# N741DA: 1983 Lockheed L-1011-385-1, registration cancelled 2004-12-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 3, 2004 - Exported to: Kyrgyzstan - Status when cancelled: Triennial form not returned - Airframe: [Lockheed L-1011-385-1](https://openairdocs.org/model/lockheed-l-1011-385-1) (registry code 5265010) - 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: 193C-1245 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 13, 1987 - Certificate issued: July 27, 1983 - Last registry action: April 20, 2004 - Mode S code: A9F68D - 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/N741DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=741DA - Page: https://openairdocs.org/deregistered/N741DA-2004-12-03 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 (30) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DLL14001986](https://openairdocs.org/sdr/DLL14001986), Oct 11, 2000: POWER SUPPLY. INOPERATIVE. R-2 DOOR EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY FOR R-2 DOOR LIGHT, OPS CHECKS GOOD. - [SDR DLL14001630](https://openairdocs.org/sdr/DLL14001630), Aug 23, 2000: FRAME. CRACKED. STA 1083 FRAME CRACKED APPROX 1 INCH BELOW FLOOR LINE LT SIDE. REPAIRED PER SRM. - [SDR DLL14001625](https://openairdocs.org/sdr/DLL14001625), Aug 22, 2000: FRAME. CRACKED. STA 1063 FRAME CRACKED APPROX 2 INCHES ABOVE FLOOR LINE LT SIDE. REPAIRED FRAME. - [SDR DLL14001624](https://openairdocs.org/sdr/DLL14001624), Aug 22, 2000: FRAME. CRACKED. STA 1103 FRAME CRACKED RT SIDE APPROX 3 INCHES BELOW FLOOR LINE MARKED. REPAIRED FRAME. - [SDR DLL14001609](https://openairdocs.org/sdr/DLL14001609), Aug 16, 2000: FRAME. CRACKED. STA 1123 FRAME CRACKED, APPROX 1 INCH ABOVE FLOOR LINE LT SIDE. REPAIRED SAME. - [SDR DLL14001608](https://openairdocs.org/sdr/DLL14001608), Aug 16, 2000: FRAME. CRACKED. STA 1123 FRAME CRACKED, APPROX 1 INCH ABOVE FLOOR LINE, LT SIDE. REPAIRED SAME. - [SDR DLL14001601](https://openairdocs.org/sdr/DLL14001601), Aug 14, 2000: BULKHEAD. CRACKED. HFEC INSP FOUND CRACK AT FS 1212 BLKD RBL 22.5 WL 182 REF OPN50424AD. REPAIRING CRACK PER SRM 53-11-00 FIG 854. - [SDR DLL14001101](https://openairdocs.org/sdr/DLL14001101), Jun 5, 2000: BULKHEAD. CRACKED. THE FS 1363 BULKHEAD WEB WAS FOUND WITH A .4 TYPICAL CRACK EMANATING FROM A FASTENER HOLE AT THE LBL 42.5 WEB JOINT AT WL 126. THE CRACKED AREA WAS TRIMMED OUT - [SDR DLL14992327](https://openairdocs.org/sdr/DLL14992327), Oct 21, 1999: LINE. FAILED. 1.5 HRS AFTER T/O, C-SYS HYD LO QTY LIGHT SAME ON AND QTY WENT MOMENTARILY TO 1/4 THEN BACK TO 3/8. FOLLOWED POM AND WITH NO PUMPS ON / NO SYS PRESS / QTY SLOWL - [SDR DLL14991925](https://openairdocs.org/sdr/DLL14991925), Aug 29, 1999: STIFFENER. CRACKED. THE RBL 22.5 VERTICAL STIFFENER ON THE CENTER WING FRONT SPAR (FS 983) WAS FOUND WITH A TYPICAL CRACK EMANATING FROM A LIGHTENING HOLE IN THE STIFFENER WEB NEAR - [SDR DLL14991475](https://openairdocs.org/sdr/DLL14991475), Jun 29, 1999: LINE. LOOSE. NR 2 ENG NACELLE PYLON OVERHEAT LOOPS A & B LIGHTS ON AFTER TAKEOFF. BOTH LOOP LIGHTS WENT OUT WHEN THROTTLE/POWER REDUCED AND HIGH PRESSURE BLEED OFF. WHEN POW - [SDR DLL14990674](https://openairdocs.org/sdr/DLL14990674), Mar 26, 1999: FIRE WIRE. DAMAGED. NR 2 ENG A LOOP WARNING OCCURRED AFTER TAKEOFF AT 1500 FT AGL. REPAIRED WIRING ON ENGINE AND IN SPLITTER AREA. - [SDR DLL14990670](https://openairdocs.org/sdr/DLL14990670), Mar 26, 1999: FIRE WIRE. CHAFED. INTERMITTENT FIRE WARNING A LOOP NR 2 ENG OCCURRED AFTER T/O AT 1500 FT AGL, EPR 1.631 OAT 11 DEG C. NR 2 IDG DISCONNECTED, HYD PUMPS B1 C1 UNLATCHED, NO FIRE. - [SDR DLL14981832](https://openairdocs.org/sdr/DLL14981832), Sep 3, 1998: FRAME. CORRODED. THE FWD GALLEY DOORWAY FRAME WAS CORRODED NEAR THE LOWER SILL AT STR 25. THE DAMAGE WAS REMOVED AND A REPAIR SECTION SPLICED IN. - [SDR DLL14981830](https://openairdocs.org/sdr/DLL14981830), Sep 3, 1998: DECK. CRACKED. THE NOSE LANDING GEAR PRESSURE DECK WAS FOUND CRACKED IN SIX LOCATIONS AT LBL 24 AND RBL 24 BETWEEN STA 395 AND 437. DOUBLER/TRIPLER REPAIRS ARE INSTALLED. - [SDR DLL14981829](https://openairdocs.org/sdr/DLL14981829), Sep 3, 1998: DECK. CRACKED. THE FUSELAGE HORIZONTAL PRESSURE DECK WAS FOUND CRACKED AT RBL 102 AND FS 380. A DOUBLER/TRIPLER REPAIR WAS ACCOMPLISHED. - [SDR DLL14981828](https://openairdocs.org/sdr/DLL14981828), Sep 3, 1998: RIB. CRACKED. THE RT WING IWS 503 RIB UPPER CAP, LT WING IWS 555 RIB UPPER CAP WERE BOTH FOUND CRACKED. ALL CRACKED PARTS WERE REPLACED. - [SDR DLL14981827](https://openairdocs.org/sdr/DLL14981827), Sep 1, 1998: BULKHEAD FITTING. CRACKED. THE RT WING PYLON BACKUP FITTING BULKHEAD WAS FOUND CRACKED. A DOUBLER REPAIR IS INSTALLED. - [SDR DLL14981575](https://openairdocs.org/sdr/DLL14981575), Jul 26, 1998: CABLE. BROKEN. L-3 DOOR TRACK LOCK PIN MECHANISM CABLE BROKEN UNABLE TO ACCOPMPLISH EMERGENCY OPS CHECK INSIDE AND OUTSIDE HANDLES. REPLACED CABLE. - [SDR DLL14991489](https://openairdocs.org/sdr/DLL14991489), Jul 1, 1998: PS2 LINE. LEAKING. NACELLE NR 2 OVERHEAT ILLUMINATED ALONG WITH NR 2 ENG NAC/PYLON OVERHEAT, A & B ILLUMINATED. FOUND PRSOV PS2 LINE LEAKING. REPLACED LINE AND LEAK CHECKED. PERFO - [SDR DLL14980946](https://openairdocs.org/sdr/DLL14980946), May 2, 1998: BULB. FAILED. EXTERIOR EMERGENCY LIGHT AT R-4 DOOR INOP. RELAMPED. - [SDR DLL14980516](https://openairdocs.org/sdr/DLL14980516), Mar 4, 1998: POWER SUPPLY. INOPERATIVE. EMERGENCY TRACK LIGHTING OUT AFTER 20 SEC IN F/C CABIN. REPLACED POWER SUPPLY. - [SDR DLL14972163](https://openairdocs.org/sdr/DLL14972163), Oct 26, 1997: WINDSHIELD. DEFECTIVE. SMOKE SMELL DETECTED IN THE COCKPIT WHILE EN ROUTE. SMOKE IDENT AND REMOVAL CHECKLIST IN THE POM WAS INITIATED. PART WAY THROUGH CHECKLIST SMOKE WAS VISUALLY DE - [SDR DLL14971396](https://openairdocs.org/sdr/DLL14971396), Jul 16, 1997: LIGHTS. OVERHEATED. GOT STRONG SMELL THROUGH OUT CABIN WENT AWAY CAME BACK AS A/C TAXIED TO GATE. FOUND O/V HEAD LIGHTS AT MID GALLEY PLASTIC CLAMP WERE BURNT REPLACED ALL 6 LIGHT - [SDR DLL14962233](https://openairdocs.org/sdr/DLL14962233), Oct 6, 1996: LIGHT. INOPERATIVE. ON LAYOVER, FOUND EMERGENCY LIGHT POWER SUPPLY AT 3R INOP. - [SDR DLL14961958](https://openairdocs.org/sdr/DLL14961958), Aug 23, 1996: BATTERY. FAILED. BATTERY CONDITION LIGHT CAME ON 3.5 HRS INTO FLT. NO AVIONIC OVERBOARD LIGHTS ON. CYCLED BATTERY CHARGER, C/B DID NOT CORRECT SITUATION. BATTERY CONDITION LIGHT - [SDR DLL14961857](https://openairdocs.org/sdr/DLL14961857), Aug 8, 1996: TRACK. DAMAGED. EMERGENCY LIGHT TRACK AT MID GALLEY DAMAGED. REPLACED SECTION OF EMERGENCY LIGHT TRACK, CHECKS GOOD. - [SDR DLL14960383](https://openairdocs.org/sdr/DLL14960383), Feb 20, 1996: RETAINING RING. SHEARED. LT LANDING GEAR TRUCK POSITION CYLINDER PISTON RETAINING RING HAD SHEARED FROM THE THREADED PORTION. LOST C-SYSTEM HYDRAULICS ON LANDING, CAUSED AUTO GROUND SPO - [SDR DLL14954714](https://openairdocs.org/sdr/DLL14954714), Dec 16, 1995: EEL POWER SUPPLY. INOPERATIVE. ON LAYOVER, FOUND EMERGENCY LIGHTS IN LOWER GALLEY INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY. CHECKS GOOD. - [SDR DLL14954407](https://openairdocs.org/sdr/DLL14954407), Nov 16, 1995: EEL LENS. MISSING. EXIT LIGHT LENS ON FWD SIDE OF FIRST CLASS GALLEY RIGHT SIDE MISSING. REPLACED LENS, LIGHT OP CHECKS NORMAL. ## FAA accident and incident reports (4) 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 19971211040569I](https://openairdocs.org/incident/19971211040569I), Dec 11, 1997: Lkheed 10113851 (N741DA), San Francisco, CA. Capt pitot heat failed. Both fms's failed. Lost rudder hydraulic limiter and mach feel. Landed overweight. - [Incident 19971026035459I](https://openairdocs.org/incident/19971026035459I), Oct 26, 1997: N741DA, Kansas City, MO. Narrative: on 10/26/97 delta airlines, inc. (dala) flight 571 departed cvg enroute to slc. The flight crew reported smoke coming from the L-1 window heat… - [Incident 19881129067249I](https://openairdocs.org/incident/19881129067249I), Nov 29, 1988: Lkheed 10113851 (N741DA), Covington - Cin, OH. Left main gear departed taxiway after exiting runway and became stuck in the mud. - [Incident 19850120002419I](https://openairdocs.org/incident/19850120002419I), Jan 20, 1985: Lkheed 10113851 (N741DA), Chicago, IL. On landing roll engine flamed out. Shutdown, discharged fire bottles. Result no pneumatic system configuration. --- 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.