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Aircraft record

N721DA1976 Lockheed L-1011-385-1

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Feb 20, 2013.

Safety record in brief:1 NTSB accident (Jun 1989)23 ADs may apply153 service difficulty reports

Registration
Deregistered
Last based in
Kansas City, KS
owner city / state
Engine
RB-211-22 · 4000 hp
Rolls-Royc
Owners
1
on record
NTSB events
1
1989
ADs may apply
23
confirm with A&P
Service reports
153
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
Kansas City, KS
Canceled
Feb 20, 2013
Airworthiness
Standard · Transport
Airworthiness date
Jun 20, 1976

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
1976
Serial number
193C-1139
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
A9A78F

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. until 2013Individual ownerKansas City, KS

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 (1)

Accident

Jun 16, 1989 · Jacks Creek, TN

FAILURE OF THE PASSENGERS TO REMAIN SEATED WITH THEIR SEAT BELTS FASTENED AS THE AIRPLANE ENCOUNTERED UNFORECAST SEVERE CLEAR AIR TURBULENCE.

Injuries
Serious
Report
ATL89FA161

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL89FA161)

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 (153)

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.

  • Lights · bulb · failedMay 15, 1999

    TWO EMERGENCY LIGHTS INOP FIRST CLASS LT TRACK. REPLACED BULBS AND HOLDER.

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

    FAA - SMOKE GOGGLES AT THREE LOCATIONS FOUND WITH CRACKS. LENS CRACKED FROM NOSE BRIDGE TO TOP. LENS CRACKED FROM NOSE BRIDGE UP FOR 1 INCH. LENS CRACKED FROM NOSE BRIDGE UP FOR 1 INCH. ALL THREE GOGGLES WERE PROPERLY STOWED AND IN THERE PROPER CLOTH POUCH. NOTED THAT GOGGLES WITH DAMAGE WERE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead cap · crackedFeb 11, 1999

    FUSELAGE BULKHEAD FS 1363 LOWER CAP, LBL 91.5, REPAIR FOR CRACK. THE LOWER CAP OF THE FS 13636 BULKEAD WAS FOUND WITH A CRACK THROUGH THE HORIZONTAL FLANGE EXTENDING INTO THE VERTICAL FLANGE AT LBL 91.5. THE SECTION OF CAP WITH THE CRACK WAS REMOVED FROM THE EXISTING SPLICE AT STRINGER 47 TO AN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fire protection · connector · corrodedSep 29, 1998

    NR 3 ENG FIRE INDICATION IN FLIGHT, POM PROCEDURE COMPLIED WITH. BOTH BOTTLES FIRED, CIRCUIT WOULD NOT TEST. REPLACED UPPER GAS GENERATOR AND AFT GEARBOX LOOP CONNECTORS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Communications · projector · inoperativeJun 15, 1998

    STRONG ODOR LIKE ELECTRICAL BURNING BETWEEN FIRST CLASS AND COACH NO SMOKE NOTICED PER CREW REPORTS APPROX 10 MIN. AFTER MOVIE STARTED B ZONE PROJECTOR INOP WITH ELECTRICAL ODOR NOTICED. ODOR WAS NOTICED IN B ZONE ONLY. OPENED AND INSPECTED ALL CEILING AREAS. FOUND ODOR TO BE ISOLATED TO B ZONE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedJun 14, 1998

    FUSELAGE SKIN FS 1693 STRG 38 : REPAIR FOR CORROSION CUTOUT. THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 1693 AND STRG 38. THE DAMAGED SKIN WAS CUTOUT OVER A 3.1 BY 6.8 AREA TO REMOVE THE CORROSION. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 365024-14, REV A.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · spar web · crackedApr 24, 1998

    WING LT, REAR SPAR WEB, OWS 77 LOWER CAP ATTACHMENT, REPAIR FOR WEB CRACK. THE LT WING REAR SPAR WEB WAS FOUND WITH A .50 LONG CRACK EMANATING FROM A FASTENER HOLE ATTACHING THE WEB TO THE LOWER SPAR CAP AT OWS 77. THE WEB CRACK WAS ROUTED OUT AND AN ALUMINUM DOUBLER AND TRIPLER INSTALLED. THE…

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

    FOUR FASTENER HOLES IN THE LOWER WING SKIN AT IWS 477 AND STRINGER 17 WERE FOUND CRACKED ON BOTH WINGS. THE CRACKS ARE THE SUBJECT OF SID AD 95-20-04, R1 (SID NR 57-3-2). THE CRACKED HOLES WERE OVERSIZED TO REMOVE THE CRACKS AND ALUMINUM BUSHINGS WERE INSTALLED. THE REPAIR WAS ACCOMPLISHED PER…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery pack · dischargedMar 11, 1998

    EMERGENCY LIGHTS DO NOT ILLUMINATE 16A/B AND 22H/J/ RT GALLEY LIFT AND LOWER GALLEY. REPLACED BATTERY PACK CHECKS OK.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery pack · dischargedMar 11, 1998

    EMERGENCY EXIT SIGN AT 3-R DOOR STOP ILLUMINATION AFTER TWO MINUTES. REPLACED BATTERY PACK, CHECKS OK.

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

Showing the 10 most recent of 153 reports.

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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