# N754DL: 1980 Lockheed L-1011-385-3, registration cancelled 2013-09-10 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 10, 2013 - Status when cancelled: Valid registration - Airframe: [Lockheed L-1011-385-3](https://openairdocs.org/model/lockheed-l-1011-385-3) (registry code 5265020) - Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555) - Data sheets: [TCDS A23WE](https://openairdocs.org/tcds/A23WE) (OpenAirDocs) - Serial number: 193Y1181 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 24, 1980 - Certificate issued: April 28, 2004 - Last registry action: April 14, 2012 - Mode S code: AA293B - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N754DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=754DL - Page: https://openairdocs.org/deregistered/N754DL-2013-09-10 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Lockheed L-1011-385-3: https://openairdocs.org/model/lockheed-l-1011-385-3.md ## Service difficulty reports (30) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DLL19001872](https://openairdocs.org/sdr/DLL19001872), Sep 26, 2000: COOLING FAN. SEIZED. AIRBORN SMELLED ELECTRICAL ARCING WITH AN UNUSUAL MOTOR NOISE ORIGINATING FROM BEHIND F/E PANEL. FOUND INSTRUMENT COOLING FAN LOCKED UP AND VERY HOT. REPLACED F - [SDR DLL19001063](https://openairdocs.org/sdr/DLL19001063), May 30, 2000: POWER SUPPLY. INOPERATIVE. EMERGENCY EXIT LIGHTS AND FUSELAGE LIGHTS INOP B ZONE LT SIDE ROW 13 - 21. REPLACED POWER SUPPLY. - [SDR DLL19992533](https://openairdocs.org/sdr/DLL19992533), Nov 16, 1999: UNSERV. WHILE TRYING TO CRANK R-2 DOOR SHUT DOOR SLIDE DEPLOYED. REPLACED SLIDE. - [SDR DLL19992439](https://openairdocs.org/sdr/DLL19992439), Nov 4, 1999: ENGINE. FAILED. NR 3 MOTOR SUFFERED CONTINOUS INFLIGHT STALLS JUST AFTER LIFTOFF. REPORTED AGL WAS APPROX 400 FT. ENG PARAMETERS WAS FLUCUATING WITH STALLS. STALLS WERE VERY LO - [SDR DLL19991923](https://openairdocs.org/sdr/DLL19991923), Aug 28, 1999: RETRACT MECH. MALFUNCTIONED. ON APPROACH GEAR WOULD NOT EXTEND NORMALLY. NO ABNORMAL INDICATIONS NOTED. EXTENDED GEAR USING MANUAL EXTENSION HANDLES. INITIAL INDICATIONS INTRANSIT LIGHT AND - [SDR DLL19991838](https://openairdocs.org/sdr/DLL19991838), Aug 16, 1999: SKIN. CORRODED. THE FUSELAGE BELLY SKIN AT FS 886 BETWEEN STR 33 AND 32 WAS FOUND WITH AN AREA OF CORROSION. THE CORROSION WAS REMOVED WITH A 3.7 X 5 CUTOUT. THE CUTOUT WAS NEA - [SDR DLL19991373](https://openairdocs.org/sdr/DLL19991373), Jun 16, 1999: SENSOR. FAILED. ON DESCENT, SMOKE ODOR IN CABIN. NR 2 PACK COMPRESSOR DISCHARGE TEMP OFF SCALE HIGH. ACM TEMP 40 DEGREES. REPLACED COMPRESSOR DISCHARGE TEMP SENSOR. - [SDR DLL19990914](https://openairdocs.org/sdr/DLL19990914), Apr 26, 1999: SWITCH. BROKEN. ELECTRICAL SMOKE ODOR IN COCKPIT ISOLATED A/C AND D/C POWER. NO EXCESSIVE LOADS ON ANY BUSS. FOUND RT WING LANDING LIGHT SWITCH BROKEN. REPLACED SWITCH. - [SDR DLL19990619](https://openairdocs.org/sdr/DLL19990619), Mar 20, 1999: INTERCOSTAL. CRACKED. A .25 INCH TYPICAL CRACK WAS FOUND IN A RELIEF RADIUS OF THE NR 4 INTERCOSTAL AT THE L3 DOOR CUT OUT AFT DOOR JAMB. THE ADJACENT FITTING INTERCOSTALS WERE UNDAM - [SDR DLL19981334](https://openairdocs.org/sdr/DLL19981334), Jun 24, 1998: SKIN. CORRODED. FUSELAGE/SKIN, FS 829-846, STRG 33-34, REPAIR FOR CORROSION CUTOUT. THE FUSELAGE BELLY SKIN BETWEEN FS 829 AND 846 WAS FOUND CORRODED AT STRINGER 33. THE CORROD - [SDR DLL19981251](https://openairdocs.org/sdr/DLL19981251), Jun 12, 1998: LINE. BROKEN. C-SYSTEM HYD RESERVOIR QTY SLOWLY DROPPED TO ZERO, ONE AND ONE HALF HOURS. SWITCHING OFF PUMPS DID NOT STOP GAUGE DROP. LOW QTY LIGHT ILLUMINATED. FOUND BROKEN - [SDR DLL19981071](https://openairdocs.org/sdr/DLL19981071), May 18, 1998: PBE. DAMAGED. PBE IN AFT LEFT CABIN FOUND DAMAGED. REPLACED PBE UNIT. - [SDR DLL15980257](https://openairdocs.org/sdr/DLL15980257), Jan 30, 1998: ENGINE. MALFUNCTIONED. NR 1 ENG ROLLED BACK DURING ENG START AND HAD SUBSEQUENT TAILPIPE FIRE. INSPECTED ENG, NO DEFECTS NOTED. STARTED NR 1 ENG WAS SUCCESSFUL. - [SDR DLL15980250](https://openairdocs.org/sdr/DLL15980250), Jan 29, 1998: HYD LINE. RUPTURED. A/C REJECTED T/O DUE TO C-SYS LOST. FOUND NR 2 ENG RT HYD PUMP PRESS LINE BAD. REPLACED SAME, GROUND OPS NORMAL. - [SDR DLL15971769](https://openairdocs.org/sdr/DLL15971769), Sep 10, 1997: LUG. CRACKED. LEFT MAIN LANDING GEAR RETRACT PIN LUG CRACKED (P/N 1642699-101), (S/N 176A). REPLACED PIN. - [SDR DLL15971193](https://openairdocs.org/sdr/DLL15971193), Jun 19, 1997: BATTERY PACK. DISCHARGED. L2 CABIN DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, CHECKS NORMAL. - [SDR DLL15970682](https://openairdocs.org/sdr/DLL15970682), Apr 16, 1997: LIGHT. INOPERATIVE. F/C EMERGENCY TRACK LIGHTING INOP. - [SDR DLL15970681](https://openairdocs.org/sdr/DLL15970681), Apr 16, 1997: LIGHT. INOPERATIVE. AFT EMERGENCY TRACK LIGHTS INOP. - [SDR DLL15962719](https://openairdocs.org/sdr/DLL15962719), Dec 11, 1996: SKIN. CORRODED. THE UPPER SURFACE OF THE CENTER WING SKIN BETWEEN RBL AND LBL 94.5 AND 115.8 WAS FOUND CORRODED FROM THE FRONT SPAR TO THE REAR SPAR AT FS 1212. THE CORROSION W - [SDR DLL15962718](https://openairdocs.org/sdr/DLL15962718), Dec 3, 1996: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND CRACKED UNDER THE RT EXTERNAL FUSELAGE TO WING BOX LONGERON. THE CRACK IS THROUGH TWO ATTACHMENT HOLES COMMON TO THE STA 983 BULKHEA - [SDR DLL15962722](https://openairdocs.org/sdr/DLL15962722), Dec 2, 1996: SPAR. CRACKED. SEVERAL HOLES IN THE RT REAR SPAR, UPPER CAP AND UPPER WING SKIN WERE FOUND CRACKED FROM THE FASTENER HOLES. - [SDR DLL15962720](https://openairdocs.org/sdr/DLL15962720), Nov 18, 1996: FRAME. CORRODED. THE P-DOME ZEE FRAME BETWEEN S-29 AND S-37 WAS FOUND CORRODED AND IN NEED OF REPLACEMENT. A NEW SECTION WAS SPLICED IN. - [SDR DLL15962615](https://openairdocs.org/sdr/DLL15962615), Nov 18, 1996: SKIN. CRACKED. THE FUSELAGE SKIN WAS SEVERLY CORRODED AND CRACKED BETS FS 629 TO 659 AND STR 32 TO 34, DIMENSIONS: 30 X 20. THIS WAS REPAIRED BY TRIMMING THE SKIN TO REMOVE AL - [SDR DLL15962723](https://openairdocs.org/sdr/DLL15962723), Nov 11, 1996: PRESS DECK. CRACKED. THE FUSELAGE HORIZ PRESSURE DECK PANEL WAS FOUND WITH A 1 INCH LONG CRACK AT RBL 102, JUST AFT OF FS 378. THE CRACK WAS CUTOUT AND REINFORCED WITH DOUBLERS. - [SDR DLL15961873](https://openairdocs.org/sdr/DLL15961873), Aug 11, 1996: BULB. FAILED. AFT SECTION E PASS LIGHTS ARE INOP. RELAMPED 2 AFT LIGHTS, CKS GOOD. - [SDR DLL15960267](https://openairdocs.org/sdr/DLL15960267), Feb 4, 1996: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT INOP AT 2L DOOR. REPLACED POWER SUPPLY, CHECKS OK. - [SDR DLL15960050](https://openairdocs.org/sdr/DLL15960050), Dec 11, 1995: FITTING. CORROSION. DURING COMPLETION OF SI 7-58-181-12AD, SURFACE CORROSION WAS FOUND IN THE UPPER WELL LOWER WEBS ON EACH OF THE EIGHT FITTINGS. IN ADDITION THE NR 1 LATCH FITTIN - [SDR DLL15952327](https://openairdocs.org/sdr/DLL15952327), May 27, 1995: WIRE. SHORTED. DURING LAYOVER, WHILE WORKING DEFERRED ITEM FOR TRIPPED GALLEY POWER BREAKERS, FOUND FWD GALLEY FEEDER WIRES BURNED BELOW FWD CARGO COMPARTMENT FLOOR. WIRES WER - [SDR DLL15951397](https://openairdocs.org/sdr/DLL15951397), Apr 5, 1995: PAN. CRACKED. CRACK IN NR 3 ENG PYLON BOX PAN FWD OF HYD SUPPLY LINE. REF SRM 54-11-00 ITEM 37. CRACK IS TO BE WELDED PER SRM 54-11-00 PG 812. - [SDR DLL15950431](https://openairdocs.org/sdr/DLL15950431), Jan 28, 1995: OVEN. FIRE. DURING CRUISE, HAD DEBRIS IN GALLEY OVEN CATCH FIRE. EXTINGUISHED FIRE USING HALON BOTTLE. REPLACED OVEN AND FIRE BOTTLE. RETURNED TO SERVICE. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19930325014969I](https://openairdocs.org/incident/19930325014969I), Mar 25, 1993: Lkheed 10113853 (N754DL), New York, NY. Pilot was experiencing a galley fire. Returned to jfk. Fires extinguished using halon extinguishers. Replaced oven. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.