# N719DA: 1976 Lockheed L-1011-385-1, registration cancelled 2013-02-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 20, 2013 - Status when cancelled: Sale reported, canceled - Airframe: [Lockheed L-1011-385-1](https://openairdocs.org/model/lockheed-l-1011-385-1) (registry code 5265010) - 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: 193C-1135 - Year built: 1976 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 30, 1976 - Last registry action: July 20, 2004 - Mode S code: A99DC8 - Location: [Kansas City, KS](https://openairdocs.org/faa-place/KS/Kansas%20City) - Owner type: Individual - Owner's area on the map: 39.1483° N, 94.6051° W: Placed by OpenAirDocs at the center of ZIP code 66115, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N719DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=719DA - Page: https://openairdocs.org/deregistered/N719DA-2013-02-20 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-1011-385-1: https://openairdocs.org/model/lockheed-l-1011-385-1.md ## Service difficulty reports (119, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DLL10982572](https://openairdocs.org/sdr/DLL10982572), Dec 16, 1998: OUTLET. SHORTED. DURING TAXI OUT, FWD GALLEY RT SERVICE OUTLET SHORTED CAUSING SPARKS AND SMOKE IN THE CABIN. A/C RETURNED TO THE GATE. FOUND FWD GALLEY COFFEE POT LEAKING ON OU - [SDR DLL10980554](https://openairdocs.org/sdr/DLL10980554), Mar 6, 1998: SKIN. CORRODED. FUSELAGE/SKIN, FS 1645-1665, STRG 38-39. REPAIR FOR CORROSION CUTOUT. THE FUSELAGE SKIN WAS FOUND CORRODED BETWEEN FS 1645 AND 1665 AND BETWEEN STRINGERS 38 AND - [SDR DLL10980549](https://openairdocs.org/sdr/DLL10980549), Mar 6, 1998: SKIN. CORRODED. THE SKIN AT FS 328 AND LBL 22 WAS FOUND CORRODED NEAR THE CORNER OF THE NOSE LANDING GEAR DOOR CUTOUT. THE EXISTING AD MANDATED MOD DOUBLERS WERE ALSO FOUND COR - [SDR DLL10980167](https://openairdocs.org/sdr/DLL10980167), Jan 20, 1998: SEQUENCE VALVE. FAILED. AFTER T/O, THE DOOR RED AND INTRANSIT LIGHTS DID NOT GO OUT. LANDING GEAR LOWERED PER PROCEDURES, RIGHT GEAR GREEN LIGHT DID NOT COME ON. MANUALLY EXTENDED GEAR - [SDR DLL10972115](https://openairdocs.org/sdr/DLL10972115), Oct 14, 1997: BULKHEAD PANEL. CRACKED. THE FUSELAGE 1212 BULKHEAD PANEL WAS FOUND WITH A TYPICAL VERTICAL CRACK AS ADDRESSED BY LAC S/B 093-53-277. THE CRACK IN THIS CASE IS LOCATED AT RBL 6 AND IS A - [SDR DLL10970776](https://openairdocs.org/sdr/DLL10970776), Apr 26, 1997: BATTERY PACK. DISCHARGED. EMERGENCY AILSE LIGHT INOP AT 16B, 22B, 27H, 21H AND 16H. REPLACED EMERGENCY POWER PACK AT CENTER GALLEY. EMERGENCY LIGHTS INOP AT RT GALLEY AND DIM IN LOWER GA - [SDR DLL10970368](https://openairdocs.org/sdr/DLL10970368), Feb 27, 1997: SOCKETS. SHORTED. EMERGENCY TRACK FLOOR LIGHTING INOP FROM RT AISLE SEAT ROW 20JH THROUGH 26JH. FOUND BULB SOCKET AT SEAT 23JH SHORTED. REPLACED SOCKET, OPS CHECKS NORMAL, DAL P/ - [SDR DLL10970300](https://openairdocs.org/sdr/DLL10970300), Jan 31, 1997: STRAP. DAMAGED. DURING ACCOMPLISHMENT OF SI 7-69959-12AD, THE AFT WEB SPLICE STRAPS AT RBL 42.5 AND LBL 42.5 WERE CUT AT THE LOWER END TO FACILITATE INSTALLATION OF THE LOWER C - [SDR DLL10962547](https://openairdocs.org/sdr/DLL10962547), Nov 19, 1996: ENGINE. MALFUNCTIONED. NR 2 ENG EPR GRADUALLY ROLLED BACK ON CLIMBOUT. OTHER ENGINE PARAMETERS FOLLOWED, FUEL AMP NO HELP. - [SDR DLL10962431](https://openairdocs.org/sdr/DLL10962431), Nov 1, 1996: FUEL FLOW REG. MALFUNCTIONED. ENG NR 2 FLAMED OUT SHORTLY AFTER TAXIING CLEAR OF RUNWAY AFTER LANDING, WAS VERY HARD TO START. REPLACED FFR ON NR 2 ENG, ENG STARTS NORMALLY. PERFORMED CKS PE - [SDR DLL10960740](https://openairdocs.org/sdr/DLL10960740), Apr 2, 1996: BATTERY PACK. DISCHARGED. EMERGENCY EXIT LIGHT AT R-4 DOOR IS INOP. REPLACED R4 DOOR BATTERY PACK, CHECK GOOD PER OPN. - [SDR DLL10960358](https://openairdocs.org/sdr/DLL10960358), Feb 17, 1996: TIRE CAP. MISSING. AT ROTATION, LOUD ENGINE VIBRATION AUDIBLE. CHECKED ENGINE VIBRATION LIGHT ON PILOT ANN ON CHANNELS A AND B, SHOWED 5.0 UNITS STEADY AND AT LEVEL OFF THROTTLE B - [SDR DLL10960395](https://openairdocs.org/sdr/DLL10960395), Jan 27, 1996: BLKHD ANGLE. CRACKED. THE 1641601-102 ANGLE INSTALLED AS PART OF THE FS 1363 BULKHEAD MODIFICATION PER DAL EO 7-47702-3AD WAS FOUND CRACKED AT A FASTENER HOLE DURING ROUTINE LAYOVER - [SDR DLL10954781](https://openairdocs.org/sdr/DLL10954781), Dec 27, 1995: CAP. BROKEN. UPON LOWERING LT GEAR LOST C-SYSTEM FLUID TO ONE-QUARTER. FOUND LEFT LANDING GEAR PHASE CONTROL MODULE CAP BROKEN. REPLACED CAP, SERVICED SYSTEM OPERATION NORMA - [SDR DLL10953239](https://openairdocs.org/sdr/DLL10953239), Jul 7, 1995: SKIN. CORROSION. DURING INSPECTION OF THE LOWER BELLY SKIN AREA, THE LOWER FUSELAGE SKIN FROM FS 1363 TO 1453 WAS FOUND TO HAVE AREAS OF SEVERE CORROSION. ACCOMPLISHED REPAIRS P - [SDR DLL10952002](https://openairdocs.org/sdr/DLL10952002), May 9, 1995: STIFFENER. CRACKED. INTERNAL STIFFENERS CRACKED RT HORIZ LE PANEL 341C, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803. - [SDR DLL10951999](https://openairdocs.org/sdr/DLL10951999), May 9, 1995: STIFFENER. CRACKED. INTERNAL STIFFENERS CRACKED LT HORIZ LE PANEL 331F, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803. - [SDR DLL10951976](https://openairdocs.org/sdr/DLL10951976), May 9, 1995: STIFFENER. CRACKED. INTERNAL STIFFENER CRACKED RT HORIZ LE PANEL 341D, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803. - [SDR DLL10951975](https://openairdocs.org/sdr/DLL10951975), May 9, 1995: STIFFENER. CRACKED. INTERNAL STIFFENER CRACKED LT HORIZ LE PANEL 331E, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803. - [SDR DLL10951974](https://openairdocs.org/sdr/DLL10951974), May 9, 1995: STIFFENER. CRACKED. INTERNAL STIFFENER CRACKED RT HORIZ LE PANEL 341E, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803. - [SDR DLL10951972](https://openairdocs.org/sdr/DLL10951972), May 9, 1995: TEAR STRAP. CORRODED. SKIN BULGED/RIVETS SHEARED FS 476 STRGR 27 TO 26. FOUND DURING INITAIL INSP AT HMV. CLEANED CORROSION PER 53-31-00 FIG 801 REPAIRED TEAR STRAP PER 53-31-00 FIG - [SDR DLL10951931](https://openairdocs.org/sdr/DLL10951931), May 6, 1995: FLOOR SUPPORT. CORRODED. C-1 B/B FLOOR SUPPORT CORRODED AT LBL3 FS 689. REPAIRED PER SRM 53-23-04. FOUND AT HMV. - [SDR DLL10951831](https://openairdocs.org/sdr/DLL10951831), May 1, 1995: FITTING. CORRODED. RT MLG FITTING CORRODED AT RETRACT ACTUATOR FTG HOLE 17. FOUND DURING HMV/CORROSION CK. REPAIRED PER SRM 57-14-00. - [SDR DLL10951830](https://openairdocs.org/sdr/DLL10951830), May 1, 1995: FITTING. CORRODED. RT MLG FITTING CORRODED AT RETRACT ACTUATOR ATTACHMENT HOLES 1 TO 6. FOUND AT HVM, REPAIRED PER SRM 57-14-00. - [SDR DLL10951828](https://openairdocs.org/sdr/DLL10951828), May 1, 1995: FLOORBEAM. CORRODED. STA 1505 FLOORBEAM CORRODED LBL 4 ON T-CAP. FOUND AT HMV. REPAIRED PER SRM 53-23-00 FIG 801. - [SDR DLL10951821](https://openairdocs.org/sdr/DLL10951821), Apr 30, 1995: STIFFENER. CRACKED. INTERNAL STIFFENERS CRACKED RT HORIZ LE PANEL 341A. FOUND DURING HMV INITIAL. REAIRED PER SRM 55-12-00 FIG 803. - [SDR DLL10951819](https://openairdocs.org/sdr/DLL10951819), Apr 30, 1995: TEAR STRAP. DISBONDED. TEAR STRAP LIFTING AFT WASTE COMPARTMENT FS 1792 AND 1809 FROM STRGR 30 TO 31, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 807. - [SDR DLL10951818](https://openairdocs.org/sdr/DLL10951818), Apr 30, 1995: FITTING. CORRODED. LT MLG RETRACT FTG CORRODED ON FACES OF FTG COMMON TO HOLES 17 THROUGH 20 AND HOLES HAVE CORROSION IN THEM. FOUND DURING HMV. REPAIRED PER SRM 57-14-00. - [SDR DLL10951817](https://openairdocs.org/sdr/DLL10951817), Apr 30, 1995: WEB. CORRODED. WEB CORRODED AND PITTED INTERIOR OF CTR WING AT FS 1103, BETWEEN RBL 22 AND RBL 42 WITHIN 4 INCHES OF CTR BOX UPPER SKIN FWD SIDE 4 AREAS OF CORROSION AT FASTEN - [SDR DLL10951816](https://openairdocs.org/sdr/DLL10951816), Apr 30, 1995: FITTING. CORRODED. RT MLG FTG CORRODED UPPER SURFACE OF LWR ATTACHMENT FOR ACTUATOR FTG. FOUND AT HMV, REPAIRED PER SRM 57-14-00. - [SDR DLL10951815](https://openairdocs.org/sdr/DLL10951815), Apr 30, 1995: FITTING. CORRODED. RT MLG FITTING IS CORRODED ON VERTICAL WALL AREA EXPOSED BY REMOVAL OF ACTUATOR FTG. FOUND AT HMV, REPAIRED PER SRM 57-14-00. - [SDR DLL10951797](https://openairdocs.org/sdr/DLL10951797), Apr 26, 1995: TRUNNION. CORROSION. RT MLG TRUNNION FWD/AFT LUG FACE HAS LIGHT CORROSION. SPOT FACED 019 DEEP ON FWD FACE AFT LUG OF FWD. TRUNNION TO REMOVE CORROSION. REWORK C/W ON R/C 1488 TO 14 - [SDR DLL10951796](https://openairdocs.org/sdr/DLL10951796), Apr 26, 1995: TRUNNION. CORROSION. RT LOCAL BLEND 010 TO REMOVE CORROSION. REWORKED SRM LIMITS 57-14-00, C/W ON RC 1488 TO 1489. - [SDR DLL10951795](https://openairdocs.org/sdr/DLL10951795), Apr 26, 1995: FITTING. CORROSION. LT MLG AFT TRUNNION FITTING A HAS CORROSION ON AFT FACE OF FWD LUG. BURNISHED FACE TO REMOVE LIGHT CORROSION. - [SDR DLL10951914](https://openairdocs.org/sdr/DLL10951914), Apr 25, 1995: FITTING. CORRODED. LT GEAR FITTING FWD TRUNNION AFT BORE HAS CORROSION ON FWD FACE AND CORROSION AND PITTING IN BORE. BORED LUG TO 4.229 TO REMOVE CORROSION. BLENDED AREAS TO REMO - [SDR DLL10951912](https://openairdocs.org/sdr/DLL10951912), Apr 25, 1995: TEAR STRAP. CORRODED. AT HMV, LWR GALLEY TEAR STRAP DISBONDED FS 935 BETWEEN STR 40 TO 45, ON FUSELAGE SKIN. REPAIRED PER SRM 53-31-00 FIG 805. - [SDR DLL10951835](https://openairdocs.org/sdr/DLL10951835), Apr 25, 1995: SPLICE. CRACKED. BLKD SPLICE TEE CRACKED LT FS 1705 WL 405 VIEWED THROUGH PANEL 313A-1 AND 311UL. - [SDR DLL10951808](https://openairdocs.org/sdr/DLL10951808), Apr 25, 1995: TRUNNION FITTING. CORROSION. LEFT GEAR FITTING AFT TRUNNION AFT BORE HAS CORROSION FWD FACE. CORR SPOT FACED .004 DEEP AND LOCALLY BLENDED AREA, REMOVED CORROSION PER SRM 57-14-00. ALL REMA - [SDR DLL10951791](https://openairdocs.org/sdr/DLL10951791), Apr 25, 1995: FITTING. CORRODED. LT GEAR FITTING AFT TRUNNION FWD BORE PITTED IN BORE. BORED LUG TO 4.7095 INCHES TO REMOVE CORROSION. - [SDR DLL10951790](https://openairdocs.org/sdr/DLL10951790), Apr 25, 1995: FITTING. CORROSION. LT GEAR FITTING FWD TRUNNION FWD BORE HAS CORROSION ON FWD/AFT SIDES AND CORROSION AND PITTING IN BORE. BORED LUG TO 4.218 0 TO REMOVE CORROSION. BURNISHED FACE - [SDR DLL10951711](https://openairdocs.org/sdr/DLL10951711), Apr 25, 1995: FAILSAFE STRAP. DISBONDED. FAILSAFE STRAP DISBONDED FS 846 BETWEEN STRINGER 31 TO 30. FOUND DURING CORROSION INSP AT HMV TASK NR C-53-130-05. CLEANED CORROSION PER SRM 53-31-00 FIG 801, I - [SDR DLL10951710](https://openairdocs.org/sdr/DLL10951710), Apr 25, 1995: TEAR STRAP. DISBONDED. TEAR STRAP DISBONDED FS 1393 BETWEEN STRGR 34 TO 35. REPAIRED DURING ACCOMPLISHMENT OF LOWER SKIN REPLACEMENT FS 1363 TO FS 1453, BETWEEN STRINGERS 31 AND 36, P - [SDR DLL10951704](https://openairdocs.org/sdr/DLL10951704), Apr 25, 1995: TEAR STRAP. DISBONDED. C1 B/B TEAR STRAP DISBONDED AT FS 519 BETWEEN STGRS 26 AND 27. REPAIRED PER SRM 53-30-00. FOUND AT HMV. - [SDR DLL10951689](https://openairdocs.org/sdr/DLL10951689), Apr 25, 1995: TEAR STRAP. DISBONDED. TEAR STRAP DISBONDED IN C1 FS 579 STRINGER 26, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 830. - [SDR DLL10951688](https://openairdocs.org/sdr/DLL10951688), Apr 25, 1995: TEAR STRAP. DISBONDED. FAIL SAFE STRAP DISBONDED AFT OF FS 703, BETWEEN STRINGER 37 TO 38. FOUND DURING CORROSION INSP AT HMV. REPAIRED PER SRM 53-31-00 FIG 804. - [SDR DLL10951687](https://openairdocs.org/sdr/DLL10951687), Apr 25, 1995: TEAR STRAP. DISBONDED. TEAR STRAP DISBONDED AT FS 559 STRINGER 25 TO 27, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 806-807. - [SDR DLL10951686](https://openairdocs.org/sdr/DLL10951686), Apr 25, 1995: ANGLE. CORRODED. AFT P-DOME CIRCUMFERENTIAL ATTACH ANGLE IS CORRODED AT STRINGER 27 AND 32. FOUND AT HMV, REPAIRED PER SRM 53-12-00 FIG 801 AND SRM 53-11-00 FIG 848. - [SDR DLL10951834](https://openairdocs.org/sdr/DLL10951834), Apr 21, 1995: BULKHEAD. CRACKED. LT MLG WHEEL WELL AFT BULKHEAD HAS 5 CRACK BETWEEN STIFFENERS (LWR MID AREA). - [SDR DLL10951657](https://openairdocs.org/sdr/DLL10951657), Apr 21, 1995: TEAR STRAP. DISBONDED. TEAR STRAP IS DISBONDED ABOVE STR 25 TO 24 AT FS 599. REPAIRED PER SRM 53-30-00. FOUND AT HMV. - [SDR DLL10951678](https://openairdocs.org/sdr/DLL10951678), Apr 20, 1995: FORMER. CRACKED. FORMER CRACKED AT STA 1103 LT SIDE W/L 198, JUST UNDER FLOOR LEVEL. REPAIRED PER SRM 53-12-00 FIG 816. FOUND AT HMV. All 119: https://openairdocs.org/deregistered/N719DA-2013-02-20/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB LAX92IA307](https://openairdocs.org/ntsb/LAX92IA307), Jul 18, 1992: Lockheed L-1011-385-1 (N719DA), Los Angeles, CA, incident, no damage. Probable cause: A FAILURE OF GROUND PERSONNEL TO ENSURE PROPER CLEARANCE BETWEEN A TAXIING AIRPLANE AND AN ADJACENT PARKED AIRPLANE. CONTRIBUTING TO THE ACCIDENT WAS A FAILURE OF GROUND PERSONNEL TO PROPERLY… ## FAA accident and incident reports (6) 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 19960623022489I](https://openairdocs.org/incident/19960623022489I), Jun 23, 1996: Lkheed 10113851 (N719DA), Salt Lake City, UT, Minor damage. Narrative: during takeoff the cap from number three (3) forward tire came off. The cap damaged the upper wing panel and wiring in the flap well. Maintenance… - [Incident 19960217006909I](https://openairdocs.org/incident/19960217006909I), Feb 17, 1996: Lkheed 10113851 (N719DA), Salt Lake City, UT, Minor damage. Narrative: on departure number three (3) aft tire blew. A large piece of the tire was ingested into number three engine requiring the crew to shut down the… - [Incident 19960118002829I](https://openairdocs.org/incident/19960118002829I), Jan 18, 1996: Lkheed 10113851 (N719DA), Salt Lake City, UT. Narrative: delta flight #152, L-1011, departed slc on 01-18-96, reported engine vibration. CFR equipment called out at 1840Z. Delta flight #152 landed slc… - [Incident 19950113004609I](https://openairdocs.org/incident/19950113004609I), Jan 13, 1995: Lkheed 10113851 (N719DA), Portland, OR, Minor damage. Narrative: on January 13, 1995, delta airlines flight 558 ingested a bird into number 3 engine shortly after take-off from Portland International Airport.… - [Incident 19920717032349I](https://openairdocs.org/incident/19920717032349I), Jul 17, 1992: Lkheed 10113851 (N719DA), Los Angeles, CA, Minor damage. Pilot struck a parked aircraft with left wing while taxiing to gate. - [Incident 19790810030439I](https://openairdocs.org/incident/19790810030439I), Aug 10, 1979: Lkheed 10113851 (N719DA), Houston, TX. Missed approach when leading edge flaps stopped extension at 7 degrees. Unable to duplicate problem after landing. --- 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.