L1011-385-50 TRISTAR PASSENGER AIRCRAFT

AIRCRAFT TECHNICAL SPECIFICATION

(Data updated as of April 1, 2006)
Click Here for Layout
Click here for Engine Specs
Certificates

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 (to be r/r N700TS)

 

 

 

 

AIRCRAFT OWNER / LESSOR:

Tristar Capital (Nevada) LLC

 

 

 

 

PASSENGER ACCOMMODATION (Recent/ Royal Blue)

300 Passengers (28C / 272Y)

Secure Cockpit Door

 

 

 

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

 

 

 

 

 

 

 

 

 

 

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

 

FEB 2006

 

OCT 2006

 

 

 

 

 

 

 

 

B CHECK

600 FH                           FEB 2006 (B-1)

 

 

 

 

 

 

 

 

C CHECK- (phased)

 3600 FH Phase

 

4 PHASES

 

 

 

718 Hours Rem

CPCP

Integrated with B Check and C Check inputs

 

 

 

 

 

 

 

 

 

 

 

 

 

 

STRUCTURAL

Inspections last completed August 2004

 

 

 

 

 

 

 

 

AST CHECK Contrator

American Airlines – MRO (AFW)

 

 

 

 

 

 

 

 

ENGINES

 

 

 

ENGINE #

1

 

2

 

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

 

 

AUXILLARY POWER UNIT

 

MANUFACTURER

 

MODEL

 

MFG SERIAL NO

 

TSN

 

 

 

 

 

 

 

 

 

Last Shop Visit & Test by: TWA 25 AUG 97

Hamilton Standard

L1011-APU

 

ST6L-73 (PT6)

 

HS #55094

P&W 74388

 

______

 

TSO

 

 

 

 

 

 

 

 

 

 

LANDING GEARS

 

 

 

 

 

 

 

 

_______

 

 

 

 

 

 

 

 

ASSEMBLY NO.

 

SERIAL No.

 

CSN

 

TBO

 

 

 

 

 

 

 

 

 

 

 

LEFT MAIN

1516854-191

 

151CJA

 

13,266

 

120 Mo

 

NEXT OVERHAUL

 

 

 

 

 

 

 

10,000 FC

 

 

 

 

 

 

 

 

 

 

 

4,431

RIGHT MAIN

1516854-192

 

461MDA

 

13,266

 

120 Mo

 

 

 

 

 

 

 

 

 

10,000 FC

 

 

 

 

 

 

 

 

 

 

 

4,431

NOSE

1516855-137

 

TW0017

 

13,266

 

120 Mo

 

 

 

 

 

 

 

 

 

10,000 FC

 

 

 

 

 

 

 

 

 

 

 

4,431

 

 

 

 

 

 

 

 

 

 

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

 

 

 

 

 

 

 

 

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

522-4280-107

 

51RV-5B

 

1

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 POSSIBLE

WITH LONG TERM CONTRACT

 

345

 

 

 

 

 

 

 

 

 

LAVATORIES

 

 

 

 

 

 

 

 

 

 

LAVATORY QUANTITY & LOCATION

2 – “A” Zone, 5 – “E” Zone

 

                                                     

 

 


 

 

 

 

 

 

 

 

 

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 a B check and RTS Check in Tucson, AZ at Hamilton Aerospace 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 and Modification includes an “A” and “B” Check, installation of the Reinforced / Secure L1011 Cockpit Door (by RSM Industries Canada), engine boroscope inspections (all are SVC) and drop-in visit to clear all open-items at American Airlines MRO at (AFW) Alliance, Fort Worth, Texas in February 2005. 

 

 

·         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.

 

The aircraft is now in process of being transferred back to N from Congolaise registry 9Q-CTS under an operating contract with LAC (Lingnes Aerienne Congolaise – LAC)  back to United States of American FAA registry N700TS, in the name of Tristar Capital (Nevada) LLC.


The aircraft, including 2 spare engines, spare APU, spare parts and manuals are the market and are available for immediate sale.