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Aircraft record

N720DA1976 Lockheed L-1011-385-1

DeregisteredUnclaimedSource: FAA, updated Oct 16, 2026

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

Safety record in brief:1 NTSB accident (substantial damage, Aug 1987)23 ADs may apply42 service difficulty reports

Registration
Deregistered
Last based in
Kansas City, KS
owner city / state
Engine
RB-211 SERIES · 22,000 lb thrust
Rolls-Royc
Owners
1
on record
NTSB events
1
substantial, 1987
ADs may apply
23
confirm with A&P
Service reports
42
since 1995

Registration

FAA Aircraft Registry · Oct 16, 2026
Last registered owner
Individual owner
City, state
Kansas City, KS
Canceled
Jun 13, 2013
Airworthiness
Standard · Transport
Airworthiness date
Feb 25, 1994

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-1136
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
A9A3D8

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 ownerKansas City, KS

Individual owners are shown by city and state only.

Safety record

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

NTSB events (1)

Accident · substantial damage

Aug 25, 1987 · Atlanta, GA

THE ACFT WAS BEING FLOWN MANUALLY FOR AN ILS APCH TO RWY 8L AT ATLANTA. THE APCH WAS ALLOWED TO BECOME UNSTABLE AT ABOUT THE MIDDLE MARKER AND THE VERTICAL SPEED WAS INCREASED TO ABOUT 1290 FEET PER MINUTE ABOUT FIVE SECONDS BEFORE TOUCHDOWN. THE IOE CAPT IN THE LEFT SEAT WAS TOLD BY THE COMPANY CK AMN THAT HE NEEDED TO GET HIS NOSE UP. AS THE IOE CAPT INITIATED FLARE, THE CK AMN ALSO APPLIED…

Damage
Substantial
Injuries
None
Report
ATL87FA240

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL87FA240)

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 (42)

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.

  • Engine controls · throttle · wornNov 3, 1999

    WHILE IN CRUISE NR 2 ENGINE POWER DECREASED AS THROTTLE WAS IN STATIONARY POSITION DURING APPROACH AT FL 100 THROTTLE WAS RETURNED TO IDLE STOP, BUT FUEL FLOW REMAINED AT 5000 LBS AND N2 WAS AT 79 PERCENT ENGINE WAS SHUT DOWN. FOUND THROTTLE RACK AND TELEX DOVETAIL WORN. REPLACED BOTH.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · stringer · crackedSep 24, 1999

    THE LBL 25.5 KEELSON STRINGER WAS FOUND WITH A 1.5 INCH LONG CRACK RUNNING FWD-AFT IN THE HORIZONTAL FLANGE AT FS 1357. THE STRINGER WAS CUT AT FS 1357 AND THE AFT END REMOVED. A NEW AFT SECTION WAS FABRICATED AND SPLICED IN PER ER/A 368337-14, REV A.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · air dist · odorSep 10, 1999

    AFTER TAKEOFF ATL, A VERY NOXIOUS ODOR CAME FROM THE AIR CONDITIONING SYSTEM IT SET OFF THE AFT SMOKE DET IN AFT LAVS. ODOR REDUCED AND SEEMED SPENT AS A/C PRESSURIZED AND WE CLIMBED TO HIGHER ALT. RAN PACKS WITH ALL THREE ENGS AT T/O PWR NO DISCREPANCIES NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Engine · seal · failedJun 27, 1999

    DURING FLT, USUALLY AT REDUCED POWER, CABIN FILLED WITH A BLUE HAZE AND LAV SMOKE DETECTORS IN FWD AND AFT LAVS WENT OFF FOR SEVERAL MINUTES. REPLACED NR 3 ENGINE DUE TO FRONT BEARING OIL LEAK.

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

    THE UPPER AFT CORNER OF THE R1 DOOR CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE SKIN ASSY AND TRIPLER. THE AREA WAS X-RAYED TO DETERMINE THE EXACT END OF THE CRACK AND REPAIRED PER L1011 SRM 53-31-00, FIG 836. THE REPAIR WAS DOCUMENTED PER ER/A 366927-14.

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

    A CRACK WAS FOUND IN SKIN ASSY OF THE UPPER FORWARD CORNER OF THE L3 DOOR CUTOUT. THE CRACK IS IN THE SKIN, DOOR SURROUND DOUBLER, AND TRIPLER. THE SKIN ASSY WAS X-RAYED TO DETERMINE THE END OF THE CRACK AND THEN REPAIRED PER L1011 SRM 53-31-00, FIG 836. THE INSPECTION AND REPAIR WAS DOCUMENTED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · hyd line · brokenDec 25, 1998

    AFTER TAKEOFF, COULD NOT RETRACT LANDING GEAR ALSO GOT TRUCK LIGHT ON, PERFORMED POM PROCEDURES AND RETUNED TO AIRPORT. MTC FOUND HYD FUSE SET AND FLEX LINE ON RIGHT GEAR TO RIGID LINE ON BOGGIE BEAM BROKEN. REPLACED LINE AND RESET FUSE, LEAK CHECKS OK. A/C DEPARTED WITHOUT FURTHER INCIDENT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · power supply · inoperativeAug 8, 1998

    EMERGENCY EXTERIOR LIGHTS INOP LEFT FWD. REPLACED BATTERY AND PWR SUPPLY, SYS NOW CKS OK.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · gearbox · failedApr 5, 1998

    BEGINNING DESCENT, -A- SYSTEM PRESSURE 0, QUANTITY REMAINED. IDG LOW OIL PRESSURE LIGHT ON, GEN DISCONNECTED. DISCONNECTED IDG. ON APPROACH NR 1 OIL QTY DROPPED, QTY BELOW 10. NR 1 ENG SHUTDOWN. AT GATE NR 1 ENG OIL QTY 0. REPLACED NR 1 ENG MAIN GEARBOX ON ROUTINE CHECK. PERFORMED TESTS 1-3-9-16…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedMar 28, 1998

    THE FUSELAGE SKIN AT FS 759 AND STRINGER 38 WAS FOUND CRACKED DUE TO CORROSION. THE CORRODED AREA WAS TRIMMED OUT AND AN EXTERNAL ALUMINUM DOUBLER WAS INSTALLED PER ER/A 364366-14, REV A.

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

Showing the 10 most recent of 42 reports.

Related aircraft

Show all 8 related aircraft

Sources

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

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