# N753DA: 1980 Lockheed L-1011-385-3, registration cancelled 2013-12-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 2, 2013 - Status when cancelled: First renewal notice - Airframe: [Lockheed L-1011-385-3](https://openairdocs.org/model/lockheed-l-1011-385-3) (registry code 5265020) - Engine: [Rolls-Royce RB-211-22 series](https://openairdocs.org/engine/rolls-royce-rb-211-22-series) (registry code 54554) - Data sheets: [TCDS A23WE](https://openairdocs.org/tcds/A23WE), [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (OpenAirDocs) - Serial number: 193W-1189 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 26, 1980 - Certificate issued: April 28, 2004 - Last registry action: April 14, 2012 - Mode S code: AA257A - 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/N753DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=753DA - Page: https://openairdocs.org/deregistered/N753DA-2013-12-02 From the FAA registry file of October 31, 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 2006FA0001155](https://openairdocs.org/sdr/2006FA0001155), Oct 9, 2006: FRAME. CRACKED. (REF NR: 06DA063) DURING C-CHECK, MAINTENANCE TASK 53-02-1000 INSP FS 983 FRAME. A CRACK, 3 INCHES) FOUND AT LT, BY A CLOSE VISUAL INSP AND CONFIRMED BY NDT. NR - [SDR DLL19001685](https://openairdocs.org/sdr/DLL19001685), Aug 31, 2000: LIGHT. INOPERATIVE. EXTERIOR LIGHT BY LT OVERWING EMERGENCY DOOR BURNED OUT. RELAMPED EXTERIOR LIGHT. - [SDR DLL19001131](https://openairdocs.org/sdr/DLL19001131), Jun 10, 2000: TIRE. DEFLATED. NR 3 FRONT TIRE DAMAGED AND FLAT UPON ARRIVAL. REMOVED AND REPLACED WHEEL ASSY. - [SDR DLL19000846](https://openairdocs.org/sdr/DLL19000846), Apr 29, 2000: ESCAPE HATCH. OPEN. COCKPIT ESCAPE HATCH OPENED DURING TAKEOFF ROLL AT 100 KIAS. ADJUSTED ESCAPE HATCH LINKAGE AND SAFTIED. DOOR OPS CHECK NORMAL. NOTE: COCKPIT ESCAPT HATCH LIGHT - [SDR DLL19000750](https://openairdocs.org/sdr/DLL19000750), Apr 18, 2000: CONTROL VALVE. INOPERATIVE. AFTER TAKEOFF WHEN GEAR HANDLE PUT IN THE UP POSITION, THE RED DOOR LIGHT AND THE RED INTRANSIT LIGHT ON FWD PNL REMAINED ILLUMINATED. ON THE S/O PNL THE LT GEA - [SDR DLL19000680](https://openairdocs.org/sdr/DLL19000680), Apr 8, 2000: LIGHT. INOPERATIVE. ON LAYOVER, FOUND EMERGENCY LIGHT ON DOOR L2 EXTERIOR INOP. RELAMPED, CKS GOOD. - [SDR DLL19992404](https://openairdocs.org/sdr/DLL19992404), Oct 30, 1999: LIGHT. INOP. ON L/O, FOUND L-2 EMERGENCY EXIT LIGHT AND L-2 EXTERIOR LIGHT INOP. - [SDR DLL19991849](https://openairdocs.org/sdr/DLL19991849), Aug 18, 1999: GCU. FAILED. ON TAKEOFF AT 0915 IN MCO FLT STATION BUS 2 FAIL LIGHT ILLUM. ABORTED TAKEOFF AT 125 KTS. APPLIED MINIMUM BRAKES DUE TO LIGHT WGT 332,000 LBS. C/W REPLACED NR 2 - [SDR DLL19991821](https://openairdocs.org/sdr/DLL19991821), Aug 14, 1999: BATTERY PACK. DISCHARGED. ON L/O, FOUND AFT LAV EMERGENCY TRACK LIGHTS INOP. REPLACED RACK FOR AFT A/C E-PATH LIGHTING ON RT AFT B/B. - [SDR DLL19991430](https://openairdocs.org/sdr/DLL19991430), Jun 24, 1999: WIRE. BROKEN. EMERGENCY LIGHTS INOP FROM ROW 10G TO ROW 16G. REPAIRED BROKEN WIRE IN TRACK AT 10G. - [SDR DLL19981680](https://openairdocs.org/sdr/DLL19981680), Aug 13, 1998: POWER SUPPLY. INOPERATIVE. F/C CABIN EMERGENCY TRACK LIGHTS GO OFF AFTER APPROX 1.5 MINUTES. REPLACED POWER SUPPLY. - [SDR DLL19981196](https://openairdocs.org/sdr/DLL19981196), Jun 4, 1998: SKIN. CRACKED. ON DESCENT SPEEDBRAKES WERE USED. WHEN SPEEDBRAKES WERE STOWED THE LT SPOILERS DID NOT RETRACT. AIRCRAFT DID SEVERE ROLL TO LT, TOOK ALMOST FULL CONTROL WHEEL T - [SDR DLL19980949](https://openairdocs.org/sdr/DLL19980949), May 3, 1998: BRAKE HOUSING. FAILED. ON L/O, FOUND NR 1F BRAKE HOUSING DAMAGED CAUSING THE DAMAGE TO THE WHEEL ASSY. THIS COULD HAVE CAUSED THE WHEEL TO SEIZE. - [SDR DLL19980881](https://openairdocs.org/sdr/DLL19980881), Apr 24, 1998: CONNECTOR. DIRTY. DURING CLIMB, NR 3 ENG FIRE WARNING FIRE HANDLE LT, DETECTOR AND BELL CAME ON WITH LOOP -A- SELECTED -B- LOOP INOP. SHUT DOWN ENG, DISCHARGED BOTTLES. CLEANED C - [SDR DLL19980580](https://openairdocs.org/sdr/DLL19980580), Mar 15, 1998: BULKHEAD CAP. CORRODED. THE LOWER CAP OF THE FS 983 BULKHEAD WAS FOUND CORRODED NEAR RBL 42.5 STR 28. THE LOWER FLANGE OF THE CAP WAS CUTOUT TO REMOVE THE DAMAGE. TWO REPAIR ANGLES WER - [SDR DLL19980548](https://openairdocs.org/sdr/DLL19980548), Mar 10, 1998: FRAME. CRACKED. REFERENCE N/R CARDS 274 AND 275 FRAME CRACK RT SIDE STA 1083 AND STA 1103 AT WATERLINE 200 AT FLOOR LONGERON ATTACH. REPAIRED PER EO764076-3. - [SDR DLL19980335](https://openairdocs.org/sdr/DLL19980335), Feb 9, 1998: SPAR. CRACKED. DURING INSPECTION OF THE LT AND RT WING REAR SPAR UPPER CAP FASTENER HOLES PER EO 7-59089-3 SEVERAL CRACK INDICATIONS WERE FOUND ON THE RT REAR SPAR. ALL NON CR - [SDR DLL15971727](https://openairdocs.org/sdr/DLL15971727), Sep 3, 1997: VALVE ACTUATOR. FAILED. 2L FUEL JETTISION VALVE DID NOT OPEN FOR JETTISION. VALVE ACTUATOR REPLACED, OPS OK. - [SDR DLL15971133](https://openairdocs.org/sdr/DLL15971133), Jun 15, 1997: FIRE DETECTOR. OIL SOAKED. NR 2 ENG SHUT DOWN DUE TO FIRE WARNING. FOUND B LOOP AT FWD GEAR BOX OIL SOAKED. REPLACED A/B LOOPS CLEANED CONNECTORS AND REPLACED NR 2 ENG FDCU. SYS CK GOOD. - [SDR DLL15970733](https://openairdocs.org/sdr/DLL15970733), Apr 9, 1997: SPAR CAP. CRACKED. SEVERAL HOLES IN THE RT WING REAR SPAR WERE FOUND CRACKED IN THE UPPER SPAR CAP BETWEEN IWS 293.58 AND IWS 346.109. THE HOLES ARE COMMON TO THE SPAR WEB AND SPA - [SDR DLL15970732](https://openairdocs.org/sdr/DLL15970732), Apr 9, 1997: FRAME. FATIGUE. A 1.5 INCH CRACK WAS FOUND IN THE SHADED AREA OF THE WEB AS SHOWN IN L1011 S/B 093-53-264. THE CRACK RUNS VERTICALLY OUT OF A FASTENER HOLE JUST BELOW THE LOWER - [SDR DLL15970714](https://openairdocs.org/sdr/DLL15970714), Apr 8, 1997: SKIN. CRACKED. THE LT WING LOWER CENTER SKIN PANEL WAS FOUND CRACKED AT APPROXIMATE IWS 562. THE CRACK IS APPROX .75 LONG AND EXTENDS FROM THE FWD, OUTB'D CORNER OF THE EXTERN - [SDR DLL15970668](https://openairdocs.org/sdr/DLL15970668), Apr 8, 1997: SKIN. CORRODED. THE UPPER SURFACE OF THE CENTER WING SKIN BETWEEN RBL AND LBL 94.5 AND 104 WAS FOUND WITH EXTENSIVE CORROSION. THE CORROSION WAS MOSTLY ISOLATED TO THE IMMEDIAT - [SDR DLL15962450](https://openairdocs.org/sdr/DLL15962450), Oct 16, 1996: RIB. CRACKED. THE LT WING IWS 555 RIB UPPER CAP AT STR 10 HAS A CRACK APPROX .875 INCH LENGTH. THE CRACK WAS STOP DRILLED, COLD WORKED AND EDDY CURRENT INSPECTED. REV B PROVI - [SDR DLL15960259](https://openairdocs.org/sdr/DLL15960259), Feb 2, 1996: SKIN. WORN. NUMBER 3 RT FLAP VANE CAME IN WITH WORN UPPER SKIN 15 TO 57 FROM INBOARD END. REPLACED SKIN SECTION PER SRM CHAPTER 57-53-00 FIG 815. - [SDR DLL15960151](https://openairdocs.org/sdr/DLL15960151), Jan 22, 1996: ACTUATOR. FAILED. ON APPROACH INTO ATL, WHEN THE GEAR WAS EXTENDED THE ACFT LOST C-SYST HYD PRESS. ON INSPECTION FOUND RT MLG RETRACT ACTUATOR LOWER END BLOWN OUT AND THE GEAR DO - [SDR DLL15954361](https://openairdocs.org/sdr/DLL15954361), Nov 13, 1995: DUCT. DETACHED. EXPERIENCED LOUD THUMP, UNKNOWN PROBLEM, OUTFLOW VALVE FULL CLOSED. FOUND COMPRESSOR OUTLET DUCT DETACHED. INSP AND REINSTALLED DUCT, LEAK CK OK NR 3 A/C PACK. - [SDR DLL15954342](https://openairdocs.org/sdr/DLL15954342), Nov 11, 1995: HARNESS. SHORTED. NR 2 GEN DISCONNECTED FROM BUS WOULD NOT RESET, VOLTS AND FREQS NORMAL, DIVERTED JFK. FOUND PIN 55 ON B1A GCU RACK CONNECTOR PUSHED BACK AND FOUND PIN 43 ON J1B - [SDR DLL15954160](https://openairdocs.org/sdr/DLL15954160), Oct 27, 1995: LATCH FITTINGS. CORRODED. DURING ACCOMPLISHMENT OF S.I. 7-58181-12AD, THE NR 7 C-1A CARGO DOOR LATCH FITTING HAD SURFACE CORROSION IN THE UPPER WELL. DRAIN HOLES HAVE BEEN ADDED IN THE C - [SDR DLL15953446](https://openairdocs.org/sdr/DLL15953446), Aug 17, 1995: EEL POWER SUPPLY. FAILED. DURING LAYOVER, COCKPIT EMERGENCY LIGHTS WOULD NOT TEST. REPLACED POWER SUPPLY, OPERATION NORMAL. ## FAA accident and incident reports (3) 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 19940531028499I](https://openairdocs.org/incident/19940531028499I), May 31, 1994: Lkheed 10113853 (N753DA), Madrid, SP, Minor damage. Cargo door light came on. Aborted taxied to gate. Main tires flat and small fire. Emergency handled correctly. - [Incident 19900522023789I](https://openairdocs.org/incident/19900522023789I), May 22, 1990: Lkheed 10113853 (N753DA), Covington - Cin, OH. NR2 air data computer unit failed after takeoff. Returned. Replaced unit. - [Incident 19900309057199I](https://openairdocs.org/incident/19900309057199I), Mar 9, 1990: Lkheed 10113853 (N753DA), Atlanta, GA. NR1 engine power rolled back to idle inflight. Precautionary landing. Fuel flow regulator faulty. --- 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.