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Aircraft record

N719DA1976 Lockheed L-1011-385-1

DeregisteredUnclaimedSource: FAA, updated Oct 18, 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 incident (Jul 1992)23 ADs may apply119 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
1992
ADs may apply
23
confirm with A&P
Service reports
119
since 1995

Registration

FAA Aircraft Registry · Oct 18, 2026
Last registered owner
Individual owner
City, state
Kansas City, KS
Canceled
Feb 20, 2013
Airworthiness
Standard · Transport
Airworthiness date
Mar 30, 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-1135
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
A99DC8

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 18, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Incident

Jul 18, 1992 · Los Angeles, CA

A FAILURE OF GROUND PERSONNEL TO ENSURE PROPER CLEARANCE BETWEEN A TAXIING AIRPLANE AND AN ADJACENT PARKED AIRPLANE. CONTRIBUTING TO THE ACCIDENT WAS A FAILURE OF GROUND PERSONNEL TO PROPERLY POSITION A PARKED AIRPLANE TO ENSURE THAT IT DID NOT ENCROACH INTO AN ADJACENT SAFETY AREA.

Injuries
None
Report
LAX92IA307

From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX92IA307)

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 (119)

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.

  • Equipment and furnishings · outlet · shortedDec 16, 1998

    DURING TAXI OUT, FWD GALLEY RT SERVICE OUTLET SHORTED CAUSING SPARKS AND SMOKE IN THE CABIN. A/C RETURNED TO THE GATE. FOUND FWD GALLEY COFFEE POT LEAKING ON OUTLET. SECURED WATER AND FOUND FWD RT SERVICE OUTLET C/B POPPED IN LWR GALLEY. COLLARED C/B FOR FWD RT SERV OUTLET. REPLACED OUTLET.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedMar 6, 1998

    THE SKIN AT FS 328 AND LBL 22 WAS FOUND CORRODED NEAR THE CORNER OF THE NOSE LANDING GEAR DOOR CUTOUT. THE EXISTING AD MANDATED MOD DOUBLERS WERE ALSO FOUND CORRODED. THE SKIN WAS TRIMMED AWAY TO REMOVE THE CORROSION AND THE MOD DOUBLERS WERE REMADE TO ENCOMPASS THE DAMAGE. THE REPAIR WAS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedMar 6, 1998

    FUSELAGE/SKIN, FS 1645-1665, STRG 38-39. REPAIR FOR CORROSION CUTOUT. THE FUSELAGE SKIN WAS FOUND CORRODED BETWEEN FS 1645 AND 1665 AND BETWEEN STRINGERS 38 AND 39. THE CORROSION DAMAGE WAS CUTOUT AND AN EXTERNAL REPAIR DOUBLER AND TRIPLER WERE INSTALLED PER ER/A 364158-14, REV A.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Landing gear · sequence valve · failedJan 20, 1998

    AFTER T/O, THE DOOR RED AND INTRANSIT LIGHTS DID NOT GO OUT. LANDING GEAR LOWERED PER PROCEDURES, RIGHT GEAR GREEN LIGHT DID NOT COME ON. MANUALLY EXTENDED GEAR, LIGHT CAME ON. LEFT MLG SEQUENCE VLV REPLACED, RT MLG RETRACT ACTUATOR REPLACED, RIGGING THE RT MLG SEQUENCE VALVE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead panel · crackedOct 14, 1997

    THE FUSELAGE 1212 BULKHEAD PANEL WAS FOUND WITH A TYPICAL VERTICAL CRACK AS ADDRESSED BY LAC S/B 093-53-277. THE CRACK IN THIS CASE IS LOCATED AT RBL 6 AND IS APPROX 1.5 LONG. UPON REMOVAL OF THE CRACK, A SHORT FASTENER EDGE DISTANCE CONDITION RESULTED, REQUIRING AN ENLARGED CUTOUT AS SHOWN ON…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery pack · dischargedApr 26, 1997

    EMERGENCY AILSE LIGHT INOP AT 16B, 22B, 27H, 21H AND 16H. REPLACED EMERGENCY POWER PACK AT CENTER GALLEY. EMERGENCY LIGHTS INOP AT RT GALLEY AND DIM IN LOWER GALLEY. REPLACED LOWER GALLEY POWER PACK.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · sockets · shortedFeb 27, 1997

    EMERGENCY TRACK FLOOR LIGHTING INOP FROM RT AISLE SEAT ROW 20JH THROUGH 26JH. FOUND BULB SOCKET AT SEAT 23JH SHORTED. REPLACED SOCKET, OPS CHECKS NORMAL, DAL P/N337201959 MFG P/N08169-1. FOUND ON NR 2 LAYOVER CHECK.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · strap · damagedJan 31, 1997

    DURING ACCOMPLISHMENT OF SI 7-69959-12AD, THE AFT WEB SPLICE STRAPS AT RBL 42.5 AND LBL 42.5 WERE CUT AT THE LOWER END TO FACILITATE INSTALLATION OF THE LOWER CAP. REPAIRED PER SRM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · engine · malfunctionedNov 19, 1996

    NR 2 ENG EPR GRADUALLY ROLLED BACK ON CLIMBOUT. OTHER ENGINE PARAMETERS FOLLOWED, FUEL AMP NO HELP.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · fuel flow reg · malfunctionedNov 1, 1996

    ENG NR 2 FLAMED OUT SHORTLY AFTER TAXIING CLEAR OF RUNWAY AFTER LANDING, WAS VERY HARD TO START. REPLACED FFR ON NR 2 ENG, ENG STARTS NORMALLY. PERFORMED CKS PER PFHB, ALL CKS OK. T/O PWR REACHED WITH PLENTY OF ROOM, NO LEAKS.

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

Showing the 10 most recent of 119 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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