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Aircraft record

N762DA1981 Lockheed L-1011-385-3

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jun 4, 2010.

Safety record in brief:1 NTSB accident (Mar 1997)22 ADs may apply29 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Engine
RB-211-22 · 4000 hp
Rolls-Royc
Owners
1
since 2004
NTSB events
1
1997
ADs may apply
22
confirm with A&P
Service reports
29
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Wells Fargo Bank Northwest NA Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Apr 28, 2004
Canceled
Jun 4, 2010
Airworthiness
Standard · Transport
Airworthiness date
Aug 21, 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-1011-385-3
Year
1981
Serial number
193Y-1210
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
400
Engines
3
Max takeoff weight
20,000 and over lb
Mode S code
AA4942

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. 2004 – 2010Wells Fargo Bank Northwest NA TrusteeSalt Lake City, UT

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident

Mar 27, 1997 · Jamaica, NY

The failure of the right wing walker, also the push back supervisor, to identify and avoid a hazardous condition, which resulted in his activity near the airplane's nose wheel during tow operations, and where he was subsequently caught under the nose wheel. A factor in the accident was the failure of the Delta Ground Operations Manual to provide adequate safety information.

Injuries
Fatal
Report
NYC97LA064

From NTSB records; matched by serial number.Read NTSB report (search CAROL for NYC97LA064)

ADs published since 1998 that may apply (22)

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-1011-385-3)
2008-12-17Lockheed Model L-1011 Series AirplanesJul 23, 2008Airframe (L-1011-385-3)
2005-15-01Lockheed Model L-1011-385 Series AirplanesAug 26, 2005Airframe (L-1011-385-3)
2004-09-28Lockheed Model L-1011 Series AirplanesJun 17, 2004Airframe (L-1011-385-3)
2000-17-10 R1Lockheed Model L-1011 Series AirplanesSep 26, 2001Airframe (L-1011-385-3)Only with: Equipped with Rolls Royce Model RB211-524 series engines.
Show all 22 ADs
ADSubjectEffectiveApplies to
2001-08-27Lockheed Model L-1011 Series AirplanesMay 14, 2001Airframe (L-1011-385-3)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-1011-385-3)
2000-17-10Lockheed Model L-1011-385 Series AirplanesOct 6, 2000Airframe (L-1011-385-3)
2000-16-08Lockheed Model L-1011-385 Series AirplanesSep 20, 2000Airframe (L-1011-385-3)Certain serial numbers: 1013–1250
2000-08-20Lockheed Model L-1011-385 Series AirplanesJun 5, 2000Airframe (L-1011-385-3)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-1011-385-3)
99-24-12Lockheed Model L-1011-385 Series AirplanesJan 4, 2000Airframe (L-1011-385-3)
99-17-13Lockheed Model L-1011-385 Series AirplanesSep 24, 1999Airframe (L-1011-385-3)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-1011-385-3)
99-09-14Lockheed Model L-1011-385 Series AirplanesJun 1, 1999Airframe (L-1011-385-3)
99-08-20Lockheed Model L-1011-385 Series AirplanesMay 19, 1999Airframe (L-1011-385-3)
99-07-05Lockheed Model L-1011-385 Series AirplanesApr 30, 1999Airframe (L-1011-385-3)
98-10-14Lockheed Model L-1011-385 Series AirplanesJun 19, 1998Airframe (L-1011-385-3)
98-09-23Lockheed Model L-1011 Series Airplanes Equipped With Rolls Royce Model RB211-22B EnginesJun 3, 1998Airframe (L-1011-385-3)Only with: Equipped with Rolls Royce RB211-22B engines.
95-26-11Lockheed Model L-1011-385 Series AirplanesJan 11, 1996Airframe (L-1011-385-3)
95-10-17Lockheed Model L-1011-385 Series AirplanesMay 23, 1995Airframe (L-1011-385-3)
95-06-51Lockheed Model L-1011-385 Series AirplanesApr 21, 1995Airframe (L-1011-385-3)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 (29)

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.

  • Airborne auxiliary power · oil syst · leakingOct 4, 1998

    AFTER T/O, HAD ODOR AS DESCRIBED IN PREVIOUS WRITE UP THIS. DISSIPATED UNTIL DESCENT INITATED, THEN WHOLE CABIN AND FLT DECK FILLED WITH A VAPOR SMOKE. FOUND APU INTERNAL OIL LEAK.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · coalescer · contaminatedOct 3, 1998

    OILY SMELL IN 1ST CLASS CABIN AND C/P SMELL SEEMED NEARLY DISAPPEARED WITH NR 2 PACK OFF. RAN ENGINES PER PFHB AND PACKS ISOLATED SMELL TO NR 1 PACK. REPLACED COALESCER.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · rear spar · crackedMay 29, 1998

    THE RT WING REAR SPAR WAS FOUND WITH TWO CRACKED FASTENER HOLES DURING ROUTINE INSPECTIONS. ONE HOLE WAS COMMON TO THE UPPER WING SKIN AND SPAR CAP AND THE OTHER TO THE SPAR WEB AND UPPER CAP. BOTH HOLES WERE APPROX AT IWS 322. BOTH HOLES WERE OVERSIZED TO REMOVE THE CRACKS, COLD WORKED AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Wings · rear spar · crackedMay 29, 1998

    THE LT WING REAR SPAR WAS FOUND WITH TWO CRACKED FASTENER HOLES COMMON TO THE UPPER WING SKIN AND SPAR CAP AT APPROX IWS 322. THE CRACKS WERE FOUND DURING ROUTINE INSPECTIONS AND WERE REMOVED BY OVERSIZING THE HOLES. THE OVERSIZE HOLES WERE COLD WORKED, BUSHED, AND NEW FASTENERS INSTALLED PER ER/A…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Exhaust · tr light · illuminatedApr 19, 1998

    REVERSER PRESSURE LIGHT ON IN FLT POM. FOUND REVERSER STOWED AND REPLACED PRSOV WITH NO HELP. SUSPECT WIRING.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · longeron · corrodedOct 17, 1997

    FUSELAGE NOSE LG WHEEL WELL LWR LONGERON LBL 22, FS353 REPAIR FOR CORROSION DAMAGE. THE NLG WHEEL WELL LONGERON AT LBL 22, FS 353 WAS FOUND WITH EXTENSIVE CORROSION REQUIRED A SECTION TO BE CUT OUT. A NEW SECTION WAS SPLICED IN PER ER/A 362972-14.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead web · corrodedOct 17, 1997

    FUSELAGE BULKHEAD FS 328 LBL 15 WL 127 REPAIR FOR CORROSION CUT OUT IN WEB. THE FS 328 NLG WHEEL WELL PRESSURE BULKHEAD WAS FOUND CORRODED AT WL 127, LBL 15. THE CORROSION REMOVAL RESULTED IN A 2.8 BY 1.6 RECTANGULAR CUT OUT IN THE WEB. A DOUBLER REPAIR WAS INSTALLED PER ER/A 362969-14AD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · gearbox · failedSep 8, 1997

    NR 3 ENG FLAME-OUT, NO OIL PRESS/NO N3/N1, N2 WINDMILLING NORMAL. OIL QUANTITY 19 QTS OCCURED IN CRZ AT FL 330. REPLACED GEARBOX.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · power supply · inoperativeJun 27, 1997

    RIGHT HAND AFT SIDE EMERGENCY TRACK LIGHTS DID NOT ILLUMINATE DURING TEST. REPLACED POWER SUPPLY, OP CKS GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · power supply · inopJun 24, 1997

    FWD RT OVHD EMERGENCY LIGHT WOULD NOT TEST. REPLACED POWER SUPPLY, CHECKS NORMAL.

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

Showing the 10 most recent of 29 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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