 -Oct - 1998 NYGE TVO 1/97 3 De -Icertank MU -2B, 12 -feb -97 13 -feb -97 korrosionskontroll

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 74(195) NYGE TVO 2/00 Märkning av infästning domkraft 01-dec-00 15-nov-00 Mu2 NYGE TVO 2/07 A Prevent FR31 radio to xmit when 06-feb-07 A 28-feb-07 RM2 off NYGE TVO 2/91 A/C Elecrical System 10-jan-91 07-aug-91 NYGE TVO 3/06 Inspect lower rudder hinge bracket 07 -dec -06 16 -nov -10 NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24 -feb -05 3 27 -nov -09 NYGE TVO 4/11 A Static Inverter controll 15 -Dec - 2011 NYGE TVO 4/86 2 Wing Pod Inspection 06 -apr -92 2 16 -nov -10 NYGE TVO 4/91 Special Inspection (next E6.) 19 -feb -91 07 -aug -91 NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29 -apr -92 12 -jun -92 NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28 -sep -94 3 07 -apr -10 NYGE TVO 4/96 Kontroll av Lagerhus i 25 -Oct - 11 -May - Utförd tidigare (ref.Ove N lista) noshjulsstyrning. 1996 1997 NYGE TVO 6/88 Allm. instruktion för metallpropeller 13 -jun -88 07 -apr -10 NYGE TVO 6/92 Elevator Trim Cable, check 07-Oct- 12-nov-92 1992 NYGE TVO 7/93 Starter Drive Splines 01 -nov -93 18 -jan -96 NYGE TVO 8/04 Kontr. av Spant vid bakre 08 -dec -04 07 -apr -10 feninfästning NYGE TVO 8/92 Wheel Parts 27 -Oct - 31 -mar -93 1992 NYGE TVO 9/88 Emergency Extension System 08-aug-88 25-Oct- 1988

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 75(195)

2.3 GFE Aircraft Mitsubishi MU-2 SE-GHB

2.3.1 Aircraft Specification Type: Serial Registration : Airframe Total Date Number: total Hours: Landing Reference: Cycles: MU-2B-20 287 SE-GHB 11585 6415 2012-11-23

2.3.2 Engines Type: Honeywell TPE331 -6-252M Serial Total Hours Total Hours remaining to Number: Since New: Cycles Overhau/HSI/GBI: Since New: Left Engine P20019 11797 11513 1916/197/116 Right Engine P20146 9513 13195 3142/1346/1342

2.3.3 Propeller Type Number: Serial Number: Overhaul Due Date: Left Propeller HC-B3TN-5C BVA 6205 2013-09-14 Right Propeller HC-B3TN-5E BVA 6253 2013-03-26

2.3.4 Avionics System: Type / Part Number: Note: Autopilot & Flight Director Century IV COM/NAV/GPS 1 Garmin GNS 530 COM/NAV/GPS 2 Garmin GNS 430 Audiopanel Bendix/King KMA-24H-70 MKR Bendix/King KR-21 DME Bendix/King KDM -706 ADF Bendix/King KDF -806 XPDR 1 Garmin GTX 330D Mode S EHS XPDR 2 Garmin GTX 330 *) Mode S EHS RDR ALT Bendix/King KRA-10A ELT Kanad ELT 406-AF-H Airspeed Indicator LH / RH Aerosonic 065A-986402-003 / 20040-161 Altimeter LH United Instr. Inc. 5934 PAD -1 Altimeter incl. encoder RH United Instr. Inc. 5035P -P40 Altitude Reporter Narco AR 850 Altitude Alerter Aero Mechanism AM 275C Vertical Speed Indicator LH Aerosonic RC-60-MS-10-3

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 76(195) Attitude Gyro & Flight Director Ind. Century 52C77 LH Attitude Gyro Ind. RH AIM 504-0006-914 Turn & Bank Ind. LH R.C Allen A5930-02 Horizontal Situation Indicator LH Bendix/King KPI-553A DG -Gyro Sperry C -14A Directional Gyro RMI Ind. LH AIM 254 -1D CDI Indicator Garmin GI -106A *) XPDR 2 without diversity configuration

2.3.5 Mission System System : Description: Fixed general installations VHF/UHF COM 1 & 2 FR31 GPS MAP JET SI-3003B Inverter 115/200VAC 400Hz 3 phase Laser Prism MIL-STD-1553 Bus LH Wing Pylon Wing Pylon NATO 14” Alcon Ejector Unit LH and RH Wing Pylon EW system ASTOR Fixed installed system ADRIAN Pod mounted system LH and RH Wing Pylon U95 N Pod mounted system LH Wing Pylon U95 Sorc Pod mounted system RH Wing Pylon A100 Pod mounted system LH Wing Pylon Missile Threat Simulator DARTS Pod mounted system LH Wing Pylon Chaff Dispenser BOX 3 Pod mounted system LH and RH Wing Pylon Precisions GPS Pos System TAPS

2.3.6 Mission Cable Harness to Hard Points Used for Mission LH NATO Hard point: RH NATO Hard point: Note: System: Adrian C & S, U95-N, A100, General Signal Harness General Signal Harness DARTS and BOX 3 AWG22 shielded x 44 AWG22 shielded x 50 U95-N and A100 MIL-STD-1553B Data Triax Cable x 1 Bus U95-N, A100 and DARTS AC Power AWG 12 x 4 115/200VAC 400 Hz 3- twisted

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 77(195) Phase 3 x 10 A AWG 16 x 2 AWG 20 x 2 Adrian C & S and BOX 3 DC Power 28 VDC 200 DC Power 28 VDC 200 AWG 2 x 2 A A Adrian C & S Coax Cable 1 x 50 Ω Coax Cable 1 x 50 Ω Prepared installation Ethernet LAN Cable

2.3.7 Antenna Layout

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 78(195)

2.3.8 Inspection due times and dates Status date November 23 rd 2012.

Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date Aircraft SE-GHB Vingstudie MU-2 AMP 2012-02-23 11477 12500 100 Hour Inspection AMP 2012-03-01 11477 11577,4 2013-03-01 200 Hour Inspection AMP 2012-03-14 11477 11677,4 2013-05-18 600 Hour Inspection AMP 2011-03-08 11412 12012 2014-04-17 1000 Hour Inspection AMP 2012-03-27 11477 12500 1200 Hour Inspection AMP 2007-07-31 11047 12247,5 1800 Hour Inspection AMP 2007-07-31 11047 12847,5 2000 Hour Inspection AMP 2012-03-22 11477 13500 1 Year Inspection AMP 2012-05-15 11477,4 2013-05-18 2 Year Inspection AMP 2012-01-23 11457,2 2014-01-22 10 Year Inspection AMP 2005-02-24 10500 2015-02-22 Engine S/N P-20019 Remaining Engine Assembly (Overhaul) AMP 13501,9 1916,85 Engine Hot Section Inspection AMP 11782,8 197,75 Engine Gearbox Inspection AMP 11702 116,95 Engine S/N P-20146 Engine Assembly (Overhaul) AMP 14727,2 3142,15 Engine Hot Section Inspection AMP 12931,8 1346,75 Engine Gearbox Inspection AMP 12927,2 1342,15

Propeller L/H O/H AMP 2008-09-15 14211,1 2013-09-14 Propeller R/H O/H AMP 2008-03-27 14144 2013-03-26

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type

2012-12-06

Document number Page 79(195)

2.3.9 Implemented Changes Status dateNovember 23 rd 2012. SB/AD etc Rev Subject Document reference Eff. date Rev Complianc Stat Remarks Reference e us

CENTURY, Century Flight Systems Inc. CENTURY SB CSB - Check for frayed Bridle Cable 21 -feb -05 31 -mar -10 2005-01

EASA, European Aviation Safety Agency EASA AD 2006 - Incorrect transponder altitude 30 -aug -06 14 -jan -10 0265 EASA AD 2009 - Portable Fire Extinguishers -Ident/Repl 25 -nov -09 07 -May - N/A N/A by current P/N installed 0251-E 2010 EASA AD 2009 - Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009 -0278 FFE ASB26 -115 Rev C 15 -dec -09 07 -May - N/A N/A by current P/N installed 0262 2010 EASA AD 2009 - Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009 -0262 22 -dec -09 07 -May - N/A N/A by current P/N installed 0278 2010 EASA AD 2010 - R1 Mode S Transponder - 11 -jan -10 R1 10 -mar -10 N/A due to model 0003 Check/Modification EASA AD 2012 - KIDDE GRAVINER HAND OPERATTED 06 -Sep - 0037 FIRE EXTINGUISHER 2012 EASA SIB 2008 - Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN 17 -dec -08 21 -sep -10 N/A by SSB 0845 incorporated 58R1 SSB0845 Rev IR EASA SIB 2009 -14 Upgrade to main unit/GPS software 24 -jun -09 28 -sep -09 N/A due to model

FAA, U.S, Federal Aviation Administration FAA, U.S AD 2000- AFM De-icing 25-jan-00 26-apr-00 N/A Due to paragraph b. 02-25 FAA, U.S AD 2000- 1 Flight in Icing Condition AFM De-icing FINNISH AD M 2435/97 FINNISH AD M 07-jul-00 02-apr-02 N/A Due to paragraph b. 09-15 FAA, U.S AD 2786/00 MAI SB 086/74-002 Rev A MAI SB

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 80(195) 2000-02-25 093/22-009 MAI SB 096/30-004 MITSUBISHI SB 226 Rev E MITSUBISHI SB 231 Rev B MITSUBISHI SB 232 Rev A FAA, U.S AD 2003- 1 Forecast Icing Conditions FINNISH AD T5007/03 JCAB AD TCD- 16-apr-04 17-May- inserted in AFM limitations 22-07 4753A-2004 MAI SN 071/00-006 Rev D 2004 MITSUBISHI SN 117 Rev D FAA, U.S AD 2005 - Prop. mounting bolt insp. HARTZELL SB 61 -279 ALERT Rev 4 29 -jul -05 14 -sep -05 14-12 FAA, U.S AD 2005 - Prop de -icer "FASTprop" 14 -Oct - 12 -Oct - N/A Due to boots p/n 18-20 2005 2005 FAA, U.S AD 2006- Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB 11-aug-06 17-nov-03 c/o in conjunction with vingstudie 13-15 241 Rev A FAA, U.S AD 2006- Safety evaluation (feathering linkage) MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06 24-aug-06 se Mitsubishi SB 229 15-07 FAA, U.S AD 2006- Detect & correct torque transducers MAI SB 095/77-002 MITSUBISHI SB 233 22-sep-06 21-sep-06 PCW see MSB 233A 17-01 Rev B FAA, U.S AD 2006- Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 27-sep-10 17-05 FAA, U.S AD 2007- Reduce max deflect elev nose-down MITSUBISHI SB 216 MITSUBISHI SB 228 25-sep-07 11-sep-07 Previously carried out i.a.w. mentioned SB's. 17-09 trim FAA, U.S AD 71- Fuel Tank Fungus Coating Peeling 01-May- 01-jan-96 N/A by s/n 14-01 1972 FAA, U.S AD 74- Windshield Outer Panes COP LFV LVA829 Rev A MITSUBISHI SB 163 Rev 30-jan-78 16-May- 11-01 2011/09/1 19:37:04 B 1974 FAA, U.S AD 75- Main Wing Flap JCAB AD TCD-1094A-76 LFV LVA1011 Rev 05-aug-75 25-mar-77 Revision C PCW by Swedair. 16-13 A MITSUBISHI SB 167 Rev D FAA, U.S AD 75- Propeller Pitch Control Lever JCAB AD TCD-1188-75 LFV LVA1012 12-aug-75 20-May- 16-20 MITSUBISHI SB 168 Rev A 1975 FAA, U.S AD 78- Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A 23-feb-78 25-nov-75 03-05 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A FAA, U.S AD 81- 1 Engine Aft Nacelles 01-apr-81 1 25-May- Previously complied with 06-01 1997 FAA, U.S AD 81- 1 Engine's Electrical wiring SB 036/71- 21-jan-82 1 02-dec-10 N/A N/A by model 25-04 003A, SB 043/71-005 FAA, U.S AD 82- Electrical Wiring Inspection 15-apr-82 09-feb-82 08-02 FAA, U.S AD 83- 2 To preclude prop. attach bolt failures FINNISH AD M 1168/83 Rev 1 FINNISH AD 28-apr-82 2 20-May- Ref. MU2B MM chap 13.4 when using bolts P/N 08-01 T5114/05 HARTZELL SI 140A Rev 9 2005 B-3339 only

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 81(195) FAA US AD 83-09- Strobe light assembles 16-Mar-12 02 FAA, U.S AD 84- Torque of Air Tube Coupling Nuts SB MAI SB 047/30-001 Rev A MITSUBISHI SB 28-jun-84 16-feb-84 12-04 047/30-001, SB 196A 196 Rev A FAA, U.S AD 84- Elevator TrimTab Bracket Insp/Repl. MAI SB 031/27-005 Rev 1 MITSUBISHI SB 18-dec-84 23-apr-85 25 -02 SB 031/27 -005 R1, SB 176E 176 Rev E FAA, U.S AD 86- NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2 13-aug-86 15-jul-04 Found SB 181 part 2 PCW. 15-03 Rev B FAA, U.S AD 86 - To assure anti -ice capability of pitot LFV LVD2015 Rev B MAI SR 020/34 -005 06 -Oct - 30 -aug -00 20-01 SB 020/34-005, SB 053A MITSUBISHI SR 053A 1986 FAA, U.S AD 86 - To prevent engine flameout in an GARRETT SB 74 -0003 Rev 6 31 -dec -87 09 -mar -09 see applicable engine for c/o 26-02 iceing SB 74-0003, SR 040/74-001 FAA, U.S AD 87 - Addit. Seal and Flap Flexible Shaft MAI SB 051/27 -007 MITSUBISHI SB 198 07 -mar -87 29 -jul -85 04-03 Insp SB 051/27-007, SB 198 FAA, U.S AD 87 - Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03 -jul -87 23 -apr -90 12-02 FAA, U.S AD 88 - Bendix Autopilot Disengagement SB LFV LVD2190 MAI SB 066/22 -006 Rev A 11 -jul -98 22 -dec -89 N/A N/A due to Autopilot model 13 -01 066/22 -006 MITSUBISHI SB 206 FAA, U.S AD 88 - 1 To minimize confusion in LFV LVD2206 MAI SB 066/22 -006 Rev A 28 -jan -89 1 25 -Jan -12 21 -01 autopilot/manua SB 066/22 -006 FAA, U.S AD 88 - To prevent flap control failure SB LFV LVD2202 MAI SB 067/27 -008 Rev A 04 -dec -88 18 -May - 23 -01 067/27 -008, SB 189B 1995 FAA, U.S AD 93 - ELECTRIC TRIM SYSTEM SB 079/27 - LFV LVD2477 MAI SB 079/27 -010 01 -jun -93 27 -mar -09 N/A by s/n 07-11 010 FAA, U.S AD 94 - Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11 -apr -94 12 -Oct - 04-16 1993 FAA, U.S AD 94 - Change of Flight Idle Blade Angel SB LFV LVD2551 MAI SB 016/71 -001 10 -jun -94 27 -mar -09 N/A by s/n 11-04 016/61-001 FAA, U.S AD 96 - Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD - 27 -dec -96 12 -nov -97 25-02 4552-96 LFV LVD2749 FAA, U.S AD 97 - Vent Check Valve Assy LFV LVD2769 16 -apr -97 05 -May - N/A N/A due to s/n. 04-13 1997 FAA, U.S AD 97 - Icing related incidents/accidents 17 -Oct - 02 -dec -98 20-14 CNL 1997 FAA, U.S AD 97 - To prevent loss of airplane FINNISH AD M 2524/98 21 -jan -98 03 -dec -10 N/A AD superseeded by AD 2010 -10 -17 25-02 ctrl/overspe FAA, U.S AD 98 - Forward fitting bolt of wingtip tank SB LFV LVD2688 MAI SB 089/57 -002 Rev A 19 -Oct - 07 -Oct - 20-39 MU-2 225, 089/57-002A MITSUBISHI SB 225 1998 1997

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 82(195) FAIRCHILD, Fairchild Aircraft FAIRCHILD SB 29- 2 In Service Hydraulic Leaks FAA, U.S AD 85-04-01 Rev 1 19-Jul-1985 02-jan-00 23-apr-85 005

FINNISH, Finnish Civil Aviation Adm. FINNISH AD M Avisningens "vervakningsanl,ggning JCAB AD TCD -4626 -97 01 -aug -97 11 -mar -10 2461/97 FINNISH AD M Justering av br,nslefl"de MHI SB JCAB AD TCD -4890 -98, MAI SB 097/73 - 12 -nov -99 27 -sep -10 2609/98 097/73-001, TCD-4890-98 001

GARMIN, Garmin GARMIN SSB IR Software Version 5.04 EASA SIB2008 -58R1 14 -nov -08 A 20 -May - 0844 2010 GARMIN SSB IR Software Version 6.04 EASA SIB2008 -58R1 14 -nov -08 0 20 -May - 0845 2010

GARRETT, AlliedSignal Aerospace GARRETT SB 74- 6 Replace Ignition Unit AD 74-0003 FAA, U.S AD 86-26-02 25-mar-94 09-mar-09 see applicable engine for c/o 0003

HARTZELL, Hartzell Propeller Inc. HARTZELL SB 61 - Propeller mounting bolt inspection MITSUBISHI SL 053/72 -003, MITSUBISHI 08 -feb -02 02 -Oct - 256 SL 080 2002 HARTZELL SB 61 - 4 Prop. mounting bolt insp. FAA, U.S AD 2005 -14 -12 04 -Oct - 14 -nov -05 Propellerbolts previously checked u/a 279 ALERT 2005 HARTZELL SB A61 - 3 Counterweight Slug Bolt Inspection EASA SIB2008 -88 , FAA, U.S AD 2009 -10 - 15 -jul -09 3 20 -sep -10 N/A by SSB 0844 313 14 HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83 -08 -01 Rev 2, LFV LVA1424 30 -mar -05 9 13 -mar -08 see previously revision Rev A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 83(195) JCAB, Japan Civil Aviation Bureau JCAB AD TCD- Rivet holes elevator hinge fitting 06-Feb- 26-mar-09 N/A by s/n 0518-68 1968 JCAB AD TCD- AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07-feb-70 30-jun-89 0642 -70 JCAB AD TCD- Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07-feb-70 15-jul-04 N/A by s/n 0643-70 JCAB AD TCD - Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25 -mar -70 26 -mar -09 N/A by model 0652-70 JCAB AD TCD - Engine Nacelle Tail Area -Modification 25 -mar -70 26 -mar -09 N/A by model 0653-70 of JCAB AD TCD - Replacement of bearing in LFV LVA457 MITSUBISHI SB 123 01 -May - 26 -mar -09 N/A by s/n 0660-70 nosegearstrut 1970 JCAB AD TCD - Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 Rev 25 -mar -72 14 -jul -04 N/A N/A by s/n. 0730-1-72 B JCAB AD TCD - Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10 -dec -86 26 -mar -09 N/A by s/n 0730 -2-86 JCAB AD TCD - Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04 -sep -72 10 -sep -72 N/A N/A due to s/n. 0859 -72 JCAB AD TCD - NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09 -Oct - 31 -dec -72 N/A N/A due to s/n. 0866 -72 1972 JCAB AD TCD - Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 Rev 12 -nov -74 16 -May - N/A N/A due to s/n. 0947A-74 A 1974 JCAB AD TCD - Inspection of Windshields MITSUBISHI SB 163 Rev B 22 -dec -78 26 -mar -09 0948A-1-78 JCAB AD TCD - Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 Rev 07 -Oct - 16 -May - 0948A-74 B 1974 1974 JCAB AD TCD - Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 Rev 06 -Oct - 23 -apr -85 1001A-76 E 1976 JCAB AD TCD - Replacement of Elevator Trim Tab FINNISH AD M 1080/82 LFV LVD1971 12 -dec -84 23 -apr -85 1001B-2-84 Bracket MITSUBISHI SB 176 Rev E JCAB AD TCD - Insp. of wingflap controlsystem FAA, U.S AD 75 -16 -13 LFV LVA1011 Rev A 06 -sep -76 25 -mar -77 Revision C PCW by Swedair. 1094A-76 MITSUBISHI SB 167 Rev D JCAB AD TCD - Insp. of propeller controllever inst. FAA, U.S AD 75 -16 -20 LFV LVA1012 06 -May - 20 -May - 1188-75 MITSUBISHI SB 168 Rev A 1975 1975 JCAB AD TCD - Engine Cowling Latches FAA, U.S AD 78 -03 -05 LFV LVA1014 Rev A 20 -sep -75 15 -jul -04 Found SB 171 and SB 180 PCW. 1202-75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 84(195) JCAB AD TCD- Insp/mod of NLG shimmydamper LFV LVA1013 MITSUBISHI SB 169 Rev B 16-jun-75 16-jun-75 1209-75 locking JCAB AD TCD- Insp./repl. of MLG fwd door LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 30-jun-89 N/A N/A due to model. 1235-75 emerg.cables JCAB AD TCD- Supp.,MLG Forward D. Actuating MITSUBISHI SB 172 14-nov-75 26-mar-09 N/A by model 1272 -75 Mech. -I&M JCAB AD TCD- Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76 24-nov-09 PCW Ref. SB 173 1284-1-76 JCAB AD TCD - Fire hazard in rear baggage 01 -jul -76 26 -mar -09 N/A by s/n 1328-76 compartment JCAB AD TCD - Barrel Nut, Inner/Outer Wing Conn. - MITSUBISHI SB 175 16 -aug -76 01 -sep -09 N/A by s/n 1353-76 Repl. JCAB AD TCD - Inspect strobelight conduit in Tiptank LFV LVA1196 18 -Oct - 22 -dec -89 Part.1 1370-76 1976 JCAB AD TCD - Insp. rear eng. cowling reg. LFV LVA1197 Rev A MITSUBISHI SB 177 06 -feb -02 25 -May - Previously complied with 1379-1-80 heatdamage Rev B 1977 JCAB AD TCD - Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12 -dec -77 24 -mar -09 ref. SB 180 1520A -77 JCAB AD TCD - Fatigue failure of the NLG strut assy. LFV LVA1546 MITSUBISHI SB 181 PART 2 12 -jul -85 15 -jul -04 PCW Found SB 181 part 2 PCW. 1768 -1-85 Rev B JCAB AD TCD - Modification of bagagecompartment LFV LVA1583 MITSUBISHI SB 182 05 -feb -02 11 -feb -80 N/A N/A due to s/n. 1817 -79 JCAB AD TCD - Insp. firewarning & emerg.power LFV LVA1740 MITSUBISHI SB 187 Rev B 05 -feb -02 27 -May - N/A N/A due to s/n. 2048-81 circuit 1981 JCAB AD TCD - Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05 -feb -02 02 -sep -81 2070-81 JCAB AD TCD - Insp./replace engine electrical LFV LVA1788 MITSUBISHI SB 191 06 -feb -02 09 -feb -82 2113-82 harness JCAB AD TCD - Flap system torquetubes supersed 01 -feb -89 24 -mar -09 PCW 2252-2-88 TCD-2252-1-87 JCAB AD TCD - Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04 -feb -83 18 -May - 2252-83 1995 JCAB AD TCD - NLG. bracket attaching to drag strut 13 -aug -83 24 -mar -09 N/A by model 2263-83 JCAB AD TCD - Engine inlet anti -ice tubing. MITSUBISHI SB 196 Rev A 05 -jun -84 10 -mar -09 PCW 2342-1-84 Torq./lock JCAB AD TCD - Engine inlet anti -ice tubing. LFV LVA1942 MITSUBISHI SB 196 Rev A 06 -feb -02 16 -feb -84 2342-84 Torq./lock JCAB AD TCD - Pitot Tube Wiring LFV LVD2015 Rev B MITSUBISHI SR 053A 16 -jun -87 15 -jul -04 SB PCW. 2450A-87

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 85(195) JCAB AD TCD- Add. seal/Tq. insp of flap flex. shaft 01-May- 09-mar-09 PCW see TCD-2451-85 2451-1-87 1987 JCAB AD TCD- Add. seal/Tq. insp of flap flex. shaft LFV LVD2037 MITSUBISHI SB 198 30-sep-85 29-jul-85 2451-85 Superseeded by TCD-2451-1-87 JCAB AD TCD- Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 23-apr-90 2545 -1-88 JCAB AD TCD- Auto-ignition System FINNISH AD M 2435/97 LFV LVD2761 01-feb-97 22-nov-01 2679A-97 MITSUBISHI SB 226 Rev E JCAB AD TCD - Insp./mod. of rudder trimtab LFV LVD2338 MITSUBISHI SB 211 28 -mar -91 14 -jul -04 N/A N/A by s7n. 3378-90 leadingedge JCAB AD TCD - Anti ice/De -ice system FINNISH AD M 2364/96 LFV LVD2347 Rev 25 -May - 31 -May - 3393A-96 1 MITSUBISHI SB 212 Rev A 1996 2010 JCAB AD TCD - Unintentional engagement of A/P...... 17 -jun -91 24 -mar -09 N/A by model 3464-91 JCAB AD TCD - Mod.of Autopilote pitchtrimsystem FINNISH AD M 2581/98 LFV LVD2450 LFV 17 -aug -98 25 -mar -99 3740A-98 MSB 216, 228 LVD 2898 LVD2898 MITSUBISHI SB 216 MITSUBISHI SB 228 JCAB AD TCD- Tiptank inst FINNISH AD M 2110/93 LFV LVD2512 10-sep-93 01-mar-94 3901-93 MITSUBISHI SB 221 JCAB AD TCD- Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592 28-nov-94 08-mar-95 3942-1-94 MITSUBISHI SB 219 Rev A JCAB AD TCD- Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01-feb-94 08-mar-95 3942-94 JCAB AD TCD - Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688 01 -apr -96 07 -Oct - 4310-96 MITSUBISHI SB 225 1997 JCAB AD TCD - Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689 01 -apr -96 30 -jul -96 4379-96 MITSUBISHI SB 229 JCAB AD TCD - Icing Limitation FAA, U.S AD 96 -25 -02 LFV LVD2749 27 -dec -96 12 -feb -02 4552 -96 JCAB AD TCD - Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI SB 14 -jul -97 02 -apr -02 4625 -97 093/22 -009 JCAB AD TCD - Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B 16 -mar -01 02 -apr -02 PCW Ref AMOC LFV Appr M15/01, TDM 01 -45 4625A -2001 JCAB AD TCD - De -ice system Modification FINNISH AD M 2461/97 LFV LVD2800 01 -May - 14 -jul -04 PCW 4626 -97 MITSUBISHI SB 232 Rev A 1997 JCAB AD TCD - Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819 01 -jun -97 25 -mar -99 4684 -97 MITSUBISHI SB 230 JCAB AD TCD - Ändring av flyghandbok LVD FINNISH AD M 2518/98 LFV LVD2922 18 -feb -98 02 -dec -98 FAA AD utförd. 4753-98 2922,FAA AD 97-20-14, MHI SN 117A MITSUBISHI SN 117 Rev D

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 86(195) JCAB AD TCD- Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 17-May- inserted in AFM limitations 4753A-2004 2004 JCAB AD TCD- Inspection of landing gear power FINNISH AD M 2574/98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model 4838-98 train MITSUBISHI SB 235 JCAB AD TCD- Inappropriate calib. of eng. trq-meter MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A. 4889 -2-2007 JCAB AD TCD- Insp. of Engine Torque Indication FINNISH AD M 2608/98 LFV LVD2924 05-nov-98 14-jul-04 PCW 4889-98 System LFV 2924, MU SB 233 MITSUBISHI SB 233 Rev B JCAB AD TCD - Check of flight idle FF LVD 2925, MU FINNISH AD M 2609/98 LFV LVD2925 04 -nov -98 27 -sep -10 4890-98 SB 234 MITSUBISHI SB 234 JCAB AD TCD - Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17 -May - 24 -mar -09 N/A by model 5030-99 1999 JCAB AD TCD - AFM revision LFV LVD3112 27 -nov -00 12 -feb -02 5432-2000 JCAB AD TCD - To prevent loss of airplane control LFV LVD3123 16 -mar -01 12 -feb -02 5547-2001 JCAB AD TCD - Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12 -sep -01 11 -Oct - 5747 -2001 2001 JCAB AD TCD - Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27 -dec -01 16 -May - 5864 -2001 2002 JCAB AD TCD - Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17 -mar -03 14 -nov -03 6127 -2003 JCAB AD TCD - Inspection of Wing Attachment MITSUBISHI SB 241 Rev A 27 -dec -06 17 -jan -07 c/o in conjunction with wingstudie 7030-2006 Hardware

LFV, Luftfartsverket LFV LVA 1011 A Kontroll av vingklaffarnas FAA, U.S AD 75-16-13 JCAB AD TCD- 05-feb-02 A 25-mar-77 Revision C PCW by Swedair. manöversystem 1094A-76 MITSUBISHI SB 167 Rev D LFV LVA 1012 Kontroll av propellerreglagets FAA, U.S AD 75-16-20 JCAB AD TCD-1188- 05-feb-02 20-May- montering 75 MITSUBISHI SB 168 Rev A 1975 LFV LVA 1013 Kontr. och mod. av låsning på nosställ JCAB AD TCD-1209-75 MITSUBISHI SB 169 05-feb-02 16-jun-75 Rev B LFV LVA 1014 A Kontr. & byte av motorinkl. FAA, U.S AD 78-03-05 JCAB AD TCD-1202- 05-feb-02 A 25-nov-75 låsanordning 75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A LFV LVA 1083 Insp. & utbyte av lina för nödöppning JCAB AD TCD-1235-75 MITSUBISHI SB 170 05-feb-02 30-jun-89 N/A N/A due to s/n. Rev A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 87(195) LFV LVA 1197 A Förhindr. av värmeskador på JCAB AD TCD-1379-1-80 MITSUBISHI SB 06-feb-02 A 25-May- Previously complied with bak.motorpl. 177 Rev B 1977 LFV LVA 1238 Kontr. & byte av infästningsdet. 06-feb-02 21-apr-09 N/A by s/n trimrod LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86-15-03 JCAB AD TCD-1768- 06-feb-02 15-mar-84 1-85 MITSUBISHI SB 181 PART 2 Rev B LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD-1817-79 MITSUBISHI SB 182 05-feb-02 11-feb-80 N/A N/A due to s/n. LFV LVA 1740 Kontr.av brandvarnings -och JCAB AD TCD -2048 -81 MITSUBISHI SB 187 05 -feb -02 31 -aug -09 N/A by s/n n"dstr"mskret Rev B LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD -2070 -81 MITSUBISHI SB 188 05 -feb -02 02 -sep -81 LFV LVA 1788 Kontroll/Utbyte av elledningar på JCAB AD TCD -2113 -82 MITSUBISHI SB 191 06 -feb -02 09 -feb -82 motor COP 2011/09/1 19:37:04 LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör JCAB AD TCD -2252 -83 MITSUBISHI SB 189 06 -feb -02 18 -May - Rev C 1995 LFV LVA 1942 Momentdragning/låsn.av koppl.i JCAB AD TCD -2342 -84 MITSUBISHI SB 196 06 -feb -02 16 -feb -84 varmlufts Rev A LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD -0643 -70 MITSUBISHI SB 114 05 -feb -02 15 -jul -04 N/A N/A by s/n. LFV LVA 439 Rev. av flyghandbok betr. JCAB AD TCD -0642 -70 MITSUBISHI SB 112 05 -feb -02 30 -jun -89 bränslespec. Rev C LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD -0652 -70 MITSUBISHI SB 119 05 -feb -02 26 -mar -09 N/A by model LFV LVA 457 Utbyte av lager i nosst,llets st"td,mp. JCAB AD TCD -0660 -70 MITSUBISHI SB 123 05 -feb -02 26 -mar -09 N/A by s/n LFV LVA 543 B Insp. och målning av integraltankar JCAB AD TCD-0730-1-72 05-feb-02 B 14-jul-04 N/A N/A by s/n. LFV LVA 645 Modifiering av el -system JCAB AD TCD -0859 -72 MITSUBISHI SB 156 05 -feb -02 08 -dec -09 N/A by A/C serial number LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD -0866 -72 05 -feb -02 31 -aug -09 N/A by s/n LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD -0947A -74 MITSUBISHI SB 05 -feb -02 A 16 -May - N/A N/A due to s/n. 162 Rev A 1974 LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74 -11 -01 FAA, U.S AD 75 -03 - 05 -feb -02 A 26 -mar -09 06 JCAB AD TCD-0948A-74 MITSUBISHI SB 163 Rev B LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar JCAB AD TCD-1001A-76 05-feb-02 A 23-apr-85 LFV LVD 1238 Kontr./byte infästn.det. 15 -apr -77 31 -aug -09 N/A by s/n höjdtrimroder LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD -1001B -2-84 MITSUBISHI SB 18 -jan -85 23 -apr -85 176 Rev E

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 88(195) LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34-005 FAA, U.S AD 86-20-01 JCAB AD TCD- 24-May- B 20-May- Rev A, MHI SR 53 2450A-87 1985 1986 LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85 29-jul-85 LFV LVD 2069 Altimeter 25 -mar -86 22 -dec -89 N/A N/A by p/n & s/n LFV LVD 2113 Modif. & revision Handbook MHI SR 26 -jan -87 15 -jan -88 006B, MAI SR 040/74-001RA LFV LVD 2190 Autopilot Switch MU2 SB 066/22 -006 FAA, U.S AD 88 -13 -01 MAI SB 066/22 -006 19 -aug -88 22 -dec -89 N/A Bendix A/P ej installerad och SB 206 Rev A MITSUBISHI SB 206 LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD -2545 -1-88 MITSUBISHI SB 19 -aug -88 28 -sep -89 201 Rev A LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88 -23 -01 JCAB AD TCD -2252 - 08 -dec -88 18 -May - 1-87 MAI SB 067/27-008 Rev A 1995 MITSUBISHI SB 189 Rev C LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88 -21 -01 Rev 1 08 -Dec -1988 12 -feb -02 LFV LVD 2338 Kont./Mod.av sidorodrets JCAB AD TCD -3378 -90 MITSUBISHI SB 211 28 -mar -91 14 -jul -04 N/A N/A by s/n. trimroderframka Mitsubishi MHI SB 211 LFV LVD 2347 1 Control Deice -system Mitsubishi SB JCAB AD TCD -3393A -96 MITSUBISHI SB 29 -May - 1 31 -May - 212A 212 Rev A 1996 2010 LFV LVD 2352 Shoulder Harness Inst. FAA AC 43 -13 23 -May - 10 -jun -91 checked OK. CHPT 9 1991 LFV LVD 2450 Elevator Trim Tab Installation MU SB JCAB AD TCD -3740A -98 MITSUBISHI SB 03 -dec -92 12 -Oct - 216 216 1993 LFV LVD 2477 Electric Trim System AD930711, MU FAA, U.S AD 93 -07 -11 MAI SB 079/27 -010 03 -jun -93 27 -mar -09 N/A by s/n SB 079/27-0-010 LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD -3901 -93 MITSUBISHI SB 221 02 -dec -93 01 -mar -94 LFV LVD 2537 Reducering av Höjdrodrets FAA, U.S AD 94-04-16 MITSUBISHI SB 216 07-apr-94 12-Oct- trimområde. FAA AD 94-04-16, SB 1993 216 LFV LVD 2538 Byte Låspinne i landställets nödutf. SB JCAB AD TCD -3942 -94 MITSUBISHI SB 219 07 -apr -94 08 -mar -95 219 Rev A LFV LVD 2551 Adj.of Ground Idle FAA AD 94 -11 -04 FAA, U.S AD 94 -11 -04 22 -jun -94 27 -mar -09 N/A by s/n LFV LVD 2592 Insp/Repl. of Lock -pin in L/G gearbox JCAB AD TCD -3942 -1-94 MITSUBISHI SB 09 -feb -95 08 -mar -95 TCD-3942-1-94, MSB 219A 219 Rev A LFV LVD 2688 Kontr/byte av infästn.bult för tiptank FAA, U.S AD 98 -20 -39 JCAB AD TCD -4310 - 09 -May - 07 -Oct - MU-2 SB 225 96 MITSUBISHI SB 225 1996 1997

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 89(195) LFV LVD 2689 Kontroll av linkage för prop.flöjning JCAB AD TCD-4379-96 MITSUBISHI SB 229 09-May- 30-jul-96 MU-2 SB 229 1996 LFV LVD 2732 Inspection/ Replacement of Prop FAA, U.S AD 96-18-14 HARTZELL SB 61- 27-sep-96 16-May- Prop. BU10873 utbytt samt mod. till BUA Hub. FAA AD 96-18-14, Hz SB 136H 261 Rev 1 2002 LFV LVD 2749 Revision av flyghandbok AFM TCD- FAA, U.S AD 96-25-02 JCAB AD TCD-4552- 21-jan-97 12-feb-02 4552 -96 96 LFV LVD 2761 Installation av autoignition system JCAB AD TCD-2679A-97 MITSUBISHI SB 14-feb-97 26-mar-99 TCD-2679A-97 226 Rev E LFV LVD 2769 Demont.av backventil i FAA, U.S AD 97 -04 -13 MITSUBISHI SB 130 18 -mar -97 05 -May - N/A N/A due to s/n. bränslesystemets MU-2 SB 130A Rev A 1997 LFV LVD 2800 Mod. av De -ice Monitoring System JCAB AD TCD -4626 -97 MITSUBISHI SB 232 28 -aug -97 27 -May - Mitsubishi SB 232, TCD-4626-97 Rev A 1998 LFV LVD 2819 Mod.av lagerboxar för JCAB AD TCD -4684 -97 MITSUBISHI SB 230 18 -nov -97 22 -jan -98 landställssystem Mitsubishi SB 230 LFV LVD 2853 Periodisk funktionskontroll av 23 -mar -98 21 -jan -11 nödutgång LFV LVD 2897 Kontroll av landst,llets drivsystem JCAB AD TCD -4838 -98 MITSUBISHI SB 235 02 -aug -98 24 -mar -09 N/A by model TCD -4838 -98, SB 235 LFV LVD 2898 Mod. av autopilotens höjdtrimsystem JCAB AD TCD -3740A -98 MITSUBISHI SB 27 -aug -98 12 -mar -99 TCD -3740A -98, SB 216, 228 216 MITSUBISHI SB 228 LFV LVD 2922 Änd.av Flyghandbok -Extra krav på JCAB AD TCD -4753 -98 MITSUBISHI SN 117 12 -nov -98 02 -dec -98 FAA AD utförd. typutbi TCD -4753 -98, MHI SN 117A Rev D LFV LVD 2924 Kontr/Just av motorernas Torque JCAB AD TCD -4889 -98 MITSUBISHI SB 233 01 -dec -98 27 -sep -99 SB 233A C/Out. indikeri MHI SB 233, TCD-4889-98 Rev B LFV LVD 2925 Kontr/just av mot bränsleflöde Flight JCAB AD TCD -4890 -98 MITSUBISHI SB 234 01 -dec -98 27 -sep -10 Id MHI SB 234 LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD -5030 -99 MITSUBISHI SB 209 18 -jun -99 24 -mar -09 N/A by model Rev B LFV LVD 3112 Revision av flyghandbok JCAB AD TCD -5432 -2000 30 -jan -01 12 -feb -02 LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD-4625A-2001 MAI SB 093/22- 02-apr-01 02-apr-02 Ref AMOC LFV Appr M15/01, TDM 01-45 009 MITSUBISHI SB 231 Rev B NYGE TDM01-45 LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD-5547-2001 02-apr-01 12-feb-02 LFV LVD 3166 Sprickkontroll av infästning till ving - JCAB AD TCD -5747 -2001 MITSUBISHI SB 20 -sep -01 11 -Oct - spetstank 236 2001 LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD -5864 -2001 MAI SB 099/27 - 09 -jan -02 16 -May - 012 MITSUBISHI SB 237 2002 LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD -6127 -2003 MITSUBISHI SB 21 -mar -03 14 -nov -03

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 90(195) 239

MAI, Mitsubishi Aircraft Internation MAI SB 047/30 - A Torque of Bleed Air Tube Coupling FAA, U.S AD 84 -12 -04 MITSUBISHI SB 196 19 -jul -84 A 16 -feb -84 001 Nuts AD 84-12-04,SB 196A Rev A MAI SB 051/27 - Add.Seal and Flap Flexible Shaft FAA, U.S AD 87 -04 -03 01 -feb -85 29 -jul -85 007 Torque AD 87-04-03, SB 198 MAI SB 067/27 - A Insp/Repl. of Flap Control System FAA, U.S AD 88 -23 -01 LFV LVD2202 29 -mar -95 A 18 -May - 008 Torque AD 88-23-01, SB 189B 1995 MAI SB 069/24 - Split Radio Bus Inspection and MAI SB 066/22 -006 Rev A 17 -nov -88 22 -dec -89 N/A N/A due to Aircraft s/n 006 Rework MAI SB 089/57 - A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98 -20 -39 05 -nov -96 A 07 -Oct - N/A N/A due to s/n. 002 1997 MAI SN 110/00 - Power Lever Position Warning 25 -feb -09 09 -nov -09 SB 240 considered 017A MAI SN 111/77 - Torque Indicating System Shift 20 -nov -08 11 -mar -09 SB 233 considered 004 Potential MAI SR 020/34 - Anti Ice Capability AD 86 -20 -01, SR FAA, U.S AD 86 -20 -01 LFV LVD2015 Rev B 06 -Oct - 30 -aug -00 N/A N/A due to s/n. 005 053A MITSUBISHI SR 053A 1986

MITSUBISHI, Mitsubishi Heavy Industries Ltd MITSUBISHI MSR **RECOVERED RECORD** B 15 -jan -88 066 B MITSUBISHI SB Bendix M4D 18 -dec -87 28 -sep -89 066 MITSUBISHI SB M-4() Autop.Engage Switch Guard Install. 11 -apr -91 12 -apr -95 N/A 076/22-008 MITSUBISHI SB C Anti -Ice Additive in Fuel -Usage of JCAB AD TCD -0642 -70 LFV LVA439 09 -Oct - C 30 -jun -89 112 1971 MITSUBISHI SB Fuel Quantity Indicator Readjustmnet JCAB AD TCD -0643 -70 LFV LVA438 01 -jan -70 15 -jul -04 N/A N/A by s/n. 114 MITSUBISHI SB The Bolt and Bolt Hole Diam. of Nose L.G JCAB AD TCD -0652 -70 LFV LVA456 10 -mar -70 26 -mar -09 N/A by model 119 MITSUBISHI SB Bearing,Oleo Strut,Nose L.G. -Repl. of JCAB AD TCD -0660 -70 LFV LVA457 01 -apr -70 26 -mar -09 N/A by s/n 123 MITSUBISHI SB Scissors Switch,Nose L.G. -Install. of 31 -aug -70 30 -jun -89 N/A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 91(195) 124 MITSUBISHI SB B Tip Tank Air Pressure Modification 28 -jun -94 B 05 -nov -09 N/A by model & s/n 128 MITSUBISHI SB B Top Coating, Wing Integral Main F.T. -SIo JCAB AD TCD -0730 -1-72 JCAB AD TCD - 05 -jan -72 B 14 -jul -04 N/A N/A by s/n. 143 0730-2-86 MITSUBISHI SB A Flex. Shafts, Flap Control Sys. -Insp. of JCAB AD TCD -0947A -74 LFV LVA828 Rev A 03 -Oct - A 16 -May - N/A 162 (AD750201) 1974 1974 MITSUBISHI SB B Insp. of Outer Pane, Front Winds. & Inst FAA, U.S AD 74 -11 -01 JCAB AD TCD - 16 -nov -78 16 -May - 163 0948A-1-78 JCAB AD TCD-0948A-74 LFV 1974 LVA829 Rev A MITSUBISHI SB A Lubr. Interval,Wheel Bearing,Main & 24 -jul -80 29 -jul -74 N/A 165 Nose MITSUBISHI SB Wing Flap 24 -jul -80 08 -jan -75 166 MITSUBISHI SB D Flap M.Jack Screw -Insp. of and/or Main FAA, U.S AD 75 -16 -13 JCAB AD TCD - 24 -jul -80 D 25 -mar -77 Revision C PCW by Swedair. 167 G 1094A-76 LFV LVA1011 Rev A MITSUBISHI SB A Propeller Pitch Control Lever -Insp. of FAA, U.S AD 75 -16 -20 JCAB AD TCD -1188 - 24 -jul -80 A 20 -May - 168 (AD761620) 75 LFV LVA1012 1975 MITSUBISHI SB B Shimmy Damper -Insp. and Modification JCAB AD TCD -1209 -75 LFV LVA1013 24 -jul -80 B 05 -nov -09 PCW 169 of MITSUBISHI SB A MLG Forward Door Em.Op. Cable -Insp. & JCAB AD TCD -1235 -75 LFV LVA1083 24 -mar -77 A 30 -jun -89 N/A N/A due to s/n 170 Re (AD762204) MITSUBISHI SB B Latches,Eng. Nacelle Upper D. -Insp.& FAA, U.S AD 78 -03 -05 JCAB AD TCD -1202 - 17 -nov -77 B 25 -nov -78 171 Mod (AD780305) 75 LFV LVA1014 Rev A MITSUBISHI SB A Drag Strut, Main L.G. -Modification of JCAB AD TCD -1284 -1-76 24 -jul -80 05 -mar -76 173 MITSUBISHI SB C Tip Tank Conduit Tube -Insp.of,and FINNISH AD M 1177/83 JCAB AD TCD - 02 -Oct - C 18 -jun -10 174 PART 1 Rew.of (AD830902) 1370A-81 LFV LVA1196 1981 MITSUBISHI SB Barrel Nut, Inner/Outer Wing Conn.- JCAB AD TCD-1353-76 26-jun-76 01-sep-09 N/A by s/n 175 Repl. MITSUBISHI SB E Elevator Trim Tab Bracket-Repl. of FAA, U.S AD 84-25-02 FINNISH AD M 26-sep-84 E 23-apr-85 176 LVD1971, AD 84-25-02, SB 031/27-005R1 1080/82 JCAB AD TCD-1001A-76 JCAB AD TCD-1001B-2-84 LFV LVD1971 MITSUBISHI SB B Mod. of Engine Nacelle Tail Area JCAB AD TCD -1379 -1-80 LFV LVA1197 Rev 11 -sep -80 B 25 -May - Previously complied with 177 (AD810601) A 1977 MITSUBISHI SB Rodd Assem., Engine Nacelle Upper D. - 27 -May - 22 -dec -89 179 R&M 1977 MITSUBISHI SB A Link, Engine Nacelle Upper D. -Repl. of FAA, U.S AD 78 -03 -05 JCAB AD TCD -1202 - 17 -nov -77 A 09 -May - 180 (AD780305) 75 JCAB AD TCD-1520A-77 LFV LVA1014 1978

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 92(195) Rev A MITSUBISHI SB B Insp. and Repl. of Nose L.G. Strut Assem FAA, U.S AD 86 -15 -03 JCAB AD TCD -1768 - 08 -apr -85 B 15 -mar -84 181 PART 2 (AD801812) 1-85 LFV LVA1546 MITSUBISHI SB Add. of Ceiling Cover, Rear Bagg. Comp. JCAB AD TCD -1817 -79 LFV LVA1583 16 -nov -79 16 -nov -79 N/A N/A due to s/n. 182 MITSUBISHI SB Turnbuckle, Control Cables -Repl. of 04 -apr -80 15 -dec -89 184 MITSUBISHI SB Down Lock Mech., Nose L.G. -Insp. of JCAB AD TCD -2070 -81 LFV LVA1753 13 -jul -81 02 -sep -81 188 MITSUBISHI SB C Flap Control Torque Tube AD 88 -23 -01, FINNISH AD M 2722/00 JCAB AD TCD - 28 -jun -94 C 18 -May - 189 SB 067/27-008 2252-1-87 JCAB AD TCD-2252-83 LFV 1995 LVA1873 LFV LVD2202 MITSUBISHI SB A Trav. Nut Repl. of L.G. Mech. Stop Assem 28 -jun -94 17 -jan -84 190 MITSUBISHI SB Engine El. Wire -Insp. and Replacement JCAB AD TCD -2113 -82 LFV LVA1788 21 -dec -81 09 -feb -82 191 of (AD820802) MITSUBISHI SB B Landing Gear Warning Horn Syst.Modif. 15 -jun -94 B 04 -dec -00 Rev A är utförd. 193 MITSUBISHI SB Master Cauting Light Visibility -Impr. of 23 -aug -82 30 -May - 194 1983 MITSUBISHI SB A Ret. of coupling nut on the bleed air tu FAA, U.S AD 84 -12 -04 JCAB AD TCD -2342 - 12 -apr -84 A 16 -feb -84 196 AD 84-12-04, SB 047/30-001 1-84 JCAB AD TCD-2342-84 LFV LVA1942 MAI SB 047/30-001 Rev A MITSUBISHI SB Add. Seal & Torque Insp. of Flap Flex.Sh FAA, U.S AD 87 -04 -03 JCAB AD TCD -2451 - 13 -feb -85 29 -jul -85 198 LVD2037, AD 87-04-03, SB 051/27-007 85 LFV LVD2037 MITSUBISHI SB A Engine Lubricating Tubing Insp. & Protec 24 -jun -94 A 06 -nov -09 PCW 199 MITSUBISHI SB B Insp of Nose Ldg Gear Drag Strut Link 24 -jun -94 A 17 -feb -88 200 MITSUBISHI SB A Generator Circuit Wires Insp. and Mod. FAA, U.S AD 87 -12 -02 JCAB AD TCD -2545 - 02 -mar -88 A 23 -apr -90 201 1-88 LFV LVD2191 MITSUBISHI SB Speed Placard Change 03 -mar -87 23 -apr -90 204 MITSUBISHI SB Bendix Autop.Disengagement Method FAA, U.S AD 88 -13 -01 JCAB AD TCD -2856 - 13 -Oct - 31 -jan -89 N/A N/A due to Autopilot model 206 Stand. 1-97 LFV LVD2190 1987 MITSUBISHI SB Rudder T.T. & Elevator T.T. Insp. & Rep. 20 -May - 14 -jan -10 207 1988 MITSUBISHI SB B Fuselage inspection JCAB AD TCD -5030 -99 LFV LVD2988 19 -apr -99 B 24 -mar -09 N/A by model 209

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 93(195) MITSUBISHI SB A Engine Ignition Unit Replacement 12-nov-96 06-mar-98 210 MITSUBISHI SB Rudder Trim Tab Modification (LVD JCAB AD TCD-3378-90 LFV LVD2338 20-nov-90 14-jul-04 N/A N/A by s/n. 211 2338) MITSUBISHI SB A Insp of Anti-ice/Deice Systems (LVD JCAB AD TCD-3393A-96 LFV LVD2347 Rev 25-apr-96 A 31-May- 212 2347), 1 2010 MITSUBISHI SB Engine Control Rod Inspection 06-dec-91 08-apr-92 214 MITSUBISHI SB Removel of Prop. Governor Speed Signal 23 -Oct - 17 -feb -92 N/A N/A due to -1 engine 215 1991 MITSUBISHI SB Elevator Trim Tab Installation (LVD 2450 FAA, U.S AD 2007 -17 -09 FAA, U.S AD 94 - 11 -sep -92 12 -Oct - 216 04-16 JCAB AD TCD-3740A-98 LFV 1993 LVD2450 LFV LVD2537 LFV LVD2898 MITSUBISHI SB A Propeller Feathering Linkage Inspection 17-jan-94 A 01-mar-94 218 MITSUBISHI SB A Emergency Gear Down G.box Lower Pin JCAB AD TCD-3942-1-94 JCAB AD TCD- 24-Oct- A 08-mar-95 219 Repl 3942-94 LFV LVD2538 LFV LVD2592 1994 MITSUBISHI SB Tip Tank Conduit Tube Insp. and Rep. JCAB AD TCD-3901-93 LFV LVD2512 10-aug-93 01-mar-94 221 MITSUBISHI SB Fuselage Waterproof Modification SR 28-jun-94 27-Oct- 222 019 1998 MITSUBISHI SB Pitot/Static System Improvement SR 064 MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 30-aug-00 223 MITSUBISHI SB C Acrylic Windsheild/Window glass Insp. FAA, U.S AD 2003 -17 -04 FINNISH AD M 30 -apr -98 C 18 -jun -10 224 UHB 3076 JCAB AD TCD-4311-95 LFV LVD2678 MITSUBISHI SB Forward fitting bult of wingtip tank LVD FAA, U.S AD 98 -20 -39 FINNISH AD M 29 -sep -95 07 -Oct - 225 2688 2351/96 JCAB AD TCD-4310-96 LFV 1997 LVD2688 MITSUBISHI SB E Auto-Ignition System Installation LVD FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S 18-sep-01 E 22-nov-01 PCW no further action (rev.E) required due to s/n. 226 2761 (2113), AD TCD-2679A-97 AD 86-26-02 FINNISH AD M 2435/97 FINNISH AD M 2786/00 JCAB AD TCD- 2679A-97 LFV LVD2761 MAI SB 086/74- 002 Rev A MITSUBISHI SB Rudder Torque Tube Modification 20 -dec -96 04 -sep -97 227 MITSUBISHI SB Elevator Trim Indicator Modification LFV FAA, U.S AD 2007 -17 -09 FINNISH AD M 13 -jul -98 25 -mar -99 Visuell kontroll utförd SB införd 228 2898 2581/98 JCAB AD TCD-3740A-98 LFV LVD2898 MITSUBISHI SB Feathering Valve/Linkage Insp. FAA, U.S AD 2006 -15 -07 JCAB AD TCD - 20 -feb -96 17 -apr -98 229 4379-96 LFV LVD2689

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 94(195) MITSUBISHI SB Mod.of Bearing Box Ldg. Gear Act. LVD JCAB AD TCD-4684-97 LFV LVD2819 05-mar-97 22-jan-98 230 2819 MITSUBISHI SB B Inst.of Trim-In-Motion Alert System FAA, U.S AD 2000-09-15 Rev 1 FINNISH AD 11-dec-02 B 03-mar-03 SL 079 performed earlier. 231 M 2460/97 UPPHÄVD FINNISH AD M 2786/00 JCAB AD TCD-4625A-2001 LFV LVD3122 MAI SB 093/22-009 NYGE TDM01-45 MITSUBISHI SB A De -Ice System Modification LVD 2800, FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH AD 06 -jun -02 A 06 -jun -02 N/C due to previuosly complied with SB 232 rev 0. 232 TCD-4626-97 M 2786/00 JCAB AD TCD-4626-97 LFV LVD2800 MAI SB 096/30-004 MITSUBISHI SB B Insp.of Engine Torque Indication System. FAA, U.S AD 2006 -17 -01 FINNISH AD M 08 -mar -07 B 18 -apr -07 Checked, previously carried out 233 TCD-4889-98, LFV 2924 2608/98 JCAB AD TCD-4889-2-2007 JCAB AD TCD-4889-98 LFV LVD2924 MITSUBISHI SB Fl.Check of the Flight Idle Fuel Flow Se FAA, U.S AD 2006 -17 -05 JCAB AD TCD - 07 -Oct - 27 -sep -10 234 TCD-4890-98, LVD 2925 4890-98 LFV LVD2925 1998 MITSUBISHI SB Inspection of landing gear power train JCAB AD TCD -4838 -98 LFV LVD2897 04 -aug -98 24 -mar -09 N/A by model 235 MITSUBISHI SB Inspection of Tip Tank Brackets JCAB AD TCD -5747 -2001 LFV LVD3166 28 -aug -01 11 -Oct - 236 2001 MITSUBISHI SB Inspection of Flap Drive Train JCAB AD TCD -5864 -2001 LFV LVD3212 13 -dec -01 16 -May - 237 2002 MITSUBISHI SB Main Landing Gear Door Safety Pin 05 -dec -02 09 -jan -03 Perf. at each 600 h. insp. 238 MITSUBISHI SB Pneumatic Line Insp. and Modification JCAB AD TCD -6127 -2003 LFV LVD3322 26 -dec -02 14 -nov -03 239 MITSUBISHI SB Inst.of Trottle Quadrant Placard 26 -feb -03 14 -nov -03 240 MITSUBISHI SB A Inspection of Wing Attachment FAA, U.S AD 2006 -13 -15 JCAB AD TCD - 21 -nov -06 A 17 -jan -07 c/o in conjunction with wingstudie 241 Hardware 7030-2006 MITSUBISHI SL System 17 -feb -89 07 -jul -91 060 MITSUBISHI SL Automatic Autopilot Disconnect System 28 -jan -02 31 -May - 078 2010 MITSUBISHI SL Diode inst.in Flap Position Ind.Curcuit 28 -jan -02 02 -apr -02 079 MITSUBISHI SL Hartzell Propeller Mounting Bolt Insp. HARTZELL SB 61 -256 05 -apr -02 02 -Oct - 080 2002 MITSUBISHI SL Pneumatic De -Ice Monitoring System 14 -jun -04 31 -May - 084 2010

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 95(195) MITSUBISHI SL Hartzell prop. mount. bolt insp. HARTZELL SB 61-279 ALERT Rev 4 17-May- 14-sep-05 085 2005 MITSUBISHI SN B Rudder Torque Tube AD 86-20-01, SB 05-nov-86 B 22-dec-89 053 020/34-005 MITSUBISHI SN D Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD 14-jun-04 D 17-May- 117 TCD -4753 -98 LFV LVD2922 2004 MITSUBISHI SN Water Ingress into Vertical Stabilizer 19-dec-03 06-mar-04 146 MITSUBISHI SN Reminders for safe operation 18 -nov -05 22 -mar -06 Genomförs enl. AMP MU -2 & DHB 148 MITSUBISHI SN Power Lever Position Warning 25 -feb -09 09 -nov -09 SB 240 considered 156A MITSUBISHI SN Torque Indicating System Shift Potential 20 -nov -08 11 -mar -09 SB 233 considered 157 MITSUBISHI SN Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09 -dec -09 11 -mar -10 161 MITSUBISHI SR Modifiering av pitotrör FAA, U.S AD 86 -20 -01 JCAB AD TCD - 23 -Oct - 20 -May - 053A 2450A-87 LFV LVD2015 Rev B MAI SR 1984 1986 020/34-005 MITSUBISHI SB 223 MITSUBISHI SR Pitot & Static System MITSUBISHI SB 223 30-apr-85 30-aug-00 064 MITSUBISHI SR Warning Horn 20-jan-86 22-dec-89 065 MITSUBISHI SR Emergency Exit Placard 17 -sep -85 03 -feb -88 067 MITSUBISHI SR Air Filter Replacement for Vacuum Syst. 25 -apr -00 17 -nov -03 072 MITSUBISHI SR Inst. tip tank placard 29 -Oct - 24 -feb -05 075 2004 MITSUBISHI STC Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10 -dec -09 11 -mar -10 See MU -2B AMP Chpt 3 100h/1y inspection SA01913SE

NARCO, Narco NARCO SB ELT10 - ELT ASSY 18 -apr -88 10 -jun -91 N/A 16

NYGE, Saab Aerotech Aircraft Services

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 96(195) NYGE TDM 00-23 Wiring Left Wing ADRIAN 22-dec-00 22-dec-97 NYGE TDM 01 -45 Installation of Trim -In -Motion Alert Syst. JCAB AD TCD -4625A -2001 LFV LVD3122 07 -May - 02 -apr -02 and Automatic A/P Disconnect syst. MITSUBISHI SB 231 Rev B 2001 NYGE TDM 02 -10 Installation of TPE331 -6-252M Engines 25 -mar -02 16 -May - 2002 NYGE TDM 02 -24 Installation Moving MAP 10 -Oct - 30 -Oct - 2002 2002 NYGE TDM 02 -32 Installation EMI film 10 -dec -02 10 -jan -04 NYGE TDM 02 -33 Viktminskning MU -2B 24 -dec -02 27 -jan -04 NYGE TDM 03 -08 8 GNS430/530 & MODE S GTX330 install. 04 -mar -03 20 -Oct - 2008 NYGE TDM 03 -11 C Astor 2 MU -2B 19 -mar -03 C 05 -nov -03 Original compliance was as per TDM rev A.The A/C installation is IAW rev C as not affected by rev B and C.F01323, F01346, F01348 NYGE TDM 03 -15 A U95 with General Control System 24 -apr -03 A 25 -feb -08 NYGE TDM 03-28 F Nav Demo Pod 19-dec-03 F 10-jan-10 Original compliance by Rev D. Not affected by rev F. NYGE TDM 05-16 Viktor Counter Weight Pod 18-nov-05 18-nov-05 NYGE TDM 06 -28 A Removable FR -31 29 -jun -07 A 15 -jun -07 NYGE TDM 06 -41 A Darts (to carry on MU -2B -20/26) 20 -nov -06 A 07 -feb -08 NYGE TDM 06 -42 A Barlast DARTS MU -2B 04 -dec -07 A 07 -feb -08 NYGE TDM 07-30 A Install. of Emergency Axe 28-feb-08 A 28-feb-08 NYGE TDM 08 -03 A Enhanced Surveillance MU -2B 28 -feb -08 A 14 -jan -10 NYGE TDM 08 -28 B ELT 406 MU -2B 29 -sep -08 B 20 -Oct - Original compliance with TDM rev A. Rev B does 2008 not affect previous complaiance. NYGE TDM 09 -23 A Electrical Wiring Feed Through 08 -sep -09 A 10 -jan -10 NYGE TDM 09 -28 A GPS Splitter 12 -Oct - A 15 -jan -10 2009 NYGE TDM 10 -25 A MU -2B Terminating Resistor 08 -apr -10 A 18 -May - C/W 2010 NYGE TDM 11 -32 A MU -2B -20/26 Alteration oil hose A 18 -May -12 NYGE TDM 11-35 A Terminating resistor A 30-Jan-12

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 97(195) NYGE TDM 12-21 A Avinstallation IK 26-Sep- 2012 NYGE TDM 12-28 A Alteration of rivet with bolt A 18-May-12 NYGE TDM 90 -09 Rep. Sprickor undre vingpanel 23 -aug -90 15 -sep -90 NYGE TDM 95 -04 4 Vingstudie 20 -sep -98 4 17 -nov -03 NYGE TDM 96 -06 Rep. sprickor "hinge,front spar flange" 11 -nov -96 14 -nov -96 NYGE TDM 97-01 TAPS 20-feb-97 01-jan-98 NYGE TDM 97 -03 Astor MU -2 25 -feb -97 01 -sep -97 NYGE TDM 98 -08 Torrluft ASTOR 27 -May - 17 -jul -98 1998 NYGE TDM 99 -03 Install. Auto Ignition 03 -mar -99 26 -mar -99 NYGE TVO 1/09 Inspektion av Stringers & struktur vinge 25 -feb -09 01 -apr -09 Inspected with remarks NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 24-jun-93 NYGE TVO 1/96 Slitage Flap Guide Rail 12 -apr -96 26 -nov -99 NYGE TVO 1/97 3 De -Icertank MU -2B, korrosionskontroll 12 -feb -97 04 -sep -97 NYGE TVO 2/00 Märkning av infästning domkraft Mu2 01 -dec -00 08 -May - 2001 NYGE TVO 2/07 A Prevent FR31 radio to xmit when RM2 06 -feb -07 A 28 -feb -07 off NYGE TVO 2/91 A/C Elecrical System 10 -jan -91 10 -jun -91 NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24 -feb -05 3 14 -jan -10 NYGE TVO 4/11 A Static inverter control 15 -Dec -11 NYGE TVO 4/86 2 Wing Pod Inspection 06 -apr -92 2 31 -May - 2010 NYGE TVO 4/91 Special Inspection (next E6.) 19 -feb -91 10 -jun -91 NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29 -apr -92 17 -aug -92 NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28 -sep -94 3 14 -jan -10 L/H & R/H NYGE TVO 4/96 Kontroll av Lagerhus i noshjulsstyrning. 25-Oct- 16-dec-96 Utförd tidigare (ref. Ove N.lista) 1996 NYGE TVO 6/88 Allm. instruktion för metallpropeller 13-jun-88 27-sep-10

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 98(195) NYGE TVO 6/92 Elevator Trim Cable, check 07-Oct- 02-feb-93 1992 NYGE TVO 7/93 Starter Drive Splines 01-nov-93 31-aug-94 NYGE TVO 8/04 Kontr. av Spant vid bakre feninfästning 08 -dec -04 14 -jan -10 NYGE TVO 8/92 Wheel Parts 27 -Oct - 08 -mar -93 1992 NYGE TVO 9/88 Emergency Extension System 08 -aug -88 18 -dec -89

PIPER, The New Piper Aircraft Inc. PIPER SB 700 A Nose Wheel Insp/Replacement FAA, U.S AD 97 -07 -03 12 -Oct - 05 -May - N/A 1981 1997

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 99(195)

2.4 GFE Aircraft Mitsubishi MU-2 SE-GHD

2.4.1 Aircraft Specification Type: Serial Registration: Airframe Total Date Number: total Hours: Landing Reference: Cycles: MU-2B-20 293 SE-GHD 11316 6411 2012-11-23

2.4.2 Engines Type: Honeywell TPE331 -6-252M Serial Total Hours Total Hours remaining to Number: Since New: Cycles Overhaul/HIS/GBl: Since New: Left Engine P20038 9616 10264 4228/628/2428 Right Engine P20052 11551 11102 3444/1642/1644

2.4.3 Propeller Type Number: Serial Number: Overhaul Due Date: Left Propeller HC-B3TN-5E BVA 6817 At overhaul 2012-11-23 Right Propeller HC-B3TN-5E BVA 7713 At overhaul 2012-11-23

2.4.4 Avionics System: Type / Part Number: Note: Autopilot & Flight Director Century IV COM/NAV/GPS 1 Garmin GNS 530 COM/NAV/GPS 2 Garmin GNS 430 Audiopanel Bendix/King KMA-24H-70 MKR Bendix/King KR-21 DME Bendix/King KDM -706 ADF Bendix/King KDF -806 XPDR 1 Garmin GTX 330D Mode S EHS XPDR 2 Garmin GTX 330 *) Mode S EHS RDR ALT Bendix/King KRA-10A ELT Kanad ELT 406-AF-H Airspeed Indicator LH / RH Aerosonic 065A-986402-003 / 20040-161 Altimeter LH United Instr. Inc. 5934 PAD -1 Altimeter incl. encoder RH ARC 42540 -3228 Altitude Reporter Narco AR 850 Altitude Alerter Aero Mechanism AM 275C Vertical Speed Indicator LH Aerosonic RC-60-MS-10-3

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 100(195) Attitude Gyro & Flight Director Ind. Century 52C77 LH Attitude Gyro Ind. RH AIM 504-0006-914 Turn & Bank Ind. LH R.C Allen A5930-02 Horizontal Situation Indicator LH Bendix/King KPI-553A DG -Gyro Sperry C -14A Directional Gyro RMI Ind. LH AIM 254 -1D CDI Indicator Garmin GI -106A *) XPDR 2 without diversity configuration

2.4.5 Mission System System : Description: Fixed general installations VHF/UHF COM 1 & 2 FR31 GPS MAP JET SI-3003B Inverter 115/200VAC 400Hz 3 phase Laser Prism Wing Pylon NATO 14” Alcon Ejector Unit LH and RH Wing Pylon EW system ADRIAN Pod mounted system RH Wing Pylon Target Towing MBV7S Inboard winch AS200 MDI (Miss Distance Indicator)

2.4.6 Mission Cable Harness to Hard Points Used for Mission LH NATO Hard point: RH NATO Hard point: Note: System: Adrian C & S General Signal Harness General Signal Harness AWG22 shielded x 44 AWG22 shielded x 50 AC Power AWG 16 x 4 115/200VAC 400 Hz 3- twisted Phase 3 x 10 A AWG 16 x 2 AWG 20 x 2 Adrian C & S DC Power 28 VDC 200 AWG 2 x 2 A Prepared installation Ethernet LAN Cable

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 101(195)

2.4.7 Antenna Layout

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 102(195)

2.4.8 Inspection due times and dates Status date November 23 rd 2012.

Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date Aircraft SE-GHD Vingstudie MU-2 AMP 2009-03-27 11158 12158,8 100 Hour Inspection AMP 2010-08-19 11260 11360 2011-08-19 200 Hour Inspection AMP 2009-12-16 11158 11358,8 2010-12-16 600 Hour Inspection AMP 2009-12-16 11158 11758,8 2012-12-15 1000 Hour Inspection AMP 2009-12-17 11158 12158,8 1200 Hour Inspection AMP 2005-05-02 10773 11973 1800 Hour Inspection AMP 2005-05-02 10773 12573 2000 Hour Inspection AMP 2004-10-14 9500 11500 1 Year Inspection AMP 2009-12-16 11158 2010-12-16 2 Year Inspection AMP 2009-12-16 11158 2011-12-16 10 Year Inspection AMP 2004-10-14 9500 2014-10-12 Engine S/N P-20038 Remaining Engine Assembly (Overhaul) AMP 15544,9 4228,8 Engine Hot Section Inspection AMP 11944,9 628,8 Engine Gearbox Inspection AMP 13744,9 2428,8 Engine S/N P-20052 Engine Assembly (Overhaul) AMP 14760,6 3444,5 Engine Hot Section Inspection AMP 12958,8 1642,7 Engine Gearbox Inspection AMP 12960,6 1644,5

Propeller L/H O/H (not installed) AMP Propeller R/H O/H (not installed) AMP

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type

2012-12-06

Document number Page 103(195)

2.4.9 Implemented Changes Status date November 23 rd 2012.

SB/AD etc Rev Subject Document reference Eff. date Rev Complianc Stat Remarks Reference e us

CENTURY, Century Flight Systems Inc. CENTURY SB CSB - Check for frayed Bridle Cable 21 -feb -05 20 -aug -10 2005-01

EASA, European Aviation Safety Agency EASA AD 2009 - Portable Fire Extinguishers -Ident/Repl 25 -nov -09 07 -May - N/A N/A by current P/N installed 0251-E 2010 EASA AD 2009 - Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009 -0278 FFE ASB26 -115 Rev C 15 -dec -09 07 -May - N/A N/A by current P/N installed 0262 2010 EASA AD 2009 - Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009 -0262 22 -dec -09 07 -May - N/A N/A by current P/N installed 0278 2010 EASA AD 2010 - R1 Mode S Transponder - 11 -jan -10 R1 10 -mar -10 N/A due to model 0003 Check/Modification EASA SIB 2008 - Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN 17 -dec -08 21 -sep -10 N/A by SSB 0845 incorporated 58R1 SSB0845 Rev IR EASA SIB 2009 -14 Upgrade to main unit/GPS software 24 -jun -09 28 -sep -09 N/A due to model

FAA, U.S, Federal Aviation Administration FAA, U.S AD 2000 - AFM De -icing 25 -jan -00 26 -apr -00 N/A Due to paragraph b. 02-25 FAA, U.S AD 2000 - 1 Flight in Icing Condition FINNISH AD M 2435/97 FINNISH AD M 07 -jul -00 1 14 -jun -02 09-15 2786/00 MAI SB 086/74-002 Rev A MAI SB 093/22-009 MAI SB 096/30-004 MITSUBISHI SB 226 Rev E MITSUBISHI SB 231 Rev B MITSUBISHI SB 232 Rev A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 104(195) FAA, U.S AD 2003- Windshield check FINNISH AD M 3076 LFV LVD2678 MAI SB 01-Oct- 20-aug-10 17-04 087/56-001 Rev B MITSUBISHI SB 224 Rev 2003 C FAA, U.S AD 2003- 1 Forecast Icing Conditions FINNISH AD T5007/03 JCAB AD TCD- 16-apr-04 1 09-jun-04 Inserted in AFM Limitation Section 22-07 4753A-2004 MAI SN 071/00-006 Rev D MITSUBISHI SN 117 Rev D FAA, U.S AD 2005 - Prop. mounting bolt insp. HARTZELL SB 61 -279 ALERT Rev 4 29 -jul -05 14 -sep -05 14-12 FAA, U.S AD 2005 - Prop de -icer "FASTprop" 14 -Oct - 12 -Oct - N/A Due to boots p/n 18-20 2005 2005 FAA, U.S AD 2006- Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB 11-aug-06 19-jun-02 c/o in conjunction with vingstudie 13-15 241 Rev A FAA, U.S AD 2006- Safety evaluation (feathering linkage) MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06 24-aug-06 se Mitsubishi SB 229 15-07 FAA, U.S AD 2006- Detect & correct torque transducers MAI SB 095/77-002 MITSUBISHI SB 233 22-sep-06 21-sep-06 PCW see MSB 233A 17-01 Rev B FAA, U.S AD 2006- Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 13-sep-10 17-05 FAA, U.S AD 2007- Reduce max deflect elev nose-down MITSUBISHI SB 216 MITSUBISHI SB 228 25-sep-07 11-sep-07 Previously carried out i.a.w. mentioned SB's. 17-09 trim FAA, U.S AD 71-14- Fuel Tank Fungus Coating Peeling 01-May-1972 01-jan-96 N/A N/A by s/n 01 FAA, U.S AD 74-11- Windshield Outer Panes LFV LVA829 Rev A MITSUBISHI SB 163 Rev 30-jan-78 01-apr-76 01 B FAA, U.S AD 75-16- Main Wing Flap JCAB AD TCD-1094A-76 LFV LVA1011 Rev 05-aug-75 06-May- Revision C PCW by Swedair. 13 A MITSUBISHI SB 167 Rev D 1977 FAA, U.S AD 75-16- Propeller Pitch Control Lever JCAB AD TCD-1188-75 LFV LVA1012 12-aug-75 24-feb-75 20 MITSUBISHI SB 168 Rev A FAA, U.S AD 78-03- Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A 23-feb-78 30-dec-77 05 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A FAA, U.S AD 81-06- 1 Engine Aft Nacelles 01-apr-81 1 06-May- Previously complied with 01 1997 FAA, U.S AD 81-25- 1 Engine's Electrical wiring SB 036/71- 21-jan-82 1 02-dec-10 N/A N/A by model 04 003A, SB 043/71-005 FAA, U.S AD 82-08- Electrical Wiring Inspection 15-apr-82 15-feb-82 02 FAA, U.S AD 83-08- 2 To preclude prop. attach bolt failures FINNISH AD M 1168/83 Rev 1 FINNISH AD 28-apr-82 2 20-May- Ref. MU2B MM chap 13.4 when using bolts P/N B- 01 T5114/05 HARTZELL SI 140A Rev 9 2005 3339 only

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 105(195) FAA US AD 83-09- Stobe light assemblies 16-Mar-12 02 FAA, U.S AD 84-12- Torque of Air Tube Coupling Nuts SB MAI SB 047/30-001 Rev A MITSUBISHI SB 28-jun-84 04-jun-84 04 047/30-001, SB 196A 196 Rev A FAA, U.S AD 84-25- Elevator TrimTab Bracket Insp/Repl. MAI SB 031/27-005 Rev 1 MITSUBISHI SB 18-dec-84 11-mar-86 02 SB 031/27 -005 R1, SB 176E 176 Rev E FAA, U.S AD 86-15- NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2 13-aug-86 15-jul-04 Found SB 181 part 2 PCW. 03 Rev B FAA, U.S AD 86 -20 - To assure anti -ice capability of pitot LFV LVD2015 Rev B, MAI SR 020/34 -005, 06 -Oct - 19 -May - 01 SB 020/34-005, SB 053A MITSUBISHI SR 053A 1986 2000 FAA, U.S AD 86 -26 - To prevent engine flameout in an GARRETT SB 74 -0003 Rev 6 MAI SR 31 -dec -87 09 -mar -09 see applicable engine for c/o 02 iceing SB 74-0003, SR 040/74-001 040/74-001 MITSUBISHI SB 226 Rev E MITSUBISHI SR 066 FAA, U.S AD 87-04- Addit. Seal and Flap Flexible Shaft MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 08-jul-85 03 Insp SB 051/27-007, SB 198 FAA, U.S AD 87-12- Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 04-May- 02 1990 FAA, U.S AD 88-13- Bendix Autopilot Disengagement SB LFV LVD2190 MAI SB 066/22-006 Rev A 11-jul-98 06-feb-89 N/A N/A due to Autopilot model 01 066/22-006 MITSUBISHI SB 206 FAA, U.S AD 88-21- 1 To minimize confusion in LFV LVD2206 MAI SB 066/22-006 Rev A 28-jan-89 1 25-Jan-12 01 autopilot/manua SB 066/22-006 FAA, U.S AD 88-23- To prevent flap control failure SB LFV LVD2202 MAI SB 067/27-008 Rev A 04-dec-88 23-mar-95 01 067/27-008, SB 189B FAA, U.S AD 93 -07 - ELECTRIC TRIM SYSTEM SB 079/27 - LFV LVD2477 MAI SB 079/27 -010 01 -jun -93 27 -mar -09 N/A by s/n 11 010 FAA, U.S AD 94 -04 - Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11 -apr -94 11 -mar -93 16 FAA, U.S AD 94 -11 - Change of Flight Idle Blade Angel SB LFV LVD2551 MAI SB 016/71 -001 10 -jun -94 27 -mar -09 N/A by s/n 04 016/61 -001 FAA, U.S AD 96 -25 - Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD - 27 -dec -96 01 -jan -97 02 4552 -96 LFV LVD2749 FAA, U.S AD 97 -04 - Vent Check Valve Assy LFV LVD2769 16 -apr -97 05 -May - N/A N/A due to s/n. 13 1997 FAA, U.S AD 97 -20 - Icing related incidents/accidents 17 -Oct - 02 -dec -98 14 CNL 1997 FAA, U.S AD 97 -25 - To prevent loss of airplane FINNISH AD M 2524/98 21 -jan -98 03 -dec -10 N/A AD superseeded by AD 2010 -10 -17 02 ctrl/overspe FAA, U.S AD 98 -20 - Forward fitting bolt of wingtip tank SB LFV LVD2688, MITSUBISHI SB 225 19 -Oct - 28 -jan -97 39 MU-2 225, 089/57-002A 1998

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 106(195)

FINNISH, Finnish Civil Aviation Adm. FINNISH AD M Kontroll av rören till strobe -kablarna MITSUBISHI SB 174 PART 1 Rev C 07 -jul -83 20 -aug -10 1177/83 FINNISH AD M Justering av br,nslefl"de MHI SB JCAB AD TCD -4890 -98 MAI SB 097/73 -001 12 -nov -99 02 -sep -10 2609/98 097/73-001, TCD-4890-98 FINNISH AD M Kontroll av vindrutor och fönster FAA, U.S AD 2003 -17 -04 MAI SB 087/56 - 21 -aug -03 20 -aug -10 3076 001 Rev B MITSUBISHI SB 224 Rev C

GARMIN, Garmin GARMIN SSB 0844 IR Software Version 5.04 EASA SIB2008 -58R1 14 -nov -08 A 24 -May - 2010 GARMIN SSB 0845 IR Software Version 6.04 EASA SIB2008 -58R 14 -nov -08 0 24 -May - 2010

GARRETT, AlliedSignal Aerospace GARRETT SB 74- 6 Replace Ignition Unit AD 74-0003 FAA, U.S AD 86-26-02 25-mar-94 6 09-mar-09 see applicable engine for c/o 0003

HARTZELL, Hartzell Propeller Inc. HARTZELL SB 61 - Propeller mounting bolt inspection MITSUBISHI SL 053/72 -003, MITSUBISHI 08 -feb -02 26 -mar -02 R/H 256 SL 080 HARTZELL SB 61 - 4 Prop. mounting bolt insp. FAA, U.S AD 2005 -14 -12 , MITSUBISHI SL 04 -Oct - 14 -nov -05 Propellerbolts previously checked u/a 279 ALERT 085 2005 HARTZELL SB A61 - 3 Counterweight Slug Bolt Inspection EASA SIB2008 -88 , MITSUBISHI SL 088 Rev 15 -jul -09 3 20 -sep -10 N/A by SSB 0844 313 A HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2 , LFV LVA1424 30-mar-05 9 13-mar-08 see previously revision Rev A

JCAB, Japan Civil Aviation Bureau JCAB AD TCD - Rivet holes elevator hinge fitting 06 -feb -68 26 -mar -09 N/A by s/n

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 107(195) 0518-68 JCAB AD TCD - AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07 -feb -70 11 -mar -86 0642-70 JCAB AD TCD - Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07 -feb -70 15 -jul -04 N/A N/A by s/n. 0643-70 JCAB AD TCD - Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25 -mar -70 26 -mar -09 N/A by model 0652-70 JCAB AD TCD - Engine Nacelle Tail Area -Modification 25 -mar -70 26 -mar -09 N/A by model 0653-70 of JCAB AD TCD - Replacement of bearing in LFV LVA457 MITSUBISHI SB 123 01 -May - 26 -mar -09 N/A by s/n 0660-70 nosegearstrut 1970 JCAB AD TCD - Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 Rev 25 -mar -72 14 -jul -04 N/A N/A by s/n. 0730-1-72 B JCAB AD TCD- Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10-dec-86 26-mar-09 N/A by s/n 0730-2-86 JCAB AD TCD- Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04-sep-72 10-sep-72 N/A N/A due to s/n. 0859-72 JCAB AD TCD- NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09-Oct- 31-dec-72 N/A N/A due to s/n. 0866-72 1972 JCAB AD TCD- Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 Rev 12-nov-74 24-Oct- N/A N/A due to s/n. 0947A-74 A 1986 JCAB AD TCD- Inspection of Windshields MITSUBISHI SB 163 Rev B 22-dec-78 26-mar-09 0948A-1-78 JCAB AD TCD- Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 Rev 07-Oct- 01-apr-76 0948A-74 B 1974 JCAB AD TCD- Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 Rev 06-Oct- 11-mar-86 1001A-76 E 1976 JCAB AD TCD- Replacement of Elevator Trim Tab FINNISH AD M 1080/82 LFV LVD1971 12-dec-84 11-mar-86 1001B-2-84 Bracket MITSUBISHI SB 176 Rev E JCAB AD TCD- Insp. of wingflap controlsystem FAA, U.S AD 75-16-13 LFV LVA1011 Rev A 06-sep-76 06-May- Revision C PCW by Swedair. 1094A-76 MITSUBISHI SB 167 Rev D 1977 JCAB AD TCD- Insp. of propeller controllever inst. FAA, U.S AD 75-16-20 LFV LVA1012 06-May- 24-feb-75 1188-75 MITSUBISHI SB 168 Rev A 1975 JCAB AD TCD- Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev A 20-sep-75 15-jul-04 Found SB 171 and SB 180 PCW. 1202-75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A JCAB AD TCD- Insp/mod of NLG shimmydamper LFV LVA1013 MITSUBISHI SB 169 Rev B 16-jun-75 25-jun-75 1209-75 locking

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 108(195) JCAB AD TCD- Insp./repl. of MLG fwd door LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 19-feb-86 N/A N/A due to model. 1235-75 emerg.cables JCAB AD TCD- Supp.,MLG Forward D. Actuating MITSUBISHI SB 172 14-nov-75 26-mar-09 N/A by model 1272-75 Mech.-I&M JCAB AD TCD- Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76 24-nov-09 PCW Ref. SB 173 1284 -1-76 JCAB AD TCD- Fire hazard in rear baggage 01-jul-76 26-mar-09 N/A by s/n 1328-76 compartment JCAB AD TCD - Barrel Nut, Inner/Outer Wing Conn. - MITSUBISHI SB 175 16 -aug -76 01 -sep -09 N/A by s/n 1353-76 Repl. JCAB AD TCD - Inspect strobelight conduit in Tiptank LFV LVA1196 18 -Oct - 28 -aug -86 Part.1 1370-76 1976 JCAB AD TCD - Inspect strobelight conduit in Tiptank MITSUBISHI SB 174 PART 1 Rev C 05 -nov -81 20 -aug -10 1370A-81 supersed TCD-1370-76 JCAB AD TCD - Insp. rear eng. cowling reg. LFV LVA1197 Rev A MITSUBISHI SB 177 06 -feb -02 06 -May - Previously complied with 1379-1-80 heatdamage Rev B 1977 JCAB AD TCD - Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12 -dec -77 24 -mar -09 ref. SB 180 1520A -77 JCAB AD TCD - Fatigue failure of the NLG strut assy. LFV LVA1546 MITSUBISHI SB 181 PART 12 -jul -85 15 -jul -04 PCW Found SB 181 part 2 PCW. 1768 -1-85 JCAB AD TCD - Modification of bagagecompartment LFV LVA1583 MITSUBISHI SB 182 05 -feb -02 11 -feb -80 N/A N/A due to s/n. 1817 -79 JCAB AD TCD - Insp. firewarning & emerg.power LFV LVA1740 MITSUBISHI SB 187 Rev B 05 -feb -02 27 -May - N/A N/A due to model. 2048-81 circuit 1985 JCAB AD TCD - Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05 -feb -02 24 -nov -81 2070-81 JCAB AD TCD - Insp./replace engine electrical LFV LVA1788 MITSUBISHI SB 191 06 -feb -02 15 -feb -82 2113-82 harness JCAB AD TCD - Flap system torquetubes supersed 01 -feb -89 24 -mar -09 PCW 2252-2-88 TCD-2252-1-87 JCAB AD TCD - Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04 -feb -83 23 -mar -95 2252-83 JCAB AD TCD - NLG. bracket attaching to drag strut 13 -aug -83 24 -mar -09 N/A by model 2263-83 JCAB AD TCD - Engine inlet anti -ice tubing. MITSUBISHI SB 196 Rev A 05 -jun -84 10 -mar -09 PCW 2342-1-84 Torq./lock JCAB AD TCD - Engine inlet anti -ice tubing. LFV LVA1942 MITSUBISHI SB 196 Rev A 06 -feb -02 04 -jun -84 2342-84 Torq./lock JCAB AD TCD - Pitot Tube Wiring LFV LVD2015 Rev B MITSUBISHI SR 053A 16 -jun -87 15 -jul -04 SB PCW. 2450A-87

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 109(195) JCAB AD TCD- Add. seal/Tq. insp of flap flex. shaft 01-May- 09-mar-09 PCW see TCD-2451-85 2451-1-87 1987 JCAB AD TCD- Add. seal/Tq. insp of flap flex. shaft LFV LVD2037 MITSUBISHI SB 198 30-sep-85 08-jul-85 2451-85 Superseeded by TCD-2451-1-87 JCAB AD TCD- Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01-jul-88 06-feb-89 2545 -1-88 JCAB AD TCD- Auto-ignition System FINNISH AD M 2435/97 LFV LVD2761 01-feb-97 22-nov-01 2679A-97 MITSUBISHI SB 226 Rev E JCAB AD TCD - Insp./mod. of rudder trimtab LFV LVD2338 MITSUBISHI SB 211 28 -mar -91 14 -jul -04 N/A N/A by s/n. 3378-90 leadingedge JCAB AD TCD - Anti ice/De -ice system FINNISH AD M 2364/96 LFV LVD2347 Rev 25 -May - 20 -aug -10 3393A-96 1 MITSUBISHI SB 212 Rev A 1996 JCAB AD TCD - Unintentional engagement of A/P...... 17 -jun -91 24 -mar -09 N/A by model 3464-91 JCAB AD TCD - Mod.of Autopilote pitchtrimsystem FINNISH AD M 2581/98 LFV LVD2450 LFV 17 -aug -98 24 -nov -98 3740A-98 MSB 216, 228 LVD 2898 LVD2898 MITSUBISHI SB 216 MITSUBISHI SB 228 JCAB AD TCD- Tiptank inst FINNISH AD M 2110/93 LFV LVD2512 10-sep-93 13-jun-94 3901-93 MITSUBISHI SB 221 JCAB AD TCD- Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592 28-nov-94 23-mar-95 3942-1-94 MITSUBISHI SB 219 Rev A JCAB AD TCD- Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01-feb-94 23-mar-95 3942-94 JCAB AD TCD - Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688 01 -apr -96 28 -jan -97 4310-96 MITSUBISHI SB 225 JCAB AD TCD - Windshield/window insp. FINNISH AD M 2331/96 LFV LVD2678 01 -nov -95 20 -aug -10 4311-95 MITSUBISHI SB 224 Rev C JCAB AD TCD - Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689 01 -apr -96 30 -jul -96 4379 -96 MITSUBISHI SB 229 JCAB AD TCD - Icing Limitation FAA, U.S AD 96 -25 -02 LFV LVD2749 27 -dec -96 01 -jan -97 4552 -96 JCAB AD TCD - Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI SB 14 -jul -97 04 -jun -02 4625 -97 093/22 -009 JCAB AD TCD - Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B 16 -mar -01 14 -jun -02 PCW Ref AMOC LFV Appr M15/01, TDM 01 -45 4625A -2001 NYGE TDM01 -45 JCAB AD TCD - De -ice system Modification FINNISH AD M 2461/97 LFV LVD2800 01 -May - 14 -jul -04 4626 -97 MITSUBISHI SB 232 Rev A 1997 JCAB AD TCD - Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819 01 -jun -97 25 -mar -99 4684-97 MITSUBISHI SB 230

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 110(195) JCAB AD TCD- Ändring av flyghandbok LVD FINNISH AD M 2518/98 LFV LVD2922 18-feb-98 02-dec-98 FAA AD utförd. 4753-98 2922,FAA AD 97-20-14, MHI SN 117A MITSUBISHI SN 117 Rev D JCAB AD TCD- Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 09-jun-04 Inserted in AFM Limitation Section 4753A-2004 JCAB AD TCD- Inspection of landing gear power FINNISH AD M 2574/98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model 4838 -98 train MITSUBISHI SB 235 JCAB AD TCD- Inappropriate calib. of eng. trq-meter MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A. 4889-2-2007 JCAB AD TCD - Insp. of Engine Torque Indication FINNISH AD M 2608/98 LFV LVD2924 05 -nov -98 14 -jul -04 PCW 4889-98 System LFV 2924, MU SB 233 MITSUBISHI SB 233 Rev B JCAB AD TCD - Check of flight idle FF LVD 2925, MU FINNISH AD M 2609/98 LFV LVD2925 04 -nov -98 13 -sep -10 4890-98 SB 234 MITSUBISHI SB 234 JCAB AD TCD - Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17 -May - 24 -mar -09 N/A by model 5030-99 1999 JCAB AD TCD - AFM revision LFV LVD3112 27 -nov -00 12 -feb -02 5432-2000 JCAB AD TCD - To prevent loss of airplane control LFV LVD3123 16 -mar -01 12 -feb -02 5547 -2001 JCAB AD TCD - Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12 -sep -01 27 -sep -01 5747 -2001 JCAB AD TCD - Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27 -dec -01 16 -jan -02 5864 -2001 JCAB AD TCD - Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17 -mar -03 12 -jun -03 6127-2003 JCAB AD TCD - Inspection of Wing Attachment MITSUBISHI SB 241 Rev A 27 -dec -06 17 -jan -07 c/o in conjunction with wingstudie 7030-2006 Hardware

LFV, Luftfartsverket LFV LVA 1011 A Kontroll av vingklaffarnas FAA, U.S AD 75-16-13 JCAB AD TCD- 05-feb-02 A 06-May- Revision C PCW by Swedair. manöversystem 1094A-76 MITSUBISHI SB 167 Rev D 1977 LFV LVA 1012 Kontroll av propellerreglagets FAA, U.S AD 75-16-20 JCAB AD TCD-1188- 05-feb-02 24-feb-75 montering 75 MITSUBISHI SB 168 Rev A LFV LVA 1013 Kontr. och mod. av låsning på nosställ JCAB AD TCD-1209-75 MITSUBISHI SB 169 05-feb-02 25-jun-75 Rev B LFV LVA 1014 A Kontr. & byte av motorinkl. FAA, U.S AD 78-03-05 JCAB AD TCD-1202- 05-feb-02 A 30-dec-77 låsanordning 75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 111(195) LFV LVA 1083 Insp. & utbyte av lina för nödöppning JCAB AD TCD-1235-75 MITSUBISHI SB 170 05-feb-02 19-feb-86 N/A N/A due to s/n. Rev A LFV LVA 1196 Isolering av strobe light från bränsle JCAB AD TCD-1370-76 MITSUBISHI SB 174 06-feb-02 20-aug-10 PART 1 Rev C LFV LVA 1197 A Förhindr. av värmeskador på JCAB AD TCD-1379-1-80 MITSUBISHI SB 06-feb-02 A 06-May- Previously complied with bak.motorpl. 177 Rev B 1977 LFV LVA 1238 Kontr. & byte av infästningsdet. 06-feb-02 21-apr-09 N/A by s/n trimrod LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86 -15 -03 JCAB AD TCD -1768 - 06 -feb -02 29 -nov -84 1-85 MITSUBISHI SB 181 PART 2 Rev B LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD -1817 -79 MITSUBISHI SB 182 05 -feb -02 11 -feb -80 N/A N/A due to s/n. LFV LVA 1740 Kontr.av brandvarnings -och JCAB AD TCD -2048 -81 MITSUBISHI SB 187 05 -feb -02 31 -aug -09 N/A by s/n n"dstr"mskret Rev B LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB 188 05-feb-02 24-nov-81 LFV LVA 1788 Kontroll/Utbyte av elledningar på JCAB AD TCD -2113 -82 MITSUBISHI SB 191 06 -feb -02 15 -feb -82 motor LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör JCAB AD TCD -2252 -83 MITSUBISHI SB 189 06 -feb -02 23 -mar -95 Rev C LFV LVA 1942 Momentdragning/låsn.av koppl.i JCAB AD TCD -2342 -84 MITSUBISHI SB 196 06 -feb -02 04 -jun -84 varmlufts Rev A LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD -0643 -70 MITSUBISHI SB 114 05 -feb -02 11 -mar -86 N/A N/A by s/n LFV LVA 439 Rev. av flyghandbok betr. JCAB AD TCD -0642 -70 MITSUBISHI SB 112 05 -feb -02 11 -mar -86 bränslespec. Rev C LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD -0652 -70 MITSUBISHI SB 119 05 -feb -02 26 -mar -09 N/A by model LFV LVA 457 Utbyte av lager i nosst,llets st"td,mp. JCAB AD TCD -0660 -70 MITSUBISHI SB 123 05 -feb -02 26 -mar -09 N/A by s/n LFV LVA 543 B Insp. och målning av integraltankar JCAB AD TCD-0730-1-72 05-feb-02 B 14-jul-04 N/A N/A by s/n. LFV LVA 645 Modifiering av el -system JCAB AD TCD -0859 -72 MITSUBISHI SB 156 05 -feb -02 08 -dec -09 N/A by A/C serial number LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD -0866 -72 05 -feb -02 31 -aug -09 N/A by s/n LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD -0947A -74 MITSUBISHI SB 05 -feb -02 A 24 -Oct - N/A N/A due to s/n. 162 Rev A 1986 LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74 -11 -01 FAA, U.S AD 75 -03 - 05 -feb -02 A 01 -apr -76 06 JCAB AD TCD-0948A-74 MITSUBISHI SB 163 Rev B LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar JCAB AD TCD -1001A -76 05 -feb -02 A 11 -mar -86

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 112(195) LFV LVD 1238 Kontr./byte infästn.det. 15-apr-77 31-aug-09 N/A by s/n höjdtrimroder LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD-1001B-2-84 MITSUBISHI SB 18-jan-85 29-mar-85 176 Rev E LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34-005 FAA, U.S AD 86-20-01 JCAB AD TCD- 24-May- B 06-nov-86 Rev A, MHI SR 53 2450A-87 MAI SR 020/34-005 MITSUBISHI 1985 SR 053A LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85 08-jul-85 LFV LVD 2069 Altimeter 25 -mar -86 23 -May - N/A N/A by p/n & s/n 1986 LFV LVD 2113 Modif. & revision Handbook MHI SR 26 -jan -87 25 -mar -87 006B, MAI SR 040/74-001RA LFV LVD 2190 Autopilot Switch MU2 SB 066/22 -006 FAA, U.S AD 88 -13 -01 MAI SB 066/22 -006 19 -aug -88 06 -feb -89 N/A Bendix A/P ej installerad och SB 206 Rev A MITSUBISHI SB 206 LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD -2545 -1-88 MITSUBISHI SB 19 -aug -88 06 -feb -89 201 Rev A LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88 -23 -01 JCAB AD TCD -2252 - 08 -dec -88 23 -mar -95 1-87 MAI SB 067/27-008 Rev A MITSUBISHI SB 189 Rev C LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88 -21 -01 Rev 1 08 -dec -88 12 -feb -02 LFV LVD 2338 Kont./Mod.av sidorodrets JCAB AD TCD -3378 -90 MITSUBISHI SB 211 28 -mar -91 14 -jul -04 N/A N/A by s/n. trimroderframka Mitsubishi MHI SB 211 LFV LVD 2347 1 Control Deice -system Mitsubishi SB JCAB AD TCD -3393A -96 MITSUBISHI SB 29 -May - 1 20 -aug -10 212A 212 Rev A 1996 LFV LVD 2352 Shoulder Harness Inst. FAA AC 43 -13 23 -May - 04 -nov -91 checked OK. CHPT 9 1991 LFV LVD 2450 Elevator Trim Tab Installation MU SB JCAB AD TCD -3740A -98 MITSUBISHI SB 03 -dec -92 11 -mar -93 216 216 LFV LVD 2477 Electric Trim System AD930711, MU FAA, U.S AD 93 -07 -11 MAI SB 079/27 -010 03 -jun -93 27 -mar -09 N/A by s/n SB 079/27-0-010 LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD -3901 -93 MITSUBISHI SB 221 02 -dec -93 13 -jun -94 LFV LVD 2537 Reducering av Höjdrodrets FAA, U.S AD 94 -04 -16 MITSUBISHI SB 216 07 -apr -94 11 -mar -93 trimområde. FAA AD 94-04-16, SB 216 LFV LVD 2538 Byte Låspinne i landställets nödutf. SB JCAB AD TCD-3942-94 MITSUBISHI SB 219 07-apr-94 23-mar-95 219 Rev A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 113(195) LFV LVD 2551 Adj.of Ground Idle FAA AD 94-11-04 FAA, U.S AD 94-11-04 22-jun-94 27-mar-09 N/A by s/n LFV LVD 2592 Insp/Repl. of Lock -pin in L/G gearbox JCAB AD TCD -3942 -1-94 MITSUBISHI SB 09 -feb -95 23 -mar -95 TCD-3942-1-94, MSB 219A 219 Rev A LFV LVD 2678 Kontr. av vindrutor och fönster MHI FAA, U.S AD 2003 -17 -04 JCAB AD TCD - 12 -mar -96 20 -aug -10 SB 224 Rev A 4311-95 MITSUBISHI SB 224 Rev C LFV LVD 2688 Kontr/byte av infästn.bult för tiptank FAA, U.S AD 98 -20 -39 JCAB AD TCD -4310 - 09 -May - 28 -jan -97 MU-2 SB 225 96 MITSUBISHI SB 225 1996 LFV LVD 2689 Kontroll av linkage för prop.flöjning JCAB AD TCD -4379 -96 MITSUBISHI SB 229 09 -May - 30 -jul -96 MU-2 SB 229 1996 LFV LVD 2732 Inspection/ Replacement of Prop FAA, U.S AD 96 -18 -14 HARTZELL SB 61 - 27 -sep -96 04 -Oct - Prop. utbytt mot BVA Hub. FAA AD 96-18-14, Hz SB 136H 261 Rev 1 1999 LFV LVD 2749 Revision av flyghandbok AFM TCD - FAA, U.S AD 96 -25 -02 JCAB AD TCD -4552 - 21 -jan -97 12 -feb -02 4552-96 96 LFV LVD 2761 Installation av autoignition system JCAB AD TCD-2679A-97 MITSUBISHI SB 14-feb-97 29-sep-99 TCD-2679A-97 226 Rev E LFV LVD 2769 Demont.av backventil i FAA, U.S AD 97-04-13 MITSUBISHI SB 130 18-mar-97 05-May- N/A N/A due to s/n. bränslesystemets MU-2 SB 130A Rev A 1997 LFV LVD 2800 Mod. av De-ice Monitoring System JCAB AD TCD-4626-97 MITSUBISHI SB 232 28-aug-97 10-jun-98 Mitsubishi SB 232, TCD-4626-97 Rev A LFV LVD 2819 Mod.av lagerboxar för JCAB AD TCD-4684-97 MITSUBISHI SB 230 18-nov-97 23-jun-98 landställssystem Mitsubishi SB 230 LFV LVD 2853 Periodisk funktionskontroll av 23-mar-98 17-dec-09 nödutgång LFV LVD 2897 Kontroll av landst,llets drivsystem JCAB AD TCD-4838-98 MITSUBISHI SB 235 02-aug-98 24-mar-09 N/A by model TCD-4838-98, SB 235 LFV LVD 2898 Mod. av autopilotens höjdtrimsystem JCAB AD TCD-3740A-98 MITSUBISHI SB 27-aug-98 24-nov-98 TCD-3740A-98, SB 216, 228 216 MITSUBISHI SB 228 LFV LVD 2922 Änd.av Flyghandbok-Extra krav på JCAB AD TCD-4753-98 MITSUBISHI SN 117 12-nov-98 02-dec-98 FAA AD utförd. typutbi TCD-4753-98, MHI SN 117A Rev D LFV LVD 2924 Kontr/Just av motorernas Torque JCAB AD TCD-4889-98 MITSUBISHI SB 233 01-dec-98 12-apr-99 indikeri MHI SB 233, TCD-4889-98 Rev B LFV LVD 2925 Kontr/just av mot bränsleflöde Flight JCAB AD TCD-4890-98 MITSUBISHI SB 234 01-dec-98 02-sep-10 Id MHI SB 234 LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD-5030-99 MITSUBISHI SB 209 18-jun-99 24-mar-09 N/A by model Rev B LFV LVD 3112 Revision av flyghandbok JCAB AD TCD-5432-2000 30-jan-01 12-feb-02 LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD -4625A -2001 MAI SB 093/22 - 02 -apr -01 14 -jun -02 Ref AMOC LFV Appr M15/01, TDM 01 -45 009 MITSUBISHI SB 231 Rev B NYGE

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 114(195) TDM01-45 LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD -5547 -2001 02 -apr -01 12 -feb -02 LFV LVD 3166 Sprickkontroll av infästning till ving - JCAB AD TCD -5747 -2001 MITSUBISHI SB 20 -sep -01 27 -sep -01 spetstank 236 LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD -5864 -2001 MAI SB 099/27 - 09 -jan -02 16 -jan -02 012 MITSUBISHI SB 237 LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD -6127 -2003 MITSUBISHI SB 21 -mar -03 12 -jun -03 239

MAI, Mitsubishi Aircraft International MAI SB 047/30 - A Torque of Bleed Air Tube Coupling FAA, U.S AD 84 -12 -04 MITSUBISHI SB 196 19 -jul -84 A 04 -jun -84 001 Nuts AD 84-12-04,SB 196A Rev A MAI SB 051/27 - Add.Seal and Flap Flexible Shaft FAA, U.S AD 87 -04 -03 01 -feb -85 08 -jul -85 007 Torque AD 87-04-03, SB 198 MAI SB 067/27 - A Insp/Repl. of Flap Control System FAA, U.S AD 88 -23 -01 LFV LVD2202 29 -mar -95 A 23 -mar -95 008 Torque AD 88-23-01, SB 189B MAI SB 069/24 - Split Radio Bus Inspection and MAI SB 066/22 -006 Rev A 17 -nov -88 06 -feb -89 N/A N/A due to Aircraft s/n 006 Rework MAI SB 086/74 - A Auto -Ignition System Installation FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH AD 05 -Oct - A 22 -nov -01 Action not required due to s/n. 002 M 2435/97 MITSUBISHI SB 226 Rev E 2000 MAI SB 089/57 - A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98 -20 -39 05 -nov -96 A 28 -jan -97 N/A N/A due to s/n. 002 MAI SN 110/00 - Power Lever Position Warning 25 -feb -09 09 -nov -09 SB 240 considered 017A MAI SN 111/77 - Torque Indicating System Shift 20 -nov -08 11 -mar -09 SB 233 considered 004 Potential MAI SR 020/34 - Anti Ice Capability AD 86 -20 -01, SR FAA, U.S AD 86 -20 -01 LFV LVD2015 Rev B 06 -Oct - 19 -May - N/A N/A due to s/n. 005 053A MITSUBISHI SR 053A 1986 2000

MITSUBISHI, Mitsubishi Heavy Industries Ltd MITSUBISHI MSB **RECOVERED RECORD** 19 -feb -86 N/A 24 -004 MITSUBISHI MSR **RECOVERED RECORD** 06 -nov -86 020

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 115(195) MITSUBISHI MSR B **RECOVERED RECORD** 25-mar-87 B 066 MITSUBISHI SB 066 Bendix M4D 18-dec-87 06-feb-89 N/A MITSUBISHI SB M-4() Autop.Engage Switch Guard 11 -apr -91 12 -apr -95 N/A 076/22-008 Install. MITSUBISHI SB 112 C Anti -Ice Additive in Fuel -Usage of JCAB AD TCD -0642 -70 LFV LVA439 09 -Oct - C 11 -mar -86 1971 MITSUBISHI SB 114 Fuel Quantity Indicator Readjustmnet JCAB AD TCD -0643 -70 LFV LVA438 01 -jan -70 15 -jul -04 N/A N/A by s/n. MITSUBISHI SB 119 The Bolt and Bolt Hole Diam. of Nose JCAB AD TCD -0652 -70 LFV LVA456 10 -mar -70 26 -mar -09 N/A by model L.G MITSUBISHI SB 123 Bearing,Oleo Strut,Nose L.G. -Repl. of JCAB AD TCD -0660 -70 LFV LVA457 01 -apr -70 26 -mar -09 N/A by s/n MITSUBISHI SB 124 Scissors Switch,Nose L.G. -Install. of 31 -aug -70 19 -feb -86 N/A MITSUBISHI SB 128 B Tip Tank Air Pressure Modification 28 -jun -94 B 05 -nov -09 N/A by model & s/n MITSUBISHI SB 143 B Top Coating, Wing Integral Main F.T. - JCAB AD TCD -0730 -1-72 JCAB AD TCD - 05 -jan -72 B 14 -jul -04 N/A N/A by s/n. SIo 0730-2-86 MITSUBISHI SB 152 Air Conditioning System- 08-nov-71 13-jun-03 N/A N/A by s/n Improvement of MITSUBISHI SB 162 A Flex. Shafts, Flap Control Sys.-Insp. of JCAB AD TCD-0947A-74 LFV LVA828 Rev A 03-Oct- A 24-Oct- N/A (AD750201) 1974 1986 MITSUBISHI SB 163 B Insp. of Outer Pane, Front Winds. & FAA, U.S AD 74-11-01 JCAB AD TCD- 16-nov-78 01-apr-76 Inst 0948A-1-78 JCAB AD TCD-0948A-74 LFV LVA829 Rev A MITSUBISHI SB 165 A Lubr. Interval,Wheel Bearing,Main & 24 -jul -80 19 -feb -86 N/A Nose MITSUBISHI SB 166 Wing Flap 24 -jul -80 11 -mar -86 N/A MITSUBISHI SB 167 D Flap M.Jack Screw -Insp. of and/or FAA, U.S AD 75 -16 -13 JCAB AD TCD - 24 -jul -80 D 06 -May - Revision C PCW by Swedair. Main G 1094A-76 LFV LVA1011 Rev A 1977 MITSUBISHI SB 168 A Propeller Pitch Control Lever -Insp. of FAA, U.S AD 75 -16 -20 JCAB AD TCD -1188 - 24 -jul -80 A 24 -feb -75 (AD761620) 75 LFV LVA1012 MITSUBISHI SB 169 B Shimmy Damper -Insp. and JCAB AD TCD -1209 -75 LFV LVA1013 24 -jul -80 B 05 -nov -09 PCW Modification of MITSUBISHI SB 170 A MLG Forward Door Em.Op. Cable - JCAB AD TCD -1235 -75 LFV LVA1083 24 -mar -77 A 19 -feb -86 N/A N/A due to s/n Insp. & Re (AD762204) MITSUBISHI SB 171 B Latches,Eng. Nacelle Upper D. -Insp.& FAA, U.S AD 78 -03 -05 JCAB AD TCD -1202 - 17 -nov -77 B 30 -dec -78 Mod (AD780305) 75 LFV LVA1014 Rev A MITSUBISHI SB 173 A Drag Strut, Main L.G. -Modification of JCAB AD TCD -1284 -1-76 24 -jul -80 01 -apr -76

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 116(195) MITSUBISHI SB 174 C Tip Tank Conduit Tube-Insp.of,and FINNISH AD M 1177/83 JCAB AD TCD- 02-Oct- C 20-aug-10 PART 1 Rew.of (AD830902) 1370A-81 LFV LVA1196 1981 MITSUBISHI SB 175 Barrel Nut, Inner/Outer Wing Conn.- JCAB AD TCD-1353-76 26-jun-76 01-sep-09 N/A by s/n Repl. MITSUBISHI SB 176 E Elevator Trim Tab Bracket-Repl. of FAA, U.S AD 84-25-02 FINNISH AD M 26-sep-84 E 11-mar-86 LVD1971, AD 84-25-02, SB 031/27- 1080/82 JCAB AD TCD-1001A-76 JCAB AD 005R1 TCD-1001B-2-84 LFV LVD1971 MITSUBISHI SB 177 B Mod. of Engine Nacelle Tail Area JCAB AD TCD-1379-1-80 LFV LVA1197 Rev 11-sep-80 B 06-May- Previously complied with (AD810601) A 1977 MITSUBISHI SB 179 Rodd Assem., Engine Nacelle Upper 27-May- 10-mar-88 D.-R&M 1977 MITSUBISHI SB 180 A Link, Engine Nacelle Upper D.-Repl. of FAA, U.S AD 78-03-05 JCAB AD TCD-1202- 17-nov-77 A 30-dec-77 (AD780305) 75 JCAB AD TCD-1520A-77 LFV LVA1014 Rev A MITSUBISHI SB 181 B Insp. and Repl. of Nose L.G. Strut FAA, U.S AD 86-15-03 JCAB AD TCD-1768- 08-apr-85 B 29-nov-84 PART 2 Assem (AD801812) 1-85 LFV LVA1546 MITSUBISHI SB 182 Add. of Ceiling Cover, Rear Bagg. JCAB AD TCD-1817-79 LFV LVA1583 16-nov-79 16-nov-79 N/A N/A due to s/n. Comp. MITSUBISHI SB 184 Turnbuckle, Control Cables -Repl. of 04-apr-80 19-feb-86 N/A MITSUBISHI SB 188 Down Lock Mech., Nose L.G. -Insp. of JCAB AD TCD -2070 -81 LFV LVA1753 13 -jul -81 24 -nov -81 MITSUBISHI SB 189 C Flap Control Torque Tube AD 88 -23 - FINNISH AD M 2722/00 JCAB AD TCD - 28 -jun -94 C 23 -mar -95 01, SB 067/27-008 2252-1-87 JCAB AD TCD-2252-83 LFV LVA1873 LFV LVD2202 MITSUBISHI SB 190 A Trav. Nut Repl. of L.G. Mech. Stop 28 -jun -94 23 -jul -82 Assem MITSUBISHI SB 191 Engine El. Wire -Insp. and JCAB AD TCD -2113 -82 LFV LVA1788 21 -dec -81 15 -feb -82 Replacement of (AD820802) MITSUBISHI SB 193 B Landing Gear Warning Horn 15 -jun -94 B 04 -dec -00 Rev A är utförd. Syst.Modif. MITSUBISHI SB 194 Master Cauting Light Visibility -Impr. 23 -aug -82 14 -feb -83 of MITSUBISHI SB 196 A Ret. of coupling nut on the bleed air FAA, U.S AD 84 -12 -04 JCAB AD TCD -2342 - 12 -apr -84 A 04 -jun -84 tu AD 84-12-04, SB 047/30-001 1-84 JCAB AD TCD-2342-84 LFV LVA1942 MAI SB 047/30-001 Rev A MITSUBISHI SB 198 Add. Seal & Torque Insp. of Flap FAA, U.S AD 87 -04 -03 JCAB AD TCD -2451 - 13 -feb -85 08 -jul -85 Flex.Sh LVD2037, AD 87-04-03, SB 85 LFV LVD2037 051/27 -007 MITSUBISHI SB 199 A Engine Lubricating Tubing Insp. & 24 -jun -94 A 06 -nov -09 PCW Protec

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 117(195) MITSUBISHI SB 200 B Insp of Nose Ldg Gear Drag Strut Link 24-jun-94 A 09-aug-88 MITSUBISHI SB 201 A Generator Circuit Wires Insp. and FAA, U.S AD 87 -12 -02 JCAB AD TCD -2545 - 02 -mar -88 A 04 -May - Mod. 1-88 LFV LVD2191 1990 MITSUBISHI SB 204 Speed Placard Change 03 -mar -87 13 -jun -88 MITSUBISHI SB 206 Bendix Autop.Disengagement FAA, U.S AD 88 -13 -01 JCAB AD TCD -2856 - 13 -Oct - 31 -jan -89 N/A N/A due to Autopilot model Method Stand. 1-97 LFV LVD2190 1987 MITSUBISHI SB 207 Rudder T.T. & Elevator T.T. Insp. & 20 -May - 17 -dec -09 Rep. 1988 MITSUBISHI SB 209 B Fuselage inspection JCAB AD TCD -5030 -99 LFV LVD2988 19 -apr -99 B 24 -mar -09 N/A by model MITSUBISHI SB 210 A Engine Ignition Unit Replacement 12 -nov -96 06 -mar -98 MITSUBISHI SB 211 Rudder Trim Tab Modification (LVD JCAB AD TCD -3378 -90 LFV LVD2338 20 -nov -90 14 -jul -04 N/A N/A by s/n. 2338) MITSUBISHI SB 212 A Insp of Anti -ice/Deice Systems (LVD JCAB AD TCD -3393A -96 LFV LVD2347 Rev 25 -apr -96 A 20 -aug -10 2347), 1 MITSUBISHI SB 214 Engine Control Rod Inspection 06 -dec -91 11 -mar -93 MITSUBISHI SB 215 Removel of Prop. Governor Speed 23-Oct- 30-jan-92 N/A N/A due to -1 engine Signal 1991 MITSUBISHI SB 216 Elevator Trim Tab Installation (LVD FAA, U.S AD 2007-17-09 FAA, U.S AD 94- 11-sep-92 11-mar-93 2450 04-16 JCAB AD TCD-3740A-98 LFV LVD2450 MITSUBISHI SB 218 A Propeller Feathering Linkage 17 -jan -94 A 18 -feb -94 Inspection MITSUBISHI SB 219 A Emergency Gear Down G.box Lower JCAB AD TCD -3942 -1-94 JCAB AD TCD - 24 -Oct - A 23 -mar -95 Pin Repl 3942-94 LFV LVD2538 LFV LVD2592 1994 MITSUBISHI SB 221 Tip Tank Conduit Tube Insp. and Rep. JCAB AD TCD -3901 -93 LFV LVD2512 10 -aug -93 13 -jun -94 MITSUBISHI SB 222 Fuselage Waterproof Modification SR 28 -jun -94 30 -sep -98 019 MITSUBISHI SB 223 Pitot/Static System Improvement SR MITSUBISHI SR 053A MITSUBISHI SR 064 28 -jun -94 19 -May - 064 2000 MITSUBISHI SB 224 C Acrylic Windsheild/Window glass FAA, U.S AD 2003 -17 -04 FINNISH AD M 30 -apr -98 C 20 -aug -10 Insp. UHB 3076 JCAB AD TCD-4311-95 LFV LVD2678 MITSUBISHI SB 225 Forward fitting bult of wingtip tank FAA, U.S AD 98 -20 -39 FINNISH AD M 29 -sep -95 28 -jan -97 LVD 2688 2351/96 JCAB AD TCD-4310-96 LFV LVD2688 MITSUBISHI SB 226 E Auto -Ignition System Installation LVD FAA, U.S AD 2000 -09 -15 Rev 1 FAA, U.S 18 -sep -01 E 22 -nov -01 PCW no further action (rev.E) required due to s/n. 2761 (2113), AD TCD-2679A-97 AD 86-26-02 FINNISH AD M 2435/97

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 118(195) FINNISH AD M 2786/00 JCAB AD TCD- 2679A-97 LFV LVD2761 MAI SB 086/74- 002 Rev A MITSUBISHI SB 227 Rudder Torque Tube Modification 20-dec-96 23-jun-98 MITSUBISHI SB 228 Elevator Trim Indicator Modification FAA, U.S AD 2007 -17 -09 FINNISH AD M 13 -jul -98 24 -nov -98 LFV 2898 2581/98 JCAB AD TCD-3740A-98 LFV LVD2898 MITSUBISHI SB 229 Feathering Valve/Linkage Insp. FAA, U.S AD 2006 -15 -07 JCAB AD TCD - 20 -feb -96 23 -jun -98 4379-96 LFV LVD2689 MITSUBISHI SB 230 Mod.of Bearing Box Ldg. Gear Act. JCAB AD TCD -4684 -97 LFV LVD2819 05 -mar -97 23 -jun -98 LVD 2819 MITSUBISHI SB 231 B Inst.of Trim -In -Motion Alert System FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH AD 11 -dec -02 B 03 -mar -03 SL 079 performed earlier. M 2460/97 UPPHÄVD FINNISH AD M 2786/00 JCAB AD TCD-4625A-2001 LFV LVD3122 MAI SB 093/22-009 NYGE TDM01-45 MITSUBISHI SB 232 A De -Ice System Modification LVD FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH AD 06 -jun -02 A 06 -jun -02 N/C due to previuosly complied with SB 232 rev 0. 2800, TCD-4626-97 M 2786/00 JCAB AD TCD-4626-97 LFV LVD2800 MAI SB 096/30 -004 MITSUBISHI SB 233 B Insp.of Engine Torque Indication FAA, U.S AD 2006 -17 -01 FINNISH AD M 08 -mar -07 B 18 -apr -07 Checked, previously carried out System. TCD-4889-98, LFV 2924 2608/98 JCAB AD TCD-4889-2-2007 JCAB AD TCD-4889-98 LFV LVD2924 MITSUBISHI SB 234 Fl.Check of the Flight Idle Fuel Flow FAA, U.S AD 2006 -17 -05 JCAB AD TCD - 07 -Oct - 02 -sep -10 Se TCD-4890-98, LVD 2925 4890-98 1998 MITSUBISHI SB 235 Inspection of landing gear power JCAB AD TCD -4838 -98 LFV LVD2897 04 -aug -98 24 -mar -09 N/A by model train MITSUBISHI SB 236 Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-01 27-sep-01 MITSUBISHI SB 237 Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-01 16-jan-02 MITSUBISHI SB 238 Main Landing Gear Door Safety Pin 05 -dec -02 09 -jan -03 Perf. at each 600 h. insp. MITSUBISHI SB 239 Pneumatic Line Insp. and JCAB AD TCD -6127 -2003 LFV LVD3322 26 -dec -02 12 -jun -03 Modification MITSUBISHI SB 240 Inst.of Trottle Quadrant Placard 26 -feb -03 12 -jun -03 MITSUBISHI SB 241 A Inspection of Wing Attachment FAA, U.S AD 2006 -13 -15 JCAB AD TCD - 21 -nov -06 A 17 -jan -07 c/o in conjunction with wingstudie Hardware 7030-2006 MITSUBISHI SL 060 System 17 -feb -89 04 -nov -91 MITSUBISHI SL 078 Automatic Autopilot Disconnect 28-jan-02 20-aug-10

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 119(195) System MITSUBISHI SL 079 Diode inst.in Flap Position Ind.Curcuit 28 -jan -02 14 -jun -02 MITSUBISHI SL 080 Hartzell Propeller Mounting Bolt Insp. HARTZELL SB 61 -256 05 -apr -02 26 -aug -02 Compliance in according to HC -SB -61 -256. MITSUBISHI SL 084 Pneumatic De -Ice Monitoring System 14 -jun -04 20 -aug -10 MITSUBISHI SL 085 Hartzell prop. mount. bolt insp. HARTZELL SB 61-279 ALERT Rev 4 17-May- 14-sep-05 2005 MITSUBISHI SN B Rudder Torque Tube AD 86-20-01, SB 05-nov-86 B 12-jun-87 053 020/34-005 MITSUBISHI SN D Icing Awareness Training Video FAA, U.S AD 2003-22-07 Rev 1 JCAB AD 14-jun-04 D 09-jun-04 117 TCD-4753-98 MITSUBISHI SN Water Ingress into Vertical Stabilizer 19 -dec -03 09 -jun -04 146 MITSUBISHI SN Reminders for safe operation 18 -nov -05 22 -mar -06 Genomförs enl. AMP MU -2 & DHB 148 MITSUBISHI SN Power Lever Position Warning 25 -feb -09 09 -nov -09 SB 240 considered 156A MITSUBISHI SN Torque Indicating System Shift 20 -nov -08 11 -mar -09 SB 233 considered 157 Potential MITSUBISHI SN Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09 -dec -09 11 -mar -10 Ref STC SA01913SE 161 MITSUBISHI SR Modifiering av pitotrör FAA, U.S AD 86 -20 -01 JCAB AD TCD - 23 -Oct - 14 -nov -86 053A 2450A-87 LFV LVD2015 Rev B MAI SR 1984 020/34-005 MITSUBISHI SB 223 MITSUBISHI SR 064 Pitot & Static System MITSUBISHI SB 223 30-apr-85 19-May- 2000 MITSUBISHI SR 065 Warning Horn 20 -jan -86 13 -jun -88 MITSUBISHI SR 067 Emergency Exit Placard 17 -sep -85 15 -jan -86 MITSUBISHI SR 072 Air Filter Replacement for Vacuum 25 -apr -00 29 -jan -01 Syst. MITSUBISHI SR 075 Inst. tip tank placard 29 -Oct - 02 -May - 2004 2005 MITSUBISHI STC Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10 -dec -09 11 -mar -10 See MU -2B AMP Chpt 3 100h/1y inspection SA01913SE

NARCO, Narco

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 120(195) NARCO SB ELT10- ELT ASSY 18-apr-88 04-nov-91 N/A ELT ASSY 16

NYGE, Saab Aerotech Aircraft Services NYGE TDM 01 -45 Installation of Trim -In -Motion Alert JCAB AD TCD -4625A -2001 LFV LVD3122 07 -May - 14 -jun -02 Syst. and Automatic A/P Disconnect MITSUBISHI SB 231 Rev B 2001 syst. NYGE TDM 02 -10 Installation of TPE331 -6-252M 25 -mar -02 13 -jun -03 Engines NYGE TDM 02 -24 Installation Moving MAP 10 -Oct - 18 -dec -02 2002 NYGE TDM 02 -32 Installation EMI film 10 -dec -02 10 -jan -04 NYGE TDM 03 -08 8 GNS430/530 & MODE S GTX330 04 -mar -03 21 -Oct - install. 2008 NYGE TDM 03 -12 Installation Ugglan 25 -mar -03 07 -apr -03 NYGE TDM 03 -15 A U95 with General Control System 24 -apr -03 A 25 -feb -08 NYGE TDM 03-28 F Nav Demo Pod 19-dec-03 F 31-aug-09 Original compliance by Rev D. Not affected by rev F. NYGE TDM 05-16 Viktor Counter Weight Pod 18-nov-05 18-nov-05 NYGE TDM 05 -35 A Installation FR -31 11 -May - A 12 -May - Approved i.a.w. DOA 21j.108.05 -35 2006 2006 NYGE TDM 06 -28 A Removable FR -31 29 -jun -07 A 18 -sep -07 NYGE TDM 06 -41 A Darts (to carry on MU -2B -20/26) 20 -nov -06 A 07 -feb -08 NYGE TDM 06 -42 A Barlast DARTS MU -2B 04 -dec -07 A 07 -feb -08 NYGE TDM 07-30 A Install. of Emergency Axe 28-feb-08 A 29-feb-08 NYGE TDM 08 -03 A Enhanced Surveillance MU -2B 28 -feb -08 A 17 -dec -09 NYGE TDM 08 -28 B ELT 406 MU -2B 29 -sep -08 B 21 -Oct - Original compliance with TDM rev A. Rev B does 2008 not affect previous complaiance. NYGE TDM 09 -24 A Electrical Wiring Feed Through 08 -sep -09 A 31 -aug -09 NYGE TDM 09 -31 A GPS Splitter 12 -nov -09 A 10 -dec -09 NYGE TDM 10-02 A Target surveillance camera 03-jun-10 A 01-Oct- 2010

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 121(195) NYGE TDM 10-03 A Pressure Bulkhead Feed Through 04-May- A 01-Oct- 2010 2010 NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10 A 25-May- 2010 NYGE TDM 11-35 A Terminating resistor A 21-Feb-12 NYGE TDM 12 -21 A Avinstallation IK A 4-Jun -12 NYGE TDM 95 -04 4 Vingstudie 20 -sep -98 4 27 -mar -09 NYGE TDM 96 -06 Rep. sprickor "hinge,front spar 11 -nov -96 14 -nov -96 flange" NYGE TDM 99 -03 Install. Auto Ignition 03 -mar -99 29 -sep -99 NYGE TVO 1/09 Inspektion av Stringers & struktur 25 -feb -09 08 -apr -09 Inspected with remarks vinge NYGE TVO 1/93 Low Volt Warning Light (BCL) 22 -jan -93 03 -mar -93 NYGE TVO 1/96 Slitage Flap Guide Rail 12 -apr -96 20 -jun -02 NYGE TVO 1/97 3 De -Icertank MU -2B, 12 -feb -97 24 -jun -98 korrosionskontroll NYGE TVO 2/00 Märkning av infästning domkraft Mu2 01 -dec -00 01 -feb -01 NYGE TVO 2/07 A Prevent FR31 radio to xmit when 06 -feb -07 A 02 -mar -07 RM2 off NYGE TVO 2/91 A/C Elecrical System 10 -jan -91 24 -jun -92 NYGE TVO 3/06 Inspect lower rudder hinge bracket 07 -dec -06 20 -aug -10 NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24 -feb -05 3 17 -dec -09 NYGE TVO 4/86 2 Wing Pod Inspection 06 -apr -92 2 20 -aug -10 NYGE TVO 4/91 Special Inspection (next E6.) 19 -feb -91 24 -jun -92 NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29 -apr -92 24 -jun -92 NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28-sep-94 3 20-aug-10 NYGE TVO 4/96 Kontroll av Lagerhus i 25 -Oct - 01 -jul -97 Utförd tidigare (ref. Ove N lista) noshjulsstyrning. 1996 NYGE TVO 6/88 Allm. instruktion för metallpropeller 13 -jun -88 17 -dec -09 NYGE TVO 6/92 Elevator Trim Cable, check 07 -Oct - 27 -Oct - 1992 1992

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 122(195) NYGE TVO 7/93 Starter Drive Splines 01-nov-93 09-aug-94 NYGE TVO 8/04 Kontr. av Spant vid bakre 08 -dec -04 17 -dec -09 feninfästning NYGE TVO 8/92 Wheel Parts 27 -Oct - 11 -mar -93 1992 NYGE TVO 9/88 Emergency Extension System 08 -aug -88 06 -feb -89

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 123(195)

2.5 GFE Aircraft Mitsubishi MU-2 SE-GHF

2.5.1 Aircraft Specification Type: Serial Registration : Airframe Total Date Number: total Hours: Landing Reference: Cycles: MU-2B-20 299 SE-GHF 12688 6751 2012-11-23

2.5.2 Engines Type: Honeywell TPE331 -6-252M Serial Total Total Hours remaining to Number: Hours Cycles overhaul/HIS/GBI: Since New: Since New: Left Engine P20388 7806 6761 3101/1288/1301 Right P27037 14603 16508 1233/352/2152 Engine

2.5.3 Propeller Type Number: Serial Number: Overhaul Due Date: Left Propeller HC -B3TN -5E BVA 6 124 2013 -01 -26 Right Propeller HC-B3TN-5E BVA 6222 2013-01-29

2.5.4 Avionics System: Type / Part Number: Note: Autopilot & Flight Director Century IV COM/NAV/GPS 1 Garmin GNS 530 COM/NAV/GPS 2 Garmin GNS 430 Audiopanel Bendix/King KMA-24H-70 MKR Bendix/King KR-21 DME Bendix/King KDM-706 ADF Bendix/King KDF -806 XPDR 1 Garmin GTX 330D Mode S EHS XPDR 1 / 2 Garmin GTX 330 *) Mode S EHS RDR ALT Bendix/King KRA-10A ELT Kanad ELT 406-AF-H Airspeed Indicator LH / RH Aerosonic 20040-161 / 20040- 0186 Altimeter LH United Instr. Inc. 5934 PAM-3 Altimeter incl. encoder RH United Instr. Inc. 5035P -P40 Altitude Reporter Narco AR 850 Altitude Alerter Aero Mechanism AM 275C

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 124(195) Vertical Speed Indicator LH Aerosonic RC-60-MS-10-3 Attitude Gyro & Flight Director Ind. Century 52C77 LH Attitude Gyro Ind. RH AIM 504-0006-914 Turn & Bank Ind. LH R.C Allen A5930-02 Horizontal Situation Indicator LH Bendix/King KPI -553A DG -Gyro Sperry C -14A Directional Gyro RMI Ind. LH AIM 254 -1D RMI/ADF adapter Bendix/King KDA-692 CDI Indicator Garmin GI-106A *) XPDR 2 without diversity configuration

2.5.5 Mission System System : Description: Fixed general installations VHF/UHF COM 1 & 2 FR31 GPS MAP JET SI-3003B Inverter 115/200VAC 400Hz 3 phase Laser Prism MIL -STD -1553 Bus LH Wing Pylon Wing Pylon NATO 14” Alcon Ejector Unit LH and RH Wing Pylon EW system ASTOR Fixed installed system ADRIAN Pod mounted system LH and RH Wing Pylon U95 N Pod mounted system LH Wing Pylon U95 Sorc Pod mounted system RH Wing Pylon U95 Sorc A100 Pod mounted system LH Wing Pylon Missile Threat Simulator DARTS Pod mounted system LH Wing Pylon Chaff Dispenser BOX 3 Pod mounted system LH and RH Wing Pylon

2.5.6 Mission Cable Harness to Hard Points Used for Mission LH NATO Hard point: RH NATO Hard point: Note: System: Adrian C & S, U95-N, A100, General Signal Harness General Signal Harness DARTS and BOX 3 AWG22 shielded x 44 AWG22 shielded x 50 U95-N and A100 MIL-STD-1553B Data MIL-STD-1553B Data Triax Cable x 1 Bus Bus U95-N, A100 and DARTS AC Power AWG 12 x 4 115/200VAC 400 Hz 3- twisted

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 125(195) Phase 3 x 10 A AWG 16 x 2 AWG 20 x 2 Adrian C & S and BOX 3 DC Power 28 VDC 200 DC Power 28 VDC 200 AWG 2 x 2 A A Adrian C & S Coax Cable 1 x 50 Ω Coax Cable 1 x 50 Ω Prepared installation Coax Cable 1 x 75 Ω Prepared installation Ethernet LAN Cable

2.5.7 Antenna Layout

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 126(195)

2.5.8 Inspection due times and dates Status date November 23 rd 2012.

Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date Aircraft SE-GHF Vingstudie MU-2 AMP 2012-05-06 12687 13700 100 Hour Inspection AMP 2012-05-15 12687 12787,1 2013-06-25 200 Hour Inspection AMP 2012-05-14 12687 12887,1 2013-06-25 600 Hour Inspection AMP 2010-09-14 12557 13157,7 2013-09-13 1000 Hour Inspection AMP 2012-05-14 12687 13700 1200 Hour Inspection AMP 11700 12900 1800 Hour Inspection AMP 11400 13200 2000 Hour Inspection AMP 11700 13700 1 Year Inspection AMP 2012-05-31 12687 2013-06-25 2 Year Inspection AMP 2012-06-20 12687 2014-06-25 10 Year Inspection AMP 2004-04-26 11800 2014-04-24 Engine S/N P-20388 Remaining Engine Assembly (Overhaul) AMP 15789,8 3101,6 Engine Hot Section Inspection AMP 13977 1288,8 Engine Gearbox Inspection AMP 13989,8 1301,6 Engine S/N P-27037 Engine Assembly (Overhaul) AMP 13921,9 1233,7 Engine Hot Section Inspection AMP 13041,1 352,9 Engine Gearbox Inspection AMP 14841,1 2152,9

Propeller L/H O/H AMP 2008-01-08 15177 2013-01-06 Propeller R/H O/H AMP 2008-01-31 15367,5 2013-01-29

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type

2012-12-06

Document number Page 127(195)

2.5.9 Implemented Changes Status date November 23 rd 2012.

SB/AD etc Rev Subject Document reference Eff. date Rev Compliance Status Remarks Reference

SB/AD etc Rev Subject Document reference Eff. date Rev Complianc Stat Remarks Reference e us

CENTURY, Century Flight Systems Inc. CENTURY SB CSB - Check for frayed Bridle Cable 21 -feb -05 15 -sep -10 2005-01

EASA, European Aviation Safety Agency EASA AD 2006 -0265 Incorrect transponder altitude 30 -aug -06 09 -dec -10 EASA AD 2009 - Portable Fire Extinguishers - 25 -nov -09 07 -May - N/A N/A by current P/N installed 0251 -E Ident/Repl 2010 EASA AD 2009 -0262 Halon 1211 Fire Extinguishers EASA AD 2009 -0278 FFE ASB26 -115 Rev C 15 -dec -09 07 -May - N/A N/A by current P/N installed Id/Repl 2010 EASA AD 2009 -0278 Halon 1211 Fire Extinguishers EASA AD 2009 -0262 22 -dec -09 07 -May - N/A N/A by current P/N installed Id/Repl 2010 EASA AD 2010 -0003 R1 Mode S Transponder - 11 -jan -10 R1 10 -mar -10 N/A due to model Check/Modification EASA AD 2012 -0037 Kidde Graviner hand operated fire 25 -Jun -12 extinguisher EASA SIB 2008 - Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN 17 -dec -08 21 -sep -10 N/A by SSB 0845 incorporated 58R1 SSB0845 Rev IR EASA SIB 2009 -14 Upgrade to main unit/GPS software 24 -jun -09 28 -sep -09 N/A due to model

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 128(195) FAA, U.S, Federal Aviation Administration FAA, U.S AD 2000 - AFM De -icing 25 -jan -00 26 -apr -00 N/A Due to paragraph b. 02-25 FAA, U.S AD 2000 - 1 Flight in Icing Condition FINNISH AD M 2435/97 FINNISH AD M 07 -jul -00 1 23 -nov -01 09-15 2786/00 MAI SB 086/74-002 Rev A MAI SB 093/22-009 MAI SB 096/30-004 MITSUBISHI SB 226 Rev E MITSUBISHI SB 231 Rev B MITSUBISHI SB 232 Rev A FAA, U.S AD 2003 - Windshield check FINNISH AD M 3076 LFV LVD2678 MAI SB 01 -Oct - 09 -sep -10 17-04 087/56-001 Rev B MITSUBISHI SB 224 Rev 2003 C FAA, U.S AD 2003 - 1 Forecast Icing Conditions FINNISH AD T5007/03 JCAB AD TCD - 16 -apr -04 17 -May - inserted in AFM 22-07 4753A-2004 MAI SN 071/00-006 Rev D 2004 MITSUBISHI SN 117 Rev D FAA, U.S AD 2005 - Prop. mounting bolt insp. HARTZELL SB 61 -279 ALERT Rev 4 29 -jul -05 17 -sep -08 L/H side 14-12 FAA, U.S AD 2005 - Prop de -icer "FASTprop" 14 -Oct - 12 -Oct - N/A Due to boots p/n 18-20 2005 2005 FAA, U.S AD 2006 - Safety evaluation wing barrel nuts) MAI SB 103/57 -004 Rev A MITSUBISHI SB 11 -aug -06 26 -apr -04 c/o in conjunction with vingstudie 13-15 241 Rev A FAA, U.S AD 2006 - Safety evaluation (feathering MAI SB 090/76 -003 MITSUBISHI SB 229 24 -aug -06 24 -aug -06 se Mitsubishi SB 229 15-07 linkage) FAA, U.S AD 2006 - Detect & correct torque MAI SB 095/77 -002 MITSUBISHI SB 233 22 -sep -06 21 -sep -06 PCW see MSB 233A 17-01 transducers Rev B FAA, U.S AD 2006 - Adjust flight idle fuel flow setting MITSUBISHI SB 234 22 -sep -06 13 -Oct - 17-05 2010 FAA, U.S AD 2007 - Reduce max deflect elev nose - MITSUBISHI SB 216 MITSUBISHI SB 228 25 -sep -07 11 -sep -07 Previously carried out i.a.w. mentioned SB's. 17-09 down trim FAA, U.S AD 71 -14 - Fuel Tank Fungus Coating Peeling 01 -May - 01 -jan -96 N/A N/A by s/n 01 1972 FAA, U.S AD 74 -11 - Windshield Outer Panes LFV LVA829 Rev A MITSUBISHI SB 163 Rev 30 -jan -78 01 -dec -10 PCW See JCAB AD TCD -0948A -1-78 01 B FAA, U.S AD 75 -16 - Main Wing Flap JCAB AD TCD -1094A -76 LFV LVA1011 Rev 05 -aug -75 03 -May - Revision C PCW by Swedair. 13 A MITSUBISHI SB 167 Rev D 1977 FAA, U.S AD 75 -16 - Propeller Pitch Control Lever JCAB AD TCD -1188 -75 LFV LVA1012 12 -aug -75 25 -apr -75 20 MITSUBISHI SB 168 Rev A FAA, U.S AD 78 -03 - Cowling Latches JCAB AD TCD -1202 -75 LFV LVA1014 Rev A 23 -feb -78 11 -aug -75 05 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 129(195) FAA, U.S AD 81-06- 1 Engine Aft Nacelles 01-apr-81 1 23-jun-97 Previously complied with 01 FAA, U.S AD 81-25- 1 Engine's Electrical wiring SB 21-jan-82 1 02-dec-10 N/A N/A by model 04 036/71-003A, SB 043/71-005 FAA, U.S AD 82-08- Electrical Wiring Inspection 15-apr-82 25-mar-82 02 FAA, U.S AD 83-08- 2 To preclude prop. attach bolt FINNISH AD M 1168/83 Rev 1 FINNISH AD 28-apr-82 2 20-May- Ref. MU2B MM chap 13.4 when using bolts P/N B- 01 failures T5114/05 HARTZELL SI 140A Rev 9 2005 3339 only FAA US AD 83 -09 - Strobe light assemblies 16 -Mar -12 02 FAA, U.S AD 84 -12 - Torque of Air Tube Coupling Nuts MAI SB 047/30 -001 Rev A MITSUBISHI SB 28 -jun -84 19 -jun -84 04 SB 047/30-001, SB 196A 196 Rev A FAA, U.S AD 84 -25 - Elevator TrimTab Bracket MAI SB 031/27 -005 Rev 1 MITSUBISHI SB 18 -dec -84 19 -mar -86 02 Insp/Repl. SB 031/27-005 R1, SB 176 Rev E 176E FAA, U.S AD 86-15- NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2 13-aug-86 15-jul-04 Found SB 181 part 2 PCW. 03 Rev B FAA, U.S AD 86-20- To assure anti-ice capability of pitot LFV LVD2015 Rev B, MAI SR 020/34-005 , 06-Oct- 17-May- 01 SB 020/34-005, SB 053A MITSUBISHI SR 053A 1986 2004 FAA, U.S AD 86-26- To prevent engine flameout in an GARRETT SB 74-0003 Rev 6 MAI SR 31-dec-87 09-mar-09 see applicable engine for c/o 02 iceing SB 74-0003, SR 040/74-001 040/74-001 MITSUBISHI SB 226 Rev E MITSUBISHI SR 066 FAA, U.S AD 87-04- Addit. Seal and Flap Flexible Shaft MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 27-jan-83 03 Insp SB 051/27-007, SB 198 FAA, U.S AD 87-12- Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 02-Oct- 02 1990 FAA, U.S AD 88-13- Bendix Autopilot Disengagement SB LFV LVD2190 MAI SB 066/22-006 Rev A 11-jul-98 01-sep-89 N/A N/A due to Autopilot model 01 066/22-006 MITSUBISHI SB 206 FAA, U.S AD 88-21- 1 To minimize confusion in LFV LVD2206 MAI SB 066/22-006 Rev A 28-jan-89 1 25-Jan-12 01 autopilot/manua SB 066/22-006 FAA, U.S AD 88-23- To prevent flap control failure SB LFV LVD2202 MAI SB 067/27-008 Rev A 04-dec-88 03-mar-95 01 067/27-008, SB 189B FAA, U.S AD 93-07- ELECTRIC TRIM SYSTEM SB 079/27- LFV LVD2477 MAI SB 079/27-010 01-jun-93 27-mar-09 N/A by s/n 11 010 FAA, U.S AD 94-04- Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11-apr-94 26-May- 16 1993 FAA, U.S AD 94-11- Change of Flight Idle Blade Angel SB LFV LVD2551 MAI SB 016/71-001 10-jun-94 27-mar-09 N/A by s/n 04 016/61-001 FAA, U.S AD 96 -25 - Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD - 27 -dec -96 19 -feb -02 02 4552-96 LFV LVD2749

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 130(195) FAA, U.S AD 97-04- Vent Check Valve Assy LFV LVD2769 16-apr-97 05-May- N/A N/A due to s/n. 13 1997 FAA, U.S AD 97-20- Icing related incidents/accidents 17-Oct- 02-dec-98 14 CNL 1997 FAA, U.S AD 97-25- To prevent loss of airplane FINNISH AD M 2524/98 21-jan-98 03-dec-10 N/A AD superseeded by AD 2010-10-17 02 ctrl/overspe FAA, U.S AD 98-20- Forward fitting bolt of wingtip tank LFV LVD2688 , MITSUBISHI SB 225 19-Oct- 30-jan-97 39 SB MU-2 225, 089/57-002A 1998

FINNISH, Finnish Civil Aviation Adm. FINNISH AD M Kontroll av rören till strobe - MITSUBISHI SB 174 PART 1 Rev C 07 -jul -83 09 -sep -10 1177/83 kablarna FINNISH AD M Justering av br,nslefl"de MHI SB JCAB AD TCD-4890-98 MAI SB 097/73-001 12-nov-99 13-Oct- 2609/98 097/73-001, TCD-4890-98 2010 FINNISH AD M 3076 Kontroll av vindrutor och fönster FAA, U.S AD 2003-17-04 MAI SB 087/56- 21-aug-03 09-sep-10 001 Rev B MITSUBISHI SB 224 Rev C

GARMIN, Garmin GARMIN SSB 0844 IR Software Version 5.04 EASA SIB2008 -58R1 14 -nov -08 A 20 -May - 2010 GARMIN SSB 0845 IR Software Version 6.04 EASA SIB2008 -58R 14 -nov -08 0 20 -May - 2010

GARRETT, AlliedSignal Aerospace GARRETT SB 74 - 6 Replace Ignition Unit AD 74 -0003 FAA, U.S AD 86 -26 -02 25 -mar -94 6 09 -mar -09 see applicable engine for c/o 0003

HARTZELL, Hartzell Propeller Inc. HARTZELL SB 61- Propeller mounting bolt inspection MITSUBISHI SL 053/72-003, MITSUBISHI 08-feb-02 19-mar-02 L/H & R/H side 256 SL 080 HARTZELL SB 61 - 4 Prop. mounting bolt insp. FAA, U.S AD 2005 -14 -12 , MITSUBISHI SL 04 -Oct - 17 -sep -08 L/H side 279 ALERT 085 2005

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 131(195) HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2 , LFV LVA1424 30-mar-05 9 13-mar-08 see previously revision Rev A

JCAB, Japan Civil Aviation Bureau JCAB AD TCD -0518 - Rivet holes elevator hinge fitting 06 -feb -68 26 -mar -09 N/A by s/n 68 JCAB AD TCD -0642 - AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07 -feb -70 17 -apr -86 70 JCAB AD TCD -0643 - Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07 -feb -70 15 -jul -04 N/A N/A by s/n. 70 JCAB AD TCD -0652 - Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25 -mar -70 26 -mar -09 N/A by model 70 JCAB AD TCD-0653- Engine Nacelle Tail Area- 25-mar-70 26-mar-09 N/A by model 70 Modification of JCAB AD TCD-0660- Replacement of bearing in LFV LVA457 MITSUBISHI SB 123 01-May- 26-mar-09 N/A by s/n 70 nosegearstrut 1970 JCAB AD TCD-0730- Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 Rev 25-mar-72 14-jul-04 N/A N/A by s/n. 1-72 B JCAB AD TCD-0730- Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10-dec-86 26-mar-09 N/A by s/n 2-86 JCAB AD TCD-0859- Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04-sep-72 10-sep-72 N/A N/A due to s/n. 72 JCAB AD TCD-0866- NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09-Oct- 31-dec-72 N/A N/A due to s/n. 72 1972 JCAB AD TCD- Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 Rev 12-nov-74 21-aug-86 N/A N/A due to s/n. 0947A-74 A JCAB AD TCD- Inspection of Windshields MITSUBISHI SB 163 Rev B 22-dec-78 26-mar-09 0948A-1-78 JCAB AD TCD- Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 Rev 07-Oct- 15-mar-86 0948A-74 B 1974 JCAB AD TCD- Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 Rev 06-Oct- 19-mar-86 1001A-76 E 1976 JCAB AD TCD- Replacement of Elevator Trim Tab FINNISH AD M 1080/82 LFV LVD1971 12-dec-84 19-mar-86 1001B-2-84 Bracket MITSUBISHI SB 176 Rev E JCAB AD TCD- Insp. of wingflap controlsystem FAA, U.S AD 75-16-13 LFV LVA1011 Rev A 06-sep-76 03-May- Revision C PCW by Swedair. 1094A-76 MITSUBISHI SB 167 Rev D 1977 JCAB AD TCD-1188- Insp. of propeller controllever inst. FAA, U.S AD 75-16-20 LFV LVA1012 06-May- 25-apr-75 75 MITSUBISHI SB 168 Rev A 1975

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 132(195) JCAB AD TCD-1202- Engine Cowling Latches FAA, U.S AD 78-03-05 LFV LVA1014 Rev A 20-sep-75 15-jul-04 Found SB 171 and SB 180 PCW. 75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A JCAB AD TCD-1209- Insp/mod of NLG shimmydamper LFV LVA1013 MITSUBISHI SB 169 Rev B 16-jun-75 11-jun-75 75 locking JCAB AD TCD-1235- Insp./repl. of MLG fwd door LFV LVA1083 MITSUBISHI SB 170 Rev A 19-sep-75 17-apr-86 N/A N/A due to model. 75 emerg.cables JCAB AD TCD-1272- Supp.,MLG Forward D. Actuating MITSUBISHI SB 172 14-nov-75 26-mar-09 N/A by model 75 Mech.-I&M JCAB AD TCD-1284- Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar-76 01-sep-09 PCW Ref. SB 173 1-76 JCAB AD TCD-1328- Fire hazard in rear baggage 01-jul-76 26-mar-09 N/A by s/n 76 compartment JCAB AD TCD-1353- Barrel Nut, Inner/Outer Wing MITSUBISHI SB 175 16-aug-76 01-sep-09 N/A by p/n 76 Conn.-Repl. JCAB AD TCD-1370- Inspect strobelight conduit in LFV LVA1196 18-Oct- 21-aug-86 Part.1 76 Tiptank 1976 JCAB AD TCD- Inspect strobelight conduit in MITSUBISHI SB 174 PART 1 Rev C 05-nov-81 09-sep-10 1370A-81 Tiptank supersed TCD-1370-76 JCAB AD TCD-1379- Insp. rear eng. cowling reg. LFV LVA1197 Rev A MITSUBISHI SB 177 06-feb-02 23-jun-77 Previously complied with 1-80 heatdamage Rev B JCAB AD TCD- Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12-dec-77 24-mar-09 ref. SB 180 1520A-77 JCAB AD TCD -1768 - Fatigue failure of the NLG strut LFV LVA1546 MITSUBISHI SB 181 PART 12 -jul -85 15 -jul -04 PCW Found SB 181 part 2 PCW. 1-85 assy. JCAB AD TCD -1817 - Modification of LFV LVA1583 MITSUBISHI SB 182 05 -feb -02 11 -feb -80 N/A N/A due to s/n. 79 bagagecompartment JCAB AD TCD -2048 - Insp. firewarning & emerg.power LFV LVA1740 MITSUBISHI SB 187 Rev B 05 -feb -02 27 -May - N/A N/A due to model. 81 circuit 1981 JCAB AD TCD -2070 - Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05 -feb -02 25 -mar -82 81 JCAB AD TCD -2113 - Insp./replace engine electrical LFV LVA1788 MITSUBISHI SB 191 06 -feb -02 25 -mar -82 Checked N/A due to color (brown) of cables i.a.w. 82 harness SB 191 JCAB AD TCD -2252 - Flap system torquetubes supersed 01 -feb -89 24 -mar -09 PCW 2-88 TCD -2252 -1-87 JCAB AD TCD -2252 - Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04 -feb -83 03 -mar -95 83 JCAB AD TCD -2263 - NLG. bracket attaching to drag strut 13 -aug -83 24 -mar -09 N/A by model 83

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 133(195) JCAB AD TCD-2342- Engine inlet anti-ice tubing. MITSUBISHI SB 196 Rev A 05-jun-84 10-mar-09 PCW 1-84 Torq./lock JCAB AD TCD-2342- Engine inlet anti-ice tubing. LFV LVA1942 MITSUBISHI SB 196 Rev A 06-feb-02 19-jun-84 84 Torq./lock JCAB AD TCD- Pitot Tube Wiring LFV LVD2015 Rev B MITSUBISHI SR 053A 16-jun-87 15-jul-04 SB PCW. 2450A -87 JCAB AD TCD-2451- Add. seal/Tq. insp of flap flex. shaft 01-May- 09-mar-09 PCW see TCD-2451-85 1-87 1987 JCAB AD TCD -2451 - Add. seal/Tq. insp of flap flex. shaft LFV LVD2037 MITSUBISHI SB 198 30 -sep -85 27 -jan -83 85 Superseeded by TCD-2451-1-87 JCAB AD TCD -2545 - Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01 -jul -88 02 -Oct - 1-88 1986 JCAB AD TCD - Auto -ignition System FINNISH AD M 2435/97 LFV LVD2761 01 -feb -97 22 -nov -01 2679A-97 MITSUBISHI SB 226 Rev E JCAB AD TCD -3378 - Insp./mod. of rudder trimtab LFV LVD2338 MITSUBISHI SB 211 28 -mar -91 14 -jul -04 N/A N/A by s/n. 90 leadingedge JCAB AD TCD - Anti ice/De -ice system FINNISH AD M 2364/96 LFV LVD2347 Rev 25 -May - 15 -sep -10 3393A -96 1 MITSUBISHI SB 212 Rev A 1996 JCAB AD TCD -3464 - Unintentional engagement of 17 -jun -91 24 -mar -09 N/A by model 91 A/P...... JCAB AD TCD - Mod.of Autopilote pitchtrimsystem FINNISH AD M 2581/98 LFV LVD2450 LFV 17 -aug -98 08 -dec -98 3740A-98 MSB 216, 228 LVD 2898 LVD2898 MITSUBISHI SB 216 MITSUBISHI SB 228 JCAB AD TCD -3901 - Tiptank inst FINNISH AD M 2110/93 LFV LVD2512 10 -sep -93 15 -mar -94 93 MITSUBISHI SB 221 JCAB AD TCD -3942 - Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592 28 -nov -94 03 -mar -95 1-94 MITSUBISHI SB 219 Rev A JCAB AD TCD -3942 - Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01 -feb -94 03 -mar -95 94 JCAB AD TCD -4310 - Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688 01 -apr -96 30 -jan -97 96 MITSUBISHI SB 225 JCAB AD TCD -4311 - Windshield/window insp. FINNISH AD M 2331/96 LFV LVD2678 01 -nov -95 09 -sep -10 95 MITSUBISHI SB 224 Rev C JCAB AD TCD -4379 - Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689 01 -apr -96 30 -jul -96 96 MITSUBISHI SB 229 JCAB AD TCD -4552 - Icing Limitation FAA, U.S AD 96 -25 -02 LFV LVD2749 27 -dec -96 19 -feb -02 96 JCAB AD TCD -4625 - Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI SB 14 -jul -97 23 -nov -01 97 093/22-009

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 134(195) JCAB AD TCD- Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B 16-mar-01 13-mar-09 PCW Ref AMOC LFV Appr M15/01, TDM 01-45 4625A-2001 NYGE TDM01-45 JCAB AD TCD-4626- De-ice system Modification FINNISH AD M 2461/97 LFV LVD2800 01-May- 14-jul-04 PCW 97 MITSUBISHI SB 232 Rev A 1997 JCAB AD TCD-4684- Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819 01-jun-97 25-mar-99 97 MITSUBISHI SB 230 JCAB AD TCD-4753- Ändring av flyghandbok LVD FINNISH AD M 2518/98 LFV LVD2922 18-feb-98 02-dec-98 FAA AD utförd. 98 2922,FAA AD 97-20-14, MHI SN MITSUBISHI SN 117 Rev D 117A JCAB AD TCD- Icing-related incidents VIDEO FAA, U.S AD 2003-22-07 Rev 1 24-feb-04 17-May- inserted in AFM 4753A-2004 2004 JCAB AD TCD-4838- Inspection of landing gear power FINNISH AD M 2574/98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model 98 train MITSUBISHI SB 235 JCAB AD TCD-4889- Inappropriate calib. of eng. trq- MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A. 2-2007 meter JCAB AD TCD-4889- Insp. of Engine Torque Indication FINNISH AD M 2608/98 LFV LVD2924 05-nov-98 14-jul-04 PCW 98 System LFV 2924, MU SB 233 MITSUBISHI SB 233 Rev B JCAB AD TCD-4890- Check of flight idle FF LVD 2925, FINNISH AD M 2609/98 LFV LVD2925 04-nov-98 13-Oct- 98 MU SB 234 MITSUBISHI SB 234 2010 JCAB AD TCD-5030- Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17-May- 24-mar-09 N/A by model 99 1999 JCAB AD TCD-5432- AFM revision LFV LVD3112 27-nov-00 12-feb-02 2000 JCAB AD TCD -5547 - To prevent loss of airplane control LFV LVD3123 16 -mar -01 12 -feb -02 2001 JCAB AD TCD -5747 - Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12 -sep -01 08 -Oct - 2001 2001 JCAB AD TCD -5864 - Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27 -dec -01 17 -jan -02 2001 JCAB AD TCD -6127 - Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17 -mar -03 09 -Oct - 2003 2003 JCAB AD TCD -7030 - Inspection of Wing Attachment MITSUBISHI SB 241 Rev A 27 -dec -06 17 -jan -07 c/o in conjunction with wingstudie 2006 Hardware

LFV, Luftfartsverket LFV LVA 1011 A Kontroll av vingklaffarnas FAA, U.S AD 75 -16 -13 JCAB AD TCD - 05 -feb -02 A 03 -May - Revision C PCW by Swedair. manöversystem 1094A-76 MITSUBISHI SB 167 Rev D 1977 LFV LVA 1012 Kontroll av propellerreglagets FAA, U.S AD 75 -16 -20 JCAB AD TCD -1188 - 05 -feb -02 25 -apr -75

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 135(195) montering 75 MITSUBISHI SB 168 Rev A LFV LVA 1013 Kontr. och mod. av låsning på JCAB AD TCD -1209 -75 MITSUBISHI SB 169 05 -feb -02 11 -jun -75 nosställ Rev B LFV LVA 1014 A Kontr. & byte av motorinkl. FAA, U.S AD 78 -03 -05 JCAB AD TCD -1202 - 05 -feb -02 A 11 -aug -75 låsanordning 75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A LFV LVA 1083 Insp. & utbyte av lina för JCAB AD TCD -1235 -75 MITSUBISHI SB 170 05 -feb -02 17 -apr -86 N/A N/A due to s/n. nödöppning Rev A LFV LVA 1196 Isolering av strobe light från JCAB AD TCD -1370 -76 MITSUBISHI SB 174 06 -feb -02 09 -sep -10 bränsle PART 1 Rev C LFV LVA 1197 A Förhindr. av värmeskador på JCAB AD TCD -1379 -1-80 MITSUBISHI SB 06 -feb -02 A 23 -jun -77 Previously complied with bak.motorpl. 177 Rev B LFV LVA 1238 Kontr. & byte av infästningsdet. 06 -feb -02 21 -apr -09 N/A by s/n trimrod LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86 -15 -03 JCAB AD TCD -1768 - 06 -feb -02 24 -aug -84 1-85 MITSUBISHI SB 181 PART 2 Rev B LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD -1817 -79 MITSUBISHI SB 182 05 -feb -02 11 -feb -80 N/A N/A due to s/n. LFV LVA 1740 Kontr.av brandvarnings -och JCAB AD TCD -2048 -81 MITSUBISHI SB 187 05 -feb -02 31 -aug -09 N/A by s/n n"dstr"mskret Rev B LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD -2070 -81 MITSUBISHI SB 188 05 -feb -02 25 -mar -82 LFV LVA 1788 Kontroll/Utbyte av elledningar på JCAB AD TCD -2113 -82 MITSUBISHI SB 191 06 -feb -02 25 -mar -82 Checked N/A due to color (brown) of cables i.a.w. motor SB 191 LFV LVA 1873 Insp./utbyte av infäst.till JCAB AD TCD -2252 -83 MITSUBISHI SB 189 06 -feb -02 03 -mar -95 torsionsrör Rev C LFV LVA 1942 Momentdragning/låsn.av koppl.i JCAB AD TCD -2342 -84 MITSUBISHI SB 196 06 -feb -02 19 -jun -84 varmlufts Rev A LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD -0643 -70 MITSUBISHI SB 114 05 -feb -02 15 -jul -04 N/A N/A by s/n. LFV LVA 439 Rev. av flyghandbok betr. JCAB AD TCD -0642 -70 MITSUBISHI SB 112 05 -feb -02 17 -apr -86 bränslespec. Rev C LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD-0652-70 MITSUBISHI SB 119 05-feb-02 26-mar-09 N/A by model LFV LVA 457 Utbyte av lager i nosst,llets JCAB AD TCD-0660-70 MITSUBISHI SB 123 05-feb-02 26-mar-09 N/A by s/n st"td,mp. LFV LVA 543 B Insp. och målning av integraltankar JCAB AD TCD-0730-1-72 05-feb-02 B 14-jul-04 N/A N/A by s/n. LFV LVA 645 Modifiering av el -system JCAB AD TCD -0859 -72 MITSUBISHI SB 156 05 -feb -02 08 -dec -09 N/A by A/C serial number LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD -0866 -72 05 -feb -02 31 -aug -09 N/A by s/n

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 136(195) LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD-0947A-74 MITSUBISHI SB 05-feb-02 A 21-aug-86 N/A N/A due to s/n. 162 Rev A LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74-11-01 FAA, U.S AD 75-03- 05-feb-02 A 26-mar-09 06 JCAB AD TCD-0948A-74 MITSUBISHI SB 163 Rev B LFV LVA 886 A Kontroll/byte av JCAB AD TCD-1001A-76 05-feb-02 A 19-mar-86 höjdtrimroderarmar LFV LVD 1238 Kontr./byte infästn.det. 15-apr-77 31-aug-09 N/A by s/n höjdtrimroder LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD-1001B-2-84 MITSUBISHI SB 18-jan-85 19-mar-86 176 Rev E LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34- FAA, U.S AD 86-20-01 JCAB AD TCD- 24-May- B 06-Oct- 005 Rev A, MHI SR 53 2450A-87 MAI SR 020/34-005 MITSUBISHI 1985 1986 SR 053A LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 198 30-sep-85 03-jun-85 LFV LVD 2069 Altimeter 25 -mar -86 07 -jul -86 N/A N/A by p/n & s/n LFV LVD 2113 Modif. & revision Handbook MHI 26 -jan -87 12 -jun -87 SR 006B, MAI SR 040/74-001RA LFV LVD 2190 Autopilot Switch MU2 SB 066/22 - FAA, U.S AD 88 -13 -01 MAI SB 066/22 -006 19 -aug -88 01 -sep -89 N/A Bendix A/P ej installerad 006 och SB 206 Rev A MITSUBISHI SB 206 LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD -2545 -1-88 MITSUBISHI SB 19 -aug -88 01 -sep -89 201 Rev A LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88 -23 -01 JCAB AD TCD -2252 - 08 -dec -88 03 -mar -95 1-87 MAI SB 067/27-008 Rev A MITSUBISHI SB 189 Rev C LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88 -21 -01 Rev 1 08 -Dec - 12 -feb -02 1988 LFV LVD 2338 Kont./Mod.av sidorodrets JCAB AD TCD -3378 -90 MITSUBISHI SB 211 28 -mar -91 14 -jul -04 N/A N/A by s/n. trimroderframka Mitsubishi MHI SB 211 LFV LVD 2347 1 Control Deice -system Mitsubishi SB JCAB AD TCD -3393A -96 MITSUBISHI SB 29 -May - 1 15 -sep -10 212A 212 Rev A 1996 LFV LVD 2352 Shoulder Harness Inst. FAA AC 43 - 23 -May - 16 -Oct - checked OK. 13 CHPT 9 1991 1991 LFV LVD 2450 Elevator Trim Tab Installation MU JCAB AD TCD -3740A -98 MITSUBISHI SB 03 -dec -92 26 -May - SB 216 216 1993 LFV LVD 2477 Electric Trim System AD930711, FAA, U.S AD 93 -07 -11 MAI SB 079/27 -010 03 -jun -93 27 -mar -09 N/A by s/n MU SB 079/27-0-010

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 137(195) LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD-3901-93 MITSUBISHI SB 221 02-dec-93 15-mar-94 LFV LVD 2537 Reducering av Höjdrodrets FAA, U.S AD 94 -04 -16 MITSUBISHI SB 216 07 -apr -94 26 -May - trimområde. FAA AD 94-04-16, SB 1993 216 LFV LVD 2538 Byte Låspinne i landställets nödutf. JCAB AD TCD -3942 -94 MITSUBISHI SB 219 07 -apr -94 03 -mar -95 SB 219 Rev A LFV LVD 2551 Adj.of Ground Idle FAA AD 94 -11 - FAA, U.S AD 94 -11 -04 22 -jun -94 27 -mar -09 N/A by s/n 04 LFV LVD 2592 Insp/Repl. of Lock -pin in L/G JCAB AD TCD -3942 -1-94 MITSUBISHI SB 09 -feb -95 03 -mar -95 gearbox TCD-3942-1-94, MSB 219A 219 Rev A LFV LVD 2678 Kontr. av vindrutor och fönster MHI FAA, U.S AD 2003 -17 -04 JCAB AD TCD - 12 -mar -96 09 -sep -10 SB 224 Rev A 4311-95 MITSUBISHI SB 224 Rev C LFV LVD 2688 Kontr/byte av infästn.bult för FAA, U.S AD 98 -20 -39 JCAB AD TCD -4310 - 09 -May - 26 -jun -00 L/H -side tiptank MU-2 SB 225 96 MITSUBISHI SB 225 1996 LFV LVD 2689 Kontroll av linkage för prop.flöjning JCAB AD TCD -4379 -96 MITSUBISHI SB 229 09 -May - 30 -jul -96 MU-2 SB 229 1996 LFV LVD 2732 Inspection/ Replacement of Prop FAA, U.S AD 96 -18 -14 HARTZELL SB 61 - 27 -sep -96 16 -nov -98 Prop. utbytt mot BVA Hub. FAA AD 96-18-14, Hz SB 136H 261 Rev 1 LFV LVD 2749 Revision av flyghandbok AFM TCD - FAA, U.S AD 96 -25 -02 JCAB AD TCD -4552 - 21 -jan -97 19 -feb -02 4552-96 96 LFV LVD 2761 Installation av autoignition system JCAB AD TCD -2679A -97 MITSUBISHI SB 14 -feb -97 15 -jun -99 TCD-2679A-97 226 Rev E LFV LVD 2769 Demont.av backventil i FAA, U.S AD 97 -04 -13 MITSUBISHI SB 130 18 -mar -97 05 -May - N/A N/A due to s/n. bränslesystemets MU-2 SB 130A Rev A 1997 LFV LVD 2800 Mod. av De -ice Monitoring System JCAB AD TCD -4626 -97 MITSUBISHI SB 232 28 -aug -97 10 -jun -98 Mitsubishi SB 232, TCD-4626-97 Rev A LFV LVD 2819 Mod.av lagerboxar för JCAB AD TCD -4684 -97 MITSUBISHI SB 230 18 -nov -97 21 -apr -98 landställssystem Mitsubishi SB 230 LFV LVD 2853 Periodisk funktionskontroll av 23-mar-98 02-feb-11 nödutgång LFV LVD 2897 Kontroll av landst,llets drivsystem JCAB AD TCD-4838-98 MITSUBISHI SB 235 02-aug-98 24-mar-09 N/A by model TCD-4838-98, SB 235 LFV LVD 2898 Mod. av autopilotens JCAB AD TCD-3740A-98 MITSUBISHI SB 27-aug-98 08-dec-98 höjdtrimsystem TCD-3740A-98, SB 216 MITSUBISHI SB 228 216, 228 LFV LVD 2922 Änd.av Flyghandbok -Extra krav på JCAB AD TCD -4753 -98 MITSUBISHI SN 117 12 -nov -98 02 -dec -98 FAA AD utförd. typutbi TCD-4753-98, MHI SN 117A Rev D LFV LVD 2924 Kontr/Just av motorernas Torque JCAB AD TCD -4889 -98 MITSUBISHI SB 233 01 -dec -98 01 -apr -99 indikeri MHI SB 233, TCD-4889-98 Rev B

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 138(195) LFV LVD 2925 Kontr/just av mot bränsleflöde JCAB AD TCD-4890-98 MITSUBISHI SB 234 01-dec-98 13-Oct- Flight Id MHI SB 234 2010 LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD-5030-99 MITSUBISHI SB 209 18-jun-99 24-mar-09 N/A by model Rev B LFV LVD 3112 Revision av flyghandbok JCAB AD TCD-5432-2000 30-jan-01 12-feb-02 LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD -4625A -2001 MAI SB 093/22 - 02 -apr -01 23 -nov -01 Ref AMOC LFV Appr M15/01, TDM 01 -45 009 MITSUBISHI SB 231 Rev B NYGE TDM01-45 LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD -5547 -2001 02 -apr -01 12 -feb -02 LFV LVD 3166 Sprickkontroll av infästning till ving - JCAB AD TCD -5747 -2001 MITSUBISHI SB 20 -sep -01 08 -Oct - spetstank 236 2001 LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD -5864 -2001 MAI SB 099/27 - 09 -jan -02 17 -jan -02 012 MITSUBISHI SB 237 LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD -6127 -2003 MITSUBISHI SB 21 -mar -03 09 -Oct - 239 2003

MAI, Mitsubishi Aircraft International MAI SB 047/30 -001 A Torque of Bleed Air Tube Coupling FAA, U.S AD 84 -12 -04 MITSUBISHI SB 196 19 -jul -84 A 19 -jun -84 Nuts AD 84-12-04,SB 196A Rev A MAI SB 051/27 -007 Add.Seal and Flap Flexible Shaft FAA, U.S AD 87 -04 -03 01 -feb -85 27 -jan -83 Torque AD 87-04-03, SB 198 MAI SB 067/27 -008 A Insp/Repl. of Flap Control System FAA, U.S AD 88 -23 -01 LFV LVD2202 29 -mar -95 A 03 -mar -95 Torque AD 88-23-01, SB 189B MAI SB 069/24 -006 Split Radio Bus Inspection and MAI SB 066/22 -006 Rev A 17 -nov -88 01 -sep -89 N/A N/A due to Aircraft s/n Rework MAI SB 086/74 -002 A Auto -Ignition System Installation FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH AD 05 -Oct - A 22 -nov -01 Action not required due to s/n. M 2435/97 MITSUBISHI SB 226 Rev E 2000 MAI SB 089/57 -002 A Insp/Repl. of Bolts for Wing Tip FAA, U.S AD 98 -20 -39 05 -nov -96 A 30 -jan -97 N/A N/A due to s/n. Tank MAI SN 110/00 - Power Lever Position Warning 25 -feb -09 09 -nov -09 SB 240 considered 017A MAI SN 111/77 -004 Torque Indicating System Shift 20 -nov -08 11 -mar -09 SB 233 considered Potential MAI SR 020/34 -005 Anti Ice Capability AD 86 -20 -01, SR FAA, U.S AD 86 -20 -01 LFV LVD2015 Rev B 06 -Oct - 21 -jan -00 N/A N/A due to s/n. 053A MITSUBISHI SR 053A 1986

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 139(195)

MITSUBISHI, Mitsubishi Heavy Industries Ltd MITSUBISHI MSB **RECOVERED RECORD** 27 -jan -83 N/A 24-004 MITSUBISHI MSR **RECOVERED RECORD** 12 -jun -87 020 MITSUBISHI MSR B **RECOVERED RECORD** 12 -jun -87 B 066 MITSUBISHI SB 066 Bendix M4D 18 -dec -87 18 -May - N/A 1988 MITSUBISHI SB M-4() Autop.Engage Switch Guard 11 -apr -91 12 -apr -95 N/A 076/22-008 Install. MITSUBISHI SB 112 C Anti -Ice Additive in Fuel -Usage of JCAB AD TCD -0642 -70 LFV LVA439 09 -Oct - C 17 -apr -86 1971 MITSUBISHI SB 114 Fuel Quantity Indicator JCAB AD TCD -0643 -70 LFV LVA438 01 -jan -70 15 -jul -04 N/A N/A by s/n. Readjustmnet MITSUBISHI SB 119 The Bolt and Bolt Hole Diam. of JCAB AD TCD -0652 -70 LFV LVA456 10 -mar -70 26 -mar -09 N/A by model Nose L.G MITSUBISHI SB 123 Bearing,Oleo Strut,Nose L.G. -Repl. JCAB AD TCD -0660 -70 LFV LVA457 01 -apr -70 26 -mar -09 N/A by s/n of MITSUBISHI SB 124 Scissors Switch,Nose L.G. -Install. of 31 -aug -70 17 -apr -86 N/A MITSUBISHI SB 128 B Tip Tank Air Pressure Modification 28 -jun -94 B 05 -nov -09 N/A by model & s/n MITSUBISHI SB 143 B Top Coating, Wing Integral Main JCAB AD TCD -0730 -1-72 JCAB AD TCD - 05 -jan -72 B 14 -jul -04 N/A N/A by s/n. F.T. -SIo 0730 -2-86 MITSUBISHI SB 162 A Flex. Shafts, Flap Control Sys. -Insp. JCAB AD TCD -0947A -74 LFV LVA828 Rev A 03 -Oct - A 21 -aug -86 N/A of (AD750201) 1974 MITSUBISHI SB 163 B Insp. of Outer Pane, Front Winds. & FAA, U.S AD 74 -11 -01 JCAB AD TCD - 16 -nov -78 15 -mar -86 Inst 0948A-1-78 JCAB AD TCD-0948A-74 LFV LVA829 Rev A MITSUBISHI SB 165 A Lubr. Interval,Wheel Bearing,Main 24-jul-80 17-jun-86 N/A & Nose MITSUBISHI SB 166 Wing Flap 24 -jul -80 10 -mar -86 MITSUBISHI SB 167 D Flap M.Jack Screw-Insp. of and/or FAA, U.S AD 75-16-13 JCAB AD TCD- 24-jul-80 D 03-May- Revision C PCW by Swedair. Main G 1094A-76 LFV LVA1011 Rev A 1977 MITSUBISHI SB 168 A Propeller Pitch Control Lever -Insp. FAA, U.S AD 75 -16 -20 JCAB AD TCD -1188 - 24 -jul -80 A 25 -apr -75 of (AD761620) 75 LFV LVA1012

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 140(195) MITSUBISHI SB 169 B Shimmy Damper-Insp. and JCAB AD TCD-1209-75 LFV LVA1013 24-jul-80 B 05-nov-09 PCW Modification of MITSUBISHI SB 170 A MLG Forward Door Em.Op. Cable- JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77 A 17-apr-86 N/A N/A due to s/n Insp. & Re (AD762204) MITSUBISHI SB 171 B Latches,Eng. Nacelle Upper D.- FAA, U.S AD 78-03-05 JCAB AD TCD-1202- 17-nov-77 B 11-aug-78 Insp.& Mod (AD780305) 75 LFV LVA1014 Rev A MITSUBISHI SB 173 A Drag Strut, Main L.G.-Modification JCAB AD TCD-1284-1-76 24-jul-80 11-aug-75 of MITSUBISHI SB 174 C Tip Tank Conduit Tube -Insp.of,and FINNISH AD M 1177/83 JCAB AD TCD - 02 -Oct - C 09 -sep -10 PART 1 Rew.of (AD830902) 1370A-81 LFV LVA1196 1981 MITSUBISHI SB 175 Barrel Nut, Inner/Outer Wing JCAB AD TCD -1353 -76 26 -jun -76 01 -sep -09 N/A by p/n Conn.-Repl. MITSUBISHI SB 176 E Elevator Trim Tab Bracket -Repl. of FAA, U.S AD 84 -25 -02 FINNISH AD M 26 -sep -84 E 19 -mar -86 LVD1971, AD 84-25-02, SB 031/27- 1080/82 JCAB AD TCD-1001A-76 JCAB AD 005R1 TCD-1001B-2-84 LFV LVD1971 MITSUBISHI SB 177 B Mod. of Engine Nacelle Tail Area JCAB AD TCD-1379-1-80 LFV LVA1197 Rev 11-sep-80 B 23-jun-77 Previously complied with (AD810601) A MITSUBISHI SB 179 Rodd Assem., Engine Nacelle Upper 27-May- 04-feb-86 D.-R&M 1977 MITSUBISHI SB 180 A Link, Engine Nacelle Upper D.-Repl. FAA, U.S AD 78-03-05, JCAB AD TCD-1202- 17-nov-77 A 29-mar-78 of (AD780305) 75 , LFV LVA1014 Rev A MITSUBISHI SB 181 B Insp. and Repl. of Nose L.G. Strut FAA, U.S AD 86-15-03 JCAB AD TCD-1768- 08-apr-85 B 24-aug-84 PART 2 Assem (AD801812) 1-85 LFV LVA1546 MITSUBISHI SB 182 Add. of Ceiling Cover, Rear Bagg. JCAB AD TCD -1817 -79 LFV LVA1583 16 -nov -79 16 -nov -79 N/A N/A due to s/n. Comp. MITSUBISHI SB 184 Turnbuckle, Control Cables -Repl. of 04 -apr -80 25 -mar -82 MITSUBISHI SB 188 Down Lock Mech., Nose L.G. -Insp. JCAB AD TCD -2070 -81 LFV LVA1753 13 -jul -81 25 -mar -82 of MITSUBISHI SB 189 C Flap Control Torque Tube AD 88- FINNISH AD M 2722/00 JCAB AD TCD- 28-jun-94 C 03-mar-95 23-01, SB 067/27-008 2252-1-87 JCAB AD TCD-2252-83 LFV LVA1873 LFV LVD2202 MITSUBISHI SB 190 A Trav. Nut Repl. of L.G. Mech. Stop 28 -jun -94 25 -mar -82 Assem MITSUBISHI SB 191 Engine El. Wire -Insp. and JCAB AD TCD -2113 -82 LFV LVA1788 21 -dec -81 25 -mar -82 Replacement of (AD820802) MITSUBISHI SB 193 B Landing Gear Warning Horn 15 -jun -94 B 04 -dec -00 Rev A är utförd. Syst.Modif. MITSUBISHI SB 194 Master Cauting Light Visibility -Impr. 23 -aug -82 27 -jan -83 of

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 141(195) MITSUBISHI SB 196 A Ret. of coupling nut on the bleed FAA, U.S AD 84-12-04 JCAB AD TCD-2342- 12-apr-84 A 19-jun-84 air tu AD 84-12-04, SB 047/30-001 1-84 JCAB AD TCD-2342-84 LFV LVA1942 MAI SB 047/30-001 Rev A MITSUBISHI SB 198 Add. Seal & Torque Insp. of Flap FAA, U.S AD 87-04-03 JCAB AD TCD-2451- 13-feb-85 27-jan-83 Flex.Sh LVD2037, AD 87-04-03, SB 85 LFV LVD2037 051/27-007 MITSUBISHI SB 199 A Engine Lubricating Tubing Insp. & 24 -jun -94 A 06 -nov -09 PCW Protec MITSUBISHI SB 200 B Insp of Nose Ldg Gear Drag Strut 24 -jun -94 A 02 -aug -88 Link MITSUBISHI SB 201 A Generator Circuit Wires Insp. and FAA, U.S AD 87-12-02 JCAB AD TCD-2545- 02-mar-88 A 02-Oct- Mod. 1-88 LFV LVD2191 1986 MITSUBISHI SB 204 Speed Placard Change 03-mar-87 18-May- 1988 MITSUBISHI SB 206 Bendix Autop.Disengagement FAA, U.S AD 88-13-01 JCAB AD TCD-2856- 13-Oct- 31-jan-89 N/A N/A due to Autopilot model Method Stand. 1-97 LFV LVD2190 1987 MITSUBISHI SB 207 Rudder T.T. & Elevator T.T. Insp. & 20-May- 28-aug-09 Rep. 1988 MITSUBISHI SB 209 B Fuselage inspection JCAB AD TCD-5030-99 LFV LVD2988 19-apr-99 B 24-mar-09 N/A by model MITSUBISHI SB 210 A Engine Ignition Unit Replacement 12 -nov -96 06 -mar -98 MITSUBISHI SB 211 Rudder Trim Tab Modification (LVD JCAB AD TCD -3378 -90 LFV LVD2338 20 -nov -90 14 -jul -04 N/A N/A by s/n. 2338) MITSUBISHI SB 212 A Insp of Anti -ice/Deice Systems (LVD JCAB AD TCD -3393A -96 LFV LVD2347 Rev 25 -apr -96 A 15 -sep -10 2347), 1 MITSUBISHI SB 214 Engine Control Rod Inspection 06 -dec -91 13 -mar -92 MITSUBISHI SB 215 Removel of Prop. Governor Speed 23 -Oct - 13 -mar -92 N/A N/A due to -1 engine Signal 1991 MITSUBISHI SB 216 Elevator Trim Tab Installation (LVD FAA, U.S AD 2007 -17 -09 FAA, U.S AD 94 - 11 -sep -92 26 -May - 2450 04-16 JCAB AD TCD-3740A-98 LFV 1993 LVD2450 LFV LVD2537 LFV LVD2898 MITSUBISHI SB 218 A Propeller Feathering Linkage 17 -jan -94 A 15 -mar -94 Inspection MITSUBISHI SB 219 A Emergency Gear Down G.box JCAB AD TCD -3942 -1-94 JCAB AD TCD - 24 -Oct - A 03 -mar -95 Lower Pin Repl 3942-94 LFV LVD2538 LFV LVD2592 1994 MITSUBISHI SB 221 Tip Tank Conduit Tube Insp. and JCAB AD TCD -3901 -93 LFV LVD2512 10 -aug -93 15 -mar -94 Rep. MITSUBISHI SB 222 Fuselage Waterproof Modification 28 -jun -94 08 -dec -98 SR 019

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 142(195) MITSUBISHI SB 223 Pitot/Static System Improvement MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 21-jan-00 SR 064 MITSUBISHI SB 224 C Acrylic Windsheild/Window glass FAA, U.S AD 2003-17-04 FINNISH AD M 30-apr-98 C 09-sep-10 Insp. UHB 3076 JCAB AD TCD-4311-95 LFV LVD2678 MITSUBISHI SB 225 Forward fitting bult of wingtip tank FAA, U.S AD 98-20-39 FINNISH AD M 29-sep-95 30-jan-97 LVD 2688 2351/96 JCAB AD TCD-4310-96 LFV LVD2688 MITSUBISHI SB 226 E Auto-Ignition System Installation FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S 18-sep-01 E 22-nov-01 PCW no further action (rev.E) required due to s/n. LVD 2761 (2113), AD TCD-2679A-97 AD 86-26-02 FINNISH AD M 2435/97 FINNISH AD M 2786/00 JCAB AD TCD- 2679A-97 LFV LVD2761 MAI SB 086/74- 002 Rev A MITSUBISHI SB 227 Rudder Torque Tube Modification 20 -dec -96 21 -apr -98 MITSUBISHI SB 228 Elevator Trim Indicator FAA, U.S AD 2007 -17 -09 FINNISH AD M 13 -jul -98 08 -dec -98 Modification LFV 2898 2581/98 , LFV LVD2898 MITSUBISHI SB 229 Feathering Valve/Linkage Insp. FAA, U.S AD 2006 -15 -07 JCAB AD TCD - 20 -feb -96 30 -jul -96 4379-96 LFV LVD2689 MITSUBISHI SB 230 Mod.of Bearing Box Ldg. Gear Act. JCAB AD TCD -4684 -97 LFV LVD2819 05 -mar -97 21 -apr -98 LVD 2819 MITSUBISHI SB 231 B Inst.of Trim -In -Motion Alert System FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH AD 11 -dec -02 B 03 -mar -03 SL079 performed earlier. M 2460/97 UPPHÄVD FINNISH AD M 2786/00 JCAB AD TCD-4625A-2001 LFV LVD3122 MAI SB 093/22-009 NYGE TDM01-45 MITSUBISHI SB 232 A De -Ice System Modification LVD FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH AD 06 -jun -02 A 06 -jun -02 N/C due to previuosly complied with SB 232 rev 0. 2800, TCD-4626-97 M 2786/00 JCAB AD TCD-4626-97 LFV LVD2800 MAI SB 096/30-004 MITSUBISHI SB 233 B Insp.of Engine Torque Indication FAA, U.S AD 2006-17-01 FINNISH AD M 08-mar-07 B 18-apr-07 Checked, previously carried out System. TCD-4889-98, LFV 2924 2608/98 JCAB AD TCD-4889-2-2007 JCAB AD TCD-4889-98 LFV LVD2924 MITSUBISHI SB 234 Fl.Check of the Flight Idle Fuel Flow FAA, U.S AD 2006-17-05 JCAB AD TCD- 07-Oct- 13-Oct- Se TCD-4890-98, LVD 2925 4890-98 LFV LVD2925 1998 2010 MITSUBISHI SB 235 Inspection of landing gear power JCAB AD TCD-4838-98 LFV LVD2897 04-aug-98 24-mar-09 N/A by model train MITSUBISHI SB 236 Inspection of Tip Tank Brackets JCAB AD TCD-5747-2001 LFV LVD3166 28-aug-01 08-Oct- 2001 MITSUBISHI SB 237 Inspection of Flap Drive Train JCAB AD TCD-5864-2001 LFV LVD3212 13-dec-01 17-jan-02 MITSUBISHI SB 238 Main Landing Gear Door Safety Pin 05 -dec -02 09 -jan -03 Perf. at each 600 h. insp.

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 143(195) MITSUBISHI SB 239 Pneumatic Line Insp. and JCAB AD TCD-6127-2003 LFV LVD3322 26-dec-02 09-Oct- Modification 2003 MITSUBISHI SB 240 Inst.of Trottle Quadrant Placard 26-feb-03 09-Oct- 2003 MITSUBISHI SB 241 A Inspection of Wing Attachment FAA, U.S AD 2006-13-15 JCAB AD TCD- 21-nov-06 A 17-jan-07 c/o in conjunction with wingstudie Hardware 7030 -2006 MITSUBISHI SL 060 System 17-feb-89 16-Oct- 1991 MITSUBISHI SL 078 Automatic Autopilot Disconnect 28 -jan -02 09 -sep -10 System MITSUBISHI SL 079 Diode inst.in Flap Position 28 -jan -02 23 -nov -01 Ind.Curcuit MITSUBISHI SL 080 Hartzell Propeller Mounting Bolt HARTZELL SB 61 -256 05 -apr -02 26 -aug -02 Compliance in according to HC -SB -61 -256. Insp. MITSUBISHI SL 084 Pneumatic De -Ice Monitoring 14 -jun -04 09 -sep -10 System MITSUBISHI SL 085 Hartzell prop. mount. bolt insp. HARTZELL SB 61 -279 ALERT Rev 4 17 -May - 17 -sep -08 L/H side 2005 MITSUBISHI SN 053 B Rudder Torque Tube AD 86 -20 -01, 05 -nov -86 B 30 -jun -87 SB 020/34 -005 MITSUBISHI SN 117 D Icing Awareness Training Video FAA, U.S AD 2003 -22 -07 Rev 1 JCAB AD 14 -jun -04 D 17 -May - TCD -4753 -98 LFV LVD2922 2004 MITSUBISHI SN 146 Water Ingress into Vertical 19 -dec -03 26 -apr -04 Stabilizer MITSUBISHI SN 148 Reminders for safe operation 18 -nov -05 22 -mar -06 Genomförs enl. AMP MU -2 & DHB MITSUBISHI SN Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered 156A MITSUBISHI SN 157 Torque Indicating System Shift 20-nov-08 11-mar-09 SB 233 considered Potential MITSUBISHI SN 161 Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09-dec-09 11-mar-10 Ref STC SA01913SE MITSUBISHI SN 164 IR Part 2, one time inspection of 25 -Jun -12 part 2 mechanical stop bearing MITSUBISHI SR Modifiering av pitotrör FAA, U.S AD 86 -20 -01 JCAB AD TCD - 23 -Oct - 06 -Oct - 053A 2450A-87 LFV LVD2015 Rev B MAI SR 1984 1986 020/34-005 MITSUBISHI SB 223 MITSUBISHI SR 064 Pitot & Static System MITSUBISHI SB 223 30 -apr -85 21 -jan -00 MITSUBISHI SR 065 Warning Horn 20 -jan -86 06 -May - 1988

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 144(195) MITSUBISHI SR 067 Emergency Exit Placard 17-sep-85 15-apr-86 MITSUBISHI SR 072 Air Filter Replacement for Vacuum 25 -apr -00 29 -apr -04 Syst. MITSUBISHI SR 075 Inst. tip tank placard 29 -Oct - 06 -apr -05 2004 MITSUBISHI STC Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10 -dec -09 11 -mar -10 See MU -2B AMP Chpt 3 100h/1y inspection SA01913SE

NARCO, Narco NARCO SB ELT10 -16 ELT ASSY 18 -apr -88 16 -Oct - N/A 1991

NYGE, Saab Aerotech Aircraft Services NYGE TDM 00 -20 Fågelkollisionskada 07 -Dec - 11 -dec -00 2000 NYGE TDM 00 -23 Wiring Left Wing ADRIAN 22 -dec -00 06 -jul -00 NYGE TDM 01-45 Installation of Trim-In-Motion Alert JCAB AD TCD-4625A-2001 LFV LVD3122 07-May- 23-nov-01 Syst. and Automatic A/P Disconnect MITSUBISHI SB 231 Rev B 2001 syst. NYGE TDM 01 -61 Installation Ceis ELT 10 -dec -01 08 -jan -02 NYGE TDM 02 -10 Installation of TPE331 -6-252M 25 -mar -02 29 -apr -04 Engines NYGE TDM 02 -24 Installation Moving MAP 10 -Oct - 31 -Oct - 2002 2002 NYGE TDM 02 -32 Installation EMI film 10 -dec -02 10 -jan -04 NYGE TDM 02 -33 Viktminskning MU -2B 24 -dec -02 09 -aug -01 NYGE TDM 03-08 8 GNS430/530 & MODE S GTX330 04-mar-03 31-Oct- install. 2008 NYGE TDM 03-11 C Astor 2 MU-2B 19-mar-03 C 04-mar-03 Original compliance was as per TDM rev A.The A/C installation is IAW rev C as not affected by rev B and C.F01324, F01341, F01342 NYGE TDM 03-15 A U95 with General Control System 24-apr-03 A 25-feb-08 NYGE TDM 03 -28 F Nav Demo Pod 19 -dec -03 F 30 -aug -05 Original compliance with previous revision not affected by rev F.F01211, M03323,R01395

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 145(195) NYGE TDM 05-03 Marcus "Installation" 16-feb-05 02-feb-06 NYGE TDM 05 -04 ADL Installation 16 -feb -05 NYGE TDM 05 -16 Viktor Counter Weight Pod 18 -nov -05 18 -nov -05 NYGE TDM 06 -28 A Removable FR -31 29 -jun -07 A 29 -nov -07 NYGE TDM 06-41 A Darts (to carry on MU-2B-20/26) 20-nov-06 A 07-feb-08 NYGE TDM 06 -42 A Barlast DARTS MU -2B 04 -dec -07 A 07 -feb -08 NYGE TDM 07 -30 A Install. of Emergency Axe 28 -feb -08 A 28 -feb -08 NYGE TDM 08 -03 A Enhanced Surveillance MU -2B 28 -feb -08 A 28 -aug -09 NYGE TDM 08-28 B ELT 406 MU-2B 29-sep-08 B 31-Oct- Original compliance with TDM rev A. Rev B does 2008 not affect previous complaiance. NYGE TDM 09-29 A GPS Splitter 12-Oct- A 10-feb-10 2009 NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr-10 A 18-May- C/W 2010 NYGE TDM 11-16 19" instrumentrack 04-Oct- 2012 NYGE TDM 11-35 A Terminating resistor 27-Jan-12 NYGE TDM 12-21 A Avinstallation IK 29-Jun-12 NYGE TDM 95 -04 4 Vingstudie 20 -sep -98 4 26 -apr -04 NYGE TDM 97 -03 Astor MU -2 25 -feb -97 23 -apr -97 NYGE TDM 98 -08 Torrluft ASTOR 27 -May - 23 -jul -98 1998 NYGE TDM 99 -03 Install. Auto Ignition 03 -mar -99 15 -jun -99 NYGE TVO 1/09 Inspektion av Stringers & struktur 25 -feb -09 08 -apr -09 Inspected with remarks vinge NYGE TVO 1/93 Low Volt Warning Light (BCL) 22-jan-93 26-May- 1993 NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-96 26-jun-00 NYGE TVO 1/97 3 De -Icertank MU -2B, 12 -feb -97 14 -May - korrosionskontroll 1997 NYGE TVO 2/00 Märkning av infästning domkraft 01 -dec -00 04 -apr -01 Mu2

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 146(195) NYGE TVO 2/07 A Prevent FR31 radio to xmit when 06-feb-07 A 02-mar-07 RM2 off NYGE TVO 2/91 A/C Elecrical System 10-jan-91 13-mar-92 NYGE TVO 3/06 Inspect lower rudder hinge bracket 07 -dec -06 09 -sep -10 NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24 -feb -05 3 28 -aug -09 NYGE TVO 4/11 Static inverter controll A 15 -Dec -11 NYGE TVO 4/86 2 Wing Pod Inspection 06-apr-92 2 09-sep-10 NYGE TVO 4/91 Special Inspection (next E6.) 19 -feb -91 16 -Oct - 1991 NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29 -apr -92 14 -Oct - 1992 NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28 -sep -94 3 09 -sep -10 R/H NYGE TVO 4/96 Kontroll av Lagerhus i 25 -Oct - 20 -mar -97 noshjulsstyrning. 1996 NYGE TVO 4/99 Kontroll av rullbälten 09 -apr -99 15 -apr -99 NYGE TVO 6/88 Allm. instruktion för 13 -jun -88 15 -sep -08 metallpropeller NYGE TVO 6/92 Elevator Trim Cable, check 07 -Oct - 20 -nov -92 1992 NYGE TVO 7/93 Starter Drive Splines 01 -nov -93 15 -mar -94 NYGE TVO 8/04 Kontr. av Spant vid bakre 08 -dec -04 09 -sep -10 feninfästning NYGE TVO 8/92 Wheel Parts 27 -Oct - 02 -apr -93 1992 NYGE TVO 9/88 Emergency Extension System 08 -aug -88 03 -nov -88

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 147(195)

2.6 GFE Aircraft Mitsubishi MU-2 SE-IOV

2.6.1 Aircraft Specification Type: Serial Registration : Airframe Total Date Number: total Hours: Landing Reference: Cycles: MU-2B-26 337 SE-IOV 11473 4130 2012-11-23

2.6.2 Engines Type: Honeywell TPE331 -6-252M Serial Total Hours Total Hours remaining Number: Since New: Cycles overhaul/HSI/GBI: Since New: Left Engine P20067 11697 10203 1598/1428/3228 Right Engine P20376 10279 10813 2884/1161/1084

2.6.3 Propeller Type Number: Serial Number: Overhaul Due Date: Left Propeller HC-B3TN-5E BUA 19597 2013-11-25 Right Propeller HC-B3TN-5E BVA 6186 2013-01-07

2.6.4 Avionics System: Type / Part Number: Note: Autopilot & Flight Director Bendix M4D COM/NAV/GPS 1 & 2 Garmin GNS 430 Audiopanel Bendix/King KMA-24H-70 MKR Bendix/King KMR 675 DME Bendix/King KN 63 ADF Bendix/King KR 87 XPDR 1 Garmin GTX 330D XPDR 2 Garmin GTX 330 *) RDR ALT Bendix/King KRA-10A ELT Kanad ELT 406-AF-H Airspeed Indicator LH / RH Aerosonic 30040-0186 / 30040- 0186 Altimeter LH United Instr. Inc. 5934 PAM-3 Altimeter incl. encoder RH United Instr. Inc. 5035P -P40 Altitude Reporter Ameri -King AK -350 Altitude Alerter Century 1D960 Vertical Speed Indicator LH Aerosonic RC-60-MS-10-3 Attitude Gyro & Flight Director Ind. Bendix GH-14

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 148(195) LH Attitude Gyro Ind. RH AIM 504-0006-914 Turn & Bank Ind. LH Bendix 4099-B Horizontal Situation Indicator LH Bendix RD-44 DG -Gyro Sperry C-14A RMI Indicator Collins 332C -10 RMI/ADF adapter Bendix/King KDA-692 CDI Indicator Garmin GI-106A *) XPDR 2 without diversity configuration

2.6.5 Mission System System : Description: Fixed general installations VHF/UHF COM FR31 GPS MAP JET SI-3003B Inverter 115/200VAC 400Hz 3 phase Laser Prism MIL -STD -1553 Bus LH Wing Pylon Wing Pylon NATO 14” Alcon Ejector Unit LH and RH Wing Pylon EW system ADRIAN Pod mounted system LH and RH Wing Pylon U95 Sorc Pod mounted system RH Wing Pylon A100 Pod mounted system LH Wing Pylon Missile Threat Simulator DARTS Pod mounted system LH Wing Pylon Chaff Dispenser BOX 3 Pod mounted system LH and RH Wing Pylon Target Towing MBV7S Inboard winch AS200 MDI (Miss Distance Indicator) Precisions GPS Pos System TAPS Radar Calibration System GPS Sphere

2.6.6 Mission Cable Harness to Hard Points Used for Mission LH NATO Hard point: RH NATO Hard point: Note: System: Adrian C & S, U95 Sorc, General Signal Harness General Signal Harness A100, DARTS and BOX 3 AWG22 shielded x 44 AWG22 shielded x 50 U95-Sorc and A100 MIL-STD-1553B Data Triax Cable x 1

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 149(195) Bus U95 Sorc, A100 and DARTS AC Power AWG 16 x 4 115/200VAC 400 Hz 3- twisted Phase 3 x 10 A AWG 16 x 2 AWG 20 x 2 Adrian C & S and BOX 3 DC Power 28 VDC 200 DC Power 28 VDC 200 AWG 2 x 2 A A Adrian C & S Coax Cable 1 x 50 Ω Coax Cable 1 x 50 Ω U95 Sorc Ethernet LAN Cable

2.6.7 Antenna Layout

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 150(195)

2.6.8 Inspection due times and dates Status date November 23 rd 2012.

Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date Aircraft SE-IOV Vingstudie MU-2 AMP 2010-10-08 11219 12250 100 Hour Inspection AMP 2012-03-01 11399 11499 2013-03-01 200 Hour Inspection AMP 2012-03-01 11399 11599 2013-03-20 600 Hour Inspection AMP 2011-01-31 11230 11830,1 2014-02-17 1000 Hour Inspection AMP 2011-01-19 1230 12250 1200 Hour Inspection AMP 2008-01-14 10835 12035 1800 Hour Inspection AMP 2005-01-03 10250 12050 2000 Hour Inspection AMP 2005-01-03 9650 11650 1 Year Inspection AMP 2012-03-02 11399 2013-03-20 2 Year Inspection AMP 2012-01-24 11384 2014-01-25 10 Year Inspection AMP 2005-01-04 10250 2015-01-02 Engine S/N P-20067 Remaining Engine Assembly (Overhaul) AMP 13072 1598,7 Engine Hot Section Inspection AMP 12901,9 1428,6 Engine Gearbox Inspection AMP 14701,9 3228,6 Engine S/N P-20376 Engine Assembly (Overhaul) AMP 14357,5 2884,2 Engine Hot Section Inspection AMP 12634,7 1161,4 Engine Gearbox Inspection AMP 12557,5 1084,2

Propeller L/H O/H AMP 2008-11-26 14361,5 2013-11-25 Propeller R/H O/H AMP 2008-01-09 13834,7 2013-01-07

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type

2012-12-06

Document number Page 151(195)

2.6.9 Implemented Changes Status date November 23 rd 2012. SB/AD etc Rev Subject Document reference Eff. date Rev Compliance Stat Remarks Reference us

EASA, European Aviation Safety Agency EASA AD 2006 - Incorrect transponder altitude 30 -aug -06 11 -feb -10 0265 EASA AD 2009 - Portable Fire Extinguishers -Ident/Repl 25 -nov -09 07 -May -2010 N/A N/A by current P/N installed 0251-E EASA AD 2009 - Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009 -0278 FFE ASB26 -115 Rev C 15 -dec -09 07 -May -2010 N/A N/A by current P/N installed 0262 EASA AD 2009 - Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009 -0262 22 -dec -09 07 -May -2010 N/A N/A by current P/N installed 0278 EASA AD 2010 - R1 Mode S Transponder - 11 -jan -10 R1 10 -mar -10 N/A due to model 0003 Check/Modification EASA AD 2012 - KIDDE GRAVINER HAND OPERATTED 06 -Sep -12 0037 FIRE EXTINGUISHER EASA SIB 2008- Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN 17-dec-08 21-sep-10 N/A by SSB 0844 incorporated 58R1 SSB0845 Rev IR EASA SIB 2009-14 Upgrade to main unit/GPS software 24-jun-09 28-sep-09 N/A due to model

FAA, U.S, Federal Aviation Administration FAA, U.S AD 2000 - AFM De -icing 25 -jan -00 26 -apr -00 N/A Due to paragraph b. 02 -25 FAA, U.S AD 2000 - 1 Flight in Icing Condition FINNISH AD M 2435/97 FINNISH AD M 07 -jul -00 22 -nov -01 Action not required due to s/n. 09-15 2786/00 MAI SB 086/74-002 Rev A MAI SB 093/22-009 MAI SB 096/30-004 MITSUBISHI SB 226 Rev E MITSUBISHI SB 231 Rev B MITSUBISHI SB 232 Rev A FAA, U.S AD 2003 - Windshield check FINNISH AD M 3076 LFV LVD2678 MAI SB 01 -Oct - 08 -mar -11 17-04 087/56-001 Rev B MITSUBISHI SB 224 Rev 2003 C

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 152(195) FAA, U.S AD 2003- 1 Forecast Icing Conditions FINNISH AD T5007/03 JCAB AD TCD- 16-apr-04 17-May-2004 inserted in AFM limitations 22-07 4753A-2004 MAI SN 071/00-006 Rev D MITSUBISHI SN 117 Rev D FAA, U.S AD 2005- Prop. mounting bolt insp. HARTZELL SB 61-279 ALERT Rev 4 29-jul-05 20-sep-05 14-12 FAA, U.S AD 2005- Prop de-icer "FASTprop" 14-Oct- 12-Oct-2005 N/A Due to boots p/n 18-20 2005 FAA, U.S AD 2006- Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB 11-aug-06 23-feb-04 c/o in conjunction with vingstudie 13-15 241 Rev A FAA, U.S AD 2006- Safety evaluation (feathering linkage) MAI SB 090/76-003 MITSUBISHI SB 229 24-aug-06 24-aug-06 se Mitsubishi SB 229 15-07 FAA, U.S AD 2006- Detect & correct torque transducers MAI SB 095/77-002 MITSUBISHI SB 233 22-sep-06 21-sep-06 PCW see MSB 233A 17-01 Rev B FAA, U.S AD 2006- Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep-06 11-feb-10 17-05 FAA, U.S AD 2007- Reduce max deflect elev nose-down MITSUBISHI SB 216 MITSUBISHI SB 228 25-sep-07 11-sep-07 Previously carried out i.a.w. mentioned SB's. 17-09 trim FAA, U.S AD 71- Fuel Tank Fungus Coating Peeling 01-May- 01-jan-96 N/A N/A by s/n 14-01 1972 FAA, U.S AD 75- Cracks and Optical Distortion LFV LVA829 Rev A 13-nov-74 21-aug-85 N/A N/A due to s/n. 03-06 FAA, U.S AD 75- Main Wing Flap JCAB AD TCD-1094A-76 LFV LVA1011 Rev 05-aug-75 05-feb-02 N/A Ej tillämplig p.g.a. s/n. 16-13 A MITSUBISHI SB 167 Rev D FAA, U.S AD 75 - Propeller Pitch Control Lever JCAB AD TCD -1188 -75 LFV LVA1012 12 -aug -75 21 -aug -85 16-20 MITSUBISHI SB 168 Rev A FAA, U.S AD 78 - Cowling Latches JCAB AD TCD -1202 -75 LFV LVA1014 Rev A 23 -feb -78 21 -aug -85 03-05 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A FAA, U.S AD 81- 1 Engine Aft Nacelles 01-apr-81 1 27-jan-86 Previously complied with 06-01 FAA, U.S AD 82- Electrical Wiring Inspection 15-apr-82 27-aug-87 08-02 FAA, U.S AD 83- 2 To preclude prop. attach bolt failures FINNISH AD M 1168/83 Rev 1 FINNISH AD 28-apr-82 2 20-May-2005 Ref. MU2B MM chap 13.4 when using bolts P/N 08-01 T5114/05 HARTZELL SI 140A Rev 9 B-3339 only FAA, U.S AD 84- Torque of Air Tube Coupling Nuts SB MAI SB 047/30-001 Rev A MITSUBISHI SB 28-jun-84 27-jan-86 12-04 047/30-001, SB 196A 196 Rev A FAA, U.S AD 84- Elevator TrimTab Bracket Insp/Repl. MAI SB 031/27-005 Rev 1 MITSUBISHI SB 18-dec-84 21-aug-85 25-02 SB 031/27-005 R1, SB 176E 176 Rev E FAA, U.S AD 86 - NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2 13 -aug -86 15 -jul -04 Found SB 181 part 2 PCW. 15-03 Rev B

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 153(195) FAA, U.S AD 86- To assure anti-ice capability of pitot LFV LVD2015 Rev B MAI SR 020/34-005 06-Oct- 27-mar-00 20-01 SB 020/34-005, SB 053A MITSUBISHI SR 053A 1986 FAA, U.S AD 86- To prevent engine flameout in an GARRETT SB 74-0003 Rev 6 31-dec-87 09-mar-09 see applicable engine for c/o 26-02 iceing SB 74-0003, SR 040/74-001 FAA, U.S AD 87- Addit. Seal and Flap Flexible Shaft MAI SB 051/27-007 MITSUBISHI SB 198 07-mar-87 27-aug-84 04 -03 Insp SB 051/27 -007, SB 198 FAA, U.S AD 87- Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03-jul-87 27-mar-09 N/A by s/n 12-02 FAA, U.S AD 88 - Bendix Autopilot Disengagement SB LFV LVD2190 MAI SB 066/22 -006 Rev A 11 -jul -98 25 -jul -89 13-01 066/22-006 MITSUBISHI SB 206 FAA, U.S AD 88 - 1 To minimize confusion in LFV LVD2206 MAI SB 066/22 -006 Rev A 28 -jan -89 1 25 -Jan -12 21-01 autopilot/manua SB 066/22-006 FAA, U.S AD 88 - To prevent flap control failure SB LFV LVD2202 MAI SB 067/27 -008 Rev A 04 -dec -88 11 -mar -96 23-01 067/27-008, SB 189B FAA, U.S AD 93 - ELECTRIC TRIM SYSTEM SB 079/27 - LFV LVD2477 MAI SB 079/27 -010 01 -jun -93 27 -mar -09 N/A by s/n 07-11 010 FAA, U.S AD 94 - Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11 -apr -94 07 -May -1993 04 -16 FAA, U.S AD 94 - Change of Flight Idle Blade Angel SB LFV LVD2551 MAI SB 016/71 -001 10 -jun -94 27 -mar -09 N/A by s/n 11 -04 016/61 -001 FAA, U.S AD 96 - Inspection / Replacement of Prop FINNISH AD M 2404/96 Rev 1 HARTZELL 16 -Oct - 01 -sep -99 Prop utbytt mot S/N BVA -series 18 -14 Hub. LVD 2732, Hx SB 136G SB 61 -261 Rev 1 LFV LVD2732 1996 FAA, U.S AD 96 - Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD - 27 -dec -96 11 -mar -02 25-02 4552-96 LFV LVD2749 FAA, U.S AD 97 - Vent Check Valve Assy LFV LVD2769 16 -apr -97 05 -May -1997 N/A N/A due to model. 04-13 FAA, U.S AD 97 - Icing related incidents/accidents 17 -Oct - 02 -dec -98 20-14 CNL 1997 FAA, U.S AD 97 - To prevent loss of airplane FINNISH AD M 2524/98 21 -jan -98 03 -dec -10 N/A AD superseeded by AD 2010 -10 -17 25-02 ctrl/overspe FAA, U.S AD 98 - Forward fitting bolt of wingtip tank SB LFV LVD2688 , MITSUBISHI SB 225 19 -Oct - 04 -dec -96 20-39 MU-2 225, 089/57-002A 1998

FINNISH, Finnish Civil Aviation Adm FINNISH AD M Kontroll av vindrutor och fönster FAA, U.S AD 2003-17-04 , MAI SB 21-aug-03 08-mar-11 3076 087/56-001 Rev B , MITSUBISHI SB 224 Rev C

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 154(195)

GARMIN, Garmin GARMIN SB 0004 Incorp.of Main Software Version 2.16 01 -May - 18 -May -2000 2000 GARMIN SSB IR Software Version 5.04 EASA SIB2008 -58R1 14 -nov -08 A 24 -May -2010 0844

GARRETT, AlliedSignal Aerospace GARRETT SB 74 - 6 Replace Ignition Unit AD 74 -0003 FAA, U.S AD 86 -26 -02 25 -mar -94 09 -mar -09 see applicable engine for c/o 0003

HARTZELL, Hartzell Propeller Inc. HARTZELL SB 61 - Propeller mounting bolt inspection MITSUBISHI SL 053/72 -003, MITSUBISHI 08 -feb -02 24 -apr -02 R/H side 256 SL 080 HARTZELL SB 61- 4 Prop. mounting bolt insp. FAA, U.S AD 2005-14-12 , MITSUBISHI SL 04-Oct- 14-nov-05 propellerbolts previously checked u/a 279 ALERT 085 2005 HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2 , LFV 30-mar-05 9 13-mar-08 see previously revision LVA1424 Rev A

JCAB, Japan Civil Aviation Bureau JCAB AD TCD - Rivet holes elevator hinge fitting 06 -feb -68 26 -mar -09 N/A by s/n 0518-68 JCAB AD TCD - AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07 -feb -70 21 -aug -85 N/A by s/n 0642-70 JCAB AD TCD - Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07 -feb -70 15 -jul -04 N/A N/A by s/n. 0643-70 JCAB AD TCD - Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25 -mar -70 26 -mar -09 N/A by model 0652-70 JCAB AD TCD - Engine Nacelle Tail Area -Modification of 25 -mar -70 26 -mar -09 N/A by model 0653-70 JCAB AD TCD - Replacement of bearing in LFV LVA457 MITSUBISHI SB 123 01 -May - 26 -mar -09 N/A by s/n 0660-70 nosegearstrut 1970

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 155(195) JCAB AD TCD- Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 25-mar-72 14-jul-04 N/A N/A by s/n. 0730-1-72 Rev B JCAB AD TCD- Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10-dec-86 26-mar-09 N/A by s/n 0730-2-86 JCAB AD TCD- Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04-sep-72 10-sep-72 N/A N/A due to model. 0859 -72 JCAB AD TCD- NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09-Oct- 31-dec-72 N/A N/A due to model. 0866-72 1972 JCAB AD TCD - Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 12 -nov -74 27 -jan -86 N/A N/A due to s/n. 0947A-74 Rev A JCAB AD TCD - Inspection of Windshields MITSUBISHI SB 163 Rev B 22 -dec -78 26 -mar -09 N/A by s/n 0948A-1-78 JCAB AD TCD - Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 07 -Oct - 21 -aug -85 N/A N/A due to s/n. 0948A-74 Rev B 1974 JCAB AD TCD - Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 06 -Oct - 27 -aug -84 1001A-76 Rev E 1976 JCAB AD TCD - Replacement of Elevator Trim Tab FINNISH AD M 1080/82 LFV LVD1971 12 -dec -84 21 -aug -85 1001B -2-84 Bracket MITSUBISHI SB 176 Rev E JCAB AD TCD - Insp. of wingflap controlsystem FAA, U.S AD 75 -16 -13 LFV LVA1011 Rev 06 -sep -76 05 -feb -02 N/A Ej tillämplig p.g.a. s/n. 1094A -76 A MITSUBISHI SB 167 Rev D JCAB AD TCD - Insp. of propeller controllever inst. FAA, U.S AD 75 -16 -20 LFV LVA1012 06 -May - 21 -aug -85 1188 -75 MITSUBISHI SB 168 Rev A 1975 JCAB AD TCD - Engine Cowling Latches FAA, U.S AD 78 -03 -05 LFV LVA1014 Rev 20 -sep -75 15 -jul -04 Found SB 171 and SB 180 PCW. 1202-75 A MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A JCAB AD TCD - Insp/mod of NLG shimmydamper LFV LVA1013 MITSUBISHI SB 169 Rev B 16 -jun -75 27 -jan -86 1209-75 locking JCAB AD TCD - Insp./repl. of MLG fwd door LFV LVA1083 MITSUBISHI SB 170 Rev A 19 -sep -75 21 -aug -85 N/A N/A due to model. 1235 -75 emerg.cables JCAB AD TCD - Supp.,MLG Forward D. Actuating MITSUBISHI SB 172 14 -nov -75 26 -mar -09 N/A by model 1272 -75 Mech. -I&M JCAB AD TCD - Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31 -mar -76 09 -nov -09 PCW Carried out ref SB 173, date 1985/08/21 1284 -1-76 JCAB AD TCD - Fire hazard in rear baggage 01 -jul -76 26 -mar -09 N/A by s/n 1328 -76 compartment JCAB AD TCD - Barrel Nut, Inner/Outer Wing Conn. - MITSUBISHI SB 175 16 -aug -76 26 -mar -09 1353 -76 Repl. JCAB AD TCD - Inspect strobelight conduit in Tiptank LFV LVA1196 18 -Oct - 27 -jan -86 N/A by s/n 1370-76 1976

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 156(195) JCAB AD TCD- Inspect strobelight conduit in Tiptank MITSUBISHI SB 174 PART 1 Rev C 05-nov-81 24-mar-09 N/A by s/n 1370A-81 supersed TCD-1370-76 JCAB AD TCD- Insp. rear eng. cowling reg. heatdamage LFV LVA1197 Rev A MITSUBISHI SB 177 06-feb-02 27-jan-86 1379-1-80 Rev B JCAB AD TCD- Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12-dec-77 24-mar-09 ref. SB 180 1520A -77 JCAB AD TCD- Fatigue failure of the NLG strut assy. LFV LVA1546 MITSUBISHI SB 181 PART 2 12-jul-85 15-jul-04 PCW Found SB 181 part 2 PCW. 1768-1-85 Rev B JCAB AD TCD - Modification of bagagecompartment LFV LVA1583 MITSUBISHI SB 182 05 -feb -02 27 -May -1986 N/A N/A due to s/n. 1817-79 JCAB AD TCD - Insp. firewarning & emerg.power circuit LFV LVA1740 MITSUBISHI SB 187 Rev B 05 -feb -02 27 -May -1981 N/A N/A due to s/n. 2048-81 JCAB AD TCD - Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05 -feb -02 27 -aug -84 2070-81 JCAB AD TCD - Insp./replace engine electrical harness LFV LVA1788 MITSUBISHI SB 191 06 -feb -02 27 -aug -84 2113-82 JCAB AD TCD - Flap system torquetubes supersed TCD - 01 -feb -89 24 -mar -09 PCW 2252 -2-88 2252 -1-87 JCAB AD TCD - Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04 -feb -83 11 -mar -96 2252 -83 JCAB AD TCD - NLG. bracket attaching to drag strut 13 -aug -83 24 -mar -09 N/A by model 2263 -83 JCAB AD TCD - Engine inlet anti -ice tubing. Torq./lock MITSUBISHI SB 196 Rev A 05 -jun -84 10 -mar -09 PCW 2342-1-84 JCAB AD TCD - Engine inlet anti -ice tubing. Torq./lock LFV LVA1942 MITSUBISHI SB 196 Rev A 06 -feb -02 27 -jan -86 2342-84 JCAB AD TCD - Pitot Tube Wiring LFV LVD2015 Rev B MITSUBISHI SR 053A 16 -jun -87 15 -jul -04 SB PCW. 2450A-87 JCAB AD TCD - Add. seal/Tq. insp of flap flex. shaft 01 -May - 09 -mar -09 PCW see TCD -2451 -85 2451-1-87 1987 JCAB AD TCD - Add. seal/Tq. insp of flap flex. shaft LFV LVD2037 MITSUBISHI SB 198 30 -sep -85 27 -aug -84 2451-85 Superseeded by TCD-2451-1-87 JCAB AD TCD - Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01 -jul -88 24 -mar -09 N/A by s/n 2545-1-88 JCAB AD TCD - Auto -ignition System FINNISH AD M 2435/97 LFV LVD2761 01 -feb -97 22 -nov -01 2679A-97 JCAB AD TCD - Bendix M4C Autopilot System MITSUBISHI SB 206 05 -nov -97 06 -nov -09 N/A Due to model 2856-1-97 JCAB AD TCD - Insp./mod. of rudder trimtab LFV LVD2338 MITSUBISHI SB 211 28 -mar -91 14 -jul -04 N/A N/A by s/n. 3378-90 leadingedge

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 157(195) JCAB AD TCD- Anti ice/De-ice system FINNISH AD M 2364/96 LFV LVD2347 25-May- 11-feb-10 3393A-96 Rev 1 MITSUBISHI SB 212 Rev A 1996 JCAB AD TCD- Unintentional engagement of A/P...... 17-jun-91 24-mar-09 N/A by model 3464-91 JCAB AD TCD- Mod.of Autopilote pitchtrimsystem FINNISH AD M 2581/98 LFV LVD2450 17-aug-98 09-nov-98 3740A-98 MSB 216, 228 LVD 2898 LFV LVD2898 MITSUBISHI SB 216 MITSUBISHI SB 228 JCAB AD TCD- Tiptank inst FINNISH AD M 2110/93 LFV LVD2512 10-sep-93 25-apr-94 3901-93 MITSUBISHI SB 221 JCAB AD TCD- Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592 28-nov-94 27-mar-95 3942-1-94 MITSUBISHI SB 219 Rev A JCAB AD TCD- Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01-feb-94 27-mar-95 3942-94 JCAB AD TCD- Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688 01-apr-96 04-dec-96 4310-96 MITSUBISHI SB 225 JCAB AD TCD- Windshield/window insp. FINNISH AD M 2331/96 LFV LVD2678 01-nov-95 08-mar-11 4311-95 MITSUBISHI SB 224 Rev C JCAB AD TCD- Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689 01-apr-96 30-jul-96 4379-96 MITSUBISHI SB 229 JCAB AD TCD- Icing Limitation FAA, U.S AD 96-25-02 LFV LVD2749 27-dec-96 11-mar-02 4552-96 JCAB AD TCD- Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI 14-jul-97 15-May-2001 4625-97 SB 093/22-009 JCAB AD TCD - Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B 16 -mar -01 13 -mar -09 PCW 4625A-2001 NYGE TDM01-45 JCAB AD TCD - De -ice system Modification FINNISH AD M 2461/97 LFV LVD2800 01 -May - 14 -jul -04 PCW 4626-97 MITSUBISHI SB 232 Rev A 1997 JCAB AD TCD - Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819 01 -jun -97 25 -mar -99 4684 -97 MITSUBISHI SB 230 JCAB AD TCD - Ändring av flyghandbok LVD 2922,FAA FINNISH AD M 2518/98 LFV LVD2922 18 -feb -98 02 -dec -98 FAA AD utförd. 4753 -98 AD 97 -20 -14, MHI SN 117A MITSUBISHI SN 117 Rev D JCAB AD TCD - Icing -related incidents VIDEO FAA, U.S AD 2003 -22 -07 Rev 1 24 -feb -04 17 -May -2004 inserted in AFM limitations 4753A -2004 JCAB AD TCD - Inspection of landing gear power train FINNISH AD M 2574/98 LFV LVD2897 04 -aug -98 24 -mar -09 N/A by model 4838 -98 MITSUBISHI SB 235 JCAB AD TCD - Inappropriate calib. of eng. trq -meter MITSUBISHI SB 233 Rev B 21 -jun -07 11 -sep -07 Previously carried out, ref. SB 233A. 4889 -2-2007 JCAB AD TCD - Insp. of Engine Torque Indication FINNISH AD M 2608/98 LFV LVD2924 05 -nov -98 14 -jul -04 PCW 4889-98 System LFV 2924, MU SB 233 MITSUBISHI SB 233 Rev B

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 158(195) JCAB AD TCD- Check of flight idle FF LVD 2925, MU SB FINNISH AD M 2609/98 LFV LVD2925 04-nov-98 11-feb-10 4890-98 234 MITSUBISHI SB 234 JCAB AD TCD- Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17-May- 24-mar-09 N/A by model 5030-99 1999 JCAB AD TCD- AFM revision LFV LVD3112 27-nov-00 12-feb-02 5432 -2000 JCAB AD TCD- To prevent loss of airplane control LFV LVD3123 16-mar-01 12-feb-02 5547-2001 JCAB AD TCD - Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12 -sep -01 18 -Oct -2001 5747-2001 JCAB AD TCD - Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27 -dec -01 17 -jan -02 5864-2001 JCAB AD TCD - Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17 -mar -03 02 -Oct -2003 6127-2003 JCAB AD TCD - Inspection of Wing Attachment MITSUBISHI SB 241 Rev A 27 -dec -06 17 -jan -07 c/o in conjunction with wingstudie 7030-2006 Hardware

LFV, Luftfartsverket LFV LVA 1011 A Kontroll av vingklaffarnas FAA, U.S AD 75-16-13 JCAB AD TCD- 05-feb-02 A 05-feb-02 N/A Ej tillämplig p.g.a. s/n. manöversystem 1094A-76 MITSUBISHI SB 167 Rev D LFV LVA 1012 Kontroll av propellerreglagets FAA, U.S AD 75-16-20 JCAB AD TCD- 05-feb-02 05-feb-02 N/A Ej tillämplig p.g.a. s/n. montering 1188-75 MITSUBISHI SB 168 Rev A LFV LVA 1013 Kontr. och mod. av låsning på nosställ JCAB AD TCD-1209-75 MITSUBISHI SB 05-feb-02 27-jan-86 169 Rev B LFV LVA 1014 A Kontr. & byte av motorinkl. FAA, U.S AD 78-03-05 JCAB AD TCD- 05-feb-02 A 21-aug-85 låsanordning 1202-75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A LFV LVA 1083 Insp. & utbyte av lina för nödöppning JCAB AD TCD-1235-75 MITSUBISHI SB 05-feb-02 21-aug-85 N/A N/A due to s/n 170 Rev A LFV LVA 1196 Isolering av strobe light från bränsle JCAB AD TCD-1370-76 MITSUBISHI SB 06-feb-02 06-feb-02 N/A by s/n 174 PART 1 Rev C LFV LVA 1197 A Förhindr. av värmeskador på JCAB AD TCD-1379-1-80 MITSUBISHI SB 06-feb-02 A 27-jan-86 bak.motorpl. 177 Rev B LFV LVA 1238 Kontr. & byte av infästningsdet. trimrod 06-feb-02 21-apr-09 N/A by s/n LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86 -15 -03 JCAB AD TCD - 06 -feb -02 27 -May -1986 1768-1-85 MITSUBISHI SB 181 PART 2 Rev B

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 159(195) LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD-1817-79 MITSUBISHI SB 05-feb-02 11-feb-80 N/A N/A due to s/n. 182 LFV LVA 1740 Kontr.av brandvarnings-och JCAB AD TCD-2048-81 MITSUBISHI SB 05-feb-02 31-aug-09 N/A by s/n n"dstr"mskret 187 Rev B LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB 05-feb-02 27-aug-84 188 LFV LVA 1788 Kontroll/Utbyte av elledningar på JCAB AD TCD-2113-82 MITSUBISHI SB 06-feb-02 27-aug-84 motor 191 LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör JCAB AD TCD -2252 -83 MITSUBISHI SB 06 -feb -02 11 -mar -96 189 Rev C LFV LVA 1942 Momentdragning/låsn.av koppl.i JCAB AD TCD -2342 -84 MITSUBISHI SB 06 -feb -02 27 -jan -86 varmlufts 196 Rev A LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD -0643 -70 MITSUBISHI SB 05 -feb -02 21 -aug -85 N/A N/A by s/n 114 LFV LVA 439 Rev. av flyghandbok betr. bränslespec. JCAB AD TCD -0642 -70 MITSUBISHI SB 05 -feb -02 21 -aug -85 N/A by model 112 Rev C LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD -0652 -70 MITSUBISHI SB 05 -feb -02 26 -mar -09 N/A by model 119 LFV LVA 457 Utbyte av lager i nosst,llets st"td,mp. JCAB AD TCD -0660 -70 MITSUBISHI SB 05 -feb -02 26 -mar -09 N/A by s/n 123 LFV LVA 543 B Insp. och målning av integraltankar JCAB AD TCD -0730 -1-72 05 -feb -02 B 14 -jul -04 N/A N/A by s/n. LFV LVA 645 Modifiering av el-system JCAB AD TCD-0859-72 MITSUBISHI SB 05-feb-02 08-dec-09 N/A by A/C serial number 156 LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD-0866-72 05-feb-02 31-aug-09 N/A by s/n & model LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD -0947A -74 MITSUBISHI SB 05 -feb -02 A 27 -jan -86 N/A N/A due to s/n. 162 Rev A LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74 -11 -01 FAA, U.S AD 75 - 05 -feb -02 A 21 -aug -85 N/A N/A due to s/n. 03-06 JCAB AD TCD-0948A-74 MITSUBISHI SB 163 Rev B LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar JCAB AD TCD -1001A -76 05 -feb -02 A 27 -aug -84 LFV LVD 1238 Kontr./byte infästn.det. höjdtrimroder 15 -apr -77 31 -aug -09 N/A by s/n LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD -1001B -2-84 MITSUBISHI 18 -jan -85 27 -May -1986 SB 176 Rev E LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34 -005 FAA, U.S AD 86 -20 -01 JCAB AD TCD - 24 -May - B 21 -aug -85 Rev A, MHI SR 53 2450A-87 MAI SR 020/34-005 1985 MITSUBISHI SR 053A LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD-2451-85 MITSUBISHI SB 30-sep-85 27-May-1986

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 160(195) 198 LFV LVD 2069 Altimeter 25 -mar -86 27 -May -1986 N/A N/A by p/n & s/n LFV LVD 2113 Modif. & revision Handbook MHI SR 26 -jan -87 19 -feb -87 006B, MAI SR 040/74-001RA LFV LVD 2190 Autopilot Switch MU2 SB 066/22 -006 FAA, U.S AD 88 -13 -01 MAI SB 066/22 - 19 -aug -88 25 -jul -89 och SB 206 006 Rev A MITSUBISHI SB 206 LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD -2545 -1-88 MITSUBISHI SB 19 -aug -88 24 -mar -09 N/A by s/n 201 Rev A LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88 -23 -01 JCAB AD TCD - 08 -dec -88 11 -mar -96 2252-1-87 MAI SB 067/27-008 Rev A MITSUBISHI SB 189 Rev C LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88 -21 -01 Rev 1 08 -Dec - 12 -feb -02 1988 LFV LVD 2338 Kont./Mod.av sidorodrets JCAB AD TCD -3378 -90 MITSUBISHI SB 28 -mar -91 14 -jul -04 N/A N/A by s/n. trimroderframka Mitsubishi MHI SB 211 211 LFV LVD 2347 1 Control Deice -system Mitsubishi SB JCAB AD TCD -3393A -96 MITSUBISHI SB 29 -May - 1 11 -feb -10 212A 212 Rev A 1996 LFV LVD 2352 Shoulder Harness Inst. FAA AC 43 -13 23 -May - 14 -jun -91 checked OK. CHPT 9 1991 LFV LVD 2450 Elevator Trim Tab Installation MU SB JCAB AD TCD -3740A -98 MITSUBISHI SB 03 -dec -92 07 -May -1993 216 216 LFV LVD 2477 Electric Trim System AD930711, MU SB FAA, U.S AD 93 -07 -11 MAI SB 079/27 - 03 -jun -93 27 -mar -09 N/A by s/n 079/27-0-010 010 LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD -3901 -93 MITSUBISHI SB 02 -dec -93 25 -apr -94 221 LFV LVD 2537 Reducering av Höjdrodrets trimområde. FAA, U.S AD 94 -04 -16 MITSUBISHI SB 07 -apr -94 07 -May -1993 FAA AD 94-04-16, SB 216 216 LFV LVD 2538 Byte Låspinne i landställets nödutf. SB JCAB AD TCD -3942 -94 MITSUBISHI SB 07 -apr -94 27 -mar -95 219 219 Rev A LFV LVD 2551 Adj.of Ground Idle FAA AD 94 -11 -04 FAA, U.S AD 94 -11 -04 22 -jun -94 27 -mar -09 N/A by s/n LFV LVD 2592 Insp/Repl. of Lock -pin in L/G gearbox JCAB AD TCD -3942 -1-94 MITSUBISHI SB 09 -feb -95 27 -mar -95 TCD-3942-1-94, MSB 219A 219 Rev A LFV LVD 2678 Kontr. av vindrutor och fönster MHI SB FAA, U.S AD 2003 -17 -04 JCAB AD TCD - 12 -mar -96 08 -mar -11 224 Rev A 4311-95 MITSUBISHI SB 224 Rev C LFV LVD 2688 Kontr/byte av infästn.bult för tiptank FAA, U.S AD 98 -20 -39 JCAB AD TCD - 09 -May - 04 -dec -96 MU-2 SB 225 4310-96 MITSUBISHI SB 225 1996 LFV LVD 2689 Kontroll av linkage för prop.flöjning JCAB AD TCD -4379 -96 MITSUBISHI SB 09 -May - 30 -jul -96 MU-2 SB 229 229 1996

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 161(195) LFV LVD 2732 Inspection/ Replacement of Prop Hub. FAA, U.S AD 96-18-14 HARTZELL SB 61- 27-sep-96 01-sep-99 Prop. utbytt mot BVA FAA AD 96-18-14, Hz SB 136H 261 Rev 1 LFV LVD 2749 Revision av flyghandbok AFM TCD- FAA, U.S AD 96-25-02 JCAB AD TCD- 21-jan-97 11-mar-02 4552-96 4552-96 LFV LVD 2761 Installation av autoignition system TCD- JCAB AD TCD-2679A-97 MITSUBISHI SB 14-feb-97 05-mar-99 2679A -97 226 Rev E LFV LVD 2769 Demont.av backventil i FAA, U.S AD 97-04-13 MITSUBISHI SB 18-mar-97 05-May-1997 N/A N/A due to s/n. bränslesystemets MU-2 SB 130A 130 Rev A LFV LVD 2800 Mod. av De -ice Monitoring System JCAB AD TCD -4626 -97 MITSUBISHI SB 28 -aug -97 10 -May -1998 Mitsubishi SB 232, TCD-4626-97 232 Rev A LFV LVD 2819 Mod.av lagerboxar för landställssystem JCAB AD TCD -4684 -97 MITSUBISHI SB 18 -nov -97 18 -mar -98 Mitsubishi SB 230 230 LFV LVD 2897 Kontroll av landst,llets drivsystem TCD - JCAB AD TCD -4838 -98 MITSUBISHI SB 02 -aug -98 24 -mar -09 N/A by model 4838-98, SB 235 235 LFV LVD 2898 Mod. av autopilotens höjdtrimsystem JCAB AD TCD -3740A -98 MITSUBISHI SB 27 -aug -98 09 -nov -98 TCD-3740A-98, SB 216, 228 216 MITSUBISHI SB 228 LFV LVD 2922 Änd.av Flyghandbok -Extra krav på JCAB AD TCD -4753 -98 MITSUBISHI SN 12 -nov -98 02 -dec -98 FAA AD utförd. typutbi TCD -4753 -98, MHI SN 117A 117 Rev D LFV LVD 2924 Kontr/Just av motorernas Torque JCAB AD TCD -4889 -98 MITSUBISHI SB 01 -dec -98 03 -jun -99 indikeri MHI SB 233, TCD -4889 -98 233 Rev B LFV LVD 2925 Kontr/just av mot bränsleflöde Flight Id JCAB AD TCD -4890 -98 MITSUBISHI SB 01 -dec -98 20 -apr -99 MHI SB 234 234 LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD -5030 -99 MITSUBISHI SB 18 -jun -99 24 -mar -09 N/A by model 209 Rev B LFV LVD 3112 Revision av flyghandbok JCAB AD TCD -5432 -2000 30 -jan -01 12 -feb -02 LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD-4625A-2001 MAI SB 02-apr-01 15-May-2001 093/22-009 MITSUBISHI SB 231 Rev B NYGE TDM01-45 LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD-5547-2001 02-apr-01 12-feb-02 LFV LVD 3166 Sprickkontroll av infästning till ving - JCAB AD TCD -5747 -2001 MITSUBISHI SB 20 -sep -01 18 -Oct -2001 spetstank 236 LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD -5864 -2001 MAI SB 09 -jan -02 17 -jan -02 099/27-012 MITSUBISHI SB 237 LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD -6127 -2003 MITSUBISHI SB 21 -mar -03 02 -Oct -2003 239

MAI, Mitsubishi Aircraft

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 162(195) International MAI SB 047/30 - A Torque of Bleed Air Tube Coupling Nuts FAA, U.S AD 84 -12 -04 MITSUBISHI SB 19 -jul -84 A 27 -jan -86 001 AD 84-12-04,SB 196A 196 Rev A MAI SB 051/27 - Add.Seal and Flap Flexible Shaft Torque FAA, U.S AD 87 -04 -03 01 -feb -85 27 -aug -84 007 AD 87-04-03, SB 198 MAI SB 066/22 - Bendix autopilot disengagement 21 -Mar -12 006 MAI SB 067/27 - A Insp/Repl. of Flap Control System FAA, U.S AD 88 -23 -01 LFV LVD2202 29 -mar -95 A 11 -mar -96 008 Torque AD 88-23-01, SB 189B MAI SB 069/24 - Split Radio Bus Inspection and Rework MAI SB 066/22 -006 Rev A 17 -nov -88 25 -jul -89 N/A N/A due to Aircraft s/n 006 MAI SB 086/74 - A Auto -Ignition System Installation FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH 05 -Oct - A 22 -nov -01 Action not required due to s/n. 002 AD M 2435/97 MITSUBISHI SB 226 Rev E 2000 MAI SB 089/57- A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98-20-39 05-nov-96 A 04-dec-96 N/A N/A due to s/n. 002 MAI SN 110/00- Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered 017A MAI SN 111/77- Torque Indicating System Shift Potential 20-nov-08 11-mar-09 SB 233 considered 004 MAI SR 020/34- Anti Ice Capability AD 86-20-01, SR FAA, U.S AD 86-20-01 LFV LVD2015 Rev 06-Oct- 27-mar-00 N/A N/A due to s/n. 005 053A B MITSUBISHI SR 053A 1986

MITSUBISHI, Mitsubishi Heavy Industries Ltd MITSUBISHI MSB A **RECOVERED RECORD** 27 -aug -84 N/A 24-002 MITSUBISHI MSB **RECOVERED RECORD** 17 -Oct - N/A 24-004 1984 MITSUBISHI MSB **RECOVERED RECORD** 27 -aug -84 N/A 27-001 MITSUBISHI MSB **RECOVERED RECORD** 27 -aug -84 N/A 27-003 MITSUBISHI MSB **RECOVERED RECORD** 27 -aug -84 N/A 27-005 MITSUBISHI MSB **RECOVERED RECORD** 27 -aug -84 N/A 27-006 MITSUBISHI MSB **RECOVERED RECORD** 27 -aug -84 N/A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 163(195) 27-007 MITSUBISHI MSB A **RECOVERED RECORD** 27 -aug -84 N/A 30-001 MITSUBISHI MSB A **RECOVERED RECORD** 27 -aug -84 N/A 32-001 MITSUBISHI MSB **RECOVERED RECORD** 27 -aug -84 N/A 32-004 MITSUBISHI MSB **RECOVERED RECORD** 27 -aug -84 N/A 32-006 MITSUBISHI MSB **RECOVERED RECORD** 07 -jul -86 N/A 32-010 MITSUBISHI MSB **RECOVERED RECORD** 27 -aug -84 N/A 34-004 MITSUBISHI MSB **RECOVERED RECORD** 27-aug-84 N/A 34-007 MITSUBISHI MSB **RECOVERED RECORD** 27-aug-84 N/A 54-001 MITSUBISHI MSB A **RECOVERED RECORD** 27-aug-84 N/A 54-002 MITSUBISHI MSB B **RECOVERED RECORD** 27-aug-84 N/A 71-003 MITSUBISHI MSB **RECOVERED RECORD** 27-aug-84 N/A 71-005 MITSUBISHI MSR B **RECOVERED RECORD** 19-feb-87 066 MITSUBISHI SB Bendix M4D 18-dec-87 25-jul-89 066 MITSUBISHI SB M-4() Autop.Engage Switch Guard 11-apr-91 07-dec-94 076/22-008 Install. MITSUBISHI SB C Anti-Ice Additive in Fuel -Usage of JCAB AD TCD-0642-70 LFV LVA439 09-Oct- C 21-aug-85 112 1971 MITSUBISHI SB Fuel Quantity Indicator Readjustmnet JCAB AD TCD-0643-70 LFV LVA438 01-jan-70 15-jul-04 N/A N/A by s/n. 114 MITSUBISHI SB The Bolt and Bolt Hole Diam. of Nose JCAB AD TCD-0652-70 LFV LVA456 10-mar-70 26-mar-09 N/A by model 119 L.G MITSUBISHI SB Bearing,Oleo Strut,Nose L.G. -Repl. of JCAB AD TCD-0660-70 LFV LVA457 01-apr-70 26-mar-09 N/A by s/n 123 MITSUBISHI SB Scissors Switch,Nose L.G. -Install. of 31-aug-70 21-aug-85 N/A 124

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 164(195) MITSUBISHI SB B Tip Tank Air Pressure Modification 28-jun-94 B 05-nov-09 N/A by model & s/n 128 MITSUBISHI SB B Top Coating, Wing Integral Main F.T.- JCAB AD TCD-0730-1-72 JCAB AD TCD- 05-jan-72 B 14-jul-04 N/A N/A by s/n. 143 SIo 0730-2-86 MITSUBISHI SB A Flex. Shafts, Flap Control Sys.-Insp. of JCAB AD TCD-0947A-74 LFV LVA828 Rev 03-Oct- A 27-jan-86 N/A due to S/N 162 (AD750201) A 1974 MITSUBISHI SB B Insp. of Outer Pane, Front Winds. & Inst FAA, U.S AD 74-11-01 JCAB AD TCD- 16-nov-78 21-aug-85 N/A 163 0948A-1-78 JCAB AD TCD-0948A-74 LFV LVA829 Rev A MITSUBISHI SB A Lubr. Interval,Wheel Bearing,Main & 24-jul-80 21-aug-85 N/A 165 Nose MITSUBISHI SB D Flap M.Jack Screw-Insp. of and/or Main FAA, U.S AD 75-16-13 JCAB AD TCD- 24-jul-80 D 05-feb-02 N/A Ej tillämplig p.g.a. s/n. 167 G 1094A-76 LFV LVA1011 Rev A MITSUBISHI SB A Propeller Pitch Control Lever-Insp. of FAA, U.S AD 75-16-20 JCAB AD TCD- 24-jul-80 A 21-aug-85 168 (AD761620) 1188-75 LFV LVA1012 MITSUBISHI SB B Shimmy Damper-Insp. and Modification JCAB AD TCD-1209-75 LFV LVA1013 24-jul-80 B 05-nov-09 PCW 169 of MITSUBISHI SB A MLG Forward Door Em.Op. Cable-Insp. JCAB AD TCD-1235-75 LFV LVA1083 24-mar-77 A 21-aug-85 N/A N/A due to s/n 170 & Re (AD762204) MITSUBISHI SB B Latches,Eng. Nacelle Upper D.-Insp.& FAA, U.S AD 78-03-05 JCAB AD TCD- 17-nov-77 B 21-aug-85 171 Mod (AD780305) 1202-75 LFV LVA1014 Rev A MITSUBISHI SB A Drag Strut, Main L.G.-Modification of JCAB AD TCD-1284-1-76 24-jul-80 21-aug-85 173 MITSUBISHI SB C Tip Tank Conduit Tube -Insp.of,and FINNISH AD M 1177/83 JCAB AD TCD - 02 -Oct - C 27 -jan -86 N/A by s/n 174 PART 1 Rew.of (AD830902) 1370A-81 LFV LVA1196 1981 MITSUBISHI SB C Tip Tank Conduit Tube Rework 02 -Oct - C 27 -jan -86 N/A N/A by A/C S/N 174 PART 2 1981 MITSUBISHI SB Barrel Nut, Inner/Outer Wing Conn. - JCAB AD TCD -1353 -76 26 -jun -76 21 -aug -85 175 Repl. MITSUBISHI SB E Elevator Trim Tab Bracket -Repl. of FAA, U.S AD 84 -25 -02 FINNISH AD M 26 -sep -84 E 21 -aug -85 176 LVD1971, AD 84-25-02, SB 031/27- 1080/82 JCAB AD TCD-1001A-76 JCAB 005R1 AD TCD-1001B-2-84 LFV LVD1971 MITSUBISHI SB B Mod. of Engine Nacelle Tail Area JCAB AD TCD-1379-1-80 LFV LVA1197 11-sep-80 B 27-jan-86 177 (AD810601) Rev A MITSUBISHI SB Rodd Assem., Engine Nacelle Upper D.- 27-May- 21-aug-85 179 R&M 1977 MITSUBISHI SB A Link, Engine Nacelle Upper D.-Repl. of FAA, U.S AD 78-03-05 JCAB AD TCD- 17-nov-77 A 21-aug-85 180 (AD780305) 1202-75 JCAB AD TCD-1520A-77 LFV LVA1014 Rev A

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 165(195) MITSUBISHI SB B Insp. and Repl. of Nose L.G. Strut Assem FAA, U.S AD 86-15-03 JCAB AD TCD- 08-apr-85 B 27-May-1986 181 PART 2 (AD801812) 1768-1-85 LFV LVA1546 MITSUBISHI SB Add. of Ceiling Cover, Rear Bagg. Comp. JCAB AD TCD-1817-79 LFV LVA1583 16-nov-79 27-May-1986 N/A N/A due to s/n. 182 MITSUBISHI SB Turnbuckle, Control Cables -Repl. of 04-apr-80 21-aug-85 184 MITSUBISHI SB Down Lock Mech., Nose L.G.-Insp. of JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 27-aug-84 188 MITSUBISHI SB C Flap Control Torque Tube AD 88 -23 -01, FINNISH AD M 2722/00 JCAB AD TCD - 28 -jun -94 C 11 -mar -96 189 SB 067/27-008 2252-1-87 JCAB AD TCD-2252-83 LFV LVA1873 LFV LVD2202 MITSUBISHI SB Engine El. Wire-Insp. and Replacement JCAB AD TCD-2113-82 LFV LVA1788 21-dec-81 27-aug-84 191 of (AD820802) MITSUBISHI SB B Landing Gear Warning Horn Syst.Modif. 15-jun-94 B 04-dec-00 Rev A är utförd. 193 MITSUBISHI SB Master Cauting Light Visibility-Impr. of 23-aug-82 27-aug-84 194 MITSUBISHI SB A Ret. of coupling nut on the bleed air tu FAA, U.S AD 84-12-04 JCAB AD TCD- 12-apr-84 A 27-jan-86 196 AD 84-12-04, SB 047/30-001 2342-1-84 JCAB AD TCD-2342-84 LFV LVA1942 MAI SB 047/30-001 Rev A MITSUBISHI SB Add. Seal & Torque Insp. of Flap Flex.Sh FAA, U.S AD 87-04-03 JCAB AD TCD- 13-feb-85 27-aug-84 198 LVD2037, AD 87-04-03, SB 051/27-007 2451-85 LFV LVD2037 MITSUBISHI SB A Engine Lubricating Tubing Insp. & 24-jun-94 A 06-nov-09 PCW 199 Protec MITSUBISHI SB B Insp of Nose Ldg Gear Drag Strut Link 24-jun-94 A 07-Oct-1988 200 MITSUBISHI SB A Generator Circuit Wires Insp. and Mod. FAA, U.S AD 87-12-02 JCAB AD TCD- 02-mar-88 A 24-mar-09 N/A by s/n 201 2545-1-88 LFV LVD2191 MITSUBISHI SB Speed Placard Change 03-mar-87 02-May-1988 204 MITSUBISHI SB Bendix Autop.Disengagement Method FAA, U.S AD 88-13-01 JCAB AD TCD- 13-Oct- 06-nov-09 N/A Due to model 206 Stand. 2856-1-97 LFV LVD2190 1987 MITSUBISHI SB Rudder T.T. & Elevator T.T. Insp. & Rep. 20-May- 11-feb-10 207 1988 MITSUBISHI SB B Fuselage inspection JCAB AD TCD-5030-99 LFV LVD2988 19-apr-99 B 24-mar-09 N/A by model 209 MITSUBISHI SB A Engine Ignition Unit Replacement 12-nov-96 06-mar-98 210 MITSUBISHI SB Rudder Trim Tab Modification (LVD JCAB AD TCD -3378 -90 LFV LVD2338 20 -nov -90 14 -jul -04 N/A N/A by s/n. 211 2338)

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 166(195) MITSUBISHI SB A Insp of Anti-ice/Deice Systems (LVD JCAB AD TCD-3393A-96 LFV LVD2347 25-apr-96 A 26-May-2010 212 2347), Rev 1 MITSUBISHI SB Engine Control Rod Inspection 06-dec-91 01-sep-92 214 MITSUBISHI SB Removel of Prop. Governor Speed 23-Oct- 28-feb-92 215 Signal 1991 MITSUBISHI SB Elevator Trim Tab Installation (LVD FAA, U.S AD 2007-17-09 FAA, U.S AD 94- 11-sep-92 07-May-1993 216 2450 04-16 JCAB AD TCD-3740A-98 LFV LVD2450 LFV LVD2537 LFV LVD2898 MITSUBISHI SB A Propeller Feathering Linkage Inspection 17-jan-94 A 25-apr-94 218 MITSUBISHI SB A Emergency Gear Down G.box Lower Pin JCAB AD TCD-3942-1-94 JCAB AD TCD- 24-Oct- A 27-mar-95 219 Repl 3942-94 LFV LVD2538 LFV LVD2592 1994 MITSUBISHI SB Tip Tank Conduit Tube Insp. and Rep. JCAB AD TCD-3901-93 LFV LVD2512 10-aug-93 25-apr-94 221 MITSUBISHI SB Pitot/Static System Improvement SR MITSUBISHI SR 053A MITSUBISHI SR 064 28-jun-94 27-mar-00 223 064 MITSUBISHI SB C Acrylic Windsheild/Window glass Insp. FAA U.S AD 2003-17-04, FINNISH AD M 30-apr-98 C 08-mar-11 224 3076, JCAB AD TCD-4311-95, LFV LVD2678 MITSUBISHI SB Forward fitting bult of wingtip tank LVD FAA, U.S AD 98-20-39 FINNISH AD M 29-sep-95 04-dec-96 225 2688 2351/96 JCAB AD TCD-4310-96 LFV LVD2688 MITSUBISHI SB E Auto -Ignition System Installation LVD FAA, U.S AD 2000 -09 -15 Rev 1 FAA, U.S 18 -sep -01 E 22 -nov -01 PCW no further action (rev.E) required due to s/n. 226 2761 (2113), AD TCD-2679A-97 AD 86-26-02 FINNISH AD M 2435/97 FINNISH AD M 2786/00 JCAB AD TCD- 2679A-97 LFV LVD2761 MAI SB 086/74- 002 Rev A MITSUBISHI SB Rudder Torque Tube Modification 20 -dec -96 10 -apr -97 227 MITSUBISHI SB Elevator Trim Indicator Modification FAA, U.S AD 2007 -17 -09 FINNISH AD M 13 -jul -98 09 -nov -98 228 LFV 2898 2581/98 JCAB AD TCD-3740A-98 LFV LVD2898 MITSUBISHI SB Feathering Valve/Linkage Insp. FAA, U.S AD 2006 -15 -07 JCAB AD TCD - 20 -feb -96 30 -jul -96 229 4379-96 LFV LVD2689 MITSUBISHI SB Mod.of Bearing Box Ldg. Gear Act. LVD JCAB AD TCD -4684 -97 LFV LVD2819 05 -mar -97 18 -mar -98 230 2819 MITSUBISHI SB B Inst.of Trim -In -Motion Alert System FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH 11 -dec -02 B 03 -mar -03 SL 079 performed earlier. 231 AD M 2460/97 UPPHÄVD FINNISH AD M 2786/00 JCAB AD TCD-4625A-2001 LFV

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 167(195) LVD3122 MITSUBISHI SB A De -Ice System Modification LVD 2800, FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH 06 -jun -02 A 06 -jun -02 N/C due to previuosly complied with SB 232 rev 232 TCD-4626-97 AD M 2786/00 JCAB AD TCD-4626-97 0. LFV LVD2800 MAI SB 096/30-004 MITSUBISHI SB B Insp.of Engine Torque Indication FAA, U.S AD 2006 -17 -01 FINNISH AD M 08 -mar -07 B 18 -apr -07 Checked, previously carried out 233 System. TCD-4889-98, LFV 2924 2608/98 JCAB AD TCD-4889-2-2007 JCAB AD TCD-4889-98 LFV LVD2924 MITSUBISHI SB Fl.Check of the Flight Idle Fuel Flow Se FAA, U.S AD 2006 -17 -05 JCAB AD TCD - 07 -Oct - 11 -feb -10 234 TCD-4890-98, LVD 2925 4890-98 LFV LVD2925 1998 MITSUBISHI SB Inspection of landing gear power train JCAB AD TCD -4838 -98 LFV LVD2897 04 -aug -98 24 -mar -09 N/A by model 235 MITSUBISHI SB Inspection of Tip Tank Brackets JCAB AD TCD -5747 -2001 LFV LVD3166 28 -aug -01 18 -Oct -2001 236 MITSUBISHI SB Inspection of Flap Drive Train JCAB AD TCD -5864 -2001 LFV LVD3212 13 -dec -01 17 -jan -02 237 MITSUBISHI SB Main Landing Gear Door Safety Pin 05 -dec -02 09 -jan -03 Perf. at each 600 h. insp. 238 MITSUBISHI SB Pneumatic Line Insp. and Modification JCAB AD TCD -6127 -2003 LFV LVD3322 26 -dec -02 02 -Oct -2003 239 MITSUBISHI SB Inst.of Trottle Quadrant Placard 26 -feb -03 02 -Oct -2003 240 MITSUBISHI SB A Inspection of Wing Attachment FAA, U.S AD 2006 -13 -15 JCAB AD TCD - 21 -nov -06 A 17 -jan -07 c/o in conjunction with wingstudie 241 Hardware 7030-2006 MITSUBISHI SL System 17 -feb -89 20 -aug -91 060 MITSUBISHI SL Automatic Autopilot Disconnect System 28 -jan -02 26 -May -2010 078 MITSUBISHI SL Diode inst.in Flap Position Ind.Curcuit 28 -jan -02 15 -May -2001 Carried out by Mitsubishi (manufacturing - 079 made) MITSUBISHI SL Hartzell Propeller Mounting Bolt Insp. HARTZELL SB 61 -256 05 -apr -02 26 -aug -02 Compliance in according to HC -SB -61 -256. 080 MITSUBISHI SL Pneumatic De -Ice Monitoring System 14 -jun -04 26 -May -2010 084 MITSUBISHI SL Hartzell prop. mount. bolt insp. HARTZELL SB 61 -279 ALERT Rev 4 17 -May - 20 -sep -05 085 2005 MITSUBISHI SN B Rudder Torque Tube AD 86 -20 -01, SB 05 -nov -86 B 22 -dec -87 053 020/34-005 MITSUBISHI SN D Icing Awareness Training Video FAA, U.S AD 2003 -22 -07 Rev 1 JCAB AD 14 -jun -04 D 17 -May -2004 117 TCD-4753-98 LFV LVD2922

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 168(195) MITSUBISHI SN Water Ingress into Vertical Stabilizer 19-dec-03 24-feb-04 146 MITSUBISHI SN Reminders for safe operation 18-nov-05 22-mar-06 Genomförs enl. AMP MU-2 & DHB 148 MITSUBISHI SN Power Lever Position Warning 25-feb-09 09-nov-09 SB 240 considered 156A MITSUBISHI SN Torque Indicating System Shift Potential 20-nov-08 11-mar-09 SB 233 considered 157 MITSUBISHI SN Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09 -dec -09 11 -mar -10 Ref STC SA01913SE 161 MITSUBISHI SR Modifiering av pitotrör FAA, U.S AD 86 -20 -01 JCAB AD TCD - 23 -Oct - 08 -May -1998 053A 2450A-87 LFV LVD2015 Rev B MAI SR 1984 020/34-005 MITSUBISHI SB 223 MITSUBISHI SR Pitot & Static System MITSUBISHI SB 223 30-apr-85 27-mar-00 064 MITSUBISHI SR Warning Horn 20-jan-86 22-dec-87 065 MITSUBISHI SR Emergency Exit Placard 17-sep-85 27-May-1986 067 MITSUBISHI SR Air Filter Replacement for Vacuum Syst. 25-apr-00 24-feb-04 072 MITSUBISHI SR Inst. tip tank placard 29-Oct- 04-apr-05 075 2004 MITSUBISHI STC Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10 -dec -09 11 -mar -10 See MU -2B AMP Chpt 3 100h/1y inspection SA01913SE

NARCO, Narco NARCO SB ELT10 - ELT ASSY 18 -apr -88 14 -jun -91 N/A 16

NYGE, Saab Aerotech Aircraft Services NYGE TDM 00 -09 Operatörsplats MU -2 11 -apr -00 12 -jan -00 NYGE TDM 00 -23 Wiring Left Wing ADRIAN 22 -dec -00 08 -Oct -1999 NYGE TDM 02 -24 Installation Moving MAP 10 -Oct - 29 -Oct -2002 2002

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 169(195) NYGE TDM 02-32 Installation EMI film 10-dec-02 10-jan-04 NYGE TDM 03 -08 8 GNS430/530 & MODE S 04 -mar -03 20 -Oct -2008 GTX330 install. NYGE TDM 05 -16 Viktor Counter Weight Pod 18 -nov -05 18 -nov -05 NYGE TDM 06 -41 A Darts (to carry on MU -2B - 20 -nov -06 A 07 -feb -08 20/26) NYGE TDM 06 -42 A Barlast DARTS MU -2B 04 -dec -07 A 07 -feb -08 NYGE TDM 07 -30 A Install. of Emergency Axe 28 -feb -08 A 07 -mar -08 NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 07-sep-09 NYGE TDM 08 -28 B ELT 406 MU -2B 29 -sep -08 B 20 -Oct -2008 Original compliance with TDM rev A. Rev B does not affect previous complaiance. NYGE TDM 09 -02 C U-95 SORC Lite MU -2B 15 -dec -09 C 29 -apr -10 Original compliance I.A.W rev is not affected by rev C. NYGE TDM 09 -07 A GPS Splitter 18 -May - A 10 -jun -09 2009 NYGE TDM 10-02 A Target surveillance camera 03-jun-10 A 01-Oct-2010 NYGE TDM 10 -03 A Pressure Bulkhead Feed 04 -May - A 04 -Oct -2010 Through 2010 NYGE TDM 10 -25 A MU -2B Terminating Resistor 08 -apr -10 A 18 -May -2010 C/W NYGE TDM 11 -35 A Terminating resistor A 27 -Jan -12 NYGE TDM 12 -21 A Avinstallation IK 14 -Aug -12 NYGE TDM 95 -04 4 Vingstudie 20 -sep -98 4 08 -mar -11 NYGE TDM 97 -01 TAPS 20 -feb -97 01 -jan -98 NYGE TDM 99 -09 Installation BRNAV MU -2 01 -nov -99 30 -Oct -1999 NYGE TVO 1/09 Inspektion av Stringers & 25 -feb -09 02 -mar -09 Inspected u/a struktur vinge NYGE TVO 1/93 Low Volt Warning Light (BCL) 22 -jan -93 07 -May -1993 NYGE TVO 1/96 Slitage Flap Guide Rail 12-apr-96 20-apr-99 NYGE TVO 1/97 3 De -Icertank MU -2B, 12 -feb -97 11 -feb -97 korrosionskontroll NYGE TVO 2/00 Märkning av infästning 01 -dec -00 29 -jan -01 domkraft Mu2

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 170(195) NYGE TVO 2/07 A Prevent FR31 radio to xmit 06-feb-07 A 27-feb-07 when RM2 off NYGE TVO 2/10 1 Visual inspection of center 19-apr-10 08-mar-11 wing NYGE TVO 2/91 A/C Elecrical System 10-jan-91 26-apr-91 NYGE TVO 3/06 Inspect lower rudder hinge 07 -dec -06 08 -mar -11 bracket NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24 -feb -05 3 11 -feb -10 NYGE TVO 4/11 A Static inverter controll A 15 -Dec -11 NYGE TVO 4/91 Special Inspection (next E6.) 19 -feb -91 07 -dec -91 NYGE TVO 4/92 Engine Install. Kontr. 29 -apr -92 19 -May -1992 rörledningar NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28 -sep -94 11 -feb -10 NYGE TVO 4/96 Kontroll av Lagerhus i 25 -Oct - 26 -aug -97 Utförd tidigare (ref. Ove N lista) noshjulsstyrning. 1996 NYGE TVO 6/88 Allm. instruktion för 13-jun-88 08-mar-11 metallpropeller NYGE TVO 6/92 Elevator Trim Cable, check 07-Oct- 19-Oct-1992 1992 NYGE TVO 7/05 RMI-nål park. ej / ILS frekvens 11-nov-05 25-nov-05 Carried out i.a.w. drawing NA-MF-199-008 & är vald NA-MF-199-009 NYGE TVO 7/93 Starter Drive Splines 01-nov-93 07-dec-94 NYGE TVO 8/92 Wheel Parts 27 -Oct - 07 -May -1993 1992

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 171(195)

2.7 GFE Aircraft Mitsubishi MU-2 SE-IUA

2.7.1 Aircraft Specification Type: Serial Registration : Airframe Total Date Number: total Hours: Landing Reference: Cycles: MU-2B-26 345 SE-IUA 10619 4226 2012-11-23

2.7.2 Engines Type: Honeywell TPE331 -6-252M Serial Total Hours Total Hours remaining Number: Since New: Cycles overhaul/HSI/GBI: Since New: Left Engine P20461 10937 9971 2876/667/2467 Right Engine P20502 7706 8168 439/835/2317

2.7.3 Propeller Type Number: Serial Number: Overhaul Due Date: Left Propeller HC-B3TN-5E BVA 6325 2013-11-25 Right Propeller HC-B3TN-5E BVA 6194 2013-01-07

2.7.4 Avionics System: Type / Part Number: Note: Autopilot & Flight Director Bendix M4D COM/NAV/GPS 1 & 2 Garmin GNS 430 Audiopanel Bendix/King KMA-24H-70 MKR Bendix/King KMR 675 DME Bendix/King KN 63 ADF Bendix/King KR 87 XPDR 1 Garmin GTX 330D XPDR 2 Garmin GTX 330 *) RDR ALT Bendix/King KRA-10A ELT Kanad ELT 406-AF-H Airspeed Indicator LH / RH Aerosonic 20040-0113 / 20040- 0161 Altimeter LH Aerosonic 101735-01555 Altimeter incl. encoder RH United Instr. Inc. 5035P -P40 Altitude Reporter Ameri -King AK -350 Altitude Alerter Century 1D960 Vertical Speed Indicator LH Aerosonic RC-60-MS-10-3 Attitude Gyro & Flight Director Ind. Bendix GH-14

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 172(195) LH Attitude Gyro Ind. RH AIM 504-0006-914 Turn & Bank Ind. LH Bendix 4099-B Horizontal Situation Indicator LH Bendix RD-44 DG -Gyro Sperry C -14A RMI Indicator Collins 332C -10 RMI/ADF adapter Bendix/King KDA-692 CDI Indicator Garmin GI-106A *) XPDR 2 without diversity configuration

2.7.5 Mission System System : Description: Fixed general installations VHF/UHF COM FR31 GPS MAP JET SI-3003B Inverter 115/200VAC 400Hz 3 phase Laser Prism MIL -STD -1553 Bus LH Wing Pylon Wing Pylon NATO 14” Alcon Ejector Unit LH and RH Wing Pylon EW system ADRIAN Pod mounted system LH and RH Wing Pylon A100 Pod mounted system LH Wing Pylon Missile Threat Simulator DARTS Pod mounted system LH Wing Pylon Chaff Dispenser BOX 3 Pod mounted system LH and RH Wing Pylon Target Towing MBV7S Inboard winch AS200 MDI (Miss Distance Indicator) Precisions GPS Pos System TAPS Radar Calibration System GPS Sphere

2.7.6 Mission Cable Harness to Hard Points Used for Mission LH NATO Hard point: RH NATO Hard point: Note: System: Adrian C & S, A100, DARTS General Signal Harness General Signal Harness and BOX 3 AWG22 shielded x 44 AWG22 shielded x 50 A100 MIL-STD-1553B Data Triax Cable x 1 Bus

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 173(195) A100 and DARTS AC Power AWG 16 x 4 115/200VAC 400 Hz 3- twisted Phase 3 x 10 A AWG 16 x 2 AWG 20 x 2 Adrian C & S and BOX 3 DC Power 28 VDC 200 DC Power 28 VDC 200 AWG 2 x 2 A A Adrian C & S Coax Cable 1 x 50 Ω Coax Cable 1 x 50 Ω Prepared installation Ethernet LAN Cable

2.7.7 Antenna Layout

Unclassified Enclosure 2 – GFE Aircrafts

Date FMV Document ID Subject type 2012-12-06

Document number Page 174(195)

2.7.8 Inspection due times and dates Status date November 23 rd 2012.

Description Maint. Ref C/Out date C/Out Hrs Due Hrs Due date Aircraft SE-IUA Vingstudie MU-2 AMP 10000 11000 100 Hour Inspection AMP 2012-04-18 10577 10679 2013-04-18 200 Hour Inspection AMP 2012-04-18 10577 10777,9 2013-05-04 600 Hour Inspection AMP 2010-10-06 10402 11002,9 2013-10-05 1000 Hour Inspection AMP 2008-04-03 10000 11000 1200 Hour Inspection AMP 2008-03-28 9961 11161,9 1800 Hour Inspection AMP 2011-07-29 10479 12300 2000 Hour Inspection AMP 2008-04-03 10000 11960 1 Year Inspection AMP 2012-04-23 10577 2 Year Inspection AMP 2011-04-18 10425 10 Year Inspection AMP 2007-06-19 8700 Engine S/N P-20461 Remaining Engine Assembly (Overhaul) AMP 13495,6 2876,3 Engine Hot Section Inspection AMP 11286,3 667 Engine Gearbox Inspection AMP 13086,3 2467 Engine S/N P-20502 Engine Assembly (Overhaul) AMP 11059,2 439,9 Engine Hot Section Inspection AMP 11455 835,7 Engine Gearbox Inspection AMP 12936,34 2317,04

Propeller L/H O/H AMP 2008-11-19 14361,5 2013-11-25 Propeller R/H O/H AMP 2008-04-03 13834,7 2013-01-07

Unclassified

Date FMV Document ID Subject type 2012-12-06 ange ange

Document number Page ange 175(195)

2.7.9 Implemented Changes Status date November 23 rd 2012. SB/AD etc Rev Subject Document reference Eff. date Rev Complianc Statu Remarks Reference e s

SB/AD etc Rev Subject Document reference Eff. date Rev Compliance Stat Remarks Reference us

EASA, European Aviation Safety Agency EASA AD 2006 - Incorrect transponder altitude 30 -aug - 14 -mar -09 0265 06 EASA AD 2009 - Portable Fire Extinguishers -Ident/Repl 25 -nov - 07 -May -2010 N/A N/A by current P/N installed 0251-E 09 EASA AD 2009 - Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009 -0278 FFE ASB26 -115 Rev C 15 -dec - 07 -May -2010 N/A N/A by current P/N installed 0262 09 EASA AD 2009 - Halon 1211 Fire Extinguishers Id/Repl EASA AD 2009 -0262 22 -dec - 07 -May -2010 N/A N/A by current P/N installed 0278 09 EASA AD 2010 - R1 Mode S Transponder - 11 -jan -10 R1 10 -mar -10 N/A due to model 0003 Check/Modification EASA AD 2012- Kidde Gravinier hand operated fire 4-May-12 0037 extinguisher EASA SIB 2008- Channel Spacing Switching GARMIN SSB0844 Rev IR GARMIN 17-dec- 21-sep-10 N/A by SSB 0844 incorporated 58R1 SSB0845 Rev IR 08 EASA SIB 2009-14 Upgrade to main unit/GPS software 24-jun-09 28-sep-09 N/A due to model

FAA, U.S, Federal Aviation Administration FAA, U.S AD 2000 - AFM De -icing 25 -jan -00 26 -apr -00 N/A Due to paragraph b. 02-25 FAA, U.S AD 2000 - 1 Flight in Icing Condition FINNISH AD M 2435/97 FINNISH AD M 07 -jul -00 1 22 -nov -01 Action not required due to s/n. 09-15 2786/00 MAI SB 086/74-002 Rev A MAI SB

Öppen/Unclassified

Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 176(195) 093/22-009 MAI SB 096/30-004 MITSUBISHI SB 226 Rev E MITSUBISHI SB 231 Rev B MITSUBISHI SB 232 Rev A FAA, U.S AD 2003- Windshield check FINNISH AD M 3076 LFV LVD2678 MAI SB 01-Oct- 07-Oct-2010 17-04 087/56-001 Rev B MITSUBISHI SB 224 Rev 2003 C FAA, U.S AD 2005 - Prop. mounting bolt insp. HARTZELL SB 61 -279 ALERT Rev 4 29 -jul -05 14 -sep -05 14-12 FAA, U.S AD 2005 - Prop de -icer "FASTprop" 14 -Oct - 12 -Oct -2005 N/A Due to boots p/n 18-20 2005 FAA, U.S AD 2006- Safety evaluation wing barrel nuts) MAI SB 103/57-004 Rev A MITSUBISHI SB 11-aug- 11-nov-02 c/o in conjunction with vingstudie 13-15 241 Rev A 06 FAA, U.S AD 2006- Safety evaluation (feathering linkage) MAI SB 090/76-003 MITSUBISHI SB 229 24-aug- 24-aug-06 se Mitsubishi SB 229 15-07 06 FAA, U.S AD 2006- Detect & correct torque transducers MAI SB 095/77-002 MITSUBISHI SB 233 22-sep- 21-sep-06 PCW see MSB 233A 17-01 Rev B 06 FAA, U.S AD 2006- Adjust flight idle fuel flow setting MITSUBISHI SB 234 22-sep- 11-Oct-2010 17-05 06 FAA, U.S AD 2007- Reduce max deflect elev nose-down MITSUBISHI SB 216 MITSUBISHI SB 228 25-sep- 11-sep-07 Previously carried out i.a.w. mentioned SB's. 17-09 trim 07 FAA, U.S AD 71-14- Fuel Tank Fungus Coating Peeling 01-May- 01-jan-96 N/A N/A by s/n 01 1972 FAA, U.S AD 75-03- Cracks and Optical Distortion LFV LVA829 Rev A 13-nov- 15-jul-86 N/A N/A due to s/n. 06 74 FAA, U.S AD 75-16- Main Wing Flap JCAB AD TCD-1094A-76 05-aug- 05-feb-02 N/A Ej tillämplig p.g.a. s/n. 13 75 FAA, U.S AD 75-16- Propeller Pitch Control Lever JCAB AD TCD-1188-75 LFV LVA1012 12-aug- 10-nov-82 20 MITSUBISHI SB 168 Rev A 75 FAA, U.S AD 78-03- Cowling Latches JCAB AD TCD-1202-75 LFV LVA1014 Rev A 23-feb-78 10-apr-87 05 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A FAA, U.S AD 81-06- 1 Engine Aft Nacelles 01-apr- 1 08-jun-87 Previously complied with 01 81 FAA, U.S AD 81-25- 1 Engine's Electrical wiring SB 036/71- 21-jan-82 1 27-mar-09 N/A by model 04 003A, SB 043/71-005 FAA, U.S AD 82-08- Electrical Wiring Inspection 15-apr- 02-aug-82 02 82 FAA, U.S AD 83-08- 2 To preclude prop. attach bolt failures FINNISH AD M 1168/83 Rev 1 FINNISH AD 28-apr- 2 20-May-2005 Ref. MU2B MM chap 13.4 when using bolts P/N B- 01 T5114/05 HARTZELL SI 140A Rev 9 82 3339 only

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 177(195) FAA, U.S AD 83-09- Strobe Light Assemblies 17-May- 27-mar-09 N/A by s/n 02 1983 FAA, U.S AD 84 -12 - Torque of Air Tube Coupling Nuts SB MAI SB 047/30 -001 Rev A MITSUBISHI SB 28 -jun -84 16 -jun -87 04 047/30-001, SB 196A 196 Rev A FAA, U.S AD 84 -25 - Elevator TrimTab Bracket Insp/Repl. MAI SB 031/27 -005 Rev 1 MITSUBISHI SB 18 -dec - 16 -jun -86 02 SB 031/27 -005 R1, SB 176E 176 Rev E 84 FAA, U.S AD 86-15- NLG Strut Assembley LFV LVA1546 MITSUBISHI SB 181 PART 2 13-aug- 15-jul-04 Found SB 181 part 2 PCW. 03 Rev B 86 FAA, U.S AD 86 -20 - To assure anti -ice capability of pitot LFV LVD2015 Rev B MAI SR 020/34 -005 06 -Oct - 15 -feb -00 01 SB 020/34 -005, SB 053A MITSUBISHI SR 053A 1986 FAA, U.S AD 86 -26 - To prevent engine flameout in an GARRETT SB 74 -0003 Rev , MITSUBISHI SB 31 -dec - 09 -mar -09 see applicable engine for c/o 02 iceing SB 74 -0003, SR 040/74 -001 226 Rev E 87 FAA, U.S AD 87 -04 - Addit. Seal and Flap Flexible Shaft MAI SB 051/27 -007 MITSUBISHI SB 198 07 -mar - 16 -May -1986 03 Insp SB 051/27 -007, SB 198 87 FAA, U.S AD 87 -12 - Generator Shield Jumper Wires MITSUBISHI SB 201 Rev A 03 -jul -87 27 -mar -09 N/A by s/n 02 FAA, U.S AD 88 -13 - Bendix Autopilot Disengagement SB LFV LVD2190 MAI SB 066/22 -006 Rev A 11 -jul -98 03 -mar -88 01 066/22-006 MITSUBISHI SB 206 FAA, U.S AD 88 -21 - 1 To minimize confusion in LFV LVD2206 MAI SB 066/22 -006 Rev A 28 -jan -89 1 25 -jan -12 01 autopilot/manua SB 066/22-006 FAA, U.S AD 88 -23 - To prevent flap control failure SB LFV LVD2202 MAI SB 067/27 -008 Rev A 04 -dec - 14 -sep -95 01 067/27-008, SB 189B 88 FAA, U.S AD 93 -07 - ELECTRIC TRIM SYSTEM SB 079/27 - LFV LVD2477 MAI SB 079/27 -010 01 -jun -93 27 -mar -09 N/A by s/n 11 010 FAA, U.S AD 94 -04 - Elevator trim tab mod. LFV LVD2537 MITSUBISHI SB 216 11 -apr - 08 -apr -93 16 94 FAA, U.S AD 94 -11 - Change of Flight Idle Blade Angel SB LFV LVD2551 MAI SB 016/71 -001 10 -jun -94 27 -mar -09 N/A by s/n 04 016/61-001 FAA, U.S AD 96 -25 - Cap. of the icing protection system FINNISH AD M 2423/97 JCAB AD TCD - 27 -dec - 12 -nov -97 02 4552-96 LFV LVD2749 96 FAA, U.S AD 97 -04 - Vent Check Valve Assy LFV LVD2769 16 -apr - 05 -May -1997 N/A N/A due to model. 13 97 FAA, U.S AD 97 -20 - Icing related incidents/accidents 17 -Oct - 02 -dec -98 14 CNL 1997 FAA, U.S AD 97 -25 - To prevent loss of airplane FINNISH AD M 2524/98 21 -jan -98 03 -dec -10 N/A AD superseeded by AD 2010 -10 -17 02 ctrl/overspe FAA, U.S AD 98 -20 - Forward fitting bolt of wingtip tank SB LFV LVD2688 MAI SB 089/57 -002 Rev A , 19 -Oct - 24 -Oct -1996 39 MU-2 225, 089/57-002A MITSUBISHI SB 225 1998

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 178(195) FINNISH, Finnish Civil Aviation Adm. FINNISH AD M Justering av br,nslefl"de MHI SB JCAB AD TCD-4890-98 , MAI SB 097/73- 12-nov- 11-Oct-2010 2609/98 097/73-001, TCD-4890-98 001 99 FINNISH AD M Kontroll av vindrutor och fönster FAA, U.S AD 2003-17-04 , MAI SB 087/56- 21-aug- 07-Oct-2010 3076 001 Rev B , MITSUBISHI SB 224 Rev C 03

GARMIN, Garmin GARMIN SB 0004 Incorp.of Main Software Version 2.16 01 -May - 18 -May -2000 2000 GARMIN SSB 0844 IR Software Version 5.04 EASA SIB2008 -58R1 14 -nov - A 19 -May -2010 08

GARRETT, AlliedSignal Aerospace GARRETT SB 74 - 6 Replace Ignition Unit AD 74 -0003 FAA, U.S AD 86 -26 -02 25 -mar - 09 -mar -09 see applicable engine for c/o 0003 94

HARTZELL, Hartzell Propeller Inc. HARTZELL SB 61 - Propeller mounting bolt inspection MITSUBISHI SL 053/72 -003, MITSUBISHI 08 -feb -02 13 -maj -02 L/H side 256 SL 080 HARTZELL SB 61 - 4 Prop. mounting bolt insp. FAA, U.S AD 2005 -14 -12 , MITSUBISHI SL 04 -Oct - 14 -nov -05 propellerbolts previously checked u/a 279 ALERT 085 2005 HARTZELL SI 140A 9 Installation of Mounting Bolt FAA, U.S AD 83-08-01 Rev 2 , LFV LVA1424 30-mar- 9 13-mar-08 see previously revision Rev A 05

JCAB, Japan Civil Aviation Bureau JCAB AD TCD - Rivet holes elevator hinge fitting 06 -feb -68 26 -mar -09 N/A by s/n 0518-68 JCAB AD TCD - AFM revision regarding fuel spec. LFV LVA439 MITSUBISHI SB 112 Rev C 07 -feb -70 16 -jul -86 N/A by s/n 0642-70

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 179(195) JCAB AD TCD- Adjustment of fuelquantitygauge LFV LVA438 MITSUBISHI SB 114 07-feb-70 15-jul-04 N/A N/A by s/n. 0643-70 JCAB AD TCD - Insp. of NLG bolts LFV LVA456 MITSUBISHI SB 119 25 -mar - 26 -mar -09 N/A by model 0652-70 70 JCAB AD TCD - Engine Nacelle Tail Area -Modification 25 -mar - 26 -mar -09 N/A by model 0653 -70 of 70 JCAB AD TCD- Replacement of bearing in LFV LVA457 MITSUBISHI SB 123 01-May- 26-mar-09 N/A by s/n 0660 -70 nosegearstrut 1970 JCAB AD TCD - Insp. and painting of maintanks LFV LVA543 Rev B MITSUBISHI SB 143 Rev 25 -mar - 14 -jul -04 N/A N/A by s/n. 0730 -1-72 B 72 JCAB AD TCD - Insp. and painting of maintanks MITSUBISHI SB 143 Rev B 10 -dec - 26 -mar -09 N/A by s/n 0730 -2-86 86 JCAB AD TCD - Mod. of electrical system LFV LVA645 MITSUBISHI SB 156 04 -sep - 10 -sep -72 N/A N/A due to model. 0859 -72 72 JCAB AD TCD - NLG gearbox and structure LFV LVA664 MITSUBISHI SB 155 09 -Oct - 31 -dec -72 N/A N/A due to model. 0866 -72 1972 JCAB AD TCD - Kontr. & mod. av klaffdrivning LFV LVA828 Rev A MITSUBISHI SB 162 Rev 12 -nov - 06 -Oct -1987 N/A N/A due to s/n. 0947A-74 A 74 JCAB AD TCD - Inspection of Windshields MITSUBISHI SB 163 Rev B 22 -dec - 26 -mar -09 N/A by s/n 0948A-1-78 78 JCAB AD TCD - Inspektion av frontrutor LFV LVA829 Rev A MITSUBISHI SB 163 Rev 07 -Oct - 15 -jul -86 N/A N/A due to s/n. 0948A-74 B 1974 JCAB AD TCD - Insp./repl. of elevator trim tab rod LFV LVA886 Rev A MITSUBISHI SB 176 Rev 06 -Oct - 16 -jun -86 1001A-76 E 1976 JCAB AD TCD - Replacement of Elevator Trim Tab FINNISH AD M 1080/82 LFV LVD1971 12 -dec - 16 -jun -86 1001B-2-84 Bracket MITSUBISHI SB 176 Rev E 84 JCAB AD TCD - Insp. of wingflap controlsystem FAA, U.S AD 75 -16 -13 LFV LVA1011 Rev A 06 -sep - 05 -feb -02 N/A Ej tillämplig p.g.a. s/n. 1094A-76 MITSUBISHI SB 167 Rev D 76 JCAB AD TCD - Insp. of propeller controllever inst. FAA, U.S AD 75 -16 -20 LFV LVA1012 06 -May - 10 -nov -82 1188-75 MITSUBISHI SB 168 Rev A 1975 JCAB AD TCD - Engine Cowling Latches FAA, U.S AD 78 -03 -05 LFV LVA1014 Rev A 20 -sep - 15 -jul -04 Found SB 171 and SB 180 PCW. 1202-75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 75 180 Rev A JCAB AD TCD - Insp/mod of NLG shimmydamper LFV LVA1013 MITSUBISHI SB 169 Rev B 16 -jun -75 08 -jun -87 1209-75 locking JCAB AD TCD - Insp./repl. of MLG fwd door LFV LVA1083 MITSUBISHI SB 170 Rev A 19 -sep - 10 -apr -78 N/A N/A due to model. 1235-75 emerg.cables 75 JCAB AD TCD - Supp.,MLG Forward D. Actuating MITSUBISHI SB 172 14 -nov - 26 -mar -09 N/A by model 1272-75 Mech.-I&M 75

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 180(195) JCAB AD TCD- Prevent failure of MLG. dragstrut MITSUBISHI SB 173 Rev A 31-mar- 28-Oct-2009 N/A Due to S/N 1284-1-76 76 JCAB AD TCD - Fire hazard in rear baggage 01 -jul -76 26 -mar -09 N/A by s/n 1328-76 compartment JCAB AD TCD - Barrel Nut, Inner/Outer Wing Conn. - MITSUBISHI SB 175 16 -aug - 26 -mar -09 1353 -76 Repl. 76 JCAB AD TCD- Inspect strobelight conduit in Tiptank LFV LVA1196 18-Oct- 06-Oct-1987 N/A by s/n 1370 -76 1976 JCAB AD TCD - Inspect strobelight conduit in Tiptank MITSUBISHI SB 174 PART 1 Rev C 05 -nov - 24 -mar -09 N/A by s/n 1370A -81 supersed TCD -1370 -76 81 JCAB AD TCD - Insp. rear eng. cowling reg. LFV LVA1197 Rev A MITSUBISHI SB 177 06 -feb -02 08 -jun -87 1379 -1-80 heatdamage Rev B JCAB AD TCD - Latch link engine nacelle door MITSUBISHI SB 180 Rev A 12 -dec - 24 -mar -09 ref. SB 180 1520A -77 77 JCAB AD TCD - Fatigue failure of the NLG strut assy. LFV LVA1546 MITSUBISHI SB 181 PART 12 -jul -85 15 -jul -04 PCW Found SB 181 part 2 PCW. 1768 -1-85 JCAB AD TCD - Modification of bagagecompartment LFV LVA1583 MITSUBISHI SB 182 05 -feb -02 08 -jun -87 N/A N/A due to s/n. 1817-79 JCAB AD TCD - Insp. firewarning & emerg.power LFV LVA1740 MITSUBISHI SB 187 Rev B 05 -feb -02 27 -May -1981 N/A N/A due to s/n. 2048-81 circuit JCAB AD TCD - Inspect NLG downlock mechanism LFV LVA1753 MITSUBISHI SB 188 05 -feb -02 16 -May -1986 2070-81 JCAB AD TCD - Insp./replace engine electrical LFV LVA1788 MITSUBISHI SB 191 06 -feb -02 16 -May -1986 2113-82 harness JCAB AD TCD - Flap system torquetubes supersed 01 -feb -89 24 -mar -09 PCW 2252-2-88 TCD-2252-1-87 JCAB AD TCD - Flapcontrolsystem torquetubes LFV LVA1873 MITSUBISHI SB 189 Rev C 04 -feb -83 14 -sep -95 2252-83 JCAB AD TCD - NLG. bracket attaching to drag strut 13 -aug - 24 -mar -09 N/A by model 2263-83 83 JCAB AD TCD - Engine inlet anti -ice tubing. MITSUBISHI SB 196 Rev A 05 -jun -84 10 -mar -09 PCW 2342-1-84 Torq./lock JCAB AD TCD - Engine inlet anti -ice tubing. LFV LVA1942 MITSUBISHI SB 196 Rev A 06 -feb -02 16 -jun -87 2342-84 Torq./lock JCAB AD TCD - Pitot Tube Wiring LFV LVD2015 Rev B MITSUBISHI SR 053A 16 -jun -87 15 -jul -04 SB PCW. 2450A-87 JCAB AD TCD - Add. seal/Tq. insp of flap flex. shaft 01 -May - 09 -mar -09 PCW see TCD -2451 -85 2451-1-87 1987 JCAB AD TCD - Add. seal/Tq. insp of flap flex. shaft LFV LVD2037 MITSUBISHI SB 198 30 -sep - 16 -May -1986

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 181(195) 2451-85 Superseeded by TCD-2451-1-87 85 JCAB AD TCD - Generator System LFV LVD2191 MITSUBISHI SB 201 Rev A 01 -jul -88 24 -mar -09 N/A by s/n 2545-1-88 JCAB AD TCD - Auto -ignition System FINNISH AD M 2435/97 LFV LVD2761 01 -feb -97 22 -nov -01 2679A-97 MITSUBISHI SB 226 Rev E JCAB AD TCD - Bendix M4C Autopilot System MITSUBISHI SB 206 05 -nov - 28 -Oct -2009 N/A Due to model 2856-1-97 97 JCAB AD TCD- Insp./mod. of rudder trimtab LFV LVD2338 MITSUBISHI SB 211 28-mar- 14-jul-04 N/A N/A by s/n. 3378-90 leadingedge 91 JCAB AD TCD- Anti ice/De-ice system FINNISH AD M 2364/96 LFV LVD2347 Rev 25-May- 07-Oct-2010 3393A-96 1 MITSUBISHI SB 212 Rev A 1996 JCAB AD TCD- Unintentional engagement of A/P...... 17-jun-91 24-mar-09 N/A by model 3464-91 JCAB AD TCD- Mod.of Autopilote pitchtrimsystem FINNISH AD M 2581/98 LFV LVD2450 LFV 17-aug- 18-nov-98 3740A-98 MSB 216, 228 LVD 2898 LVD2898 MITSUBISHI SB 216 MITSUBISHI 98 SB 228 JCAB AD TCD - Tiptank inst FINNISH AD M 2110/93 LFV LVD2512 10 -sep - 01 -feb -94 3901-93 MITSUBISHI SB 221 93 JCAB AD TCD - Inspection of landing gear lower pin FINNISH AD M 2238/95 LFV LVD2592 28 -nov - 01 -feb -94 3942-1-94 MITSUBISHI SB 219 Rev A 94 JCAB AD TCD - Change lockingpin ldg LFV LVD2538 MITSUBISHI SB 219 Rev A 01 -feb -94 01 -feb -94 3942-94 JCAB AD TCD- Fwd. Fitting Bolt FINNISH AD M 2351/96 LFV LVD2688 01-apr- 24-Oct-1996 4310-96 MITSUBISHI SB 225 96 JCAB AD TCD - Windshield/window insp. FINNISH AD M 2331/96 LFV LVD2678 01 -nov - 07 -Oct -2010 4311-95 MITSUBISHI SB 224 Rev C 95 JCAB AD TCD - Feathering Valve/Linkage insp. FINNISH AD M 2352/96 LFV LVD2689 01 -apr - 30 -jul -96 4379-96 96 JCAB AD TCD- Icing Limitation FAA, U.S AD 96-25-02 LFV LVD2749 27-dec- 12-nov-97 4552-96 96 JCAB AD TCD- Mod.of Trimsystem/AFM Revision FINNISH AD M 2460/97 UPPHÄVD MAI SB 14-jul-97 09-feb-01 4625-97 093/22-009 JCAB AD TCD- Mod of trim system/AFM revision LFV LVD3122 MITSUBISHI SB 231 Rev B 16-mar- 13-mar-09 PCW 4625A-2001 NYGE TDM01-45 01 JCAB AD TCD- De-ice system Modification FINNISH AD M 2461/97 LFV LVD2800 01-May- 14-jul-04 PCW 4626-97 MITSUBISHI SB 232 Rev A 1997 JCAB AD TCD- Mod. of Bearing box Ldg. Act. FINNISH AD M 2495/97 LFV LVD2819 01-jun-97 25-mar-99 4684-97 MITSUBISHI SB 230

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 182(195) JCAB AD TCD- Ändring av flyghandbok LVD FINNISH AD M 2518/98 LFV LVD2922 18-feb-98 02-dec-98 FAA AD utförd. 4753-98 2922,FAA AD 97-20-14, MHI SN 117A MITSUBISHI SN 117 Rev D JCAB AD TCD - Icing -related incidents VIDEO FAA, U.S AD 2003 -22 -07 Rev 1 24 -feb -04 11 -dec -03 4753A-2004 JCAB AD TCD - Inspection of landing gear power FINNISH AD M 2574/98 LFV LVD2897 04 -aug - 24 -mar -09 N/A by model 4838 -98 train MITSUBISHI SB 235 98 JCAB AD TCD- Inappropriate calib. of eng. trq-meter MITSUBISHI SB 233 Rev B 21-jun-07 11-sep-07 Previously carried out, ref. SB 233A. 4889 -2-2007 JCAB AD TCD - Insp. of Engine Torque Indication FINNISH AD M 2608/98 LFV LVD2924 05 -nov - 14 -jul -04 PCW 4889 -98 System LFV 2924, MU SB 233 MITSUBISHI SB 233 Rev B 98 JCAB AD TCD - Check of flight idle FF LVD 2925, MU FINNISH AD M 2609/98 LFV LVD2925 04 -nov - 11 -Oct -2010 4890 -98 SB 234 98 JCAB AD TCD - Inspect the fuselage frame LFV LVD2988 MITSUBISHI SB 209 Rev B 17 -May - 24 -mar -09 N/A by model 5030 -99 1999 JCAB AD TCD - AFM revision LFV LVD3112 27 -nov - 12 -feb -02 5432 -2000 00 JCAB AD TCD - To prevent loss of airplane control LFV LVD3123 16 -mar - 12 -feb -02 5547-2001 01 JCAB AD TCD - Inspection of Tip Tank Brackets LFV LVD3166 MITSUBISHI SB 236 12 -sep - 10 -Oct -2001 5747-2001 01 JCAB AD TCD - Flap Drive Train Inspection LFV LVD3212 MITSUBISHI SB 237 27 -dec - 17 -jan -02 5864-2001 01 JCAB AD TCD - Pneumatic Line insp. LFV LVD3322 MITSUBISHI SB 239 17 -mar - 09 -sep -03 6127-2003 03 JCAB AD TCD - Inspection of Wing Attachment MITSUBISHI SB 241 Rev A 27 -dec - 17 -jan -07 c/o in conjunction with wingstudie 7030-2006 Hardware 06

LFV, Luftfartsverket LFV LVA 1011 A Kontroll av vingklaffarnas FAA, U.S AD 75-16-13 JCAB AD TCD- 05-feb-02 A 05-feb-02 N/A Ej tillämplig p.g.a. s/n. manöversystem 1094A-76 MITSUBISHI SB 167 Rev D LFV LVA 1012 Kontroll av propellerreglagets FAA, U.S AD 75-16-20 JCAB AD TCD-1188- 05-feb-02 05-feb-02 N/A Ej tillämplig p.g.a. s/n. montering 75 MITSUBISHI SB 168 Rev A LFV LVA 1013 Kontr. och mod. av låsning på nosställ JCAB AD TCD-1209-75 MITSUBISHI SB 169 05-feb-02 08-jun-87 Rev B LFV LVA 1014 A Kontr. & byte av motorinkl. FAA, U.S AD 78 -03 -05 JCAB AD TCD -1202 - 05 -feb -02 A 10 -apr -87 låsanordning 75 MITSUBISHI SB 171 Rev B MITSUBISHI SB 180 Rev A

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 183(195) LFV LVA 1083 Insp. & utbyte av lina för nödöppning JCAB AD TCD-1235-75 MITSUBISHI SB 170 05-feb-02 10-apr-78 N/A N/A due to s/n Rev A LFV LVA 1196 Isolering av strobe light från bränsle JCAB AD TCD -1370 -76 MITSUBISHI SB 174 06 -feb -02 06 -Oct -1987 N/A by s/n PART 1 Rev C LFV LVA 1197 A Förhindr. av värmeskador på JCAB AD TCD -1379 -1-80 MITSUBISHI SB 06 -feb -02 A 08 -jun -87 bak.motorpl. 177 Rev B LFV LVA 1238 Kontr. & byte av infästningsdet. 06-feb-02 21-apr-09 N/A by s/n trimrod LFV LVA 1546 Sprickundersökning av nosställ FAA, U.S AD 86 -15 -03 JCAB AD TCD -1768 - 06 -feb -02 08 -jun -87 1-85 MITSUBISHI SB 181 PART 2 Rev B LFV LVA 1583 Modifiering av bagageutrymme JCAB AD TCD -1817 -79 MITSUBISHI SB 182 05 -feb -02 08 -jun -87 N/A N/A due to s/n. LFV LVA 1740 Kontr.av brandvarnings-och JCAB AD TCD-2048-81 MITSUBISHI SB 187 05-feb-02 31-aug-09 N/A by s/n n"dstr"mskret Rev B LFV LVA 1753 Kontroll av låsmekanism i nosställ JCAB AD TCD-2070-81 MITSUBISHI SB 188 05-feb-02 16-May-1986 LFV LVA 1788 Kontroll/Utbyte av elledningar på JCAB AD TCD -2113 -82 MITSUBISHI SB 191 06 -feb -02 02 -aug -82 motor LFV LVA 1873 Insp./utbyte av infäst.till torsionsrör JCAB AD TCD -2252 -83 MITSUBISHI SB 189 06 -feb -02 14 -sep -95 Rev C LFV LVA 1942 Momentdragning/låsn.av koppl.i JCAB AD TCD -2342 -84 MITSUBISHI SB 196 06 -feb -02 16 -jun -87 varmlufts Rev A LFV LVA 438 Justering av bränslemängdsmätare JCAB AD TCD -0643 -70 MITSUBISHI SB 114 05 -feb -02 16 -jul -86 N/A N/A by s/n LFV LVA 439 Rev. av flyghandbok betr. JCAB AD TCD -0642 -70 MITSUBISHI SB 112 05 -feb -02 16 -jul -86 N/A by model bränslespec. Rev C LFV LVA 456 Inspektion av bultar i nossst,ll JCAB AD TCD -0652 -70 MITSUBISHI SB 119 05 -feb -02 26 -mar -09 N/A by model LFV LVA 457 Utbyte av lager i nosst,llets st"td,mp. JCAB AD TCD -0660 -70 MITSUBISHI SB 123 05 -feb -02 26 -mar -09 N/A by s/n LFV LVA 543 B Insp. och målning av integraltankar JCAB AD TCD-0730-1-72 05-feb-02 B 14-jul-04 N/A N/A by s/n. LFV LVA 645 Modifiering av el -system JCAB AD TCD -0859 -72 MITSUBISHI SB 156 05 -feb -02 08 -dec -09 N/A by A/C serial number LFV LVA 664 Nosställsväxellåda och struktur JCAB AD TCD -0866 -72 05 -feb -02 31 -aug -09 N/A by s/n & model LFV LVA 828 A Kontr. & mod. av klaffdrivning JCAB AD TCD -0947A -74 MITSUBISHI SB 05 -feb -02 A 06 -Oct -1987 N/A N/A due to s/n. 162 Rev A LFV LVA 829 A Inspektion av frontrutor FAA, U.S AD 74 -11 -01 FAA, U.S AD 75 -03 - 05 -feb -02 A 15 -jul -86 N/A N/A due to s/n. 06 JCAB AD TCD-0948A-74 MITSUBISHI SB 163 Rev B LFV LVA 886 A Kontroll/byte av höjdtrimroderarmar JCAB AD TCD -1001A -76 05 -feb -02 A 16 -jun -86

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 184(195) LFV LVD 1238 Kontr./byte infästn.det. 15-apr- 27-mar-09 N/A se LVA 886A & FAA AD 84-25-02 höjdtrimroder 77 LFV LVD 1971 Elevator Trim Tab MU2 SB 176E JCAB AD TCD -1001B -2-84 18 -jan -85 16 -jun -86 LFV LVD 2015 B Pitot Tube Wiring MAI SR 020/34 -005 FAA, U.S AD 86 -20 -01 JCAB AD TCD - 24 -May - B 29 -jan -87 Rev A, MHI SR 53 2450A-87 MAI SR 020/34-005 MITSUBISHI 1985 SR 053A LFV LVD 2037 Flap Flexible Shaft MU2 SB 198 JCAB AD TCD -2451 -85 MITSUBISHI SB 198 30 -sep - 16 -May -1986 85 LFV LVD 2069 Altimeter 25 -mar - 18 -aug -87 N/A N/A by p/n & s/n 86 LFV LVD 2113 Modif. & revision Handbook MHI SR 26 -jan -87 06 -Oct -1987 006B, MAI SR 040/74-001RA LFV LVD 2190 Autopilot Switch MU2 SB 066/22 -006 FAA, U.S AD 88 -13 -01 MAI SB 066/22 -006 19 -aug - 03 -mar -88 och SB 206 Rev A MITSUBISHI SB 206 88 LFV LVD 2191 Generator System MU2 SB 201A JCAB AD TCD -2545 -1-88 MITSUBISHI SB 19 -aug - 24 -mar -09 N/A by s/n 201 Rev A 88 LFV LVD 2202 Kontr. av koppl. för tors.rör till klaff FAA, U.S AD 88 -23 -01 JCAB AD TCD -2252 - 08 -dec - 14 -sep -95 1-87 MAI SB 067/27-008 Rev A 88 MITSUBISHI SB 189 Rev C LFV LVD 2206 Modifiering av Autopilot FAA, U.S AD 88 -21 -01 Rev 1 08 -Dec - 12 -feb -02 1988 LFV LVD 2338 Kont./Mod.av sidorodrets JCAB AD TCD -3378 -90 MITSUBISHI SB 211 28 -mar - 14 -jul -04 N/A N/A by s/n. trimroderframka Mitsubishi MHI SB 91 211 LFV LVD 2347 1 Control Deice -system Mitsubishi SB JCAB AD TCD -3393A -96 MITSUBISHI SB 29 -May - 1 07 -Oct -2010 212A 212 Rev A 1996 LFV LVD 2352 Shoulder Harness Inst. FAA AC 43 -13 23 -May - 19 -jun -91 checked OK. CHPT 9 1991 LFV LVD 2450 Elevator Trim Tab Installation MU SB JCAB AD TCD -3740A -98 MITSUBISHI SB 03 -dec - 08 -apr -93 216 216 92 LFV LVD 2477 Electric Trim System AD930711, MU FAA, U.S AD 93 -07 -11 MAI SB 079/27 -010 03 -jun -93 27 -mar -09 N/A by s/n SB 079/27-0-010 LFV LVD 2512 TIP TANK INST. (NXT 100H) JCAB AD TCD -3901 -93 MITSUBISHI SB 221 02 -dec - 16 -nov -94 93 LFV LVD 2537 Reducering av Höjdrodrets FAA, U.S AD 94 -04 -16 MITSUBISHI SB 216 07 -apr - 08 -apr -93 trimområde. FAA AD 94-04-16, SB 94 216 LFV LVD 2538 Byte Låspinne i landställets nödutf. SB JCAB AD TCD -3942 -94 MITSUBISHI SB 219 07 -apr - 01 -feb -94 219 Rev A 94

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 185(195) LFV LVD 2551 Adj.of Ground Idle FAA AD 94-11-04 FAA, U.S AD 94-11-04 22-jun-94 27-mar-09 N/A by s/n LFV LVD 2592 Insp/Repl. of Lock -pin in L/G gearbox JCAB AD TCD -3942 -1-94 MITSUBISHI SB 09 -feb -95 01 -feb -94 TCD-3942-1-94, MSB 219A 219 Rev A LFV LVD 2678 Kontr. av vindrutor och fönster MHI FAA, U.S AD 2003 -17 -04 JCAB AD TCD - 12 -mar - 07 -Oct -2010 SB 224 Rev A 4311-95 MITSUBISHI SB 224 Rev C 96 LFV LVD 2688 Kontr/byte av infästn.bult för tiptank FAA, U.S AD 98 -20 -39 JCAB AD TCD -4310 - 09 -May - 24 -Oct -1996 MU-2 SB 225 96 MITSUBISHI SB 225 1996 LFV LVD 2689 Kontroll av linkage för prop.flöjning JCAB AD TCD-4379-96 MITSUBISHI SB 229 09-May- 30-jul-96 MU-2 SB 229 1996 LFV LVD 2732 Inspection/ Replacement of Prop FAA, U.S AD 96-18-14 HARTZELL SB 61- 27-sep- 01-sep-99 Prop. utbytt mot BVA Hub. FAA AD 96-18-14, Hz SB 136H 261 Rev 1 96 LFV LVD 2749 Revision av flyghandbok AFM TCD- FAA, U.S AD 96-25-02 JCAB AD TCD-4552- 21-jan-97 12-nov-97 4552-96 96 LFV LVD 2757 Sprickkontr. av landst,l.Side Brace FAA, U.S AD 97-01-01 Rev 1 14-feb-97 12-nov-97 Stud AD 97-01-01 LFV LVD 2761 Installation av autoignition system JCAB AD TCD-2679A-97 MITSUBISHI SB 14-feb-97 29-mar-99 TCD-2679A-97 226 Rev E LFV LVD 2769 Demont.av backventil i FAA, U.S AD 97-04-13 MITSUBISHI SB 130 18-mar- 05-May-1997 N/A N/A due to s/n. bränslesystemets MU-2 SB 130A Rev A 97 LFV LVD 2799 **RECOVERED RECORD** 09-feb-01 LFV LVD 2800 Mod. av De -ice Monitoring System JCAB AD TCD -4626 -97 MITSUBISHI SB 232 28 -aug - 12 -May -1998 Mitsubishi SB 232, TCD-4626-97 Rev A 97 LFV LVD 2819 Mod.av lagerboxar för JCAB AD TCD -4684 -97 MITSUBISHI SB 230 18 -nov - 12 -jun -98 landställssystem Mitsubishi SB 230 97 LFV LVD 2853 Periodisk funktionskontroll av 23 -mar - 07 -Oct -2010 nödutgång 98 LFV LVD 2897 Kontroll av landst,llets drivsystem JCAB AD TCD -4838 -98 MITSUBISHI SB 235 02 -aug - 24 -mar -09 N/A by model TCD-4838-98, SB 235 98 LFV LVD 2898 Mod. av autopilotens höjdtrimsystem JCAB AD TCD -3740A -98 MITSUBISHI SB 27 -aug - 18 -nov -98 TCD-3740A-98, SB 216, 228 216 MITSUBISHI SB 228 98 LFV LVD 2922 Änd.av Flyghandbok -Extra krav på JCAB AD TCD -4753 -98 MITSUBISHI SN 117 12 -nov - 02 -dec -98 FAA AD utförd. typutbi TCD-4753-98, MHI SN 117A Rev D 98 LFV LVD 2924 Kontr/Just av motorernas Torque JCAB AD TCD -4889 -98 MITSUBISHI SB 233 01 -dec - 23 -feb -00 indikeri MHI SB 233, TCD-4889-98 Rev B 98 LFV LVD 2925 Kontr/just av mot bränsleflöde Flight JCAB AD TCD -4890 -98 MITSUBISHI SB 234 01 -dec - 11 -Oct -2010 Id MHI SB 234 98 LFV LVD 2988 Sprickkontroll av kroppsspant JCAB AD TCD -5030 -99 MITSUBISHI SB 209 18 -jun -99 24 -mar -09 N/A by model Rev B

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 186(195) LFV LVD 3112 Revision av flyghandbok JCAB AD TCD-5432-2000 30-jan-01 12-feb-02 LFV LVD 3122 Modifiering av autopilotsystemet JCAB AD TCD -4625A -2001 MAI SB 093/22 - 02 -apr - 09 -feb -01 009 MITSUBISHI SB 231 Rev B NYGE 01 TDM01-45 LFV LVD 3123 Ändring av flyghandbok JCAB AD TCD -5547 -2001 02 -apr - 12 -feb -02 01 LFV LVD 3166 Sprickkontroll av infästning till ving - JCAB AD TCD -5747 -2001 MITSUBISHI SB 20 -sep - 10 -Oct -2001 spetstank 236 01 LFV LVD 3212 Kontroll av vridaxel till vingklaff. JCAB AD TCD -5864 -2001 MAI SB 099/27 - 09 -jan -02 17 -jan -02 012 MITSUBISHI SB 237 LFV LVD 3322 Kontroll av tryckluftsledningar JCAB AD TCD -6127 -2003 MITSUBISHI SB 21 -mar - 09 -sep -03 239 03

MAI, Mitsubishi Aircraft International MAI SB 047/30 - A Torque of Bleed Air Tube Coupling FAA, U.S AD 84 -12 -04 MITSUBISHI SB 196 19 -jul -84 A 16 -jun -87 001 Nuts AD 84-12-04,SB 196A Rev A MAI SB 051/27 - Add.Seal and Flap Flexible Shaft FAA, U.S AD 87 -04 -03 01 -feb -85 16 -May -1986 007 Torque AD 87-04-03, SB 198 MAI SB 066/22 - A Bendix Autopilot Disengagement AD FAA, U.S AD 88 -13 -01 FAA, U.S AD 88 -21 - 06 -jun -89 03 -mar -89 Data transferred/updated on WO C05770 006 88-13-01, AD 88-21-01 R1 01 Rev 1 LFV LVD2190 MAI SB 069/24-006 MAI SB 067/27 - A Insp/Repl. of Flap Control System FAA, U.S AD 88 -23 -01 LFV LVD2202 29 -mar - A 14 -sep -95 008 Torque AD 88-23-01, SB 189B 95 MAI SB 069/24 - Split Radio Bus Inspection and MAI SB 066/22 -006 Rev A 17 -nov - 03 -mar -88 N/A N/A due to Aircraft s/n 006 Rework 88 MAI SB 086/74 - A Auto -Ignition System Installation FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH AD 05 -Oct - A 22 -nov -01 Action not required due to s/n. 002 M 2435/97 MITSUBISHI SB 226 Rev E 2000 MAI SB 089/57 - A Insp/Repl. of Bolts for Wing Tip Tank FAA, U.S AD 98 -20 -39 05 -nov - A 24 -Oct -1996 N/A N/A due to s/n. 002 96 MAI SB 093/22 - Trim -In -Motion Alert System FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH AD 08 -jul -97 09 -feb -01 009 M 2460/97 UPPHÄVD JCAB AD TCD-4625- 97 LFV LVD3122 MITSUBISHI SB 231 Rev B MAI SN 110/00 - Power Lever Position Warning 25 -feb -09 09 -nov -09 SB 240 considered 017A MAI SN 111/77 - Torque Indicating System Shift 20 -nov - 11 -mar -09 SB 233 considered 004 Potential 08 MAI SR 020/34 - Anti Ice Capability AD 86 -20 -01, SR FAA, U.S AD 86 -20 -01 LFV LVD2015 Rev B 06 -Oct - 15 -feb -00 N/A N/A due to s/n.

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 187(195) 005 053A MITSUBISHI SR 053A 1986

MITSUBISHI, Mitsubishi Heavy Industries Ltd MITSUBISHI MSB A **RECOVERED RECORD** A 18 -jul -86 N/A 24-002 MITSUBISHI MSB **RECOVERED RECORD** 18 -jul -86 N/A 24-004 MITSUBISHI MSB **RECOVERED RECORD** 18 -jul -86 N/A 27-001 MITSUBISHI MSB **RECOVERED RECORD** 18 -jul -86 N/A 27-003 MITSUBISHI MSB **RECOVERED RECORD** 18 -jul -86 N/A 27-005 MITSUBISHI MSB **RECOVERED RECORD** 18 -jul -86 N/A 27-006 MITSUBISHI MSB **RECOVERED RECORD** 18 -jul -86 N/A 27-007 MITSUBISHI MSB A **RECOVERED RECORD** A 18 -jul -86 N/A 30-001 MITSUBISHI MSB A **RECOVERED RECORD** A 18 -jul -86 N/A 32-001 MITSUBISHI MSB **RECOVERED RECORD** 18 -jul -86 N/A 32-004 MITSUBISHI MSB **RECOVERED RECORD** 18 -jul -86 N/A 32-006 MITSUBISHI MSB **RECOVERED RECORD** 18 -jul -86 N/A 32-010 MITSUBISHI MSB **RECOVERED RECORD** 18 -jul -86 N/A 34-004 MITSUBISHI MSB **RECOVERED RECORD** 18 -jul -86 N/A 34-007 MITSUBISHI MSB **RECOVERED RECORD** 18 -jul -86 N/A 54-001 MITSUBISHI MSB A **RECOVERED RECORD** A 18 -jul -86 N/A 54-002 MITSUBISHI MSB B **RECOVERED RECORD** B 18 -jul -86 N/A

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 188(195) 71-003 MITSUBISHI MSB **RECOVERED RECORD** 18 -jul -86 N/A 71-005 MITSUBISHI MSR B **RECOVERED RECORD** B 06 -Oct - 066 1987 MITSUBISHI SB Bendix M4D 18 -dec - 06 -mar -89 Info transfererad till SB 066/222 -006 ref C05770 066 87 MITSUBISHI SB M-4() Autop.Engage Switch Guard 11-apr- 16-nov-94 076/22-008 Install. 91 MITSUBISHI SB C Anti-Ice Additive in Fuel -Usage of JCAB AD TCD-0642-70 LFV LVA439 09-Oct- C 16-jul-86 112 1971 MITSUBISHI SB Fuel Quantity Indicator Readjustmnet JCAB AD TCD-0643-70 LFV LVA438 01-jan-70 15-jul-04 N/A N/A by s/n. 114 MITSUBISHI SB The Bolt and Bolt Hole Diam. of Nose JCAB AD TCD-0652-70 LFV LVA456 10-mar- 26-mar-09 N/A by model 119 L.G 70 MITSUBISHI SB Bearing,Oleo Strut,Nose L.G. -Repl. of JCAB AD TCD-0660-70 LFV LVA457 01-apr- 26-mar-09 N/A by s/n 123 70 MITSUBISHI SB Scissors Switch,Nose L.G. -Install. of 31-aug- 17-jul-86 N/A 124 70 MITSUBISHI SB B Tip Tank Air Pressure Modification 28-jun-94 B 05-nov-09 N/A by model & s/n 128 MITSUBISHI SB B Top Coating, Wing Integral Main F.T.- JCAB AD TCD-0730-1-72 JCAB AD TCD- 05-jan-72 B 14-jul-04 N/A N/A by s/n. 143 SIo 0730-2-86 MITSUBISHI SB A Flex. Shafts, Flap Control Sys.-Insp. of JCAB AD TCD-0947A-74 LFV LVA828 Rev A 03-Oct- A 06-Oct-1987 N/A 162 (AD750201) 1974 MITSUBISHI SB B Insp. of Outer Pane, Front Winds. & FAA, U.S AD 74-11-01 JCAB AD TCD- 16-nov- 15-jul-86 N/A 163 Inst 0948A-1-78 JCAB AD TCD-0948A-74 LFV 78 LVA829 Rev A MITSUBISHI SB A Lubr. Interval,Wheel Bearing,Main & 24-jul-80 03-mar-77 N/A 165 Nose MITSUBISHI SB D Flap M.Jack Screw-Insp. of and/or FAA, U.S AD 75-16-13 JCAB AD TCD- 24-jul-80 D 05-feb-02 N/A Ej tillämplig p.g.a. s/n. 167 Main G 1094A-76 LFV LVA1011 Rev A MITSUBISHI SB A Propeller Pitch Control Lever-Insp. of FAA, U.S AD 75-16-20 JCAB AD TCD-1188- 24-jul-80 A 10-nov-82 168 (AD761620) 75 LFV LVA1012 MITSUBISHI SB B Shimmy Damper-Insp. and JCAB AD TCD-1209-75 LFV LVA1013 24-jul-80 B 05-nov-09 PCW 169 Modification of MITSUBISHI SB A MLG Forward Door Em.Op. Cable- JCAB AD TCD-1235-75 LFV LVA1083 24-mar- A 17-jul-86 N/A N/A due to s/n 170 Insp. & Re (AD762204) 77

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 189(195) MITSUBISHI SB B Latches,Eng. Nacelle Upper D.-Insp.& FAA, U.S AD 78-03-05 JCAB AD TCD-1202- 17-nov- B 10-apr-78 171 Mod (AD780305) 75 LFV LVA1014 Rev A 77 MITSUBISHI SB A Drag Strut, Main L.G. -Modification of JCAB AD TCD -1284 -1-76 24 -jul -80 A 06 -feb -06 N/A N/A due to s/n 173 MITSUBISHI SB C Tip Tank Conduit Tube -Insp.of,and FINNISH AD M 1177/83 JCAB AD TCD - 02 -Oct - C 06 -Oct -1987 N/A by s/n 174 PART 1 Rew.of (AD830902) 1370A -81 LFV LVA1196 1981 MITSUBISHI SB C Tip Tank Conduit Tube Rework 02-Oct- C 06-Oct-1987 N/A N/A by A/C S/N 174 PART 2 1981 MITSUBISHI SB Barrel Nut, Inner/Outer Wing Conn. - JCAB AD TCD -1353 -76 26 -jun -76 24 -aug -76 175 Repl. MITSUBISHI SB E Elevator Trim Tab Bracket -Repl. of FAA, U.S AD 84 -25 -02 FINNISH AD M 26 -sep - E 16 -jun -86 176 LVD1971, AD 84-25-02, SB 031/27- 1080/82 JCAB AD TCD-1001A-76 JCAB AD 84 005R1 TCD-1001B-2-84 LFV LVD1971 MITSUBISHI SB B Mod. of Engine Nacelle Tail Area JCAB AD TCD-1379-1-80 LFV LVA1197 Rev 11-sep- B 08-jun-87 177 (AD810601) A 80 MITSUBISHI SB Rodd Assem., Engine Nacelle Upper 27-May- 08-jun-78 179 D.-R&M 1977 MITSUBISHI SB A Link, Engine Nacelle Upper D. -Repl. of FAA, U.S AD 78 -03 -05 JCAB AD TCD -1202 - 17 -nov - A 10 -apr -78 180 (AD780305) 75 JCAB AD TCD-1520A-77 LFV LVA1014 77 Rev A MITSUBISHI SB B Insp. and Repl. of Nose L.G. Strut FAA, U.S AD 86-15-03 JCAB AD TCD-1768- 08-apr- B 18-aug-87 181 PART 2 Assem (AD801812) 1-85 LFV LVA1546 85 MITSUBISHI SB Add. of Ceiling Cover, Rear Bagg. JCAB AD TCD-1817-79 LFV LVA1583 16-nov- 08-jun-87 N/A N/A due to s/n. 182 Comp. 79 MITSUBISHI SB Turnbuckle, Control Cables -Repl. of 04-apr- 14-nov-86 184 80 MITSUBISHI SB Down Lock Mech., Nose L.G.-Insp. of JCAB AD TCD-2070-81 LFV LVA1753 13-jul-81 16-May-1986 188 MITSUBISHI SB C Flap Control Torque Tube AD 88-23- FINNISH AD M 2722/00 JCAB AD TCD- 28-jun-94 C 14-sep-95 189 01, SB 067/27-008 2252-1-87 JCAB AD TCD-2252-83 LFV LVA1873 LFV LVD2202 MITSUBISHI SB Engine El. Wire-Insp. and JCAB AD TCD-2113-82 LFV LVA1788 21-dec- 02-aug-82 191 Replacement of (AD820802) 81 MITSUBISHI SB B Landing Gear Warning Horn 15-jun-94 B 04-dec-00 Rev A är utförd. 193 Syst.Modif. MITSUBISHI SB Master Cauting Light Visibility-Impr. 23-aug- 16-May-1986 194 of 82 MITSUBISHI SB A Ret. of coupling nut on the bleed air FAA, U.S AD 84-12-04 JCAB AD TCD-2342- 12-apr- A 16-jun-87 196 tu AD 84-12-04, SB 047/30-001 1-84 JCAB AD TCD-2342-84 LFV LVA1942 84

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 190(195) MAI SB 047/30-001 Rev A MITSUBISHI SB Add. Seal & Torque Insp. of Flap FAA, U.S AD 87 -04 -03 JCAB AD TCD -2451 - 13 -feb -85 16 -May -1986 198 Flex.Sh LVD2037, AD 87-04-03, SB 85 LFV LVD2037 051/27-007 MITSUBISHI SB A Engine Lubricating Tubing Insp. & 24 -jun -94 A 06 -nov -09 PCW 199 Protec MITSUBISHI SB B Insp of Nose Ldg Gear Drag Strut Link 24 -jun -94 A 19 -Mar -12 200 MITSUBISHI SB A Generator Circuit Wires Insp. and FAA, U.S AD 87 -12 -02 JCAB AD TCD -2545 - 02 -mar - A 24 -mar -09 N/A by s/n 201 Mod. 1-88 LFV LVD2191 88 MITSUBISHI SB Speed Placard Change 03 -mar - 14 -apr -89 204 87 MITSUBISHI SB Bendix Autop.Disengagement FAA, U.S AD 88 -13 -01 , JCAB AD TCD - 13 -Oct - 28 -Oct -2009 N/A Due to model 206 Method Stand 2856-1-97, LFV LVD2190 1987 MITSUBISHI SB Rudder T.T. & Elevator T.T. Insp. & 20 -May - 07 -Oct -2010 207 Rep. 1988 MITSUBISHI SB B Fuselage inspection JCAB AD TCD -5030 -99 LFV LVD2988 19 -apr - B 24 -mar -09 N/A by model 209 99 MITSUBISHI SB A Engine Ignition Unit Replacement 12 -nov - 06 -mar -98 210 96 MITSUBISHI SB Rudder Trim Tab Modification (LVD JCAB AD TCD -3378 -90 LFV LVD2338 20 -nov - 14 -jul -04 N/A N/A by s/n. 211 2338) 90 MITSUBISHI SB A Insp of Anti-ice/Deice Systems (LVD JCAB AD TCD-3393A-96 LFV LVD2347 Rev 25-apr- A 07-Oct-2010 212 2347), 1 96 MITSUBISHI SB Engine Control Rod Inspection 06 -dec - 08 -May -1992 214 91 MITSUBISHI SB Removel of Prop. Governor Speed 23 -Oct - 08 -May -1992 215 Signal 1991 MITSUBISHI SB Elevator Trim Tab Installation (LVD FAA, U.S AD 2007-17-09 FAA, U.S AD 94- 11-sep- 08-apr-93 216 2450 04-16 JCAB AD TCD-3740A-98 LFV 92 LVD2450 LFV LVD2537 LFV LVD2898 MITSUBISHI SB A Propeller Feathering Linkage 17 -jan -94 A 01 -feb -94 218 Inspection MITSUBISHI SB A Emergency Gear Down G.box Lower JCAB AD TCD -3942 -1-94 JCAB AD TCD - 24 -Oct - A 01 -feb -94 219 Pin Repl 3942-94 LFV LVD2538 LFV LVD2592 1994 MITSUBISHI SB Tip Tank Conduit Tube Insp. and Rep. JCAB AD TCD -3901 -93 LFV LVD2512 10 -aug - 01 -feb -94 221 93 MITSUBISHI SB Pitot/Static System Improvement SR MITSUBISHI SR 053A MITSUBISHI SR 064 28 -jun -94 15 -feb -00 223 064

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Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 191(195) MITSUBISHI SB C Acrylic Windsheild/Window glass FAA, U.S AD 2003-17-04 FINNISH AD M 30-apr- C 07-Oct-2010 224 Insp. UHB 3076 JCAB AD TCD-4311-95 LFV LVD2678 98 MITSUBISHI SB Forward fitting bult of wingtip tank FAA, U.S AD 98 -20 -39 FINNISH AD M 29 -sep - 24 -Oct -1996 225 LVD 2688 2351/96 JCAB AD TCD-4310-96 LFV 95 LVD2688 MITSUBISHI SB E Auto-Ignition System Installation LVD FAA, U.S AD 2000-09-15 Rev 1 FAA, U.S 18-sep- E 22-nov-01 PCW no further action (rev.E) required due to s/n. 226 2761 (2113), AD TCD-2679A-97 AD 86-26-02 FINNISH AD M 2435/97 01 FINNISH AD M 2786/00 JCAB AD TCD- 2679A-97 LFV LVD2761 MAI SB 086/74- 002 Rev A MITSUBISHI SB Rudder Torque Tube Modification 20 -dec - 08 -sep -97 227 96 MITSUBISHI SB Elevator Trim Indicator Modification FAA, U.S AD 2007 -17 -09 FINNISH AD M 13 -jul -98 18 -nov -98 228 LFV 2898 2581/98 JCAB AD TCD-3740A-98 LFV LVD2898 MITSUBISHI SB Feathering Valve/Linkage Insp. FAA, U.S AD 2006 -15 -07 JCAB AD TCD - 20 -feb -96 30 -jul -96 229 4379-96 LFV LVD2689 MITSUBISHI SB Mod.of Bearing Box Ldg. Gear Act. JCAB AD TCD -4684 -97 LFV LVD2819 05 -mar - 12 -jun -98 230 LVD 2819 97 MITSUBISHI SB B Inst.of Trim -In -Motion Alert System FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH AD 11 -dec - B 03 -mar -03 SL 079 performed earlier. 231 M 2460/97 UPPHÄVD FINNISH AD M 02 2786/00 JCAB AD TCD-4625A-2001 LFV LVD3122 MAI SB 093/22-009 NYGE TDM01-45 MITSUBISHI SB A De -Ice System Modification LVD FAA, U.S AD 2000 -09 -15 Rev 1 FINNISH AD 06 -jun -02 A 06 -jun -02 N/C due to previuosly complied with SB 232 rev 0. 232 2800, TCD-4626-97 M 2786/00 JCAB AD TCD-4626-97 LFV LVD2800 MAI SB 096/30 -004 MITSUBISHI SB B Insp.of Engine Torque Indication FAA, U.S AD 2006 -17 -01 FINNISH AD M 08 -mar - B 18 -apr -07 Checked, previously carried out 233 System. TCD-4889-98, LFV 2924 2608/98 JCAB AD TCD-4889-2-2007 JCAB 07 AD TCD-4889-98 LFV LVD2924 MITSUBISHI SB Fl.Check of the Flight Idle Fuel Flow FAA, U.S AD 2006-17-05 JCAB AD TCD- 07-Oct- 11-Oct-2010 234 Se TCD-4890-98, LVD 2925 4890-98 LFV LVD2925 1998 MITSUBISHI SB Inspection of landing gear power JCAB AD TCD-4838-98 LFV LVD2897 04-aug- 24-mar-09 N/A by model 235 train 98 MITSUBISHI SB Inspection of Tip Tank Brackets JCAB AD TCD -5747 -2001 LFV LVD3166 28 -aug - 10 -Oct -2001 236 01 MITSUBISHI SB Inspection of Flap Drive Train JCAB AD TCD -5864 -2001 LFV LVD3212 13 -dec - 17 -jan -02 237 01 MITSUBISHI SB Main Landing Gear Door Safety Pin 05-dec- 09-jan-03 Perf. at each 600 h. insp. 238 02

Öppen/Unclassified

Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 192(195) MITSUBISHI SB Pneumatic Line Insp. and JCAB AD TCD-6127-2003 26-dec- 09-sep-03 239 Modification 02 MITSUBISHI SB Inst.of Trottle Quadrant Placard 26 -feb -03 02 -jun -03 240 MITSUBISHI SB A Inspection of Wing Attachment FAA, U.S AD 2006 -13 -15 JCAB AD TCD - 21 -nov - A 17 -jan -07 c/o in conjunction with wingstudie 241 Hardware 7030 -2006 06 MITSUBISHI SL 060 System 17-feb-89 24-jul-91 MITSUBISHI SL 078 Automatic Autopilot Disconnect 28-jan-02 07-Oct-2010 System MITSUBISHI SL 079 Diode inst.in Flap Position Ind.Curcuit 28-jan-02 09-feb-01 Carried out by Mitsubishi (manufacturing-made) MITSUBISHI SL 080 Hartzell Propeller Mounting Bolt Insp. HARTZELL SB 61 -256 05 -apr - 26 -aug -02 Compliance in according to HC -SB -61 -256. 02 MITSUBISHI SL 084 Pneumatic De -Ice Monitoring System 14 -jun -04 07 -Oct -2010 MITSUBISHI SL 085 Hartzell prop. mount. bolt insp. HARTZELL SB 61 -279 ALERT Rev 4 17 -May - 14 -sep -05 2005 MITSUBISHI SN B Rudder Torque Tube AD 86 -20 -01, SB 05 -nov - B 26 -Oct -1987 053 020/34-005 86 MITSUBISHI SN D Icing Awareness Training Video FAA, U.S AD 2003 -22 -07 Rev 1 JCAB AD 14 -jun -04 D 11 -dec -03 117 TCD-4753-98 LFV LVD2922 MITSUBISHI SN Water Ingress into Vertical Stabilizer 19 -dec - 30 -apr -04 146 03 MITSUBISHI SN Reminders for safe operation 18 -nov - 22 -mar -06 Genomförs enl. AMP MU -2 & DHB 148 05 MITSUBISHI SN Power Lever Position Warning 25 -feb -09 09 -nov -09 SB 240 considered 156A MITSUBISHI SN Torque Indicating System Shift 20 -nov - 11 -mar -09 SB 233 considered 157 Potential 08 MITSUBISHI SN Repl Air Filter for Vacuum System MITSUBISHI STCSA01913SE 09 -dec - 11 -mar -10 Ref STC SA01913SE 161 09 MITSUBISHI SR Modifiering av pitotrör FAA, U.S AD 86 -20 -01 JCAB AD TCD - 23 -Oct - 12 -May -1998 053A 2450A-87 LFV LVD2015 Rev B MAI SR 1984 020/34-005 MITSUBISHI SB 223 MITSUBISHI SR Pitot & Static System MITSUBISHI SB 223 30 -apr - 15 -feb -00 064 85 MITSUBISHI SR Warning Horn 20 -jan -86 13 -Oct -1987 065 MITSUBISHI SR Emergency Exit Placard 17 -sep - 18 -aug -87 067 85

Öppen/Unclassified

Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 193(195) MITSUBISHI SR Air Filter Replacement for Vacuum 25-apr- 14-dec-01 072 Syst. 00 MITSUBISHI SR Inst. tip tank placard 29 -Oct - 29 -apr -05 075 2004 MITSUBISHI STC Inst of a Vacuum System Air Filter MITSUBISHI SN 161 10 -dec - 11 -mar -10 See MU -2B AMP Chpt 3 100h/1y inspection SA01913SE 09

NARCO, Narco NARCO SB ELT10 - ELT ASSY 18 -apr - 19 -jun -91 N/A 16 88

NYGE, Saab Aerotech Aircraft Services NYGE TDM 00 -18 Förstärkning av tidigare utförd skarv - 19 -Oct - 27 -Oct -2000 Reparation utförd reparation kroppsida 2000 NYGE TDM 00 -21 Domkraftskada 12 -dec - 09 -feb -01 00 NYGE TDM 00 -23 Wiring Left Wing ADRIAN 22 -dec - 25 -jan -00 00 NYGE TDM 02 -24 Installation Moving MAP 10 -Oct - 18 -dec -02 2002 NYGE TDM 02 -32 Installation EMI film 10 -dec - 10 -jan -04 02 NYGE TDM 03 -08 8 GNS430/530 & MODE S GTX330 04 -mar - 8 16 -Oct -2008 install. 03 NYGE TDM 03 -28 F Nav Demo Pod 19 -dec - F 21 -jan -10 Doubler/Grommet/Connector remain to install. Ref. 03 defectlog No:869 Original compliance by Rev D. Not affected by rev F. NYGE TDM 05 -16 Viktor Counter Weight Pod 18 -nov - 18 -nov -05 05 NYGE TDM 06 -41 A Darts (to carry on MU -2B -20/26) 20 -nov - A 07 -feb -08 06 NYGE TDM 06 -42 A Barlast DARTS MU -2B 04 -dec - A 07 -feb -08 07 NYGE TDM 07 -30 A Install. of Emergency Axe 28 -feb -08 A 28 -feb -08 NYGE TDM 08-03 A Enhanced Surveillance MU-2B 28-feb-08 A 07-sep-09

Öppen/Unclassified

Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 194(195) NYGE TDM 08-28 B ELT 406 MU-2B 29-sep- B 16-Oct-2008 Original compliance with TDM rev A. Rev B does not 08 affect previous complaiance. NYGE TDM 09 -32 A GPS Splitter 12 -nov - A 21 -jan -10 09 NYGE TDM 10 -02 A Target surveillance camera 03 -jun -10 A 15 -jun -10 NYGE TDM 10 -03 A Pressure Bulkhead Feed Through 04 -May - A 15 -jun -10 2010 NYGE TDM 10-25 A MU-2B Terminating Resistor 08-apr- A 18-May-2010 C/W 10 NYGE TDM 11-35 A Terminating resistor 30-Jan-12 NYGE TDM 12 -21 A Avinstalltion IK 14 -Aug -12 NYGE TDM 95 -04 4 Vingstudie 20 -sep - 31 -mar -08 98 NYGE TDM 99 -12 Avionic Modification SE -IUA 14 -dec - 07 -feb -00 99 NYGE TVO 1/09 Inspektion av Stringers & struktur 25 -feb -09 02 -mar -09 Inspected u/a vinge NYGE TVO 1/93 Low Volt Warning Light (BCL) 22 -jan -93 08 -apr -93 NYGE TVO 1/96 Slitage Flap Guide Rail 12 -apr - 09 -feb -00 96 NYGE TVO 1/97 3 De -Icertank MU -2B, 12 -feb -97 10 -mar -97 korrosionskontroll NYGE TVO 2/00 Märkning av infästning domkraft Mu2 01 -dec - 09 -feb -01 00 NYGE TVO 2/07 A Prevent FR31 radio to xmit when 06 -feb -07 A 02 -mar -07 RM2 off NYGE TVO 2/10 1 Visual inspection of center wing 19 -apr - 1 09 -jul -10 10 NYGE TVO 2/91 A/C Elecrical System 10 -jan -91 08 -May -1992 NYGE TVO 3/06 Inspect lower rudder hinge bracket 07-dec- 07-Oct-2010 06 NYGE TVO 3/96 3 Wing Spar Flange Inspection. 24-feb-05 3 01-jun-09 NYGE TVO 4/11 A Static inverter control 15 -Dec -12 NYGE TVO 4/86 2 Wing Pod Inspection 06 -apr - 2 07 -Oct -2010 92

Öppen/Unclassified

Datum Diarienummer Ärendetyp 2012-12-06 ange ange

Dokumentnummer Sida ange 195(195) NYGE TVO 4/91 Special Inspection (next E6.) 19-feb-91 08-May-1992 NYGE TVO 4/92 Engine Install. Kontr. rörledningar 29 -apr - 09 -nov -92 92 NYGE TVO 4/94 3 Fwd. Wing Tiptank Attachment 28 -sep - 3 07 -Oct -2010 94 NYGE TVO 4/96 Kontroll av Lagerhus i 25 -Oct - 19 -aug -97 Utförd tidigare (ref. Ove N. lista) noshjulsstyrning. 1996 NYGE TVO 6/88 Allm. instruktion för metallpropeller 13-jun-88 09-jul-10 NYGE TVO 6/92 Elevator Trim Cable, check 07 -Oct - 09 -nov -92 1992 NYGE TVO 7/05 RMI -nål park. ej / ILS frekvens är vald 11 -nov - 01 -nov -05 05 NYGE TVO 7/93 Starter Drive Splines 01 -nov - 16 -nov -94 93 NYGE TVO 8/04 Kontr. av Spant vid bakre 08 -dec - 30 -nov -09 feninfästning 04 NYGE TVO 8/92 Wheel Parts 27 -Oct - 08 -apr -93 1992