# N714DA: 1974 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-1090 - Year built: 1974 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 25, 1974 - Last registry action: July 20, 2004 - Mode S code: A98B35 - 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/N714DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=714DA - Page: https://openairdocs.org/deregistered/N714DA-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 (41) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DLL10981924](https://openairdocs.org/sdr/DLL10981924), Sep 15, 1998: POWER SUPPLY. INOPERATIVE. F/C EMERGENCY TRACK LIGHTING INOP. REPLACED POWER SUPPLY, OPS CHECK NORMAL. - [SDR DLL10981441](https://openairdocs.org/sdr/DLL10981441), Jul 10, 1998: BULB. FAILED. EXTERIOR EMERGENCY LIGHT AT L3 DOOR INOP. RELAMPED SAME, CHECKS GOOD. - [SDR DLL10981352](https://openairdocs.org/sdr/DLL10981352), Jun 26, 1998: POWER SUPPLY. INOPERATIVE. EMER LIGHT PWR SUPPLY INOP 3L. REPLACED PWR SUPPLY. - [SDR DLL10981351](https://openairdocs.org/sdr/DLL10981351), Jun 26, 1998: POWER SUPPLY. INOPERATIVE. SEVERAL AISLE EMER LIGHTS OUT NEAR CENTER CABIN. REPLACED POWER SUPPLY. - [SDR DLL10981127](https://openairdocs.org/sdr/DLL10981127), May 26, 1998: POWER SUPPLY. INOPERATIVE. ON L/O FOUND LOWER GALLEY EMERGENCY LIGHT PWR SUPPLY INOP. REPLACED EMER LIGHT PWR SUPPLY, OPS NML. - [SDR DLL10980449](https://openairdocs.org/sdr/DLL10980449), Feb 20, 1998: BULKHEAD WEB. CRACKED. THE FS 1212 BULKHEAD WEB WAS FOUND WITH A .25 LONG CRACK AT RBL 42.5. THE CRACK WAS ROUTED OUT AND A LOCAL DOUBLER REPAIR INSTALLED PER ER/A 364062-14AD, REV A. - [SDR DLL10971623](https://openairdocs.org/sdr/DLL10971623), Aug 15, 1997: SPAR CAP. CRACKED. TWO CENTER WING INTERMEDIATE SPAR CAPS WERE FOUND TO HAVE CRACKS IN THE TYPICAL MANNER DEPICTED IN L1011 SRM 57-11-00, FIGURE 809 AND LAC S/B 093-57-087. THE CR - [SDR DLL10971624](https://openairdocs.org/sdr/DLL10971624), Aug 13, 1997: SKIN. CRACKED. A CRACK WAS FOUND EMANATING FROM EXISTING STOP DRILL IN THE LT UPPER WING SKIN ALONG THE AFT EDGE AT APPROX IWS T395. CRACK HAS PREVIOUSLY BEEN STOP DRILLED 5 T - [SDR DLL10971369](https://openairdocs.org/sdr/DLL10971369), Jul 12, 1997: PRIORITY VALVE. FAILED. C-SYS HYD WENT TO .25 LOW QTY WHEN GEAR WAS EXTENDED. ALL POM PROCEDURES COMPLIED WITH. GEAR EXTENED NORMALLY. NO NOSE WHEEL STEERING. MTC FOUND CAP FOR DIFFERE - [SDR DLL10971087](https://openairdocs.org/sdr/DLL10971087), Jun 5, 1997: MEGAPHONE. INOPERATIVE. FWD CABIN MEGAPHONE INOP. REPLACED MEGAPHONE, TESTS GOOD. - [SDR DLL10971080](https://openairdocs.org/sdr/DLL10971080), Jun 4, 1997: PWR SUPPLY. INOPERATIVE. GALLEY AISLE EMERG LT INOP. REPLACED PWR SUPPLY, OPN NORMAL. - [SDR DLL10970828](https://openairdocs.org/sdr/DLL10970828), May 3, 1997: COALESCER BAG. DIRTY. AFTER T/O, STRONG FUMES IN AFT CABIN. SMOKE DET IN AFT LAVS WENT OFF. FUMES CLEARED SHORTLY AFTER MAX VENTILATION. REPLACED NR 2 PACK COALESCER BAG. INSP ENG IN - [SDR DLL10970814](https://openairdocs.org/sdr/DLL10970814), May 1, 1997: BATTERY PACK. DISCHARGED. FIRST CLASS ESCAPE PATH LIGHTS INOP. REPLACED BATTERY PACK. - [SDR DLL10962775](https://openairdocs.org/sdr/DLL10962775), Dec 26, 1996: MEGAPHONE. INOPERATIVE. FC MEGAPHONE INOP. REPLACED SAME. - [SDR DLL10962260](https://openairdocs.org/sdr/DLL10962260), Sep 24, 1996: TORQUE BOX. CRACKED. THE RT WING FLAP VANE I/B TRACK NR 2 TORQUE BOX WAS FOUND CRACKED. THE TORQUE BOX WAS REPLACED. - [SDR DLL10962268](https://openairdocs.org/sdr/DLL10962268), Sep 16, 1996: DECK. CRACKED. THE NLG PRESSURE DECK PANEL BETWEEEN FS 328 TO 349 ON THE UPPER SURFACE OF THE PANEL ON BOTH SIDES OF LBL 22 WAS FOUND TO BE CORRODED. THE CORROSION WAS CUT OUT - [SDR DLL10962261](https://openairdocs.org/sdr/DLL10962261), Sep 16, 1996: SKIN. CORROSION. SKIN CORROSION WAS FOUND BETWEEN FS 1675 TO 1695 AND FROM JUST BELOW STR 38 TO SLIGHTLY ABOVE STR 39. THE CORROSION WAS TRIMMED OUT AND REINFORCED WITH A DOUBLE - [SDR DLL10962257](https://openairdocs.org/sdr/DLL10962257), Sep 16, 1996: RIB FITTING. CORROSION. THE RT MLG ATTACH RIB FITTING HAD CORROSION REMOVED FROM THE LUG FACES AND BORE OF THE FWD AND AFT LUGS OF THE OF THE FORWARD TRUNNION LUG SET AND THE FWD AND A - [SDR DLL10962264](https://openairdocs.org/sdr/DLL10962264), Sep 11, 1996: SILL. CORROSION. THE L2 DOOR LOWER SILL AND THE UNDERLYING AREA OF THE O/B LONGERON BELOW WAS FOUND WITH CORROSION. THE CORROSION WAS BLENDED OUT AND THE AREA WAS REINFORCED. - [SDR DLL10962259](https://openairdocs.org/sdr/DLL10962259), Sep 10, 1996: RIB. CRACKED. LT WING PYLON SUPPORT UPPER RIB CAP AT IWS 529-555 HAS A CRACKED CASTELLATION. THE DAMAGE WAS CUT OUT AND REPLACED. - [SDR DLL10962122](https://openairdocs.org/sdr/DLL10962122), Sep 6, 1996: SKIN. CRACKED. NR 2 FLAP VANE INBOARD TRACK HAS A CRACK APPROX 20 INCHES LONG. REPLACED TRACK. - [SDR DLL10962265](https://openairdocs.org/sdr/DLL10962265), Sep 5, 1996: SKIN. CORROSION. THE FUSELAGE SKIN AT FS 469 TO 489 AT STR 39 TO 42 SURROUNDING THE PNEUMATIC BLEED AIR EXHAUST WAS FOUND WITH CORROSION. THE CORROSION WAS TRIMMED OUT AND REINF - [SDR DLL10962263](https://openairdocs.org/sdr/DLL10962263), Sep 4, 1996: RIB. CRACKED. BOTH SIDES IWS 503 RIB UPPER CAP WAS FOUND WITH SEVERAL ATTACH TAB CRACKS IN THE TYPICAL LOCATIONS AFT OF STR 24, AS WELL AS FWD OF STR 24. THESE FWD CRACKS NEC - [SDR DLL10962266](https://openairdocs.org/sdr/DLL10962266), Aug 30, 1996: DECK. CRACKED. THE FUSELAGE HORIZ PRESSURE DECK PANEL WAS FOUND WITH A CRACK AT RBL 102 AND FS 378. THE CRACK WAS TRIMMED OUT AND REINFORCED WITH DOUBLERS AND TRIPLERS. - [SDR DLL10962062](https://openairdocs.org/sdr/DLL10962062), Aug 30, 1996: RIB. CRACKED. A CRACK WAS FOUND ON THE LEFT HAND WING IWS 503 UPPER RIB CAP CASTELLATION. ER/A 271804-14AD WAS WRITTEN TO ACCOMPLISH RIB REPLACEMENT AT NEXT AIRCRAFT HMV. REV - [SDR DLL10961872](https://openairdocs.org/sdr/DLL10961872), Aug 11, 1996: POWER SUPPLY. INOPERATIVE. R3 EMERGENCY LIGHT INOP. REPLACED PWR SUPPLY, CHECKS GOOD. - [SDR DLL10961398](https://openairdocs.org/sdr/DLL10961398), Jun 10, 1996: ENGINE. FAILED. AT 0340 NUMBER 3 ENGINE APPEARED TO HAVE THE SOUND OF A COMPRESSOR STALL. VIB WENT TO 3.0 OIL, FUEL, TEMPS AND PRESSURE NORMAL, 12000/280 KNOTS A/C YAWED, ENGIN - [SDR DLL10961276](https://openairdocs.org/sdr/DLL10961276), May 26, 1996: MEGAPHONE. INOPERATIVE. MEGAPHONE IN FIRST CLASS INOP. - [SDR DLL10960685](https://openairdocs.org/sdr/DLL10960685), Mar 19, 1996: CONTROL CABLE. MISROUTED. ON TAXIOUT, DURING FLT CONTROL CHECK, RUDDER JAMMED WOULD NOT CYCLE TO LEFT. FLIGHT RETURNED TO BLOCK. FOUND PEDAL ADJUSTMENT CONTROL CABLE HOOKED ON RIGHT PEDA - [SDR DLL10960607](https://openairdocs.org/sdr/DLL10960607), Mar 19, 1996: BATTERY PACK. DISCHARDED. EMERGENCY LIGHTS BATTERY PACK INOP L2 DOOR. REPLACED SAME. SYSTEM CHECKS GOOD. - [SDR DLL10960195](https://openairdocs.org/sdr/DLL10960195), Jan 25, 1996: WATERLINE. ELONGATED. WHILE ACCOMPLISHING THE CENTER WEB SPLICE ON THE FS 1363 BKHD PER SI 7-69959-14AD, OPN 0319, THE POTABLE WATER LINE CUTOUT WAS DAMAGED AND ELONGATED THROUGH THE - [SDR DLL10954569](https://openairdocs.org/sdr/DLL10954569), Nov 23, 1995: ACCUMULATOR. CRACKED. NOTICED C-SYSTEM HYDRAULIC QUANTITY BELOW ONE-FOURTH AND DECREASING. TURNED OFF C-SYSTEM PUMP S/O SWITCHED TO ATM. QUANTITY CEASED DECREASING, LOWERED LANDING G - [SDR DLL10954347](https://openairdocs.org/sdr/DLL10954347), Nov 11, 1995: EEL POWER SUPPLY. INOPERATIVE. EMERGENCY EXIT SIGN AND OUTSIDE LIGHT AT 2L DOOR ARE INOP. REPLACED POWER SUPPLY AT 2L DOOR, OPS CKS NORMAL. - [SDR DLL10954199](https://openairdocs.org/sdr/DLL10954199), Oct 30, 1995: STIFFENER. CRACKED. THE INSPECTION BY EO 7-39578-3, FOUND CRACKS IN THE VERTICAL STIFFENERS AT RBL 22.5 AND LBL 10. THE RBL 22.5 STIFFENER HAD ITS UPPER LIGHTENING HOLE DAMAGED AND - [SDR DLL10953993](https://openairdocs.org/sdr/DLL10953993), Oct 13, 1995: CLAMP. WORN. PIREP, ABOUT 30 MINUTES AFTER T/O PRIOR TO TOP OF CLIMB, GOT A VALID J-AREA OVERHEAT. FOUND CLAMP LEAKING AT FUSELAGE ISOLATION VALVE IN HYD SV CTR. REPLACED CL - [SDR DLL10961592](https://openairdocs.org/sdr/DLL10961592), Sep 6, 1995: STIFFENER. CRACKED. THE NLG PRESSURE DECK RISER ALONG RBL 66 WAS FOUND CRACKED AT FS 445 DURING LTR CHECK IN ATL. THE CRACKED WAS TRIMMED OUT AND A FILLER/DOUBLER REPAIR WAS INSTAL - [SDR DLL10954206](https://openairdocs.org/sdr/DLL10954206), Sep 6, 1995: RIB CAP. CRACKED. DURING THE ACCOMPLISHMENT OF SI 7-59208-12AD ON THE RT WING, 2 CRACKS WERE FOUND ON CASTELLATIONS OF THE IWS 555 UPPER RIB CAP. REPAIRED PER DL ERA 271818-14AD. - [SDR DLL10954202](https://openairdocs.org/sdr/DLL10954202), Sep 5, 1995: RIB. CRACKED. DURING THE COMPLETION OF SI 7-59208-2AD ON THE LT WING, A CRACK WAS FOUND ON A CASTELLATION OF THE IWS 503 UPPER RIB CAP. THE CRACK IS BETWEEN STR 18 AND 19 AND - [SDR DLL10953686](https://openairdocs.org/sdr/DLL10953686), Aug 28, 1995: FITTING. CRACKED. COMPLYING WITH DL INSPECTION SI 7-66332-12 AND AD T95-18-52, AFT P-DOME TO STRINGER SPLICE FITTINGS WERE FOUND CRACKED AT STRINGERS NR 5 AND NR 10. FITTINGS WER - [SDR DLL10951674](https://openairdocs.org/sdr/DLL10951674), Apr 24, 1995: FRAMES. CRACKED. DURING SPECIAL INSPECTION, THE FOLLOWING MAIN FUSELAGE FRAMES WERE FOUND CRACKED, RT SIDE FS 509, 609, 669, 1023, 1043, 1063, 1103, 1163, 1685, 1705. LEFT SIDE - [SDR DLL10950327](https://openairdocs.org/sdr/DLL10950327), Jan 22, 1995: FUEL LINE. LEAKING. DURING CRUISE, NR 1 FUEL PRESSURE LIGHT ILLUMINATED. OBSERVED LOOSING FUEL FROM AREA UNDERNEATH NR 1 ENGINE POD. SHUTDOWN NR 1 ENGINE RETURNED TO HNL. FOUND MIS ## NTSB investigations (3) 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 DCA87MA012](https://openairdocs.org/ntsb/DCA87MA012), Nov 13, 1986: Lockheed L1011 (N714DA), Newark, NJ, substantial damage - [NTSB FTW86IA020](https://openairdocs.org/ntsb/FTW86IA020), Oct 26, 1985: Lockheed L-1011-385-1 (N714DA), Dallas/Ft.Worth, TX, incident, no damage - [NTSB FTW80IA018](https://openairdocs.org/ntsb/FTW80IA018), Nov 25, 1979: Lockheed L-1011 (N714DA), Mineral Wells, TX, incident, no damage, 1 fatal ## FAA accident and incident reports (5) 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 19851025058809I](https://openairdocs.org/incident/19851025058809I), Oct 25, 1985: Lkheed 10113851 (N714DA), Dallas, TX, Minor damage. Engine start interrupted due to anticipated ATC delay. Fire on restart with passenger panic, some used slides. - [Incident 19830716040229I](https://openairdocs.org/incident/19830716040229I), Jul 16, 1983: Lkheed 10113851 (N714DA), Boston, MA. Noticed a moderate electrical type odor. Had eye irritation. Returned. Found all systems operating normal. - [Incident 19811224085539I](https://openairdocs.org/incident/19811224085539I), Dec 24, 1981: Lkheed 10113851 (N714DA), Chicago, IL. Rejected takeoff due to low oil pressure light. Inspection found nothing. Replaced filters, returned to service. - [Incident 19810125006899I](https://openairdocs.org/incident/19810125006899I), Jan 25, 1981: Lkheed 10113851 (N714DA), Boston, MA. After departure unable to retract left main gear. Returned and bled hydraulic system. - [Incident 19791125045739I](https://openairdocs.org/incident/19791125045739I), Nov 25, 1979: Lkheed 10113851 (N714DA), Mineral Wells, TX. Captain had fatal heart attack en route l a to atlanta. First officer diverted to dallas. --- 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.