Aircraft Technical Specification

L1011-385-50 TRISTAR AIRCRAFT TECHNICAL SPECIFICATION (Data updated as of 1 DEC 2004) GENERAL DESCRIPTION

MANUFACTURER Lockheed

MODEL DESIGNATION L-1011-385-1-50

DATE OF MANUFACTURE April 1974

SERIAL NUMBER 193B-1066

FUSELAGE NUMBER 66

REGISTRATION (Gambian): 9Q-CTS (ex-C5-WAL)

AIRCRAFT OWNER / LESSOR: Tristar Capital (Nevada) LLC

PASSENGER ACCOMMODATION (New Interior / Royal Blue) 300 Passengers (28C / 272Y)

CERTIFICATION

CERTIFICATE NUMBER ISSUE DATE EXPIRE DATE

CERTIFICATE OF AIRWORTHINESS 279 30 DEC 03 30 DEC 04

CERTIFICATE OF REGISTRATION 279 20 JAN 03 30 JAN 09

FAR STAGE 3 / NOISE STATEMENT 1 FEB 03 N/A

RADIO STATION LICENCE TP 422A36 29 DEC 03 31 DEC 04

DESIGN WEIGHTS

POUNDS KILOGRAMS MAXIMUM TAXI - WEIGHT 452,000 205,455

MAXIMUM BRAKE RELEASE GROSS WEIGHT 450,000 204,545

MAXIMUM LANDING WEIGHT 358,000 162,727

MAXIMUM ZERO FUEL WEIGHT 320,000 145,177

OPERATING EMPTY WEIGHT 246,300 111,741

REMARKS: Factory Stage 3 Noise Compliant / Up to 36,000 lbs of Cargo

FUEL SYSTEMS

LBS US GALLONS FUEL TANKS TANK CAPACITY 159,560 23,815 STANDARD FUEL QUANTITY INDICATION UNITS LBS

Page: 1 of 5 AIRFRAME MAINTENANCE SCHEDULE AND STATUS

CURRENT AT TOTAL HOURS TOTAL CYCLES HR:CYC RATIO 01 SEP 2004 69,622 22,094 3.15

INTERVAL HRS INT. CALENDAR LAST CHECK NEXT CHECK

A CHECK 300 FH NTE 75 Days JUNE 2004 OCT 2004

B CHECK 600 FH DEC 2004 (B-1)

C CHECK- (phased) 3600 FH Phase 4 PHASES 722 Hours Rem

CPCP Integrated with B Check and C Check inputs

STRUCTURAL Inspections last completed August 2004

CHECK CONTRACTOR AEROINVERSIONES – PERU &GAMCO, UAE

ENGINES

ENGINE 1 ENGINE 2 ENGINE 3

SERIAL NUMBER 10253 10091 10065

MODEL RR RB211-22B RB211-22B RB211-22B

CURRENT TSN 52,154 53,279 52,564

CURRENT CSN 15,918 17,530 17,829

TSO 52,154 53,279 48,286

CSO 15,918 17,530 16,339

TSSV 3 33 4,295

CSSV 3 8 1,493

SCOPE LAST SV REPAIR REPAIR REPAIR

CYCLES TO LIMIT 2,118 223 609

CYCLES LIMITER LPT SHAFT HPC Disk 1/2 LP Shaft

HOURS TO LIMIT N/A N/A N/A

REMARKS Last Engine Shop Visits and Test Cells on all engines Accomplished By TWA

Page: 2 of 5 AUXILLARY POWER UNIT

MANUFACTURER MODEL MFG TSN TSO S E R I A L

Last Shop Visit & Test Hamilton Standard ST6L-73 HS #55094 ______by: TWA L1011-APU (P P&W 74388 25 AUG T 97 6)

LANDING GEARS

ASSEMBLY NO. SERIAL No. CSN TBO NEXT OVERHAUL

LEFT MAIN 1516854-191 151CJA 13,266 120 Mo 4,431 10,000 FC

RIGHT MAIN 1516854-192 461MDA 13,266 120 Mo 4,431 10,000 FC

NOSE 1516855-137 TW0017 13,266 120 Mo 4,431 10,000 FC

WHEEL MANUFACTURER BENDIX HEAVY

BRAKE MANUFACTURER BENDIX HEAVY

AVIONICS

COMMUNICATIONS (ATA 23)

MANUFACTURER PART NO. MODEL QTY

HF TRANSCEIVER COLLINS 622-3371-001 628T-1 2 VHF TRANSCEIVER 8.33Mhz BENDIX 064-5001-0101 2 VHF TRANSCEIVER COLLINS 522-4088-210 618M-4A 1

SELCAL DECODER MOTOROLA NA135PH50 - 1

SATCOM N/A - - -

CVR FAIRCHILD 93A100-30 - 1

TAPE REPRODUCER Telephonic - 1

Page: 3 of 5 VIDEO PLAYER Avicom PAU-3 - 2

INDICATING/RECORDING SYSTEMS (ATA 31)

FLIGHT DATA RECORDER HONEYWELL 981-6009-001 - 1

DFDAU TELEDYNE 2222228 - 1

NAVIGATION (ATA 34)

AIR DATA COMPUTER SPERRY 2593200-951 - 2

GPS / RNAV-A TRIMBLE / FreeFlight 81440-02-241D TNL 2101 2

INS DELCO 7886580-011 Carousel 4A 3

MARKER BEACON COLLINS 522-2996-011 51Z-4 1

WEATHER RADAR SPERRY-RCA 2070410-0101 AVQ-30X 2

GPWS COLLINS 622-2615-216 FPC-75 1

VHF NAVIGATION – FMI COLLINS 522-4280-105 51RV-5B 1 522-4280-107 1 ILS NAVIGATION - FMI COLLINS 792-6021-002 ILS-700 2

ATC TRANSPONDER COLLINS 622-7878-201 TTR-720 2

DME COLLINS 622-2921-001 860E-3 2

ADF COLLINS 777-1492-004 51&-7 2

TCAS / CHANGE 7 COLLINS 622-8971-022 TPR-920 1

INTERIOR CONFIGURATION

SEATING MANUFACTURER MODEL PART NO. PITCH QUANTITY

F SEATS N/A N/A 0

C SEATS Burns C02775 40 “ 28

Y SEATS PTC 901 or 881 various 33”-34” 272

TOTAL SEATING 300

MAXIMUM SEATING – 345Y IS WITH LONG TERM CONTRACT 345 POSSIBLE

LAVATORIES

LAVATORY QUANTITY & LOCATION 2 – “A” Zone, 5 – “E” Zone

Page: 4 of 5 GALLEYS

GALLEY STANDARD Lockheed / TWA

GALLEY LOCATION MANUFACTURER PART NO. CARTS / OVENS

Fwd Svc Ctr Lockheed 1533841-101 4 / 2

Mid Svc Ctr Lockheed 1535723-101 4

Lower Deck Lockheed Various 12 / 8

STATUS OF AIRCRAFT

Aircraft was removed from lease and service from the NE AIRLINES AOC on 8/15/2004.

Aircraft went through an A / B checks in Tucson, AZ JUL 2003 and A check in MAR 2004 including “Return To Service Check” All fuel pumps upgraded (per A/D) and aircraft received new interior & new paint. Latest Checks to include an and “A” Check and RTS (Return to Service) are in progress at Dallas, Texas (Dalfort) and are scheduled to be completed on our AUG 2004.

 TCAS 7.0 Software Revision and Modification

Collins TPR-920 Processor and the TTR-720 ATC Transponder MOD 7 upgraded at OEM.

 COMMUNICATION and NAVIGATION UPGRADES

To meet JAA-1 European Standards & RVSM requirements, the following are accomplished: Replacement of VHF Communications Transceivers with 8.33mhz spacing 618M-4A. Replacement of ILS Navigation Receivers with ILS-700. Replacement of VOR Navigation Receivers with 51RV-5B. Installation of (1) Trimble TNL-2101 GPS / RNAV-A Navigation Unit (in progress).

Supplemental Data

The interior configuration has been changed from 3 class (TWA) to accommodate 28C/272Y passengers during the Return to Service and B-1 Check at Hamilton Aerospace Technologies in Tucson, Arizona.

Aircraft was returned from Lease by NE AIRLINES (Pty) Ltd and deregistered from Swaziland to Gambia as C5-WAL and the airline (WAL) never took delivery of the aircraft as the company was unable to commence operations.

Now the aircraft is being transferred to registry 9Q-TSC in Dem. Republic of The Congo and is under an operating contract with LAC (Lingnes Aerienne Congolaise – LAC).

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