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Aircraft record

N308GB1976 Lockheed L-1011-385-1-15

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Sep 13, 2013.

Safety record in brief:No NTSB accidents or incidents since 198223 ADs may apply37 service difficulty reports

Registration
Deregistered
Last based in
Roswell, NM
owner city / state
Engine
RB-211 SERIES · 22,000 lb thrust
Rolls-Royc
Owners
1
since 2006
NTSB events
None
since 1982
ADs may apply
23
confirm with A&P
Service reports
37
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Great Southwest Aviation INC
Owner type
Corporation
City, state
Roswell, NM
Certificate issued
Nov 13, 2006
Canceled
Sep 13, 2013
Airworthiness
Standard · Transport
Airworthiness date
May 15, 1996

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-1011-385-1-15
Year
1976
Serial number
193U1133
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
A33DA2

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. 2006 – 2013Great Southwest Aviation INCRoswell, NM

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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-1011-385-1-15)
2008-12-17Lockheed Model L-1011 Series AirplanesJul 23, 2008Airframe (L-1011-385-1-15)
2005-15-01Lockheed Model L-1011-385 Series AirplanesAug 26, 2005Airframe (L-1011-385-1-15)
2004-09-28Lockheed Model L-1011 Series AirplanesJun 17, 2004Airframe (L-1011-385-1-15)
2000-17-10 R1Lockheed Model L-1011 Series AirplanesSep 26, 2001Airframe (L-1011-385-1-15)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-1011-385-1-15)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-1011-385-1-15)
2000-17-10Lockheed Model L-1011-385 Series AirplanesOct 6, 2000Airframe (L-1011-385-1-15)
2000-16-08Lockheed Model L-1011-385 Series AirplanesSep 20, 2000Airframe (L-1011-385-1-15)Certain serial numbers: 1013–1250
2000-08-20Lockheed Model L-1011-385 Series AirplanesJun 5, 2000Airframe (L-1011-385-1-15)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-1011-385-1-15)
99-24-12Lockheed Model L-1011-385 Series AirplanesJan 4, 2000Airframe (L-1011-385-1-15)
99-17-13Lockheed Model L-1011-385 Series AirplanesSep 24, 1999Airframe (L-1011-385-1-15)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-1011-385-1-15)
99-09-14Lockheed Model L-1011-385 Series AirplanesJun 1, 1999Airframe (L-1011-385-1-15)
99-08-20Lockheed Model L-1011-385 Series AirplanesMay 19, 1999Airframe (L-1011-385-1-15)
99-07-05Lockheed Model L-1011-385 Series AirplanesApr 30, 1999Airframe (L-1011-385-1-15)
99-02-05Lockheed Model L-1011-385-1 Series AirplanesFeb 19, 1999Airframe (L-1011-385-1-15)Only with: Equipped with lower deck galleys.
98-10-14Lockheed Model L-1011-385 Series AirplanesJun 19, 1998Airframe (L-1011-385-1-15)
98-09-23Lockheed Model L-1011 Series Airplanes Equipped With Rolls Royce Model RB211-22B EnginesJun 3, 1998Airframe (L-1011-385-1-15)Only with: Equipped with Rolls Royce RB211-22B engines.
95-26-11Lockheed Model L-1011-385 Series AirplanesJan 11, 1996Airframe (L-1011-385-1-15)
95-10-17Lockheed Model L-1011-385 Series AirplanesMay 23, 1995Airframe (L-1011-385-1-15)
95-06-51Lockheed Model L-1011-385 Series AirplanesApr 21, 1995Airframe (L-1011-385-1-15)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 (37)

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.

  • Landing gear · actuator · failedNov 28, 2003

    LT GEAR, IN TRANSITION, DOOR. FE DOOR LIGHTS ON; GEAR RETRACTED. REMOVED AND REPLACED LANDING GEAR DOOR LT ACTUATOR IAW MM 32-33-08. COMPLETED TEST IAW MM 32-61-07. ALL SYSTEMS CHECKED NORMAL, NO GEAR SWING.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · uplock sensor · out of adjustNov 28, 2003

    THE RED LANDING GEAR DOOR AND INTRANSIT LIGHT REMAINED ON AFTER GEAR RETRACTION AND THE LT GEAR ON DOOR LIGHT ON THE F/E PANEL REMAINED ON. SHIMMED AND RESECURED MAIN LANDING GEAR LT DOOR UPLOCK SENSOR IAW MM 32-61-07. GEAR SWING OPERATIONAL CHECK GOOD IAW MM 32-30-00.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · panel · brokenSep 15, 2003

    ON POST-FLIGHT FOUND RT WING INBOARD SPOILER PANEL NR 2 INBOARD WING TRAILING EDGE BRACKET BROKEN. REMOVED AND REPLACED UPPER CAP AT T/E STATION 137.0 & 226.6 IAW SR SRM 57-22-00. REMOVED AND RE-INSTALLED T/E UPPER PANELS AT NR 2 SPOILER AREA IAW SRM 51-40-1. REMOVED AND REPLACED RT WING NR 2…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Air conditioning and pressurization · switch · unserviceableAug 23, 2003

    AVIONIC AIR, FWD AND MID LIGHT COMING ON IN FLIGHT. AIRCRAFT GOING INTO GROUND MODE WITH AIRCRAFT DEPRESSURIZING. FUEL DUMP, AND RETURN TO MIA FOR LANDING WITHOUT INCIDENT. REMOVED AND REPLACED LT AND RT GROUND. SAFETY SENSORS IAW CURRENT MFG. MANUAL CHAPTER 32. OPERATIONAL CHECK SATISFACTORY…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · compressor · damagedJul 11, 2003

    LOG PAGE 23902 NR 3 ENGINE VIBRATION 4 UNITS BOTH A & B CHANNELS IN NORMAL POSITION NR 3 ENGINE SHUTDOWN AT 1340 Z. INSPECTED NR 3 ENGINE; FOUND METAL ON EXHAUST TAIL PIPE; BOROSCOPED ENGINE, FOUND DISCREPANCIES ON HIGH PRESSURE COMPRESSOR OUT OF LIMITS AND REJECTED ENGINE S/N 14637 IAW RB211 MM…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · engine · vibrationJun 10, 2003

    ABORTED TAKE OFF AT 130 KTS 470,000 LBS DUE TO NR 3 ENGINE VIBRATION WARNING AT 2.8 UNITS. BRAKES OK, TIRES OK. RETURNED TO RAMP. LUBED FAN BLADES, PERFORMED INSPECTION IAW L1011 MM 71-91-00. ALL PARAMETTERS WITHIN LIMITS ON RUN UP NR 3 ENGINE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · controller · malfunctionedFeb 23, 2002

    NR 1 PACK OVERHEAT, SMELLED SMOKE IN COCKPIT. RETURNED TO RAMP. RESET TEMPERATURE CONTROLLER NR 1 PACK, OPS CHECK NORMAL IAW MM 21-62-01. AIRCRAFT RETURNED TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · engine · malfunctionedJan 10, 2002

    NR 2 ENGINE STARTS AFTER 2 MINUTES ENGINE ROLL BACK TO ZERO AND SHUT DOWN.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · indicatorJan 5, 2002

    LOG PAGE 21540. DISCREPANCY: #1 ENGINE STARTER ACCELERATES N3 TO 46% VERY RAPIDILY THEN CUTS OUT BEFORE FULL ENGINE LIGHT UP. CORRECTIVE ACTION: REMOVED AND REPLACED N3 INDICATOR IAW MM 77-12-03 OPS CK NORMAL IAW MM 71-00. AIRCRAFT RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · sensor · failedDec 16, 2001

    LANDING GEAR LEVER COULD NOT BE RAISED, HAD TO DEPRESS BUTTON TO RAISE SELECTOR. TROUBLESHOOT SYSTEM, REMOVED AND REPLACED RT MLG AIR/GROUND SENSOR IAW MM 32-63-01, OPS CHECKED SYSTEM NORMAL IAW MM 32-63-0. AIRCRAFT RETURNED TO SERVICE.

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

Showing the 10 most recent of 37 reports.

Related aircraft

Show all 8 related aircraft

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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