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Aircraft record

N754DL1980 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 Sep 10, 2013.

Safety record in brief:No NTSB accidents or incidents since 198222 ADs may apply30 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Engine
RB-211 SERIES · 22,000 lb thrust
Rolls-Royc
Owners
1
since 2004
NTSB events
None
since 1982
ADs may apply
22
confirm with A&P
Service reports
30
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
Sep 10, 2013
Airworthiness
Standard · Transport
Airworthiness date
Apr 24, 1980

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
1980
Serial number
193Y1181
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
AA293B

Engine

Make and model
Rolls-Royc Rb-211 Series
Type
Turbo-fan
Power
22,000 lb thrust

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 – 2013Wells 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 (0)

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

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 (30)

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.

  • Air conditioning and pressurization · cooling fan · seizedSep 26, 2000

    AIRBORN SMELLED ELECTRICAL ARCING WITH AN UNUSUAL MOTOR NOISE ORIGINATING FROM BEHIND F/E PANEL. FOUND INSTRUMENT COOLING FAN LOCKED UP AND VERY HOT. REPLACED FAN, INSPECTED ALL WIRING IN AREA.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · power supply · inoperativeMay 30, 2000

    EMERGENCY EXIT LIGHTS AND FUSELAGE LIGHTS INOP B ZONE LT SIDE ROW 13 - 21. REPLACED POWER SUPPLY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Equipment and furnishings · unservNov 16, 1999

    WHILE TRYING TO CRANK R-2 DOOR SHUT DOOR SLIDE DEPLOYED. REPLACED SLIDE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Engine · engine · failedNov 4, 1999

    NR 3 MOTOR SUFFERED CONTINOUS INFLIGHT STALLS JUST AFTER LIFTOFF. REPORTED AGL WAS APPROX 400 FT. ENG PARAMETERS WAS FLUCUATING WITH STALLS. STALLS WERE VERY LOUD AND NOTICABLE IN AIRCRAFT STRUCTURE. UPON INSPECTION OF ENG INLET AND EXHAUST, METAL SHAVINGS WERE FOUND IN TAIL PIPE AND RT CORE COWL.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · retract mech · malfunctionedAug 28, 1999

    ON APPROACH GEAR WOULD NOT EXTEND NORMALLY. NO ABNORMAL INDICATIONS NOTED. EXTENDED GEAR USING MANUAL EXTENSION HANDLES. INITIAL INDICATIONS INTRANSIT LIGHT AND GEAR DOOR LIGHTS ONLY.

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

    THE FUSELAGE BELLY SKIN AT FS 886 BETWEEN STR 33 AND 32 WAS FOUND WITH AN AREA OF CORROSION. THE CORROSION WAS REMOVED WITH A 3.7 X 5 CUTOUT. THE CUTOUT WAS NEAR AN EXISTING BELLY SKIN REPLACEMENT REPAIR. AN ALUMINUM DOUBLER AND TRIPLER WERE INSTALLED TO REPAIR THE CUTOUT AND INCORPORATE THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · sensor · failedJun 16, 1999

    ON DESCENT, SMOKE ODOR IN CABIN. NR 2 PACK COMPRESSOR DISCHARGE TEMP OFF SCALE HIGH. ACM TEMP 40 DEGREES. REPLACED COMPRESSOR DISCHARGE TEMP SENSOR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · switch · brokenApr 26, 1999

    ELECTRICAL SMOKE ODOR IN COCKPIT ISOLATED A/C AND D/C POWER. NO EXCESSIVE LOADS ON ANY BUSS. FOUND RT WING LANDING LIGHT SWITCH BROKEN. REPLACED SWITCH.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · intercostal · crackedMar 20, 1999

    A .25 INCH TYPICAL CRACK WAS FOUND IN A RELIEF RADIUS OF THE NR 4 INTERCOSTAL AT THE L3 DOOR CUT OUT AFT DOOR JAMB. THE ADJACENT FITTING INTERCOSTALS WERE UNDAMAGED. THE CRACK WAS ALLOWED TO CONINUE INSERVICE PER THE REQUIREMENTS OF LACO S/B 93-53-270 AND WILL BE REPAIRED WITH A NEW INTERCOSTALS.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedJun 24, 1998

    FUSELAGE/SKIN, FS 829-846, STRG 33-34, REPAIR FOR CORROSION CUTOUT. THE FUSELAGE BELLY SKIN BETWEEN FS 829 AND 846 WAS FOUND CORRODED AT STRINGER 33. THE CORRODED ARE OF SKIN WAS REMOVED WITH A 10 BY 9.5 CUTOUT. THE DAMAGE WAS REPAIRED WITH AN EXTERNAL REPAIR DOUBLER PER ER/A 365086-14, REV A.

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

Showing the 10 most recent of 30 reports.

Related aircraft

Show all 8 related aircraft

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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