Aviation, Inc

Aircraft Record General lnformatiori

Manufacturer e12-..:iS 12 d... ~ Model C -1,Q / -fi- 0 g~ ~ Serial ______Registration Number Lt/ /.,5?~ 6? Date of Manufacture / c2 - !/ - / U)I

Engine(s} currently installed:

Manufacturer ______Model ______Serial ______Manufacturer Model ______Serial ______

Propeller(s) currently installed:

Manufacturer ______Model ______

HUB Model ______Serial ______Serial ______

Blade Model ______Serial ______Serial ______Serial ______

Blade Model ______Serial ______Serial Serial ______

© 1992 ASA ~ Description of Inspections, Test~, Repairs ~nd Alterations \ RECORDING TODAYS TOTAL I DATE Entries must be endorsed with Name, Rating and Cert1f1cate Number of TACH FLIGHT TIME IN \ Technician or Repair Facility. (See back pages for other specific entries.) 19 __ TIME SERVICE \•

DATE: 4/21/2012 L.ur-Stevu,s llviation Hobbs: 48.7 5172 suite C W·/Ylilitary J..IWY AITT: 5829. 6 Chesapeake, VII 23321

© 1991 ASA 'E RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations JACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

DATE: 5/19/2012 kar-Stl!.vens flviation Hobbs: 85.0 5172 suit"' c W·/Ylilitary I-IWY ACTT:5865.9 Chesapeake, V.tl 23321

CtJmp/ietl wicl, AP 2000-07-16 f>qrq r.i;/ 6tJth engines due qgq1n 735·0 JltJ/,/,s· rlircrqfl dps· Cl,ecA'ed di'/ grtJund q// t ...... ,,-,-L'.J ~,ressures ntJrmq/, /ltJ /eqA's ntJcetl qc chi, cime· Jbl,n · 5t?ndt. 1/0'r· 3527277//&P ~

0 - - .SQ~ DATE RECORDING TODAYS TOTAL Description of Inspections, Tests Repa·, TACH . ' rs and Alt . FLIGHT TIME IN Entries must be endorsed with Name, Rating and c rt·f· erat1ons 19 ___ TIME . . R . e i icate Numb SERVICE T ech nic1an or epair Facility. (See back pages for oth . . er of er specific entries.)

MAKE: Cessna Aerodyne Corporation DATE: 11/9/2012 MODEL· 421B NC TSN: 5896.9 - SIN: 421 B0822 Repair Station No. HO1 R-199K HOBBS: 116 REG. NO: N1592G B 5198 West Military Highway WORK ORDER: 19987 Chesapeake, VA 23321 USA Phone: (757) 488-2898 Airframe Entries (1) Completed Annual Inspection in accordance with manufacturer's instructions and recommendations ...... (2) Completed left engine 1oo hour inspection in accordance with the manufacturer's instructions and recommendations. Compression check: No compression check. Engine removed and repaired with new piston rings installed. Cleaned, gapped and tested spark plugs. Checked ignition timing. Cleaned engine ...... (3) Completed right engine 100 hour inspection in accordance with the manufacturer's instructions and recommendations. Compression check: #1-72/80, #2-75/80, #3-66/80, #4-64/80, #5-73/80, # 6-70/80. Cleaned, gapped and tested spark plugs. Checked ignition timing. Cleaned engine ..... : ....(4) Completed left propeller 100 hour inspection in accordance with the manufacturer's instructions and recommendations. Denicked blades...... (5) Completed right propeller 100 hour inspection in accordance with the manufacturer's instructions and recommendations. Denicked blades ...... (6) Complied with AD 2000-01-16 "Crack ~nd Corrosion in Exhaust System" Part B by visual inspection of the exhaust systems of tne left and right engine. Part B due again in 50 hours at 166.0 hobbs or 5946.9 ACTT ...... (7) Complied with AD 2007-05-15 uTo Prevent Failure of the Starter Adapter Assembly and or Crankshaft Gear'' by inspection of the starter adapter viscous damper and shaft-gear backlash check in accordance with Part 2 and removal and inspection of the starter adapter assembly in accordance with Part 3 of Continental Mandatory Service Bulletin MSB-94-4G. Part 2 due again at 5996.9 ACTT. Part 3 due again 6296.9 ACTT...... (8) Complied with AD 2007-05-15 "To Prevent Failure of the Starter Adapter Assembly and or Crankshaft Gear'' by inspection of the starter adapter viscous damper and shaft-gear backlash check in accordance with Part 2 of Continental Mandatory Service Bulletin MSB-94-4G. Part 2 due again at 5996.9 ACTT. Part 3 due at 5999.0 ACTT ...... (9) lr1stalled new ELT battery. The D&M Model 8.1, sin: 9268 ELT system installed in this aircraft was inspected and tested according to the applicable ELT manufacturer's instructions and the requirements of 14 CFR 91.207 d) and was determined to be in an airworthy condition. ELT BATTERY EXPIRES JANUARY 2015 ...... (1 0) 'lnstalled new heater hobbs meter. Old hobbs meter read 1475.5. New hobbs meter reads o...... (11) Removed left wheel assembly. Disassembled, cleaned and inspected. Installed n~w brake disc. Reassembled wheel. Installed new brake pads. Installed new brake shim. Reinstalled wrieel assembly...... (12) Removed right wheel assembly. Disassembled, cleaned and inspected. Installed new brake disc. Reassembled wheel. Installed new brake pads. Installed new brake shim. Reinstalled wheel assembly...... (13) Removed left engine fire bottle. Removed existing squib. Installed new squib pin: 13083-5. Reinstalled fire bottle. Replacement of squib due every 5 years. Next due Novembar 2017 ...... (14) Removed right engine fire bottle. Removed existing squib. Installed new squib pin: 13083-5. Reinstalled fire bottle.

1 of 2 i:> 1991 ASA C DATE RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations JACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of 19 TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

Replacement of squib due every 5 years. Next due November 2017 ...... (15) Installed new co-pilot's aft seat stop ...... (17) Installed new seat track stop on left rear outboard seat track ...... (18) Installed new left aux fuel tank sump drain valve ...... (19) Installed new taxi light lamp...... (20) Installed new rotating beacon light lamp...... (21) Installed new instrument air filter...... (22) installed new left and right vacuum regulator filters ...... (23) Installed new left and right main, left and right aux and left nacelle fuel tank cap o'rings ...... (24) Straightened right nacelle locker stay strut...... (25) Tightened right nacelle locker lock mechanism retaining nut...... (26) Adjusted upper cabin entry door stay strut to allow door to stay open when opened ...... (27) Cleaned and treated de-ice boots with Goodrich Age and Shine Master...... (28) Removed, cleaned, serviced, charged, tested and reinstalled battery...... (29) Changed right engine oil and filter. Installed 12 quarts of Phillips 20W-50 XC oil and Tempest AA48110-2 filter. Inspected removed filter. No contamination ...... (30) Installed new right alternator field capacitor adel clamp.

The aircraft identified hereon was inspected in accordance with an AN AL INSPECTION, found to be in an AIRWORTHY condition and approved for return to service.

DATE: 11/9/2012 SIGNED: Work Order: 19987 J.R. Smith Printed by EBis 3 (datcomedia.com) Certified Repair talion No. HO1R-199K

0 1991 ASA DATE RECORDING TODAYS TOTAL Description of Inspection::..~ r·ests, Repairs and Alterations •• ftll ,. lr!I 1i,.UT TIUI: IU f ,_• • ;_,.,,_.,...... , ..+ bo o nrll"\rcod ut.ith tili:J m ~tian ~nrl r.ortifit·•ate Number of 19_ ,,, ; {) a ;pecific entries.) PRECISION AVIATION, INC. I 8124 Lockheed, Houston, Texas 77061 - (713) 644-7383 9/2012 TEST & INSPECTION · FUNCTIONAL TEST I: 5897 Tl-1 : 11 6.1 OPERATING LIMITS LEVEL FLIGHT ~- REJECT □ 20° BANK L & R ~ REJECT □ 20° DIVE FINAL ~ REJECT □ ned OPER. 20° c·LIMB :: -::-....:-~. ~ck INSP. ~ REJECT □ COMPENSATION. MECH[]~ .~AST ~ WEST .-. work NORTH - SOUTH STOCK: - =¾~~ SCALE ERROR GK:[] - REJECT □ 20023 FRICTION BY DATE ____ ~□> REJECT □ 3.com) SH---IP___ M_E_N_T_: - DAMPING OK-Et-:-- REJ'71J1 HEELING ERROR R •._ 1 L BY ____ DATE ____ COMMENTS ______CUSTOMER:

© 1991 ASA MAKE: Cess,:ia Aerodyne Corporation DATE: 3/18/2013 DAT MODEL: 4216 A/C TSN: 5920.2 ions - SIN. 42180822 ✓/ft Repair Station No. HO1 R-199K HOBBS. 139.3 REG NO: N1592G 5198 West Military Highway · of 19_ WORK ORDER: 20109 Chesapeake, VA 23321 USA ies.) Phone: (757) 488-2898 - Airframe Entries (1).Troubleshoot customer report of left engine oil leak. Removed engine cowling. Cleaned engine. Performed engine ground run and inspected engine. Replaced o'ring seals on front nose case through bolts. Replaced reduction gear cover gasket. Performed second ground run and found to be satisfactory ...... (2) Troubleshoot customer report that left main fuel tank boost pump is ," inoperative. ,Found pump motor to be faulty. Drained fuel from left main tank. Removed panels as necessary to gain access to and '\. ·remove pump pin: 1C6-10 from left main fuel tank. Installed overhauled fuel pump pin: 1C6-10, sin: 9AC131 . Pump overhauled by Fleet Support Services, Inc. under Work Order No. 18101 -54999. Refueled tank. Performed pump pressure check as per 421 Service Manual. Operational and leak check satisfactory. Reinstalled previously removed panels...... (3) Troubleshoot leaking left ..... ·main fuel. tank transfer pump p/n: 6508092-4 due to fuel leak. Found contamination inside pump. Installed serviceable transfer pump pin: 6508Q92-1 . Operational and leak check satisfactory.

The article .fr:1entified hereon was inspected and repaired in acco with current Federal Aviation Regulations, was found to be airwortl:ly for the work performed and is approved for return to service.

DATE: 3/18/2013 SIGNED: Work Order: 20109 J.R. Smith Printed by EBis 3 (datcomedia.com~ Certified Repair Station No. HO1 R-199K - - -~ - --- -~---

- , ~ - I l ~ - - © 199 1 ASA n---••-•an- nf lncnAr-tions. Tests. Repairs and Alterations JP"avr- TftTAI d Certificate Number of :>r other specific entries.) DATE t'J0- ol-/3 ACHRS /S-t 8

THIS /c 7-?~ I}- TRANSPONDER S/N L/ 3 7:2 S- HAS BEEN TESTED AND FOUND TO BE IN COMPLIANCE WITH THE REQUIREMENTS OF CFR 91.413(PART 43 APP F).

SIGNED~_zs-_ -_IJ_/)__;_~__ .- _ ___..q____ _ INSPECTOR BAY AVIONICS, LTD. HM1R197K ' \ Date May 1, 2013 Hours 158.1 !\'lake & Model Cessna 421B N1592G \

I · . -Found pit_ot line from pitot ~be to pressure bulkhead leaking and replaced. !_. ound copilot airspeed indicator ·Moqel 8030, serial # 181872 leaking around glass r~ moved for repair. Capped pitot & static lines. See certification maintenance entry !his date.

This aircraft found to be airworthy with respect to the work perfqrmed under \\'ork order #24100. ~ 'J Inspector Bay Avionics, _Ltd, CRS# HM1R197K lolcrance Altimeter Encoder Altitude Tolerance -!- Error Error (feet) (feet) Reading (Toi. +/- 125 rations - ft.) 1ber of DATE 20 -It) F":-J 1.000 70 Jr-.\ entries.) 20 ;-/~ ...~ 2,000 70 ~ 19 20 I) t"') 3,000 70 ~ 20 0 !> 5,000 70 ~o - 2S - 10 0 10,000 80 ,)..-0 30 '-ll'J 0 15.000 90 :~o - 30 rJ C, 20,000 100 ~o 3S r-/0 0 25,000 120 f , ( } - 40 0 - .,n;, 30,000 140 bo 60 +1c - S-0 35,000 i60 - 80 -r/O .:.-.. ~I 40,000 180 ----- l) .,_..- 90 -)~ 50,000 250 ---- 100 -l-0 -ro 110 -,o ·-)-0 120 -/0 - .s~ TABLE IV - PRESSURE - ALTITUDE DIFFERENCE 130 ,0 -100 (Scale Error Test) 140 r) --100 ISS -10 -/CO Pressure Altitude 180 0 -.r:-/0 0 j ~esult _ . (Inches of Hg) Difference (feet) I 1 o\. ... ,_ •1.5 ft. 20S / 28.10 - 1,727 230 ~ t 25S __,.,. .... 28.50 - 1,340 - -863 ·- 280 ,,.- 29.00 - 29.50 -392 - 29.92 0 - 30.50 +531 Tolerance (feet) - 30.90 +893 ,,.- 100 - 30.99 +974 -- 75

Notes: 75 ------30

l ~-c;3 iPA-~ - 3 £:lt'-lll2Y2-______

Calibration Due Date oS--lt.-lJ 991 ASA i - - - ·- - -

Date May 16, 2013 Hours 0164.5 !\·lake & Model Cessna 421B N1592G

Removed airspeed indicator, part #8030, serial # 181872 and shipped for rt~ pa ir. R~installed repaired airspeec;l indicator. Performed static leak test in ,iccordance with CFR 91.4·1 l .. part 34, appendix E.

f hi :; aircraft found to be airworthy with respect to the work performed under · \\·ork order #24120. ~ '

Signed ~=-- I Ac, Inspector Bay Avioni_cs, Ltd, CRS# .HM1R197K

© 1991 A SA - ~ .?ftTI :!]!HJ JL -;O;AT~E;--~11~11::s:;:r.n:a:n:111:r- TlT:n :n::av:.. 71-: ....: ..: .:-. -,-=-~--:------1 Alterations- t 19 __ ! Number of DATE cific entries.) - LANDMARK 19_ ,_ AVIATION Norfolk, International Airport FAA Repair Station PIQR321K

Dat~T.T. ___ Acrft. Mfr~~/A: Model ~PB ,S/N~l8()B22.. ---- -~ Reg. No.~ , Eng. Mfr. b, 14 , Eng. Model \uA , Eng. S/N "Jl> The aircraft or engine logbook was not available. This form is to be attached to the logbook and I becomes part of the permanent records. The following maintenance was performed: Aircraft · Make Model SIN l?#./<~G.1<$9¥~~~eR')Rr ~.d£

~ -~~ /

·- - - -

C> 1991 ASA DATE RECORDING ,.. TODAYS TOTAL Description of Inspection , TACH FLIGHT TIME IN Entries must be endorsed with Name, 19 __ TIME SERVICE Technician or Repair Facility. (See back pag

ANDMARK 6101 Burton Station Rd. Norfolk, Va. VIATI 23502 757 857-3413 WO# A00726 Aircraft# N1592G Landin s Total Time Make Cessna Hobbs Model 421B Date 6/4/2013 SIN 421 B0822

1 Avionics Buss will not come on line. Duplicated customers complaint. Troubleshot and checked LH Avionics wing stub circuit breaker. No issue found. Exercised Avionics circuit breaker switch on Main switch panel and Avionics came on line. Gained access and removed intermittant 50Amp Circuit Breaker switch P/N·CM3589-50 and installed new Circuit breaker switch P/N: CM3589-50. System ops checks good.

~he mainianance operations describe Dove wera perfom1ed and inspected in accordance with the applicable rules c,f 14CFR part 43, and with respect ,,o the worl< f"rlbtme,'.!Jhtain;r., s app, ~ed torretum to service. I, r /, •

· 11-~----• ~- ___ Dale#~- CRS#PIQR321K I

~ 1991 ASA j DATI MAKE· Cessna Aerodyne Corporation DATE 6/20/2013 MODEL 421B AJC TSN 59636 --ns SIN: 421B0822 jQ Repair Station No. HO1R-1 99K HOBBS 182 7 . 19_ REG. NO: N1592G 5198 West Military Highway ... WORK ORDER 20201 Chesapeake, VA 23321 USA .) Aircraft # Phone: (757) 488-2898 Make Airframe Entries - Model (4) Complied with Airworthiness Directive 2000-01-'16 by visual inspection of the left and right engine exhaust systems in - accordance with the te).1 of the AD. No defects noted ...... (6) Disassembled co-pilot's arm rest and repaired broken mounting S/N brackets with repair brackets fabricated from 2024-T3 aluminum sheet. Reassembled and reinstalled co-pilot's arm rest. - 1. Air-condi The article identified hereon was inspElcted and repaired in ace r h current Federal Aviation Regulations, was found to be airworthy for the worl(. - performed and is approved for return to service. , Researc 5052-0 c DATE: 6/20/2013 SIGNED: Work Order: 20201 LA-ORF J.R Smith Printed by EBis 3 (datcomedia.com) with 2.5 Certified Rep ir Station No. HO1 R-199K Work pe 2. Resolde

EPfX AVIATION, UC 2802 All'J)Olt Drive, 5{.lite 1 EPIJJ(_ _~ - Chesapeal

10/25/13 Signed:_ emoved glareshield. Removed JPI EDM-760 sin 04280. Shipped to JPI under RMA 40197. Reinstalled Pl EDM-760 sin 04280 after repair under their work order 40197. Reinstalled glare shield. Power on hecks OK. Re programmed fuel quantity to reflect actual fuel capacity of aircraft.

William Rickard AP2960304

10 1991 ASA 6101 Burton Station Rd. LANDMARK Norfolk, VA 23502 - s·AVIATION 757 857-3413 Reference WO#: S01627 Aircraft# N1592G Total Time Make: Cessna Hobbs 182.9 I L------t------f l Model: 421 B Date 6/26/13 S/N: 42180822

1. Air-conditioner was not cooling. Troubleshot system and AC system was depleted due to hole in compressor discharge line. Researched refrigerant line and determined refrigerant line is not available from manufacturer. Fabricated new line from · 5052-0 aluminum tubing .500 inch OD and .035 inch wall thickness and double flared in accordance Landmark Aviation ORF _ LA-ORF-025 Procedures Form. Installed refrigerant line P/N Landmark-ORF S1627-074. Evacuated system and serviced with 2.5 pounds R-12 refrigerant and leak checked. No leaks found. Performed engine run and operational checked normal. Work performed IAW Landmark Aviation FQCS Procedures, AC43.13.1 b and Cessna 421 B Service Manual Section 2. f 2. Resoldered wire on left alternator noise suppressant capacitor as required. Operational check good.

The maintenance operations described above were performed and inspected in accordance with the applicable rules of 14CFR part 43, and with respect to the work performed; this aircraft is approved for return to service.

Date: ~:J { -/ ] CRS# PIQR321 K

Datr October J6, 2013 Hohbs 2)2.0 Make & Model Cessna 42JB N J592G

Removed Garm in GTX-330 transponder, part #011 -00455-00, serial #84113 193, shipped to Garmi n for repair. Reinstalled GTX-330 upon return from Garmin. Ground operational checks good.

This aircraft found to be airworthy with respect to the work performed under Work order #24173.

Signed~ J ~ ~ · Inspector

~ y A.\_:;:nics, Ltd, CRS# HMI RI 97K © 1991 ASA r DATE RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alt t· - E . . era ions TACH FLIGHT TIME IN ntnes must be endorsed with Name, Rating and Certificate N b DATE T h · · R · F •. um er of 19 TIME SERVICE ec nic1an or epair ac1l1ty. (See back pages for other specific entries.) 19_ -

6101 Burton Station Rd. Norfolk, Va. 23502 757 857-3413 WO# A00818 Aircraf Aircraft# N1592G Landin s 0 Total Time 6003.5 MakE Make Cessna Hobbs 222.6 Mode Model 421B Date 12/20/2013 SIN S/N 421 B0822 1 Remov1 1 Removed the following Equipment: HSI 610-1 (IN830A) P/N: 506-0021-901 S/N: 10086 (3.1 Lbs) and Pilot's VSI P/N: C661009-0101 SIN: 18068 00009-( (1 .8 Lbs) . Install Aspen EFD1000 System consisting of the following: EFD1000 P/N: 910-00001-001 S/N: 13572 (2.6Lbs), ACU PIN: 910-00004- 001 SIN: 13922 (.8Lbs) , RSM PIN: 910-00003-001 SIN: 15431 (.5Lb), Configuration Module P/N: 910-00005-004 SIN: 15011 (.1 Lbs) Tone The mail Generator PIN: 903-00001-005. Installed units in accordance with Aspen Avionics STC # SA10822SC , Aspen Avionics lnstal:ation Manual to the we Document# 900-00003-001 Revision AP, dated June 2013, AML STC Document# 035-00007-002 Rev. A dated Oct. 5, 2010 and as shown in Landmark Aviation Drawing# A00818-EFD1000 Rev. A, dated 12/5/2013. Unit ground checks good per the manufacture Installation manual Signed:) instructions. Refer to Landmark Aviation FAA form 337 dated 12/20/2013.~ pdated Aircraft Equipment List and weight and Balance records. J 2 Installed Aspen SVT per Aspen Avionics Tech Note 2011-10 Revision B dated January 16, 2012. Ops checks good. ,Z ~emoved and replaced broken Alt Fuel Time Ar.nunciator light wilh !"lew PIN: 10-04165.(EI AL-1) Ops checks good. 1

1he maintenance operations deJcribed above were pe,tormed and in-,pected in a,;cordance with the applicable rules of 14CFR part 43, and wfth respect :,,::µ& •~;~ rfilurn to seNice Date•4-/.0/4 3 CRS# PIQR321 K

e 1991 ASA - ' ' ~ DATE RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate NumbQr of 19 TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries...) r ? t AN D MA R K 6101 Burton Station Rd. Norfolk, Va. I, ~~____,.V___,~....___.___,_I---"' 1<---.._,N,___~2..:....35.:...:0:...::2~ 7.:...:5:...:.7.t....::..:.85:..:.7.....:•3:..:4..:..13=...... -_____~~----..:.. W.:...:O:...:.#;...;A:....:..0:..:0..:..8..:....37;______-4 ~ Aircraft# N1592G Landin s Total Time 6003.5 Make Cessna Hobbs 222.6 Model 4218 Date 11312014 SIN 421 80822

1 Removed Garmin GNS530 P/N: 011-00550-10 S/N: 78412378 for bench repairs. Removed and replaced bad memory battery with new PIN: 360- 00009-00. Installed repaired Garmin GNS530 PIN: 011-00550-10 SIN: 78412378. Unit ops checks good.

Signed:.,__..____ ....,.______; ______Date: CRS# PIQR321 K

© 1991 ASA - TOTAL Description of Inspections, Tests, Repairs and Alterations DATE RECORDING TODAYS FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of ,. YACH ~ SERVICE Technician or Repair Facility. (See back pages for other specific entries.) 19 ' TIME . -

- LANDM ARK - AVIATION Norfolk, International Airport FAA Repair Station PIQR321K

Date) lh$'x.T. ---Acrft. MrG2rrm Model tf?J}?

Reg. No.~ !:Q},G , Eng. Mfr. ,/ , Eng. Model ./ , Eng. SIN ----- The aircraft or engine logbook was not available. This form is to be attached to the logbook and becomes part of the Rt! anent records. 'I: e fo lowin maintenance was performed: • i" . ' -

Signature ._.,.._..,._,y....~~..,..~ Certificate No. PAQR,3<\ }< LA-ORF-00

© 1991A~ ------RECORDING TODAY~ TnTAI DATE 1tions r.;:.;...;;:::~-.:;;:::-:---;:-:--::~;-;:---:-:---.------..... er of LANDMARK 6101 Burton Station Rd. Norfolk, Va. tries.) 23502 757 857-3413 WO# 501815 Aircraft # N 1592G Landin s NA Total Time 6003.5 Make Cessna Hobbs 222.6 Model 4218 Date 1/22/2014 SIN 42180822

1 Complied with an Annual Inspection IAW the procedures of FAR 91.409(a)(1) and CFR Part 43, Appendix "D" as a guide and was determined to be airworthy condition. 2 Installed new placard PIN 5217566-6 in the aft baggage section IAW Cessna 4218 Aircraft Flight Manual. 3 Fabricated new placards to state "Fuel Tank and Sump Drain "& "Fuel Strainer Drain Daily" and installed adjacent to fuel sump valves and strainer on LH and RH Wing IAWCessna 4218 MM Section 2. 4 Removed RH fowl weather window PIN 5111603-6, SN unknown and replaced with PMA approved Perkins Aircraft Services RH fowl weather window PIN PAS5111603-6, SIN 17390 IAW Cessna 4218 MM Section 3. 5 Inspect fittings and found both '8' nuts on the back of the oil pressure gauges to be slightly loose. Secured fittings as required and performed ground run-up. Leak check and operational qheck normal. 6 After inspection of the door striker pins it was noted that no defects were present. The "play'' in the strike pins is a normal characteristic of the assembly. No further action taken. 7 Inspected RH cabin card table and found the upper hardware to just be loosely attached to the wall fastener. Secured hardware and found no further defects with the card table. Work performed IAW Cessna 4218 MM Section 3. 8 Inspected damage to longeron under the center floor just inboard of the co-pilot seat and found small crack resulting from wire bundle adel clamp being pulled out. Performed repairs cold working deformed metal back in to shape and installing fabricated double PIN Landmark-ORF-51815-86 constructed of 0.040" 2024 T3 aluminum, using CR3213-04-02 Cherrymax rivets. Double alodined and primed prior to installation. Work performed IAW Cessna 4218 MM Section 13 and AC 43.13- 1(b) Section 4 . 9 Removed leaking check valve from LH wing leading edge just outboard of the nacelle and replaced with new PIN S2218-1 IAW Cessna 4218 MM Section 11 . Fuel leak check good. No leaks noted. f'ioioressed small areas of corrosion present aft of LH exhaust near flap and treated area with alodine and primer. Painted touched up to match. Work performed IAW W eessna 4218 MM Section 2. 11 Accessed LH and RH tip tanks by defueling LH and RH wings and opening top fuel cap access plate and AFT tank access plate. Removed old sealant from around the dome nuts in tip tank and resealed as required with PR1440 81/2 IAW Cessna 4218 MM Section 11 . Cleaned debris from tank and closed tank using new gaskets PIN 082340046 and PIN 0823400-175. Fueled aircraft and performed leak check with no leaks noted. 12 Inspected LH aileron and noted deformations in the skin and aft rib. Removed LH aileron PIN 5024000-65 and trim tab and replaced with serviceable PIN 5024000- 65 from Preferred Airparts Inc., using original trim tab. Cleaned, repainted and balanced LH aileron prior to installation. Work performed IAW Cessna 4218 MM Section 2 and Section 5. 13 Installed new LH and RH 18 flap actuator bolt cover PIN CM2692-36J1S and painted to match IAW Cessna 4218 MM Section 2. 8 Accessed and inspected skin on RH outboard upper wing surface and found skin and under lying gusset to be damaged. After parts were found to not be available, it was advised to fabricate a patch and gusset to perform the repair. Fabricated a gusset PIN ORF-S1815-87, .025" 202413 Aluminum and doubler P/N ORF-51815-88 out of 0.040" 2024 T3 aluminum and installed using rivets 2 each PIN CR3212-5-2, 2 each PIN CR3212-5-3 and 2 each PIN CR3212-4-3 Cherry Max Rivets. Work performed IAW Cessna 4218 MM Section 16 and AC43.13 Chapter 4, Section 4. 15 Received Micro Vortex Generators Spares Kit PIN 5020, cleaned area and installed one new vortex generator PIN 1001 on RH wing in the location of the missing vortex generator IAW Micro Aerodynamics 4218 Micro Vortex Generators Spares Kit Instructions. Painted VG to match IAW Cessna 4218 MM Section 2.

© 1991 ASA DATE RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations JACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of 19 ___ TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

16 Removed and inspected RH wing locker door prop rod and found the arm to be slightly bent preventing the operator to close and open the door property. Cold straightened the prop rod arm and reinstalled. Operational check normal. Wort< performed IAW Cessna 4218 MM Section 3. 17 Accessed and removed RH aileron PIN 5024000-2. Received serviceable PIN 5024000-2 and inspected. Transferred original static discharger to serviceable aileron - and balanced. Installed RH aileron and performed operational· check . Wort< performed IAW Cessna 421 B MM Section 5. 18 Removed LH outboard exhaust shield and replaced with new PIN 5155122-6 IAW Cessna 4218 MM Section 9. t'f9?Removed and replaced two loose rivets on LH oil filter housing bracket and installed two new rivets PIN CR3213- 6-3 IAW AC43.13-18 Chapter 4 Section 4 and W cessna 4218 MM Section 16. 20 Removed ground lead from LH engine alternator and replaced ring terminal on the engine case end with new ring terminal PIN F66-56N IAW AC43.13-1 b Chapter 11. ground run-up and alternat~r optional check normal. 21 Accessed and removed LH alternator PIN ALV-9510 SIN 190286 and installed overhauled PIN AVL-9510 SIN A128577 with new gasket PIN 653981 IAW Cessna 421 B MM Section 14. Ground Run-up and operational check nomal. Leak check good with no leaks noted. 22 Inspected LH and RH propeller control fevers and found LH prop control cable to be dry and required lubrication. After cleaning and lubrication, the LH propeller control operational check was normal. After inspection of the RH propeller control system, it was noted that the cable was dry and required lubrication as well as the propeller governor was extremely difficult to actuate. Lubricated RH propeller cable and removed RH propeller governor PIN DCDFS290O7A/T 4 , SIN 741123 sent RH propeller governor to New England Propeller for repair. Received and installed RH propeller governor PIN DCDFS290O7A/T4, SIN 741123 after repair by New England Propeller Service CRS#RC2R130L, under WO#CR-40506. Wort< completed IAW Cessna 421 B MM Section 10-6.

23 Inspected LH mixture control cable and linkage and determined the reason for excessive force being requried to actuate the mixture controls was due to inadequate lubrication.Cleaned, lubricated and actuated LH mixture cable and linkage and found operational check normal. Wort< performed IAW Cessna 4218 MM Section 2.

24 Inspected LH and RH alternate air cable and linkage and determined the reason for excessive force being requried to actuate the mixture controls was due to inadequate lubrication.Cleaned, lubricated and actuated LH and RH alternate air cables and linkage and found operational check normal. Wort< performed IAW Cessna 4218 MM Section 2. 25 Replaced (1) loose cherrymax rivet OB alt of LH nacelle with new PIN CR3212-5-4 IAW AC43.13-1b Chapter 4 Section 4. 26 Inspected RH upper forward engine cowling and determined cracked material to have been previously repaired with a doubler but had suffered a rivet failure.Removed and replaced failed rivet with 1 each PIN CR3212-4-3 Cherry Max Rivet IAW Cessna 421 B MM Section 16. 27 Replaced 2 rivets missing on wing panel aft of RH engine exhaust with new PIN CR3212-4-3 IAW Cessna 421B MM Section 16. 28 Accessed and removed RH alternator PIN ALV-9510 SIN J091387 and installed overhauled PIN AVL-9510 SIN F012705 with new gasket PIN 653981 IAW Cessna 421 B MM Section 14. Ground Run-up and operational check nomal. Leak check good with no leaks noted. 29 Replaced broken static wick on rudder with new PIN C592001 -0201 IAW Cessna 421B MM Section 6. 30 Accessed and inspected dent in the RH leading edge and found damage to be negligible IAW Cessna 4218 Section 16. 31 Removed RH brake caliper and disassembled, cleaned and inspected. Found debris and dirt had damaged the packings and allowed hydraulic fluid to leak Repla~d packings with new PIN MS28775-132, reassembled, and bled brakes IAW Cleveland PIN 30-100 CMM and Cessna 421B Section 4. Ground test.and operational check normal. LA-ORF-007,--A -, ~ 1991 ASA . ' DATE RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alteratro~ s~ i TACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of I 19 TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

I 32 Removed DM 8.1 EL T PIN C589512-0103 SIN 9268 due to corrosion and replaced with overhauled unit SIN 14394E IAW Cessna 421B MM Section 13. Inspected ' - ELT IAW FAR 91.207(d) and no defects noted. Battery due replacement FE8-2016. 33 Accessed and removed rudder and tab assembly and removed damaged rudder tab PIN 5133015-1 from rudder. Received and inspected repaired rudder tab PIN 5133015-1 and found to be servicable. Cleaned, prepped, primed and painted rudder trim tab, transfer static discharger from old tab and installed on exsisting rudder. Fabricated balance fixture and balanced rudder and tab assembly before reinstalling on aircraft and installed on aircraft. Work performed IAW Cessna 421B MM Section 7.

34 Removed LH Engine Fire Extinguisher PIN 30111102, SIN 00424A1, removed discharge squib and shipped to Aerospace Turbine Rotables Inc. for 5 Year hydrostatic test. Received fire extinguisher PIN 3011 1102, SIN 00424A 1 from Aerospace Turbine Rotables Inc, CRS# NV2R045L under WO# W048169, inspected, and installed squibs and reinstalled left engine fire extinguisher in aircraft. Work performed IAW Cessna 421B MM Section 13-88. 35 Removed RH Engine Fire Extinguisher PIN 30111102, SIN 07441A1, removed discharge squib and shipped to Aerospace Turbine Rotables Inc. for 5 Year hydrostatic test. Received fire extinguisher PIN 30111102, SIN 07441A 1 from Aerospace Turbine Rotables Inc, CRS# NV2R045L under WO# W048167, inspected, and installed squibs and reinstalled right engine fire extinguisher in aircraft. Work performed IAW Cessna 421B MM Section 13-88. 36 Complied with AD 2000-01-16 "Cracks and Corrosion In Exhaust System" Part (b) visual inspection and Part (e) pressure test of the exhaust system on Left Engine. Replaced exhaust to waste gate gasket with new PIN 24096-300N, Part (b) due again (each 50 Hours) at ACTT 6053.5 or Hobbs time 272.6. Part (e) due again (each 100 hour or 12 months) at ACTT 6103.5 or Hobbs time of 322.6 or Jan. 2015. Part (c) due 412016. 37 Complied with AD 2000-01-16 "Cracks and Corrosion In Exhaust System" Part (b) visual inspection and Part (e) pressure test of the exhaust system on Right Engine. No defects were found at this time. Part (b) due again (each 50 Hours) at ACTT 6053.5 or Hobbs time 272.6. Part (e) due again (each 100 hours or 12 months) at ACTT 6103.5 or Hobbs time of 322.6 or Jan. 2015. Part (c) due 212015 .. 38 Replaced left prop deice brush holders with 2 each new PIN 840012 IAW Cessna 4218 MM Section 13-68. 39 Removed tail beacon cleaned and lube gearing and motor. Reinstalled and operational checked good. 40 Repaired high amperage indication on prop deice amp meter by cleaning amp meter shunt, replaced prop amp meter terminals and cleaning all connections. Operational checked normal. Work completed IAW Cessna 4218 MM Section 13-88.

AD's researched through Bi-Weekly 2014-01 Researched and Inspected continuing airworthy Items from aircraft records DATE: 1/22/14, MODEL:421B, SIN: 421B, TT:6003.5, HM:222.6, REG No.N1592G, WO# S01815 I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH THE INSPECTION AND PROCEDURES OF FAR 91.409(a)(1),CFR PART 43 APPEND! DAS A GUIDE. TYPE OF INSPECTION:ANNUAL INSPECTION AND THE AIRCRAFT IS DETERMINED TO BE IN AIRWORTHY CONDITION AND IS AP...,..J.¥C~ R RETUR S . VICE. PERTINENT DETAILS ARE ON FILE AT THIS AGENCY. SIG S M. OGLE,INSPECTOR FOR LANDMARK AVIATION, NORFOLK, VA.