# N765DA: Lockheed L-1011-385-3, registration cancelled 2001-04-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 23, 2001 - Exported to: Portugal - 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) - Data sheets: [TCDS A23WE](https://openairdocs.org/tcds/A23WE) (OpenAirDocs) - Serial number: 193H-1206 - Type of aircraft: Fixed wing multi engine - Certificate issued: August 1, 1991 - Last registry action: August 15, 2000 - Mode S code: AA5467 - Owner when cancelled: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC) - Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta) - Owner type: Corporation - Owner's area on the map: 33.7490° N, 84.3880° W: Placed by OpenAirDocs: center of Atlanta, GA, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N765DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=765DA - Page: https://openairdocs.org/deregistered/N765DA-2001-04-23 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 (43) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DLL19010014](https://openairdocs.org/sdr/DLL19010014), Jan 4, 2001: CIRCUIT BREAKER. FAILED. BATTERY CONDITION LIGHT ON CAT. REPLACED C/B AND REPAIRED WIRE TO C/B. - [SDR DLL19002311](https://openairdocs.org/sdr/DLL19002311), Nov 28, 2000: GIRT BAR. DISCONNECTED. DOOR 3L CABIN DOOR HARD TO OPEN OR CLOSE - GIRT BAR HAS TO BE MANUALLY PLACED IN RETAINER WHEN CLOSED, CORRECTIVE ACTION REATTACHED GIRT BAR IN HOOK LOCK ASSEMB - [SDR DLL19001038](https://openairdocs.org/sdr/DLL19001038), May 26, 2000: UNKNOWN. ODOR. F/A REPORTED THAT ON APPROACH A BURNING SMELL WAS AROUND ROW 22. INVESTIGATED CABIN GALLEY AND SERVICE AREAS ABOVE AND BELOW FLOOR LEVEL. RAN ALL PNEUMATIC ELEC - [SDR DLL19000921](https://openairdocs.org/sdr/DLL19000921), May 9, 2000: POWER SUPPLY. DISCHARGED. POWER SUPPLY FOR EMERGENCY ESCAPE PATH LIGHTING SYSTEM ONLY LAST 1 MINUTE. - [SDR DLL19000777](https://openairdocs.org/sdr/DLL19000777), Apr 21, 2000: SPOILER PANEL. DEPLOYED. SPLR PANELS NR 1 AND NR 3 ON LT WING DEPLOYED ON T/O. NO INDICATIONS IN COCKPIT, LOCKED UP, WILL NOT COME DOWN. ABORTED T/O AT 100 KTS. REPLACED BELL CRANK AT S - [SDR DLL19992666](https://openairdocs.org/sdr/DLL19992666), Dec 7, 1999: UNKNOWN. ODOR. ODOR APPEARED IN CABIN DURING LAST 5 - 10 MINUTES OF FLIGHT PRIMARILY IN THE REAR OF B-ZONE. FORWARD TO MCO AND PLAC PER MEL 25-99-06. FLIGHT ATTENDANTS REPORTE - [SDR DLL19991857](https://openairdocs.org/sdr/DLL19991857), Aug 19, 1999: BULKHEAD WEB. DAMAGED. TOOLING DAMAGE WAS FOUND ON THE NLG WHEEL WELL BULKHEAD AT APPROX FS 416, RBL 22 ON THE LWR SURFACE O/B FILLET RADIUS INSIDE THE RT ECS COMPT (NLG BLKHD WEB CAP - [SDR DLL19991828](https://openairdocs.org/sdr/DLL19991828), Aug 12, 1999: RIB. CRACKED. LT AND RT WING UPPER RIB CAP AT IWS 555 FOUND CRACKED DURING ROUTINE INSPECTION ERA 333431-14 REV B. - [SDR DLL19991334](https://openairdocs.org/sdr/DLL19991334), Jun 13, 1999: MODULE. FAILED. AFTER DROPPING GEAR, 3 GREEN GEAR LIGHTS. C-SYS PRESSURE STARTED DECREASING, FLUID LOSS INDICATED. DOOR LIGHTS FOR MAIN GEAR REMAINED OPEN. WENT THRU CHECK LIST - [SDR DLL19982575](https://openairdocs.org/sdr/DLL19982575), Dec 6, 1998: BLADE. LACK OF LUBE. NR 2 ENGINE HAD HIGH FAN VIBS BOTH A AND B CHANNELS, SHOWED APPROX 2.7 UNITS. FAN VIBS INCREASED WHEN THROTTLES RETARTED TO IDLE. SHUT DOWN NUMBER TWO ENGINE PE - [SDR DLL17981507](https://openairdocs.org/sdr/DLL17981507), Jul 20, 1998: POWER SUPPLY. INOPERATIVE. ON LAYOVER, CHECK FOUND AFT LEFT HAND OVERHEAD EMERGENCY LIGHTS WON'T TEST. REPLACED ASSOCIATED BATTERY PACK AT 2L AND ADDITIONAL PACK AT 3R. ALL EMER LIGHTS TE - [SDR DLL17981280](https://openairdocs.org/sdr/DLL17981280), Jun 17, 1998: POWER SUPPLY. INOPERATIVE. ON LAYOVER, FOUND EMERGENCY BATTERY PACK NOT CHARGING. REPLACED EMERGENCY LIGHT BATTERY PACK. - [SDR DLL17981046](https://openairdocs.org/sdr/DLL17981046), May 16, 1998: ENGINE. FAILED. ON T/O, THE NR 1 ENG GAVE LOUD BANG. VIBES PEGGED OUT AT 5 PLUS AND EGT LT CAME ON. SHUT NR 1 ENG DOWN AND LANDED ATL. REPLACE NUMBER ONE ENGINE. - [SDR DLL17980682](https://openairdocs.org/sdr/DLL17980682), Mar 29, 1998: COUNTERBALANCE. INOPERATIVE. AIRCRAFT ARRIVED WITH L3 EMERGENCY HANDLE PARTIALLY OPEN. REPLACED COUNTERBALANCE AND RIGGED DOOR. - [SDR DLL17972049](https://openairdocs.org/sdr/DLL17972049), Oct 13, 1997: POWER SUPPLY. INOPERATIVE. OVERHEAD EMER ESCAPE PATH LIGHTS FAILED TO OPERATE DURING TEST. REPLACE POWER SUPPLY. - [SDR DLL17971958](https://openairdocs.org/sdr/DLL17971958), Sep 25, 1997: SKIN. CRACKED. THE LOWER CENTER BOX SKIN ON THE LT WING WAS FOUND CRACKED AT THE S-14 RUNOUT AT WS 248. THE CRACK RUNS FORE AND AFT THROUGH THE OUTBOARD MOST FASTENERS OF S-14 - [SDR DLL17971959](https://openairdocs.org/sdr/DLL17971959), Sep 24, 1997: FRAME. CORRODED. DURING ACCOMPLISHMENT OF SI 7-63916-12AD PART II, A 2 INCH LONG CRACK WAS FOUND IN THE WEB OF THE RIGHT HAND FS 983 FRAME. THE CRACK RUNS VERTICALLY IN THE WEB - [SDR DLL17971336](https://openairdocs.org/sdr/DLL17971336), Jun 28, 1997: SKIN. PUNCTURED. EXTENSIVE DAMAGE WAS INCURRED TO THE FUSELAGE SKIN PANEL BETWEEN STA 539 AND 639 BETWEEN STR 42 AND 48. THE DAMAGE CONSISTED OF FOUR LARGE SKIN PUNCTURES, TWO D - [SDR DLL17970301](https://openairdocs.org/sdr/DLL17970301), Feb 18, 1997: VALVE. LEAKING. AREA E OVERHEAT ON CLIMB-OUT. RETURNED TO BASE. FOUND NR 3 PACK VALVE LEAKING AT AFT END. REPLACED NR 3 PACK VALVE. VALVE P/N 217002711 OFF KC16803 ON 065. - [SDR DLL17970438](https://openairdocs.org/sdr/DLL17970438), Feb 9, 1997: RCCB. FAILED. COULD NOT SHUT OFF 2R INBOARD BOOST PUMP. DIVERTED TO JFK. REPLACED 2R INBD PUMP RCCB, OPS CK OK. - [SDR DLL17962418](https://openairdocs.org/sdr/DLL17962418), Oct 30, 1996: BATTERY PACK. NOT SEATED. HALF OF THE EMERGENCY EGRESS PATH LIGHTS INOP. RESEATED BATTERY PACKS, OPS NORMAL. - [SDR DLL17961313](https://openairdocs.org/sdr/DLL17961313), May 29, 1996: BATTERY. MISSING. FOUND CAPTAIN'S EMERGENCY FLASHLIGHT SEAL BROKEN AND BATTERY EMPTY DUE LIGHT MOUNTED 180 DEGREES WRONG. REPLACED FLASHLIGHT AND BATTERY. - [SDR DLL17954181](https://openairdocs.org/sdr/DLL17954181), Oct 4, 1995: FITTING. CORRODED. THE LT MLG ATTACH FITTING WAS FOUND CORRODED ON THE UPPER FLANGE. DURING REMOVAL, FASTENER HOLES WERE FOUND OVERSIZED AND SPOT FACED IN ACCORDANCE WITH THE SRM. - [SDR DLL17954194](https://openairdocs.org/sdr/DLL17954194), Oct 3, 1995: LATCH FITTINGS. CORRODED. THE NR 1 THROUGH NR 8 C-1A CARGO DOOR LATCH FITTINGS WERE FOUND WITH PITTING IN THE UPPER WELLS. DRAIN HOLES WILL BE DRILLED IN ALL EIGHT FITTINGS PER DL ERA 27 - [SDR DLL17954193](https://openairdocs.org/sdr/DLL17954193), Oct 3, 1995: BULKHEAD. OVERSIZED HOLES. SEVERAL FASTENER HOLES BETWEEN STR 21 AND 22 WERE OVERSIZED TO A .25 DIAMETER. FASTENER REMOVAL ACCOMPLISHMENT OF EO 7-69959-12AD, REPAIRED PER DL ERA 271854-14 - [SDR DLL17954192](https://openairdocs.org/sdr/DLL17954192), Oct 3, 1995: DOOR SILL. CORRODED. THE LOWER DOOR SILL INBOARD CAP FITTINGS WERE FOUND CORRODED AND REQUIRED REPLACEMENT. REPAIRED PER DL ERA 271846-14. - [SDR DLL17954191](https://openairdocs.org/sdr/DLL17954191), Oct 3, 1995: LONGERON. CRACKED. THE OUTER CAP ANGLE OF THE LT UPPER LONGERON IN THE FUSELAGE AFTER BODY AT STA 1860 WAS FOUND CRACKED IN THE RADIUS. REPAIRED PER DL ERA 271830-14. - [SDR DLL17954190](https://openairdocs.org/sdr/DLL17954190), Oct 3, 1995: ANGLE. OVERSIZED HOLES. SEVERAL FASTENERS IN THE BASE HOR FLANGE OF THE FAIL-SAFE ANGLE WERE FOUND TO BE OVERSIZED, WING TO FUSELAGE. REPAIRED PER DL ERA 271865-14 AD. - [SDR DLL17954189](https://openairdocs.org/sdr/DLL17954189), Oct 3, 1995: REAR SPAR. CRACKED. DURING THE ACCOMPLISHMENT OF EO 7-59089-3, CRACK INDICATIONS WERE FOUND EMANATING FROM TWO FASTENER HOLES COMMON TO THE UPPER WING SKIN AND THE UPPER SPAR CAP. - [SDR DLL17954188](https://openairdocs.org/sdr/DLL17954188), Oct 3, 1995: ANGLE. OVERSIZED HOLE. DURING REMOVAL OF EXISTING FASTENERS AT RT 1203, THE UPPER FWD HOLE COMMON TO THE VERTICAL LEG OF THE FAIL-SAFE ANGLE, SKIN PANEL, FRAME FITTING, AND OVERWING T - [SDR DLL17954184](https://openairdocs.org/sdr/DLL17954184), Oct 3, 1995: ATTACH FITTING. DAMAGED. TOOLING DAMAGE WAS INCURRED DURING RE-WORK TO AN INBOARD .6250 INCH FASTENER HOLE THROUGH THE RT MAIN LDG ATTACH FITTING. REPAIRED IAW DL ERA 271908-14 AD. - [SDR DLL17954182](https://openairdocs.org/sdr/DLL17954182), Oct 3, 1995: SKIN. SHORT EDGE DIST. WHEN PICKING UP FASTENER LOCATIONS IN THE SKIN ATTACH FLANGE OF THE 1363 BULKHEAD CAP, NINE .25 INCH FASTENER HOLES ON BOTH THE LT AND RT SIDES WERE FOUND WITH - [SDR DLL17954179](https://openairdocs.org/sdr/DLL17954179), Oct 3, 1995: ACTUATOR FITIING. DAMAGED. THE LT AND RT WING MLG ACTUATOR SUPPORT FITTING HAD THREE FASTENERS, IPC 57-14-0 FIG 1 ITEMS 280, 285, 300 ENT. THESE VERE REPLACED WITH HLT 104 BOLTS PER SRM 5 - [SDR DLL17953739](https://openairdocs.org/sdr/DLL17953739), Sep 19, 1995: SKIN. DENTED. AT HMV, LT WING NR 1 FLAP VANE WAS FOUND WITH DENTED SKIN ON INNER SKIN PANEL. INSTALLED REPAIR DOUBLERS PER SRM 51-50-01. - [SDR DLL17953738](https://openairdocs.org/sdr/DLL17953738), Sep 19, 1995: SKIN. DAMAGED. AT HMV, LT WING NR 1 FLAP VANE WAS FOUND WITH HEAVY WEAR DAMAGE TO OUTER SKIN AT THE INBD END OF VANE. REPAIRED PER SRM 57-53-00, FIG 805. - [SDR DLL17953737](https://openairdocs.org/sdr/DLL17953737), Sep 19, 1995: SKIN. CRACKED. AT HMV, LEFT WING NR 1 FLAP VANE WAS FOUND WITH UPPER SKIN CRACKED ALONG A RIB AT 40 INCHES FROM INBD END. REPAIRED PER SRM 57-53-00. - [SDR DLL17954038](https://openairdocs.org/sdr/DLL17954038), Sep 14, 1995: FITTINGS. CORRODED. THE LOWER DOOR SILL I/B CAP FITTINGS AT FS 901 RT AND LT SIDES, WERE FOUND CORRODED AND REQUIRED REPLACEMENT. ACCOMPLISHED REPAIRS PER DL ERA 271846-14. - [SDR DLL17954195](https://openairdocs.org/sdr/DLL17954195), Sep 12, 1995: BLKHD SKIN. CRACKED. ON 8-9-91 CRACKS WERE DISCOVERED IN THE FS 328 CANTED BULKHEAD STRUCTURE DURING HMV. THIS DAMAGE WAS REPAIRED BY LAC DWG 1646545 PER ER/A 226719-14. AFTER THAT, - [SDR DLL17954037](https://openairdocs.org/sdr/DLL17954037), Sep 12, 1995: LONGERON. CRACKED. FUSELAGE, AFTERBODY, LLT LONGERON ASSY FS 1860 WL 328.942, REPAIR OF CRACKED LONGERON. THE OUTER CAP ANGLE OF THE LT UPPER LONGERON IN THE FUSELAGE AFTERBODY AT - [SDR DLL17953782](https://openairdocs.org/sdr/DLL17953782), Sep 8, 1995: FRAME. CRACKED. DURING HMV, 1363 BULKHEAD FRAME AT APPROX WL 160 ON RT SIDE IS CRACKED AT THE SECOND FASTENER FROM BOTTOM FWD ROW. INSTALLED REPAIR AS PER SRM 53-11-00 FIG 843. - [SDR DLL17953723](https://openairdocs.org/sdr/DLL17953723), Sep 7, 1995: FLOORBEAM. CORRODED. DURING HMV, UPPER SURFACE OF FLOORBEAM AND SUPPORT ANGLE CORRODED AT FS 846 AT RBL 40. REPAIRED PER SRM 53-21-00 PG 849 TO 852. - [SDR DLL17953707](https://openairdocs.org/sdr/DLL17953707), Sep 7, 1995: FLOORBEAM. CORRODED. DURING HMV, FS 901 FLOOR SUPPORT BEAM CORRODED AT LBL 49, 60, AND RBL 49, 70. REPLACED BEAM CAP PER SRM 53-21-00 PG 849 TO 852. - [SDR DLL17953692](https://openairdocs.org/sdr/DLL17953692), Sep 3, 1995: COWL. WORN. AT HMV, NR 2 ENGINE RT COWL PANEL WAS FOUND WITH WEAR DAMAGE AT LOWER FORWARD CORNER OF PANEL. ACCOMPLISHED REPAIRS PER SRM 51-50-01, FIG 2. ## Other aircraft with N765DA - [Cancelled 2020-02-03](https://openairdocs.org/deregistered/N765DA-2020-02-03): DJI PHANTOM 3 PROFESSION, S/N P76DCE29010962. Registration expired, pending cancellation. Owner: [Mudd Inc DBA](https://openairdocs.org/faa-owner/MUDD%20INC%20DBA), [Cedar Falls, IA](https://openairdocs.org/faa-place/IA/Cedar%20Falls) --- 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.