# N723DA: 1977 Lockheed L-1011-385-1, registration cancelled 2013-05-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 6, 2013 - Status when cancelled: Registration expired, pending cancellation - 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-1150 - Year built: 1977 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 18, 1977 - Certificate issued: August 16, 2006 - Last registry action: August 18, 2009 - Mode S code: A9AEFD - Owner when cancelled: [Trans Atlantic Airlines](https://openairdocs.org/faa-owner/TRANS%20ATLANTIC%20AIRLINES) - Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York) - Owner type: Corporation - Owner's area on the map: 40.7139° N, 74.0079° W: Placed by OpenAirDocs at the center of ZIP code 10007, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N723DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=723DA - Page: https://openairdocs.org/deregistered/N723DA-2013-05-06 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 (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DLL10980658](https://openairdocs.org/sdr/DLL10980658), Mar 19, 1998: TRUNNION. CRACKED. FUSELAGE FS 449 BULKHEAD LBL 21 NLG TRUNNION FITTING, REPAIR FOR CRACK. THE 1543141 NLG TRUNNION FITTING WAS FOUND WITH A TYPICAL CRACK AT THE FS 449 BULKHEAD A - [SDR DLL10980117](https://openairdocs.org/sdr/DLL10980117), Jan 15, 1998: BULB. FAILED. L2 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED, CK'S NORMAL. - [SDR DLL10972355](https://openairdocs.org/sdr/DLL10972355), Nov 11, 1997: SPAR WEB. CORRODED. THE REAR SPAR OF THE CENTER WING WAS FOUND CORRODED JUST INBD OF THE UPPER AFT CENTER WING TO OUTER WING JOINT FITTING AT LBL 100. THE CORROSION WAS MACHINED AW - [SDR DLL10971135](https://openairdocs.org/sdr/DLL10971135), Jun 14, 1997: GEAR BOX. FAILED. IN FLT CRUISE FL350 NR 3 ENG N3 WENT TO ZERO FOLLOWED BY LOSS OF OIL PRESSURE. NR 3 ENG SHUT DOWN WITH NO OTHER ABNORMAL INDICATIONS. REPLACED NR 3 ENG GEARBOX. - [SDR DLL10971126](https://openairdocs.org/sdr/DLL10971126), Jun 11, 1997: POWER PACK. INOPERATIVE. EMERG LIGHTS INOP AT R3 EXIT SIGN EXTERIOR LIGHT AND AISLE LIGHT AT 35H AND 24H. REPLACED EMERG POWER PACK ABOVE 37HJ. - [SDR DLL10970783](https://openairdocs.org/sdr/DLL10970783), Apr 21, 1997: SKIN. CREASED. THE LEFT ELEVATOR BETWEEN STA 174 AND 193 HAS THREE CREASES ON THE UPPER SKIN. THE DEPTH OF THE CREASES ARE APPROXIMATELY 0.036 AND 0.027. THE UPPER SKIN OF THE - [SDR DLL10970713](https://openairdocs.org/sdr/DLL10970713), Apr 3, 1997: PRESSURE DECK. CORROSION. THE NOSE LANDING GEAR HORIZONTAL PRESSURE DECK WAS FOUND WITH CORROSION AT STA 336 TO 341 RBL 9. THE CORROSION WAS REMOVED LEAVING A 1.25 BY 5.25 CUTOUT. THE SU - [SDR DLL10970712](https://openairdocs.org/sdr/DLL10970712), Mar 31, 1997: BULKHEAD. CRACKED. UPON INSPECTION, A CRACK WAS FOUND IN THE NLG FITTING AT STA 449 BULKHEAD. THIS CRACK BEGINS IN A SEAL RETAINER HOLE AT LBL 21, AND EXTENDS APPROXIMATELY 2.0 AF - [SDR DLL10970692](https://openairdocs.org/sdr/DLL10970692), Mar 24, 1997: PRESSURE DECK. CORRODED. THE NOSE LANDING GEAR HORIZONTAL PRESSURE DECK WAS FOUND WITH CORROSION AT STA 336 TO 341 RBL 9. THE CORROSION WAS REMOVED LEAVING A 1.25 BY 5.25 CUTOUT. THIS C - [SDR DLL10962778](https://openairdocs.org/sdr/DLL10962778), Dec 27, 1996: LENS. MISSING. WORKING MCO FLOOR TRACK LIGHTING AT 4C INOP. REPLACED RED LENS, CKS OK. REMOVED MCO/PLAC. - [SDR DLL10961280](https://openairdocs.org/sdr/DLL10961280), May 27, 1996: SWITCH. STUCK. DURING CK OUT, EMERG LIGHTS WOULD NOT ARM. FOUND LOWER GALLEY EMERG LIGHT SWITCH STUCK. CLEANED AND CYCLED SWITCH, CHECKS GOOD. - [SDR DLL10961252](https://openairdocs.org/sdr/DLL10961252), May 21, 1996: PANEL. INOPERATIVE. WHILE PERFORMING EMERGENCY EVACUATION TEST PER OPERATION 68111 DURING B-LETTER CHECK, LOWER GALLEY EVAC SIGNAL PANEL FAILED TO SOUND OR LIGHT. REPLACED PANEL, C - [SDR DLL10961025](https://openairdocs.org/sdr/DLL10961025), Apr 26, 1996: SKIN. DENTED. THE FUSELAGE SKIN AT F.S. 605 AND STR 27 HAS BEEN CUT OUT DUE TO GROUND DAMAGE. ACCOMPLISHED REPAIRS PER DL ERA 273710-14. - [SDR DLL10960438](https://openairdocs.org/sdr/DLL10960438), Feb 26, 1996: WIRE. BROKEN. LEFT FLOOR TRACK LIGHTS JUST AFT OF 2L DOOR, ROWS 20 TO 26 INOP. REPAIRED BROKEN WIRE IN FLOOR TRACK AT SEAT 27B AND OPERATION NORMAL. - [SDR DLL10960076](https://openairdocs.org/sdr/DLL10960076), Jan 12, 1996: WIRE. BROKEN. EMERGENCY FLOOR TRACK LIGHT OUT AT SEAT 27 H, J. REPAIRED BROKEN WIRE IN FLOOR TRACK. - [SDR DLL10954514](https://openairdocs.org/sdr/DLL10954514), Nov 2, 1995: SKIN. CRACKED. THE RT HORIZ STAB L/E WAS FOUND WITH EXTENSIVE DAMAGE FWD OF THE FRONT SPAR BETWEEN STA 'H' LE 332.7 TO 455.2. ACCOMPLISHED REPAIRS PER DL ERA 272204-14. - [SDR DLL10954510](https://openairdocs.org/sdr/DLL10954510), Nov 2, 1995: SKIN. CRACKED. THE RT HORIZ STAB L/E WAS FOUND WITH EXTENSIVE DAMAGE FWD OF THE FRONT SPAR BET STA-H LE 332.7 TO 455.2. A REPLACEMENT FROM A/C 781 IS BEING SPLICED IN. AS A RE - [SDR DLL10954508](https://openairdocs.org/sdr/DLL10954508), Nov 2, 1995: RIB. CRACKED. THE RT HORIZ STAB L/E INTERMEDIATE RIB LOCATED AT 'H' LE 414.405 WAS FOUND CRACKED. THE CRACK WAS LOCATED IN THE UPPER FLANGE RADUIS OF THE UPPER CAP ON THE AFT - [SDR DLL10954507](https://openairdocs.org/sdr/DLL10954507), Nov 2, 1995: AUX SPARS. CRACKED. THE RT HORIZONTAL STABILIZER L/E AUXILIARY SPARS WERE FOUND WITH NUMEROUS CRACKS. THE CRACKS ARE LOCATED ON BOTH THE UPPER AND LOWER CAPS. SPLICED IN NEW SECTIO - [SDR DLL10954509](https://openairdocs.org/sdr/DLL10954509), Oct 25, 1995: SKIN. CRACKED. THE RT HORIZ STAB L/E WAS FOUND WITH EXTENSIVE DAMAGE FWD OF THE FRONT SPAR BETWEEN STA 'H' LE 332.7 TO 455.2. REPAIRED PER DL ERA 272226-14. - [SDR DLL10954506](https://openairdocs.org/sdr/DLL10954506), Oct 23, 1995: STRUCTURE. CRACKED. THE RT HORIZ STAB L/E WAS FOUND WITH EXTENSIVE DAMAGE FWD OF THE FRONT SPAR BETWEEN STA-H LE 332.7 TO 455.2. THE DAMAGE CONSISTS OF CRACKED SKIN PANELS, CRACKED - [SDR DLL10954050](https://openairdocs.org/sdr/DLL10954050), Oct 18, 1995: RIBS. CRACKED. HORIZONTAL STAB RT NR 3 L/E PANEL HAS 4 RIBS CRACKED. REPAIRED PER SRM 55-12-00 FIG 802. - [SDR DLL10954225](https://openairdocs.org/sdr/DLL10954225), Oct 17, 1995: RIBS. CRACKED. DURING INSPECTION, FOUND RT STABILZER L/E PANEL WITH 8 CRACKED RIB ASSEMBLIES. REPAIRED PER SRM 55-12-00. - [SDR DLL10954051](https://openairdocs.org/sdr/DLL10954051), Oct 17, 1995: RIBS. CRACKED. DURING A ROUTINE INSPECTION, NR 6 RT HORIZONTAL LEADING EDGE WAS FOUND TO HAVE ALL OF THE RIBS CRACKED AT THE T/E. DOUBLERS WERE INSTALLED PER SRM 55-12-00 FIG - [SDR DLL10954169](https://openairdocs.org/sdr/DLL10954169), Sep 25, 1995: SKIN. OVERSIZED HOLES. DURING REPAIR OF 1363 BULKHEAD, FOUND SEVERAL FASTENER HOLES BETWEEN STR'S 21 AND 23 AND STR'S 43-45 WERE OVERSIZED TO A .3885 INCH DIAMETER AND .344 INCH DIAME - [SDR DLL10954530](https://openairdocs.org/sdr/DLL10954530), Sep 1, 1995: BLKHD FITTING. CRACKED. DURING ACCOMPLISHMENT OF AN INSPECTION OF THE AFT PRESSURE BULKHEAD STR SPLICE FITTINGS PER SI 7-66332-12, THE STR 8 AND 58 FITTINGS WERE FOUND TO BE CRACKED AN - [SDR DLL10953688](https://openairdocs.org/sdr/DLL10953688), Aug 25, 1995: FITTINGS. 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 8 AND NR 58. FITTINGS WER - [SDR DLL10954164](https://openairdocs.org/sdr/DLL10954164), Jul 13, 1995: BLKHD WEB. CRACKED. DURING INSPECTION, THE SUBJECT AIRCRAFT WAS FOUND WITH A CRACK IN THE FUSELAGE 1363 BULKHEAD WEB. THE CRACK IS LOCATED AT LBL 85 EXTENDING DIAGONALLY UPWARD. AC - [SDR DLL10952765](https://openairdocs.org/sdr/DLL10952765), Jun 23, 1995: SKIN. CRACKED. NR 3 RT FLAP VANE HAD A CRACK 3 INCHES LONG, TOP SIDE SKIN 60 INCHES FROM I/B END. REPAIRED CRACK AS PER SRM FLUSH REPAIR 5753-00. - [SDR DLL10952764](https://openairdocs.org/sdr/DLL10952764), Jun 22, 1995: TRUNNION FITTING. RUSTED. LANDING GEAR FWD TRUNNION FITTING HAS RUST BACK OF GLAND NUT. REMOVED RUST PER SRM 51-21-01. - [SDR DLL10952773](https://openairdocs.org/sdr/DLL10952773), Jun 21, 1995: SKIN. CRACKED. DURING LETTER CHECK, FOUND LEFT WING NR 2 FLAP VANE WITH A 2 INCH CRACK IN UPPER SKIN AT 60 INCHES FROM I/B END OF FLAP. REPAIRED PER SRM 57-53-0. - [SDR DLL10952668](https://openairdocs.org/sdr/DLL10952668), Jun 18, 1995: BLKHD CLIP. CRACKED. DURING INSPECTION, FOUND FS 1223 CANTED BULKHEAD CLIP CRACKED. REPAIRED PER SRM 53-11-00 PG 859. - [SDR DLL10952742](https://openairdocs.org/sdr/DLL10952742), Jun 17, 1995: BLKHD ANGLE. CRACKED. RT SIDE FS 1223 CANTED BULKHEAD ANGLE IS CRACKED. REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE PER SRM 53-11-00 PG 859, FOUND AT LETTER CHECK. - [SDR DLL10952741](https://openairdocs.org/sdr/DLL10952741), Jun 17, 1995: SKIN. DENTED. DURING LETTER CHECK, FOUND LEFT WING NR 2 FLAP VANE WITH DENT IN SKIN. REPAIRED PER SRM 57-53-00. - [SDR DLL10953099](https://openairdocs.org/sdr/DLL10953099), Jun 13, 1995: BEAM. CRACKED. DURING INSPECTION, NR 2 RT SPOILER BEAM WAS FOUND TO HAVE A CRACK AT THE ACTUATOR FITTING. BEAM WAS REPLACED AND NEW SKINS AND HONEYCOMB BONDED PER SRM 57-52-00 - [SDR DLL10952620](https://openairdocs.org/sdr/DLL10952620), Jun 9, 1995: SPAR. CRACKED. ON DESCENT WITH FLAPS UP AND SPEED BRAKE LEVER PULLED FULL AFT, THE 2R SPOILER ONLY COMES UP TO TOP OF DLC RANGE. AIRPLANE TRIES TO ROLL LEFT, NEEDED ABOUT 30 D - [SDR DLL10951639](https://openairdocs.org/sdr/DLL10951639), Apr 18, 1995: DECODER. FAILED. ON TAXI IN AFTER LANDING, HAD HEAVY ELECTRICAL BURNING ODOR IN MID GALLEY AREA. FOUND FWD DECODER MID RT ROW ZONE C FAULTY. REPLACED DECODER OPERATION NORMAL. ## 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 NYC97LA129](https://openairdocs.org/ntsb/NYC97LA129), Jun 27, 1997: Lockheed L-1011-385-1 (N723DA), Covington, KY, no damage. Probable cause: the failure of the primary and secondary elevator driveshafts, and the failure of maintenance personnel to detect the failure of the primary shaft during scheduled inspections. ## 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. - [Accident 19970627046249A](https://openairdocs.org/incident/19970627046249A), Jun 27, 1997: N723DA, Covington/Cinci, KY, No damage. (-23) During acft push back, lt. galley lift fell approx. 5 ft. from upper positin to lower galley. Flight attendant in lift was injured & was removed from… - [Incident 19890104015369I](https://openairdocs.org/incident/19890104015369I), Jan 4, 1989: Lkheed 10113851 (N723DA), West Palm Beach, FL. Noise after takeoff. Returned. A cargo container was loose and voiding ping not installed. Door seal out of track. - [Incident 19880911054749I](https://openairdocs.org/incident/19880911054749I), Sep 11, 1988: Lkheed 10113851 (N723DA), Dallas-Ft Worth, TX, Minor damage. Failure of right air turbine motor on gear retraction on takeoff. Pieces of rubber from exhaust ducting on runway. - [Incident 19841011066399I](https://openairdocs.org/incident/19841011066399I), Oct 11, 1984: Lkheed 10113851 (N723DA), Falmouth, MA. Inclement weather prevented landing at destination. Did not have enough fuel to reach weather alternate. - [Incident 19801218085399I](https://openairdocs.org/incident/19801218085399I), Dec 18, 1980: Lkheed 10113851 (N723DA), Chicago, IL. Flight aborted takeoff due to oil pressure warning light. Replaced nr 2 engine oil pressure and scavenger filters. ## Other aircraft with N723DA - [Registered now](https://openairdocs.org/aircraft/N723DA): Cirrus Design SR20, S/N 9593, built 2023 --- 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.