# N763DL: 1979 Lockheed L-1011-385-3, registration cancelled 2010-06-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 4, 2010
- Status when cancelled: Triennial form not returned
- 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: 193Y-1197
- Year built: 1979
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 19, 1981
- Certificate issued: April 28, 2004
- Last registry action: April 20, 2010
- Mode S code: AA4D03
- 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: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N763DL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=763DL
- Page: https://openairdocs.org/deregistered/N763DL-2010-06-04

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 (94, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DLL19982227](https://openairdocs.org/sdr/DLL19982227), Oct 28, 1998: FUEL PUMP. MALFUNCTIONED. WHILE CLIMBING THRU 30000 FT NOTICED NBR 2 ENG FUEL PRESS. LIGHT ILLUM. REF. POM MANUAL.INITIALLY LIGHT WAS INTERM.-AFTER 1 MIN. WENT TO STEADY.F/O NOTICED N1 A
- [SDR DLL19982095](https://openairdocs.org/sdr/DLL19982095), Oct 8, 1998: BATTERY PACK. DISCHARGED. ON A/C LAYOVER CHECK, FOUND F/C TRACK LIGHT INOP. LIGHT BATTERY PACK BAD. REPLACED PACK LOCATED IN FWD BAG BIN, P/N 337701962 S/N 0417.
- [SDR DLL19981074](https://openairdocs.org/sdr/DLL19981074), May 19, 1998: CIRCUIT BREAKER. MALFUNCTIONED. AT ALTITUDE COULD NOT GET FUEL OUT OF TANK NR 1, IMBALANCE AT 5000 LBS BETWEEN TANKS 1 AND 3. WITH TANK PUMPS FOR ENGINE NR 3 UNLATCHED FUEL QUANTITY CONTINUED 
- [SDR DLL19980077](https://openairdocs.org/sdr/DLL19980077), Jan 12, 1998: FIRE WARNING. FALSE WARNING. NR 3 ENG FIRE WARNING INFLIGHT. SHUT DOWN ENG IAW POM. FUEL AND IGN OFF, FIRE HDL PULLED, HYD PUMP OFF AND IDG DISC. REPLACED UPPER AND LOWER GAS GENERATOR LOOP
- [SDR DLL19980078](https://openairdocs.org/sdr/DLL19980078), Jan 10, 1998: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH A CRACK EMANATING FROM TWO DRAIN MAST HOLES AT FS 1836 BETWEEN STRINGERS 39 AND 40. THE SKIN WAS CUT OUT TO REMOVE THE CRACKS A
- [SDR DLL19980076](https://openairdocs.org/sdr/DLL19980076), Jan 9, 1998: SPAR. CRACKED. DURING INSPECTION OF THE LT WING REAR SPAR, 3 FASTENER HOLES WERE FOUND WITH CRACK INDICATIONS. THE HOLES WERE OVERSIZED, COLDWORKED, INSPECTED, BUSHED, AND NEW
- [SDR DLL19972521](https://openairdocs.org/sdr/DLL19972521), Dec 2, 1997: DUCT. FAILED. ON T/O, HP DUCT BLEW CAUSING FIRE WARNING, ALT FIRE BOTTLE DISCHARGED. REPLACED ENGINE.
- [SDR DLL19971989](https://openairdocs.org/sdr/DLL19971989), Sep 18, 1997: COUNTERBALANCE. FAILED TEST. L-3 COUNTERBALANCE FAILED SI 72565-12. REPLACED COUNTERBALANCE.
- [SDR DLL19971988](https://openairdocs.org/sdr/DLL19971988), Sep 8, 1997: COUNTERBALANCE. FAILED. L-2 COUNTERBALANCE FAILED SEPICAL INSPECTION 72565-12. REPLACED COUNTERBALANCE.
- [SDR DLL19971566](https://openairdocs.org/sdr/DLL19971566), Aug 9, 1997: BATTERY. DISCHARGED. FWD RT FLT ATT FLASHLIGHT INOP. REPLACED BATTERY, CKS NML.
- [SDR DLL19971471](https://openairdocs.org/sdr/DLL19971471), Jul 27, 1997: CONNECTOR. DIRTY. DURING L/O, FOUND EMERGENCY LIGHTS, TRACK LIGHTS INOP, RT SIDE FROM 34HJ TO 41HJ. T-S PER MM. CLEANED CONNECTOR BEHIND WALL PANEL AT 41HJ, OPS CK OK.
- [SDR DLL19970822](https://openairdocs.org/sdr/DLL19970822), May 2, 1997: BATTERY PACK. DISCHARGED. EXTERIOR EMERGENCY LT AT L1 DOOR INOP. REPLACED BATTERY PACK.
- [SDR DLL19970314](https://openairdocs.org/sdr/DLL19970314), Feb 19, 1997: POWER PACK. WEAK. 1R EMERGENCY LIGHT POWER PACK WEAK, FAILED TO ILLUMINATE. EMERGENCY LIGHTS LONGER THAN 30 SECONDS ON LAYOVER CHECK.
- [SDR DLL16960968](https://openairdocs.org/sdr/DLL16960968), Apr 22, 1996: FITTING. OUT OF POSITION. THE UPPER STABILIZER POWER SERVO FITTINGS ATTACHED TO THE 1860 BULKHEAD WERE ORIGINALLY MISPLACED. AFTER REALIGNMENT, THE FITTINGS' INBOARD ATTACH FASTENERS DID
- [SDR DLL16954356](https://openairdocs.org/sdr/DLL16954356), Nov 12, 1995: CONTROLLER. FAILED. PASSING 17,000 FT, UNABLE TO MAINTAIN CABIN PRESSURE. WENT TO MANUAL WITH AFT OUTFLOW VALVE TO REGAIN CONTROL. REPLACED CABIN PRESSURE CONTROLLER, BITE CK OK.
- [SDR DLL16954336](https://openairdocs.org/sdr/DLL16954336), Nov 11, 1995: SPINNER. LOOSE. NR 1 ENG HIGH VIB STARTED AT 2.5, THEN UP TO 4.0, NORMAL AT IDLE. VIBS FELT IN FLT DECK, NR 1 ENG SHUTDOWN AT FL 310. LANDED WITHOUT FURTHER INCIDENT. FOUND FAI
- [SDR DLL16952460](https://openairdocs.org/sdr/DLL16952460), May 30, 1995: IDG. FAILED. ON CLIMBOUT, NR 1 GEN BREAKER OPEN LIGHT CAME ON, GENERATOR WOULD NOT PARALLEL, LANDED LGW. REPLACED NR 1 IDG, OPERATION NORMAL.
- [SDR DLL16950472](https://openairdocs.org/sdr/DLL16950472), Feb 1, 1995: FRAME SEGMENTS. CRACKED. DURING AIRCRAFT HMV IN ATL, THE FRAME SEGMENTS ON THE AFT PRESSURE DOME BETWEEN S23 AND S44 WERE FOUND WITH CRACK IN THE LOWER FLANGE RADII. THE DAMAGE WAS TRIM
- [SDR DLL16950320](https://openairdocs.org/sdr/DLL16950320), Jan 22, 1995: INTERCOSTAL. CRACKED. AT HMV, FOUND THE INTERCOSTAL CAP CRACKED BETWEEN FS 1778 TO FS 1792, AT LBL 40. REPLACED CAP PER SRM 51-10-05.
- [SDR DLL16950299](https://openairdocs.org/sdr/DLL16950299), Jan 20, 1995: TEAR STRAP. DISBONDED. DURING HMV, FOUND TEAR STRAP AT FS 923 STR 21 AND 22 DISBONDED. REPAIRED PER SRM 53-30-00 PG 807.
- [SDR DLL16950276](https://openairdocs.org/sdr/DLL16950276), Jan 20, 1995: HINGES. RUSTY. AT HMV, HINGES AND BUSHINGS THAT ARE ATTACHED RT MAIN GEAR FITTING FOR UPPER HINGE DOOR WERE FOUND CORRODED. REPAIRED PER SRM 57-14-00 FIG 804.
- [SDR DLL16950275](https://openairdocs.org/sdr/DLL16950275), Jan 20, 1995: FITTING. RUSTY. AT HMV, THE RIGHT MAIN GEAR FITTING AT UPPER LATERAL BRACE LUG WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 57-14-00 FIG 804.
- [SDR DLL16950273](https://openairdocs.org/sdr/DLL16950273), Jan 20, 1995: TRUNION FITTING. RUSTY. AT HMV, THE RIGHT MAIN LANDING GEAR FWD TRUNNION ATTACH FITTING WAS FOUND CORRODED AT THE FWD TRUNNION LUG AND IN AREA OF AFT LUG. REPAIRED PER SRM 57-14-00 FIG
- [SDR DLL16950272](https://openairdocs.org/sdr/DLL16950272), Jan 20, 1995: TEAR STRAP. DELAMINATED. AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DELAMINATED BETWEEN FS 729 AND 846 BETWEEN STRINGERS 32-31. REPAIRED PER SRM 53-31-00 FIG 804.
- [SDR DLL16950271](https://openairdocs.org/sdr/DLL16950271), Jan 20, 1995: SKIN DOUBLER. CORRODED. AT HMV, FOUND INTERIOR FUSELAGE SKIN DOUBLER FOR SKIN SPLICE AT FS 727 AT BL-0 CORRODED. REPAIRED PER SRM 53-31-00 FIG 836.
- [SDR DLL16950270](https://openairdocs.org/sdr/DLL16950270), Jan 20, 1995: SKIN. CORRODED. AT HMV, FOUND CORROSION ON FUSELAGE SKIN UNDER AND AROUND TEAR STAP AT FS 1615 BETWEEN STRINGERS 34-37. REMOVED LIGHT CORRROSION AND CHECKED WITHIN LIMITS PER S
- [SDR DLL16950269](https://openairdocs.org/sdr/DLL16950269), Jan 20, 1995: STRINGER. CORRODED. AT HMV, FOUND STRINGER CORRODED INSIDE MESC FWD OF STA 963 S-34. REPLACED STRINGER SECTION PER SRM 53-13-00 PG 896.
- [SDR DLL16950268](https://openairdocs.org/sdr/DLL16950268), Jan 20, 1995: STRINGER. CORRODED. AT HMV, FOUND FUSELAGE STRINGER 32 INSIDE MESC WITH CORROSION DAMAGE JUST FORWARD OF FS 963. REPLACED DAMAGED SECTION OF STR BETWEEN STA 933-983 PER SRM 53-13-0
- [SDR DLL16950266](https://openairdocs.org/sdr/DLL16950266), Jan 20, 1995: TRUNNION FITTING. RUSTY. HMV, THE RIGHT MAIN LANDING GEAR TRUNNION FITTING WAS FOUND CORRORDED BETWEEN FWD TRUNNION LUGS. REMOVED CORROSION PER SRM 57-14-00 FIG 804.
- [SDR DLL16950265](https://openairdocs.org/sdr/DLL16950265), Jan 20, 1995: TRUNNION FITTING. RUSTY. AT HMV, THE RIGHT MAIN LANDING GEAR TRUNION FITTING BETWEEN LATERAL BRACE LUGS ARE RUSTY. REPAIRED PER SRM 57-14-00 FIG 804.
- [SDR DLL16950323](https://openairdocs.org/sdr/DLL16950323), Jan 18, 1995: SKIN. CORRODED. AT HMV, THE 0.020 INCH BONDED INTERNAL SKIN WAS FOUND CORRODED AT FS 933, BETWEEN STRINGERS 30 AND 31. REPAIRED PER SRM 53-31-00 FIG 836.
- [SDR DLL16950294](https://openairdocs.org/sdr/DLL16950294), Jan 15, 1995: FLOOR SUPPORT. CORRODED. AT HMV, FOUND CABIN FLOOR SUPPORT AT FS 888-901 AT LBL 46.5 CORRODED. REPLACED SUPPORT PER SRM 51-10-05 PG.1.
- [SDR DLL16950133](https://openairdocs.org/sdr/DLL16950133), Jan 13, 1995: TEAR STRAP. LOOSE. DURING HMV, A TEAR STRAP WAS FOUND LOOSE AT FS 1370 BETWEEN STR 33 AND 34. REPAIRED PER SRM 53-31-00 PG 830.
- [SDR DLL16950401](https://openairdocs.org/sdr/DLL16950401), Jan 12, 1995: SKIN. CORROSION. DURING HMV, FOUND CORROSION ON FUSELAGE SKIN BETWEEN FS 729 AND FS 846, STRINGER 332 AND 33. ROUTED OUT INTERNAL BONDED DOUBLER, AND REMOVED CORROSION AS PER SR
- [SDR DLL16950189](https://openairdocs.org/sdr/DLL16950189), Jan 10, 1995: FLOOR BEAM. CRACKED. AT HMV, FOUND HORIZONAL TRUSS MEMBER AT LT FS 1103, CRACKED UPPER TAB. REPAIRED PER SRM 53-21-00 PAGES 853-855.
- [SDR DLL16950103](https://openairdocs.org/sdr/DLL16950103), Jan 10, 1995: DOUBLER. DISBONDED. AT HMV, FOUND FUSELAGE SKIN BONDED DOUBLER AT FS 1625 JUST OUTBOARD OF STRINGER 6 DISBONDED. REPAIRED PER SRM 53-31-00 PG 960.
- [SDR DLL16950131](https://openairdocs.org/sdr/DLL16950131), Jan 9, 1995: RIB. MODIFIED. REF EO 7-59089-3 AT RIGHT WING IWS 319 RIB CAP BOTTOM HOLE ON VERTICAL FLANGE CANNOT BE REAMED OR COLD WORKED DUE TO INTERFERENCE WITH THE RIB CAP. CUT RIB CAP 
- [SDR DLL16950130](https://openairdocs.org/sdr/DLL16950130), Jan 9, 1995: RIB. MODIFIED. REF EO 7-59089-3 IN COMPLIANCE OF VA 31733 AT RIGHT WING IWS293 BOTTOM HOLE ON VERTICAL RIB FLANGE CANNOT BE REAMED OR COLD WORKED DUE TO INTERFERENCE TO RIB CA
- [SDR DLL16950129](https://openairdocs.org/sdr/DLL16950129), Jan 9, 1995: RIB. MODIFIED. REF EO 7-59089 AT LEFT WING IWS 319, BOTTOM HOLE ON VERICAL FLANGE CANNOT BE REAMED OR COLD WORKED DUE TO INTERFERENCE OF RIB CAP. CUT RIB FLANGE FOR TOOL CLEAR
- [SDR DLL16950128](https://openairdocs.org/sdr/DLL16950128), Jan 9, 1995: RIB. MODIFIED. REF EO 7-59089 IN COMPLIANCE OF VA 31733AT LEFT WING RIB CAP AT IWS 293, BOTTOM HOLE ON VERTICAL FLANGE CANNOT BE REAMED OR COLD WORKED, DUE TO INTERFERENCE FRO
- [SDR DLL16950405](https://openairdocs.org/sdr/DLL16950405), Jan 7, 1995: FITTING. CORRODED. DURING HMV, FOUND LT MLG SUPPORT FITTING UPPER FLANGE HOLES 1, 2, 3, 4, 5, AND 6 WERE CORRODED. REAMED HOLES 1 THROUGH 6, AND REMOVED CORROSION PER SRM 57-14-00
- [SDR DLL16950104](https://openairdocs.org/sdr/DLL16950104), Jan 7, 1995: P-DOME. CRACKED. AT HMV, FOUND AFT P-DOME CRACKED AFT OF STRINGER 43 ATTACH FITTING UNDER Z-ANGLE. REPAIRED PER SRM 53-11-00 PG 812, 813.
- [SDR DLL16950399](https://openairdocs.org/sdr/DLL16950399), Jan 6, 1995: FITTING. CORROSION. DURING HMV, LT MLG RETRACT ACTUATOR FITTING HOLES 1, 2, 3, 4, 5, AND 6 FOUND TO HAVE CORROSION. REAMED HOLES 1 THROUGH 6 TO REMOVE CORROSION, AND INSTALLED BUSH
- [SDR DLL16950383](https://openairdocs.org/sdr/DLL16950383), Jan 6, 1995: FLOOR BEAM CAP. CORROSION. DURING OVERHAUL AT STA 1763 THE FLOOR BEAM UPPER FLANGE TOP SURFACE HAD DEEP CORROSION SEVERAL PLACES LB 62 LBL 88. REMOVED AND INSTALLED T-CAP PER SRM 53-21-00
- [SDR DLL16950382](https://openairdocs.org/sdr/DLL16950382), Jan 6, 1995: FLOOR BEAM. CORRODED. DURING OVERHAUL THE CABIN FLOOR BEAM LOWER SURFACE OF UPPER CAP WAS CORRODED AT SEVERAL FASTENER HOLES FS 884 RBL10. MANUFACTURED AND INSTALLED REPAIR PARTS PER
- [SDR DLL16950324](https://openairdocs.org/sdr/DLL16950324), Jan 6, 1995: PRESSURE DECK. CORRODED. AT HMV, FOUND PRESSURE DECK CORRODED AFT OF STIFFENER AT FS 349, AND OUTBOARD OF BL 0 UNDER THE RT FWD LAV. REPAIRED PER SRM 53-11-00 PG 922.
- [SDR DLL16950308](https://openairdocs.org/sdr/DLL16950308), Jan 6, 1995: FLOOR BEAM. CORRODED. DURRING OVERHAUL FOUND, FLOOR BEAM UPPER FLANGE TOP SURFACE CORRODED AT STA 1763, LBL 36 TO LBL 54. ALSO, SEVERAL PLACES ON LWR SURFACE AT SAME CLIP NUT HOLES. 
- [SDR DLL16950307](https://openairdocs.org/sdr/DLL16950307), Jan 6, 1995: FLOOR BEAM. CORRODED. DURING OVERHAUL, CABIN FLOOR BEAM CAP FROM RBL 42.5 TO RBL 74.5 WAS FOUND CORRODED. ALSO, CORROSION ON UNDERSIDE AT FASTENER HOLES FS 901. REMOVED CAP, INSTALLE
- [SDR DLL16950298](https://openairdocs.org/sdr/DLL16950298), Jan 6, 1995: SEAT TRACK. CORRODED. AT HMV, FOUND FS 1318 CENTER INBOARD SEAT TRACK CORRODED AT FS 1318 AVBOVE HYDTRAULIC SERVICE CENTER. REPLACED TRACK PER SRM 53-21-00.
- [SDR DLL16950296](https://openairdocs.org/sdr/DLL16950296), Jan 6, 1995: FLOOR BEAM. CORRODED. AT HMV, FOUND CABIN FLOOR SUPPORT CORRODED ON LOWER SURFACE APP FS 900 AT RBL 30. REPLACED FLOOR SUPPORT PER SRM 51-10-05.

All 94: https://openairdocs.org/deregistered/N763DL-2010-06-04/reports.md

## 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 19920201005619I](https://openairdocs.org/incident/19920201005619I), Feb 1, 1992: Lkheed 10113853 (N763DL), Portland, OR. Fire warning on APU generator when switched from ground power. Fired bottles. Smoke from failed generator.

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