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Aircraft record

N306GB1976 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 Apr 26, 2013.

Safety record in brief:No NTSB accidents or incidents since 198223 ADs may apply30 service difficulty reports

Registration
Deregistered
Last based in
Okla City, OK
owner city / state
Engine
RB-211 SERIES · 22,000 lb thrust
Rolls-Royc
Owners
1
on record
NTSB events
None
since 1982
ADs may apply
23
confirm with A&P
Service reports
30
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
Okla City, OK
Canceled
Apr 26, 2013
Airworthiness
Standard · Transport
Airworthiness date
Jan 21, 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
193U-1138
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
A33634

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. until 2013Individual ownerOkla City, OK

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 (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.

  • Navigation · battery · dischargedSep 26, 1999

    MIA - FLT 707 - ON TAKEOFF, NR 2 INS INOPERATIVE BATTERY WARNING AND ISU WARNING LIGHT ON. DUMPED 25.2K FUEL AND RETURNED TO MIA. REMOVED AND REPLACED NR 2 INS BATTERY. SYSTEM CHECKED NORMAL IAW MM 34-40-0. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · engine · failedApr 16, 1999

    MIA - FLT 508 - NR 1 ENGINE SHUT DOWN AT 5:44 GMT, DUE LOW OIL PRESSURE AND TOTAL LOSS OF OIL, OIL PRESS 5 TO 6 PSI INDICATED ON WINDMILLED. ZERO QTY IND LOW OIL PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED ENGINE IAW ARROW AIL FOR L-1011-7104A. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · engine · vibratesJan 15, 1999

    MIA - FLT 501 - DURNG CLIMB, NR 2 EN AVM 2.5, LT ON, VIB FELT IN PEDALS VIB DECREASE WHEN POWER REDUCED, AVM SELECTED TO LOW POSITION (MED AND HIGH POSITIONS BELOW .8). REMOVED AND REPLACED BLADES IAW MM 72-31-11 RAN ENGIEN COMPLETED VIB SURVEY TEST NR 1 VIB WITHIN LIMITS. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Engine fuel and control · ffr · out of adjustJan 8, 1999

    BQN - FLT 508 - ABORTED TAKEOFF. NR 3 ENGINE SLOW TO ACCELERATE. MAX EPR ON TAKEOFF ROLL 1.200 (1500 RQD FOR REDUCED T/O POWER). RETURNED TO RAMP. ADJUSTED FUEL FLOW REGULATOR AND RUN NR 3 ENGINE PER MM 71-00-00, OPS CHECK NORMAL. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · valve · lack of lubeDec 23, 1998

    ON T/O ROLL AT K DTW, NR 3 ENGINE UPON REACHING 1.3 EPR TGT REACHED 800 DEGREES, ABORTED T/O AND RETURNED TO RAMP. CHECKED ENGINE BY 70-00-00, PG 204. NO DEFECTS NOTED, LUBED EPR CONTROL VALVE, RAN ENGINE TO T/O WITH TGT OF 585 DEGREES MAX.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · fuel control · out of adjustDec 21, 1998

    NR 3 ENGINE SLOW TO SPOOL, ABOVE 1.3 EPR. DURING TAKEOFF ROLL IN DTW ABORTED TAKEOFF. AFTER FURTHER RUN-UP ON THE TAXI WAY, ENGINE OPERATED NORMALLY. ADJUSTED FUEL CONTROL IAW M/M 73-21-00.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · switch · inopDec 3, 1998

    ON TAKEOFF, GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR CONTROL SWITCH. OPERATION CHECKED NORMAL IAW M/M 32-31-14. (NO FUEL DUMPED).

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · idg · failedOct 8, 1998

    AIRCRAFT ARRIVED MIAMI WITH NR 2 IDG DISCONNECTED DUE TO THE FACT THAT WHEN NR 2 GENERATOR IS CONNECTED AND NR 1 AND NR 3 GENERATORS BUS TRIPS. REPLACED LOAD CONTROLLER AND GEN BREAKER, STILL HAD PROBLEM, NEEDED AND IDG. PLACED ITEM ON DMI.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · strap · looseSep 9, 1998

    INVESTIGATE BULGE AT FS 846 TO 865 STR 30 ZONE 130. AREA ABOUT BULGE DE-RIVITED, SECTION OF FAIL-SAFE STRAP REMOVED. REMOVED CORROSION STR 30 CUT AT FS 839, FS 859 AND FS 879. FRAME CUT AT FS 869 BETWEEN STR 29 AND 31, REPAIR LAID OUT, ALL NEW HOLES DRILLED, STRINGER SPLICE, DOUBLERS REMOVED.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedSep 9, 1998

    EVIDENCE OF CORROSION BLEND OUT ON LWR SKIN OF MLG T/BOX PLEASE ASSESS DAMAGE A7 = IWI 360. REPAIR CARRIED OUT AND ADHESIVE CURING AREA SAND AND IS OK FOR INSPECTION. REPAIR CARRIED OUT IAW SRM 51-25-00 AND BWIA APPROVED DRAWING NR BW-45-57A/4502 CON 104/98 W/O JWN 24000 CCF 4099 LOG PAGE 10467.

    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 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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