# N755DL: 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-211-22 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: 193Y1184 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 7, 1980 - Certificate issued: April 28, 2004 - Last registry action: April 14, 2012 - Mode S code: AA2CF2 - 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/N755DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=755DL - Page: https://openairdocs.org/deregistered/N755DL-2013-09-10 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 (35) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DLL19001775](https://openairdocs.org/sdr/DLL19001775), Sep 14, 2000: LATCH. OUT OF ADJ. ON LIFT OFF DOOR LIGHT ILLUMINATED, CHECKED S/O''S PANEL AND BOTH FWD AND AFT CARGO DOOR LIGHTS REMAINED ON. FOUND LOCK MECHANISM OUT OF ADJUSTMENT. RIGGED PER - [SDR DLL19001220](https://openairdocs.org/sdr/DLL19001220), Jun 27, 2000: WIRE. BROKEN. FOUND DURING LAYOVER THREE FOOT SECTION OF EMERGENCY TRACK LIGHTING AT LEFT SIDE OF MIDDLE GALLEY INOPERATIVE - REPAIRED BROKEN WIRE IN TRACK - [SDR DLL19000949](https://openairdocs.org/sdr/DLL19000949), May 12, 2000: LIGHT. MALFUNCTIONED. ON L/O, FOUND 2R EXTERIOR EMERGENCY LIGHT ON CONSTANTLY. REPLACED POWER SUPPLY. - [SDR DLL19992546](https://openairdocs.org/sdr/DLL19992546), Nov 18, 1999: UNKNOWN. ODOR. NUMEROUS COMPLAINTS OF SMOKE ODOR IN CABIN. INSPECTED CABIN AND GALLEYS FOR FAULTS AND FOUND NONE. OPERATED AIR CONDITIONING SYSTEM FOR 30 MINUTES WITH NO FAULT - [SDR DLL19992131](https://openairdocs.org/sdr/DLL19992131), Sep 23, 1999: CONTROL CABLE. OUT OF ADJ. MAIN LT GEAR DOOR LIGHT ON WITH DOOR INTRANS LIGHTS ON GEAR ANNUNICATOR. RAN POM CK LIST, CYCLED GEAR AUTOMATICALLY AND USING MECHANICAL RELEASE HANDLES, NO HEL - [SDR DLL19992127](https://openairdocs.org/sdr/DLL19992127), Sep 22, 1999: SNUBBER. BROKEN. ON ARRIVAL, LEFT MAIN LANDING GEAR DOOR HANGING DOWN. MTC FOUND LEFT MLG DOOR SNUBBER ROD BROKEN. REPLACED LEFT MLG DOOR SNUBBER ROD. DOOR OPS NORMAL. - [SDR DLL19991434](https://openairdocs.org/sdr/DLL19991434), Jun 23, 1999: STIFFENER. CRACKED. THE LBL 30 VERTICAL STIFFENER ON THE CENTER WING FRONT SPAR WAS FOUND CRACKED AT A LIGHTENING HOLE 12 FROM THE UPPER END OF THE STIFFENER. THE UPPER END OF THE - [SDR DLL19990983](https://openairdocs.org/sdr/DLL19990983), May 5, 1999: REGULATOR. FAILED. CAPTS 02 MASK HAS CONTINUOUS FLOW IN ON POSITION ON REGULATOR PANEL. PANEL SWITCH MUST BE TURNED OFF TO CEASE FLOW. CREW 02 PRESSURE NOW AT 800 PSI. REPLACED CA - [SDR DLL19982534](https://openairdocs.org/sdr/DLL19982534), Dec 9, 1998: SKIN. CRACKED. THE LT WING LOWER SKIN WAS FOUND WITH A 1.25 INCH LONG CRACK BETWEEN FASTENER HOLES AT THE END OF STRINGER 16 (OWS 130). THE CRACK WAS ROUTED OUT OF THE SKIN AN - [SDR DLL19981299](https://openairdocs.org/sdr/DLL19981299), Jun 18, 1998: VIBRATION LIGHT. ILLUMINATED. NR 3 VIBRATION LIGHT CAME ON. INDICATED APPROX 2.9 BOTH A AND B. ACCOMPANIED BY ENGINE VIBRATION. SHUT DOWN ENGINE VIAPOM. CRUISE AT 350. NO THROTTLE MOVEMENT A - [SDR DLL15980591](https://openairdocs.org/sdr/DLL15980591), Mar 16, 1998: BATTERY PACK. DISCHARGED. AFT CABIN EMERGENCY FLOOR LIGHTS INOP BOTH SIDES. REPLACED BATTERY PACK. - [SDR DLL15980590](https://openairdocs.org/sdr/DLL15980590), Mar 16, 1998: POWER SUPPLY. INOPERATIVE. AFT CABIN FLOOR EMERGENCY LIGHTS ON BOTH SIDES INOP. REPLACED POWER SUPPLY. - [SDR DLL15980589](https://openairdocs.org/sdr/DLL15980589), Mar 16, 1998: BATTERY PACK. DISCHARGED. BATTERY DISCHARGED RAPIDLY BY DEFECTIVE BATTERY CHARGER/ POWER SUPPLY. REPLACED BATTERY PACK. - [SDR DLL15980587](https://openairdocs.org/sdr/DLL15980587), Mar 16, 1998: POWER SUPPLY. INOPERATIVE. BATTERY PACK WOULD NOT LIGHT CABIN OVERHEAD, AFT GALLEY OR OUTSIDE ESCAPE SLIDE LIGHTS DURING TEST. - [SDR DLL15972698](https://openairdocs.org/sdr/DLL15972698), Dec 19, 1997: REAR SPAR. CRACKED. THE LT AND RT REAR SPAR UPPER CAP TO WEB ATTACH HOLES WERE OVERSIZED BEYOND REPAIRABLE LIMITS TO REMOVE CRACKS. THE REAR SPARS WERE SUBSEQUENTLY MODIFIED BY REP - [SDR DLL15970461](https://openairdocs.org/sdr/DLL15970461), Mar 7, 1997: SKIN. CORROSION. DURING INSPECTION, CORROSION WAS FOUND IN THE MATING SURFACE BETWEEN THE L3 DOOR TRIPLER PAD-UP LIP AND THE UPPER EDGE OF THE FUSELAGE SKIN. REMOVAL OF THE CORR - [SDR DLL15970448](https://openairdocs.org/sdr/DLL15970448), Mar 7, 1997: SILL. CORROSION. THE L-2 PASSENGER DOOR SURROUND LOWER SILL WAS FOUND WITH CORROSION ON ITS OUTER CAP AT STA 895. THE CORROSION WAS REMOVED FROM THE UPPER AND LOWER SURFACES OF - [SDR DLL15970449](https://openairdocs.org/sdr/DLL15970449), Mar 5, 1997: REAR SPAR. CRACKED. DURING ACCOMPLISHMENT OF E.O. 7-59089-3, SEVERAL HOLES IN THE LT WING REAR SPAR WERE FOUND CRACKED IN THE UPPER SPAR CAP BETWEEN IWS 293.58 AND IWS 346.109. THE - [SDR DLL15970415](https://openairdocs.org/sdr/DLL15970415), Mar 4, 1997: PRESSURE DECK. CRACKED. THE FUSELAGE HORIZONTAL PRESSURE DECK PANEL WAS FOUND WITH A 1.75 INCH LONG CRACK. THE CRACK IS LOCATED AT RBL 102, JUST AFT OF FS 378, AND EXTENDS DIAGONALLY I - [SDR DLL15970414](https://openairdocs.org/sdr/DLL15970414), Mar 4, 1997: SPAR CAP. CRACKED. DURING ACCOMPLISHEMENT OF EO 7-59089-3, 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 - [SDR DLL15970413](https://openairdocs.org/sdr/DLL15970413), Mar 4, 1997: BULKHEAD PANEL. CORROSION. THE AFT PRESSURE BULKHEAD LOWER GORE PANEL WAS FOUND CORRODED IN SEVERAL AREAS BETWEEN STRINGERS 31 AND 33. THE BONDED GORE DOUBLER WAS FOUND CORRODED BETWEEN S - [SDR DLL15970412](https://openairdocs.org/sdr/DLL15970412), Mar 4, 1997: SKIN. CORROSION. DURING ROUTINE FLOOR PANEL OPEN-UP AT HMV, THE UPPER SURFACE OF THE CENTER WING SKIN BETWEEN RBL AND LBL 94.5 AND 115.8 WAS FOUND TO HAVE CORROSION. THE CORROSI - [SDR DLL15970411](https://openairdocs.org/sdr/DLL15970411), Mar 4, 1997: BULKHEAD FRAME. CORROSION. THE AFT P-DOME ZEE FRAME WAS FOUND WITH CRACKS DUE TO CORROSION IN THE ZEE ANGLE AND WEB. THE DAMAGED FRAME SEGMENTS WERE CUT AND REMOVED AND WILL BE SPLICE REP - [SDR DLL15970410](https://openairdocs.org/sdr/DLL15970410), Mar 4, 1997: SKIN. DENTED. THE L-3 DOOR OUTER SKIN AT THE LOWER AFT CORNER WAS FOUND DENTED AND GOUGED 4.25 FWD OF THE AFT DOOR EDGE. THE RESULTING CUTOUT MEASURES 3.0 WIDE BY 8.7 TALL. N - [SDR DLL15970307](https://openairdocs.org/sdr/DLL15970307), Feb 11, 1997: SKIN. CRACKED. DURING INSPECTION OF THE RT WING LOWER SKIN AT THE OUTBOARD END OF STRINGER 18 PER E.O. 7-70043-3, A CRACK WAS FOUND EMANATING FROM THE STRINGER END, FORWARD FA - [SDR DLL15970068](https://openairdocs.org/sdr/DLL15970068), Jan 15, 1997: POWER SUPPLY. MALFUNCTIONED. DURING TEST OF THE EMERGENCY LIGHTING SYSTEM, IT WAS DISCOVERED THAT THE TRACK LIGHTS IN FIRST CLASS EXTINGUISHED AFTER TOO SHORT A TIME PERIOD. THE POWER SUPPL - [SDR DLL15962706](https://openairdocs.org/sdr/DLL15962706), Dec 18, 1996: SOCKET. BROKEN. EMERGENCY PATH LIGHTS SOCKET BROKEN AT ROW 22G AND 27C. INSTALLED NEW LIGHT SOCKETS, OPS CHECK OK. - [SDR DLL15962575](https://openairdocs.org/sdr/DLL15962575), Nov 23, 1996: VIB MONITOR. MALFUNCTIONED. NR 2 ENGINE WAS SHUTDOWN ON DESCENT APPROX 20K FT. HIGH VIBS BOTH CHANNELS 2.6 VIBS. NO OTHER ABNORMAL ENGINE INDICATIONS, NO ICING PRESENT. REPLACED ENG VIB MO - [SDR DLL15962155](https://openairdocs.org/sdr/DLL15962155), Sep 22, 1996: LIGHT. INOPERATIVE. EMERGENCY LIGHT INOP AT SEAT 32C. REPLACED LIGHT SOCKET, BULB AND LENS. - [SDR DLL15961558](https://openairdocs.org/sdr/DLL15961558), Jun 29, 1996: LIGHTS. BROKEN. ON L/O, FOUND EMERGENCY FLOOR TRACK LIGHTS 1B, 12E, 24G INOP. REPLACED LAMP HOLDERS ON 1B, 12E, 24G, EMERGENCY LIGHTS CK GOOD. - [SDR DLL15960633](https://openairdocs.org/sdr/DLL15960633), Mar 21, 1996: LIGHT. BROKEN. EMERGENCY LIGHT CAME APART L1 DOOR EXIT SIGN. REPLACED LIGHT ASSY. - [SDR DLL15960292](https://openairdocs.org/sdr/DLL15960292), Feb 6, 1996: CONTROL CABLE. JAMMED. ON TAXI OUT - RUDDER PEDAL WOULD NOT MOVE LEFT - RIGHT MOVEMENT OK. FOUND CAPTAIN'S FORE/AFT RUDDER POSITION HAND CRANK MECHANISM JAMMED. FREED CABLE. OPERATION - [SDR DLL15960103](https://openairdocs.org/sdr/DLL15960103), Jan 16, 1996: BATTERY PACK. DISCHARGED. OVERHEAD EMERGENCY LIGHTS AT 20AB INOP. REPLACED DEFECTIVE BATTERY PACK AT 22AB OVERHEAD AND LIGHTS CHECK GOOD. - [SDR DLL15954392](https://openairdocs.org/sdr/DLL15954392), Oct 31, 1995: VANE. CRACKED. DURING SHOP INSPECTION, NR 1 RT FLAP VANE WAS FOUND WITH WEAR DAMAGE AT OUTBOARD RUB STRIP 8 INCHES FROM TRAILING EDGE. REPAIRED PER SRM 57-53-00. - [SDR DLL15954649](https://openairdocs.org/sdr/DLL15954649), Oct 17, 1995: SKIN. WORN. NR 3 RT FLAP VANE UPPER SKIN HAD A WORN AND SCRATCHED SPOT. REPLACED SKIN SECTION PER SRM 57-53-00. ## 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 19940516028869I](https://openairdocs.org/incident/19940516028869I), May 16, 1994: Lkheed 10113853 (N755DL), Los Angeles, CA. Using engine NR2 to taxi after pushback. Jet blast injured 2 ground crewmen servicing another aircraft. --- 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.