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Aircraft record

N1732D1981 Lockheed L-1011-385-1

DeregisteredUnclaimedSource: FAA, updated Oct 19, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Aug 30, 2011.

Safety record in brief:No NTSB accidents or incidents since 198223 ADs may apply19 service difficulty reports

Registration
Deregistered
Last based in
Amman
owner city / state
Engine
RB-211-22 · 4000 hp
Rolls-Royc
Owners
1
on record
NTSB events
None
since 1982
ADs may apply
23
confirm with A&P
Service reports
19
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Last registered owner
Individual owner
City, state
Amman
Canceled
Aug 30, 2011
Airworthiness
Standard · Transport
Airworthiness date
Jun 20, 1981

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Lockheed
Model
L-1011-385-1
Year
1981
Serial number
193C-1213
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
358
Engines
3
Max takeoff weight
20,000 and over lb
Mode S code
A126F4

Engine

Make and model
Rolls-Royc Rb-211-22
Type
Turbo-fan
Power
4000 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 1958 – 1961Individual ownerNew Orleans, LA · different airframe: Cessna 170a S/N 20175
  2. until 2011Individual ownerAmman

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

ADs published since 1998 that may apply (23)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2008-11-02 R1Lockheed Model L-1011 Series AirplanesDec 18, 2009Airframe (L-1011-385-1)
2008-12-17Lockheed Model L-1011 Series AirplanesJul 23, 2008Airframe (L-1011-385-1)
2005-15-01Lockheed Model L-1011-385 Series AirplanesAug 26, 2005Airframe (L-1011-385-1)
2004-09-28Lockheed Model L-1011 Series AirplanesJun 17, 2004Airframe (L-1011-385-1)
2000-17-10 R1Lockheed Model L-1011 Series AirplanesSep 26, 2001Airframe (L-1011-385-1)Only with: Equipped with Rolls Royce Model RB211-524 series engines.
Show all 23 ADs
ADSubjectEffectiveApplies to
2001-08-27Lockheed Model L-1011 Series AirplanesMay 14, 2001Airframe (L-1011-385-1)Serial numbers per Lockheed Service Bulletin 093-30-060, dated March 6, 2001, and Lockheed Service Bulletin 093-30-057, dated April 27, 1984
2000-21-01Lockheed Model L-1011-385 Series AirplanesNov 24, 2000Airframe (L-1011-385-1)
2000-17-10Lockheed Model L-1011-385 Series AirplanesOct 6, 2000Airframe (L-1011-385-1)
2000-16-08Lockheed Model L-1011-385 Series AirplanesSep 20, 2000Airframe (L-1011-385-1)Certain serial numbers: 1013–1250
2000-08-20Lockheed Model L-1011-385 Series AirplanesJun 5, 2000Airframe (L-1011-385-1)Only with: Equipped with high pressure bleed valve controller Hamilton Standard P/N 739084-2 or 739084-3 (Lockheed P/N 672286-103 or 672286-105).
99-13-08 R1Lockheed Model L-1011-385 Series AirplanesMay 22, 2000Airframe (L-1011-385-1)
99-24-12Lockheed Model L-1011-385 Series AirplanesJan 4, 2000Airframe (L-1011-385-1)
99-17-13Lockheed Model L-1011-385 Series AirplanesSep 24, 1999Airframe (L-1011-385-1)Serial numbers per Lockheed Service Bulletin 093-27-306, dated January 14, 1998
99-13-08Lockheed Model L-1011-385 Series AirplanesJul 28, 1999Airframe (L-1011-385-1)
99-09-14Lockheed Model L-1011-385 Series AirplanesJun 1, 1999Airframe (L-1011-385-1)
99-08-20Lockheed Model L-1011-385 Series AirplanesMay 19, 1999Airframe (L-1011-385-1)
99-07-05Lockheed Model L-1011-385 Series AirplanesApr 30, 1999Airframe (L-1011-385-1)
99-02-05Lockheed Model L-1011-385-1 Series AirplanesFeb 19, 1999Airframe (L-1011-385-1)Only with: Equipped with lower deck galleys.
98-10-14Lockheed Model L-1011-385 Series AirplanesJun 19, 1998Airframe (L-1011-385-1)
98-09-23Lockheed Model L-1011 Series Airplanes Equipped With Rolls Royce Model RB211-22B EnginesJun 3, 1998Airframe (L-1011-385-1)Only with: Equipped with Rolls Royce RB211-22B engines.
95-26-11Lockheed Model L-1011-385 Series AirplanesJan 11, 1996Airframe (L-1011-385-1)
95-10-17Lockheed Model L-1011-385 Series AirplanesMay 23, 1995Airframe (L-1011-385-1)
95-06-51Lockheed Model L-1011-385 Series AirplanesApr 21, 1995Airframe (L-1011-385-1)Serial numbers per Lockheed Service Bulletin 093-28-A091, dated March 8, 1995

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (19)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Pneumatic · pneu duct · failedNov 29, 1999

    WHILE ADVANCING PWR FOR A NO PACK T/O, A LOUD BANG WAS HEARD FOLLOWED BY A CABIN PRESSURE SURGE. J-AREA OVERHEAT, POM PROCEDURES COMPLETED. RETURNED TO GATE. MTC FOUND NR 2 DUCT BLOWN BEHIND AFT B/B WALL ON LEFT SIDE OF LAV TANK.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · filter module · leakingNov 21, 1999

    ON TAXI, IN BRAKE PRESSURE LOST B SYSTEM PRESSURE LOW AND QTY LESS THAN 1/4 NORMAL BRAKES ACCUMULATOR PRESSURE LOW. FOUND HIGH PRESSURE FILTER MODULE LEAKING FROM WEEP HOLE. REPLACED HI PRESS FILTER MOD PER M/M (P/N 297001913) (S/N 0943) OFF (S/N 0715) LOG NUMBER C346311001.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead panel · gougedJul 16, 1999

    FUSELAGE / AFT PRESSURE BULKHEAD / GORE PANEL / STRG. 11 : GOUGE REPAIR. THE AFT PRESSURE BULKHEAD WAS GOUGED BY A LOOSE DIAGONAL BRACE. THE GOUGE WAS ON THE AFT SIDE OF THE GORE PANEL AT FS 1809 NEAR STRINGER 11. THE GOUGE WAS CUTOUT WITH A 1.0 HOLE AND REPAIRED WITH AN ALUMINUM DOUBLER PER ER/A…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Hydraulic power · o ring · tornDec 15, 1998

    C SYSTEM QUANTITY GAUGE INDICATED ONE-QUARTER AFTER GEAR AND FLAPS WERE RETRACTED. PRESSURE STAYED NORMAL 3000 PSI LOW QTY LIGHT STAYED OFF. PRODCEDURE ACCOMPLISHED, SYSTEM SHUT DOWN. WHEN GEAR WAS EXTENDED LOW QTY CAME ON. SYSTEM WORKED NORMALLY. (ATM WAS USED TO LOWER GEAR). FOUND O RING BAD ON…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · engine · failedMay 23, 1998

    NR 3 ENG AT CRUISE 37,000 FT, HIGH VIBS INDICATED 2.6-2.8 UNITS. VERIFIED WITH BOTH A AND B PICKUPS. ALSO, FELT SLIGHT AIRFRAME VIB, SWITCHED TO LOW MED HIGH SETTINGS. MED HIGH WERE NORM BUT LOW FREQ PICK UP IND HIGH VIB READINGS. ENG SHUT DOWN ACCOMPLISHED. REPLACED ENGINE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · bulb · failedMar 14, 1998

    WHILE CLIMBING THROUGH FL 35.5 NR 3 ENG FLAMED OUT. IT APPEARS THE NR 3 ENG TANK VLV BECAME UNLATCHED. RELATCHED THE NR 3 ENG TANK VLV SWITCH LIGHT AND RESTARTED ENG, BOTH LIGHT BULBS IN FLOW BAR WERE BURNED OUT. REPLACED NR 3 ENG TANK VLV SWITCH LENS ASSY VALVE AND LIGHT LENS OPERATES GOOD.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · tire · failedAug 9, 1997

    BLEW BOTH NOSE TIRES UPON LANDING. TWO C-SYSTEM HYDRAULIC LINES DAMAGED ON NLG ASSEMBLY AND AIR/GROUND SENSOR DAMAGED BY TIRE DEBRIS. NOSE WHEEL ASSEMBLIES ALREADY REPLACED, MAINTENANCE IN PROGRESS REPLACING HYDRAULIC LINES AND REPAIRING AIR/GROUND SENSOR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · engine · failedJul 6, 1997

    NR 2 ENG ROLLED BACK, RAMP REPORTS TAIL PIPE FIRE. REPLACED ENGINE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · gearbox · failedMar 5, 1997

    IN CLIMBOUT AT 28,500 FT AND CLIMB 1 POWER NR 3 FLAMED OUT, NO INDICATIONS IN COCKPIT. NO ATTEMPT TO RESTART ENG, RETURNED TO SLC. METAL ON ENG 3 MASTER CHIP DET. REPLACED MAIN GEARBOX AND STEP A SIDE GEAR BOX.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedSep 3, 1996

    THE BONDED FUSELAGE SKIN ASSEMBLY AROUND THE C2 CARGO DOOR WAS FOUND CORRODED NEAR STA 1551 AND STR 29. THE CORROSION WAS REMOVED WITH A CUTOUT IN THE OUTER SKIN, BONDED DOUBLER AND DOOR DOUBLER. THE CUTOUT WILL BE REPAIRED USING STANDARD SRM REPAIR TECHNIQUES.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 19 reports.

Related aircraft

Show all 8 related aircraft

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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