# N759DA: 1981 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: 193Y-1176
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 20, 1991
- Certificate issued: April 28, 2004
- Last registry action: June 26, 2012
- Mode S code: AA3BC4
- 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/N759DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=759DA
- Page: https://openairdocs.org/deregistered/N759DA-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 (66, newest 50)

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

- [SDR DLL19982499](https://openairdocs.org/sdr/DLL19982499), Dec 6, 1998: ENGINE. FLAMED OUT. NR 1 ENG FLAMED OUT AT 39000 FT. SHUTDOWN ENG PER POM. RELIGHT NR 1 PER POM. REPLACED ENGINE DRIVEN FUEL PUMP.
- [SDR DLL19982048](https://openairdocs.org/sdr/DLL19982048), Oct 4, 1998: AIR DISTR. ODOR. A/C DIVERTED COS DUE TO ODOR SIMILAR TO SULPHUR SMELL AT SEATS 22 AND 23 DF. A/C LANDED OVERWEIGHT 38K. CONTRACT MAINT INSPECTED AREA AND PERFORMED OVERWEIGHT L
- [SDR DLL19981675](https://openairdocs.org/sdr/DLL19981675), Aug 14, 1998: FUEL PUMP. FAILED. NR 1 ENG FLAME-OUT AT FL 31.0, OIL FILTER PRESSURE LIGHT NOT ON. N3 ABOVE 20 PERCENT OTHER PARAMETERS WIND MILL NORMAL. USING CROSSFEED NR 3 TO NR 1 AT TIME WIT
- [SDR DLL19981178](https://openairdocs.org/sdr/DLL19981178), Jun 3, 1998: COMPUTER. MALFUNCTIONED. AUTO SPOILERS DEPLOYED AT FL280. REPLACED FCES COMPUTER.
- [SDR DLL19980534](https://openairdocs.org/sdr/DLL19980534), Mar 7, 1998: COMPRESSOR. STALLED. JUST AFTER LEVEL OFF AT FL 370, NR 3 ENGINE HAD A PRESUMED COMPRESSOR STALL AND THE TGT WENT TO 850. ENGINE SHUTDOWN PERPOM. ESTIMATE TIME AT 850 TGT AT 5 SECON
- [SDR DLL16970452](https://openairdocs.org/sdr/DLL16970452), Mar 10, 1997: LIGHT. INOPERATIVE. AFT CABIN EMERGENCY LIGHTS FAIL TEST.
- [SDR DLL16961649](https://openairdocs.org/sdr/DLL16961649), Jul 8, 1996: POWER SUPPLY. FAILED. AFT LT CEILING EMERGENCY LIGHTS FAIL TO TEST. REPLACED AFT LT POWER SUPPLY, LIGHTS CHECK NORMAL.
- [SDR DLL16961040](https://openairdocs.org/sdr/DLL16961040), Apr 30, 1996: CHECK VALVE. FAILED. AFTER TAKEOFF, TOWER INFORMED FUEL WAS VENTING FROM LEFT WING. PASSENGER INFORMED OF FUEL VENTING FROM LEFT WING TIP. CONFIRMED THIS. 2L TANK NOT FEEDING. TURNE
- [SDR DLL16960482](https://openairdocs.org/sdr/DLL16960482), Mar 3, 1996: POWER SUPPLY. INOPERATIVE. TWO EMERGENCY LIGHT POWER SUPPLIES HAVE CHARGE LIGHT INOP. REPLACED POWER SUPPLIES.
- [SDR DLL16953199](https://openairdocs.org/sdr/DLL16953199), Jul 25, 1995: FUEL FLOW REG. FAILED. DURING CRUISE FL 370, NR 1 ENGINE DID NOT RESPOND TO THROTTLE THEN FLAMED OUT, RESTARTED ON SECOND ATTEMPT, THEN FLAMED OUT AGAIN ON SHORT FINAL AT ORY. PER FIM
- [SDR DLL16951932](https://openairdocs.org/sdr/DLL16951932), May 5, 1995: FUEL PUMP. FAILED. DURING CRUISE, HAD NR 1 ENGINE FUEL PRESSURE LIGHT ILLUMINATED, THEN ENGINE FLAMED-OUT, ALL AIR STARTS WERE UNSUCCESSFUL, DIVERTED TO KEF. REPLACED HP FUEL PUMP
- [SDR DLL16951034](https://openairdocs.org/sdr/DLL16951034), Mar 3, 1995: STRAP. CORRODED. AT HMV, FOUND CENTER STRAP TO BE CORRODED. INTERNAL CENTER STRAP AT STA 910 STR 33. REPAIRED PER SRM 53-31-00 FIG 825.
- [SDR DLL16951404](https://openairdocs.org/sdr/DLL16951404), Mar 1, 1995: SPAR CAP. CRACKED. DURING HMV COMPLYING WITH AD 93-17-10 AND 94-05-01, CRACKS WERE FOUND IN THE RIGHT WING REAR SPAR UPPER CAP FASTENER HOLES AT IWS 293.58 AND IWS 346.109. THE HO
- [SDR DLL16950948](https://openairdocs.org/sdr/DLL16950948), Mar 1, 1995: STRAP. DISBONDED. AT HVM, FOUND TEAR STRAP DISBONDED AT FS 930 BETWEEN STR 31 AND 32. REPAIRED PER SRM 53-31-00 FIG 804.
- [SDR DLL16950928](https://openairdocs.org/sdr/DLL16950928), Mar 1, 1995: TEAR STRAP. DISBONDED. AT HMV,FOUND TEAR STRAP DISBONDED, STA 930 BETWEEN STRINGER 31 AND 32. PEELED TEAR STRAP BACK, NO CORROSION FOUND. INSTALLED REPAIR PER SRM 53-31-00 FIG 804.
- [SDR DLL16951031](https://openairdocs.org/sdr/DLL16951031), Feb 28, 1995: SKIN. CORRODED. AT HMV, FOUND FUSELAGE SKIN CORRODED UNDER TEARSTRAP BETWEEN STA 1605 AND 1625 AT STRINGER 29. REPAIRED PER SRM 53-31-00 PG 965.
- [SDR DLL16950805](https://openairdocs.org/sdr/DLL16950805), Feb 24, 1995: FAIL SAFE STRAP. DELAMINATED. AT HMV, FOUND FUSELAGE SKIN FAIL SAFE TEAR STRAP DELAMINATED AT FS 709-729 ABOVE STRINGER 40. REPAIRED PER SRM 53-31-00, PG 830.
- [SDR DLL16950802](https://openairdocs.org/sdr/DLL16950802), Feb 24, 1995: FAIL SAFE STRAP. DELAMINATED. AT HMV, FOUND C-1 FUSEALGE SKIN FAIL SAFE TEAR STRAP DELAMINATED AT FS 889-869 BETWEEN STRINGERS 37 AND 30. REPAIRED PER SRM 53-31-00.
- [SDR DLL16950801](https://openairdocs.org/sdr/DLL16950801), Feb 24, 1995: STRAP. CORRODED. AT HMV, C-2 STRAP COMMON TO STRINGER 33 IS CORRODED ON LEFT SIDE OF THE STRINGER, JUST AFT OF TEAR STRAP AT FS 1695. REPAIRED PER SRM 53-31-00.
- [SDR DLL16950800](https://openairdocs.org/sdr/DLL16950800), Feb 24, 1995: FAIL SAFE STRAP. DELAMINATED. AT HMV, FOUND FUSELAGE SKIN FAIL SAFE TEAR STRAP DELAMINATED IN FWD CARGO AREA, FS 886-901 AT STRINGER 23, 30, AND 34. REPAIRED PER SRM 53-31-00 PG 830.
- [SDR DLL16950799](https://openairdocs.org/sdr/DLL16950799), Feb 24, 1995: LONGERON. CRACKED. AT HMV, FOUND LONGERON AT FS 983 BETWEEN STRINGERS 45 AND 46 CRACKED. REPLACED LONGERON.
- [SDR DLL16950798](https://openairdocs.org/sdr/DLL16950798), Feb 24, 1995: SEAT TRACK. CORRODED. AT HMV, FOUND CABIN SEAT TRACK AT FS 1705 AND 1725, 4TH FROM LEFT SIDE, CORRODED. REPLACED TRACK, PER SRM 53-21-00.
- [SDR DLL16950797](https://openairdocs.org/sdr/DLL16950797), Feb 24, 1995: SKIN. DENTED. AT HMV, FOUND FUSELAGE SKIN DENTED AT FS 220 BETWEEN STRINGERS 3 AND 4. REPAIRED PER SRM 53-31-0.
- [SDR DLL16950796](https://openairdocs.org/sdr/DLL16950796), Feb 24, 1995: RIB CAPS. CUT. AT HMV, RIB CAPS AT IWS 293.38 AND 319.83 WERE CUT TO FACILITATE REMOVAL AND COLD WORK OF FASTENERS IN REAR SPAR REWORK. REF EO 7-59089-3. REPAIRED RIBS PER SRM
- [SDR DLL16950950](https://openairdocs.org/sdr/DLL16950950), Feb 23, 1995: FLOORBEAM. CORRODED. FLOORBEAM STA 1823 TO 1842 LBL 71 LBL 44 CORRODED AT FLOOR PANEL ATTACH HOLES, TWO PLACES. DAMAGE FOUND AT HMV. REPAIRED PER SRM 53-21-00 PAGES 866 TO 868.
- [SDR DLL16950803](https://openairdocs.org/sdr/DLL16950803), Feb 22, 1995: STRINGER. CORRODED. AT OVERHAUL STRINGER 32 AT LOWER SIDE OF SKIN ATTACH FLANGE (FS 953) WAS FOUND CORRODED. INSTALLED NEW SECTION OF STRINGER WITH SPLICE REPAIR PER SRM 53-13-00, 
- [SDR DLL16950838](https://openairdocs.org/sdr/DLL16950838), Feb 21, 1995: SKIN. CORRODED. DURING HMV, FOUND LOWER FUSELAGE SKIN CORRODED AT FS 629-649 BETWEEN STRINGER 32 AND 34. CLEANED CORROSION AND INSTALLED REPAIR PER SRM 53-31-00 FIG 825.
- [SDR DLL16950837](https://openairdocs.org/sdr/DLL16950837), Feb 21, 1995: FLOORBEAM. CORRODED. DURING HMV, FOUND CORROSION ON CABIN FLOORBEAM FS 886 RBL 30. REPAIRED PER SRM 53-21-00 PG 866-868.
- [SDR DLL16950831](https://openairdocs.org/sdr/DLL16950831), Feb 21, 1995: SEAT TRACK. CORRODED. DURING HMV, FOUND CABIN SEAT ATTACH TRACK CORRODED AT FS 1665 TO 1725 AT RBL 42. REPLACED TRACK PER SRM 53-21-00 FIG 820.
- [SDR DLL16950927](https://openairdocs.org/sdr/DLL16950927), Feb 19, 1995: ACT FITTING. DAMAGED. AT HMV, FOUND HOLES DAMAGED IN LMLG ACTUATOR FITTING. DRILLED HOLES 17 THROUGH 20 TO .628 TO REMOVE DAMAGE. CORROSION REMOVED. ALL REMAINING WORK DONE ON JPC 03
- [SDR DLL16950926](https://openairdocs.org/sdr/DLL16950926), Feb 19, 1995: ACT FITTING. CORRODED. AT HMV, FOUND HOLES CORRODED HOLES 1, 2, 4, 6, IN LMLG ACTUATOR FITTING CORRODED. REF TASK C-32-730-01. REAMED HOLES 1, 2, 4, 5 AND 6 TP .688. REMOVED DAMAGE AN
- [SDR DLL16950735](https://openairdocs.org/sdr/DLL16950735), Feb 17, 1995: STRAP. DELAMINATED. C-1 B/B FAILSAFE STRAP DELAMINATED, F/S 749-769, STRINGERS 30 AND 34. ACTUAL LOCATION F/S 860, STRINGERS 30 AND 34. DAMAGE FOUND AT HMV, REPAIRED PER SRM 53-31-
- [SDR DLL16950669](https://openairdocs.org/sdr/DLL16950669), Feb 17, 1995: TEAR STRAP. DISBONDED. FS 860 TEAR STRAP DISBONDED BETWEEN STR 27-29 AND STR 35-36. DAMAGE FOUND AT HMV, REPAIRED PER SRM 53-31-00 PG 830.
- [SDR DLL16950924](https://openairdocs.org/sdr/DLL16950924), Feb 15, 1995: STATIC WICK. FAILED CHECK. AT HMV, FOUND STATIC WICK BASES 34 AND 43 FAILED MEG CHECK. REPLACED STATIC WICK BASES 34 AND 43. REQ PANELS INSTALLED ON AC STATIC ARRESTER BASES.
- [SDR DLL16951032](https://openairdocs.org/sdr/DLL16951032), Feb 14, 1995: DECK. CORRODED. AT HMV, FOUND CORROSION DAMAGE ON PRESSURE DECK AT FS 359 LEFT OF FORWARD LAV 18 INCHES. REPAIRED PER SRM 53-11-00 FIG 840.
- [SDR DLL16951030](https://openairdocs.org/sdr/DLL16951030), Feb 14, 1995: BLKHD FRAME. CORRODED. AT HMV, FOUND FRAME CORRODED ON P-DOME LOWER INBOARD SIDE JUST AFT OF WHERE STRINGER 25 ENDS. REPAIRED PER SRM 53-11-00 FIG 809.
- [SDR DLL16951029](https://openairdocs.org/sdr/DLL16951029), Feb 14, 1995: BLKHD FRAME. CORRODED. AT HMV, FOUND P-DOME FRAME CORRODED AT LOWER END OVER A 2FT SECTION. AT THE FORWARD SIDE OF P-DOME LEFT SIDE JUST AFT OF AFT CARGO AREA STRINGER 41. REPAIRED PE
- [SDR DLL16950836](https://openairdocs.org/sdr/DLL16950836), Feb 14, 1995: FLOORBEAM. CORRODED. DURING HMV, FOUND CABIN FLOORBEAM AT FS 923 CORRODED AT LBL 31. REPAIRED PER SRM 53-21-00 PG 866-868,_AND FLOORBEAM AT FS 901 CORRODED AT LBL 42 AND 47. REPAIRE
- [SDR DLL16950835](https://openairdocs.org/sdr/DLL16950835), Feb 14, 1995: FLOORBEAM. CORRODED. DURING HMV, FOUND CABIN FLOOR SUPPORT BEAM AT FS 281 WITH CORROSION DAMAGE AT LBL 74 TO RBL 74. REPAIRED PER SRM 53-21-00 PG 823-824.
- [SDR DLL16950811](https://openairdocs.org/sdr/DLL16950811), Feb 14, 1995: TEARSTRIP. DISBONDED. DURING OVERHAUL, FOUND TEARSTRIP DISBONDED AT FS 1735 STR 29-31. REPAIR PER SRM 53-31-00 FIG 804.
- [SDR DLL16950810](https://openairdocs.org/sdr/DLL16950810), Feb 14, 1995: TEARSTRIP. DISBONDED. DURING OVERHAUL, FOUND TEARSTRIP DISBONDED AT FS 1695 STR 30-29, FS 1635 STR 38-39, FS 1635 STR 40-41.
- [SDR DLL16950808](https://openairdocs.org/sdr/DLL16950808), Feb 14, 1995: FLOORBEAM. CORRODED. DURING OVERHAUL, FOUND FLOORBEAM CORRODED AT STA 1725, LBL 34-58. REPAIRED PER SRM 53-21-00.
- [SDR DLL16950736](https://openairdocs.org/sdr/DLL16950736), Feb 14, 1995: STRAP. DISBONDED. TEAR STRAP DISBONDED - C-2 F/S 1735 BETWEEN STR 34 AND 35. REPAIRED PER SRM 53-31-00 PAGE 830. DAMAGE FOUND AT HMV.
- [SDR DLL16950949](https://openairdocs.org/sdr/DLL16950949), Feb 13, 1995: STRAP. DISBONDED. AT HMV, FOUND TEAR STRAP DISBONDED AT FS 1605 AND 1625 BETWEEN STRINGER 29 AND 30. REPAIRED PER SRM 53-31-00 FIG 804.
- [SDR DLL16950923](https://openairdocs.org/sdr/DLL16950923), Feb 13, 1995: TEAR STRAP. DISBONDED. AT HMV, FOUND TEAR STRAP DISBONDED C2 BIN BETWEEN 1605 TO 1625, STRINGER 29 AND 30. LIFTED TEAR STRAP AND REMOVED CORROSION, TREATED AND PAINTED AREA. FABRICATE
- [SDR DLL16950840](https://openairdocs.org/sdr/DLL16950840), Feb 13, 1995: ANGLE. CRACKED. DURING HMV, FOUND STIFFENER ANGLE CRACKED FROM EDGE TO RADIUS, APPROX 2 INCHES INSIDE ACCESS PANEL 311UL OF NR 2 ENGINE INTAKE (LEFT SIDE OF S DUCT LOOKING UP A
- [SDR DLL16950839](https://openairdocs.org/sdr/DLL16950839), Feb 13, 1995: ANGLE. CRACKED. DURING HMV, FOUND STIFFENER ANGLE CRACKED FROM EDGE TO RADIUS 2 INCHES. CRACK LOCATED INSIDE ACCESS PANEL 311UR, AT NR 2 ENGINE INTAKE. REPAIRED PER SRM 54-12-0
- [SDR DLL16950834](https://openairdocs.org/sdr/DLL16950834), Feb 13, 1995: FAILSAFE STRAP. DISBONDED. DURING HMV, FOUND FUSELAGE SKIN FAILSAFE TEARSTRAP DISBONDED AT FS 1443 BETWEEN STRINGESR 30 AND 31, AND FS 1535 BETWEEN STRINGERS 33-34. REPAIRED PER SRM 53-31
- [SDR DLL16950833](https://openairdocs.org/sdr/DLL16950833), Feb 13, 1995: FAILSAFE STRAP. DISBONDED. DURING HMV, FOUND FUSELAGE SKIN FAILSAFE TEARSTRAP DISBONDED AT FS 1545 TO FS 565 BETWEEN STRINGERS 30 TO 37. REPAIRED PER SRM 53-31-00 PG 830.
- [SDR DLL16950809](https://openairdocs.org/sdr/DLL16950809), Feb 13, 1995: TEARSTRIP. DISBONDED. DURING OVERHAUL, FOUND TEARSTRIP DISBONDED AT FS 1605-1625 STR 32-33, FS 1605-1625 STR 33-34, FS 809-829 STR 31.

All 66: https://openairdocs.org/deregistered/N759DA-2013-09-10/reports.md

## 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 19980125003079I](https://openairdocs.org/incident/19980125003079I), Jan 25, 1998: N759DA, Salt Lake City, UT, Minor damage. Narrative: aircraft was parked at gate, Salt Lake City int'l. baggage cart hit aircraft, causing minor damage to aircraft at cargo door opening. Repair made by…
- [Incident 19920217008499I](https://openairdocs.org/incident/19920217008499I), Feb 17, 1992: Lkheed 10113853 (N759DA), Portland, OR, Minor damage. NR2 engine core cowling separated from aircraft on landing. Cowling recovered by CFR.
- [Incident 19911002055289I](https://openairdocs.org/incident/19911002055289I), Oct 2, 1991: Lkheed 10113853 (N759DA), Portland, OR. Compressor stalls on NR2 engine. High oil temperature. Low oil pressure. Dumped fuel. Landed safely on return.

## Other aircraft with N759DA

- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N759DA-undated): Cessna 182Q, S/N 18265900. Triennial form not returned

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