# N721DA: 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-1139
- Year built: 1976
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 20, 1976
- Last registry action: July 20, 2004
- Mode S code: A9A78F
- 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/N721DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=721DA
- Page: https://openairdocs.org/deregistered/N721DA-2013-02-20

From the FAA registry file of November 4, 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 (153, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DLL10991068](https://openairdocs.org/sdr/DLL10991068), May 15, 1999: BULB. FAILED. TWO EMERGENCY LIGHTS INOP FIRST CLASS LT TRACK. REPLACED BULBS AND HOLDER.
- [SDR DLL10990844](https://openairdocs.org/sdr/DLL10990844), Apr 16, 1999: SMOKE GOGGLES. CRACKED. FAA - SMOKE GOGGLES AT THREE LOCATIONS FOUND WITH CRACKS. LENS CRACKED FROM NOSE BRIDGE TO TOP. LENS CRACKED FROM NOSE BRIDGE UP FOR 1 INCH. LENS CRACKED FROM N
- [SDR DLL10990305](https://openairdocs.org/sdr/DLL10990305), Feb 11, 1999: BULKHEAD CAP. CRACKED. FUSELAGE BULKHEAD FS 1363 LOWER CAP, LBL 91.5, REPAIR FOR CRACK. THE LOWER CAP OF THE FS 13636 BULKEAD WAS FOUND WITH A CRACK THROUGH THE HORIZONTAL FLANGE EXTE
- [SDR DLL10982013](https://openairdocs.org/sdr/DLL10982013), Sep 29, 1998: CONNECTOR. CORRODED. NR 3 ENG FIRE INDICATION IN FLIGHT, POM PROCEDURE COMPLIED WITH. BOTH BOTTLES FIRED, CIRCUIT WOULD NOT TEST. REPLACED UPPER GAS GENERATOR AND AFT GEARBOX LOOP C
- [SDR DLL10981266](https://openairdocs.org/sdr/DLL10981266), Jun 15, 1998: PROJECTOR. INOPERATIVE. STRONG ODOR LIKE ELECTRICAL BURNING BETWEEN FIRST CLASS AND COACH NO SMOKE NOTICED PER CREW REPORTS APPROX 10 MIN. AFTER MOVIE STARTED B ZONE PROJECTOR INOP WIT
- [SDR DLL10981275](https://openairdocs.org/sdr/DLL10981275), Jun 14, 1998: SKIN. CORRODED. FUSELAGE SKIN FS 1693 STRG 38 : REPAIR FOR CORROSION CUTOUT. THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 1693 AND STRG 38. THE DAMAGED SKIN WAS CUTOUT OVER A 3.1
- [SDR DLL10980921](https://openairdocs.org/sdr/DLL10980921), Apr 24, 1998: SKIN. CRACKED. FOUR FASTENER HOLES IN THE LOWER WING SKIN AT IWS 477 AND STRINGER 17 WERE FOUND CRACKED ON BOTH WINGS. THE CRACKS ARE THE SUBJECT OF SID AD 95-20-04, R1 (SID N
- [SDR DLL10980896](https://openairdocs.org/sdr/DLL10980896), Apr 24, 1998: SPAR WEB. CRACKED. WING LT, REAR SPAR WEB, OWS 77 LOWER CAP ATTACHMENT, REPAIR FOR WEB CRACK. THE LT WING REAR SPAR WEB WAS FOUND WITH A .50 LONG CRACK EMANATING FROM A FASTENER H
- [SDR DLL10980561](https://openairdocs.org/sdr/DLL10980561), Mar 11, 1998: BATTERY PACK. DISCHARGED. EMERGENCY EXIT SIGN AT 3-R DOOR STOP ILLUMINATION AFTER TWO MINUTES. REPLACED BATTERY PACK, CHECKS OK.
- [SDR DLL10980560](https://openairdocs.org/sdr/DLL10980560), Mar 11, 1998: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS DO NOT ILLUMINATE 16A/B AND 22H/J/ RT GALLEY LIFT AND LOWER GALLEY. REPLACED BATTERY PACK CHECKS OK.
- [SDR DLL10972492](https://openairdocs.org/sdr/DLL10972492), Nov 28, 1997: CONNECTOR. DIRTY. NR 2 ENG FIRE LOOP -A- FLICKERED SWITCHED TO -B- LOOP, 3 MIN LATER -B- LOOP CAME ON STEADY SHUT ENG DOWN, FIRED ONE BOTTLE-B- LOOP ON AT GATE. REPLACED FIRE DET
- [SDR DLL10971911](https://openairdocs.org/sdr/DLL10971911), Sep 28, 1997: BATTERY PACK. DISCHARGED. FOUND ON L/O AFT EMERGENCY TRACK LIGHTS INOP. REPLACED AFT BATTERY PACK OP CKS NORMAL.
- [SDR DLL10970691](https://openairdocs.org/sdr/DLL10970691), Mar 27, 1997: SKIN. CORROSION. THE FUSELAGE LT SIDE LOWER BELLY SKIN WAS FOUND CORRODED JUST OUTBOARD OF THE LOWER CENTERLINE AT STRINGER 33 AFT OF FS 464. REMOVAL OF ALL CORROSION RESULTS IN
- [SDR DLL10970168](https://openairdocs.org/sdr/DLL10970168), Dec 18, 1996: BULKHEAD CAP. CRACKED. FS 449 BULKHEAD FOUND CRACKED IN HORIZONTAL FLANGE OF THE CAP. THE LOCATION IS FBL 19 AND EXTENDS FROM THE FORWARD EDGE, THROUGH AN EXISTING SEAL RETAINER HOLE,
- [SDR DLL10962601](https://openairdocs.org/sdr/DLL10962601), Nov 28, 1996: POWER PACK. INOPERATIVE. DURING L/O CK, FOUND EMERGENCY LIGHTS INOP AT L-1 CABIN DOOR. REPLACED POWER PACK AT L-1 DOOR, OPS CKS OK.
- [SDR DLL10961478](https://openairdocs.org/sdr/DLL10961478), Jun 6, 1996: FRAME. CRACKED. DURING LETTER CHECK, CRACKS WERE FOUND AT WL 280.6. THE CRACKS WERE REPAIRED PER SI 7-69003-12AD.
- [SDR DLL10961477](https://openairdocs.org/sdr/DLL10961477), Jun 6, 1996: SKIN. CRACKED. DURING LETTER CHECK, THE LOWER WING SKIN ON THE RT WING AT STR 18 RUNOUT WAS FOUND CRACKED. CRACK WAS REPAIRED PER DAL EO 7-70043-3.
- [SDR DLL10960403](https://openairdocs.org/sdr/DLL10960403), Feb 17, 1996: FLT CONTROLS. LACK OF LUBE. AIRCRAFT HARD TO ROLL RIGHT, BUT ROLLS NORMAL BACK TO THE LEFT. TURNING OFF B-AILERON SERVO INBD, CAUSED UNCOMMANDED HARD LEFT ROLL. INSPECTION OF FLT CONTROL S
- [SDR DLL10960048](https://openairdocs.org/sdr/DLL10960048), Jan 7, 1996: LIGHT. MISSING. EMERGENCY LIGHT MISSING AT SEAT 1CD. RELAMPED AND REPLACED, CHECKS GOOD.
- [SDR DLL10954605](https://openairdocs.org/sdr/DLL10954605), Dec 2, 1995: HYD LINE. LEAKING. C-SYSTEM HYD QUANTITY DECREASED TO BELOW HALF FULL. TURNED OFF C-SYS PUMPS. FOUND LINE ABOVE C-SYSTEM RETURN FILTER LEAKING. REPLACED LINE, OPERATION NORMAL.
- [SDR DLL10954456](https://openairdocs.org/sdr/DLL10954456), Nov 21, 1995: ROLLER/BRACKET. MISSING. ON TAKEOFF, FLAPS DID NOT COME UP BEYOND 8 DEGREES, RETURNED ATL. FOUND NR 3 RT FLAP IB ACTUATING ROLLER AND BRACKET MISSING. REPLACED ROLLER AND BRACKET INSTAL
- [SDR DLL10954420](https://openairdocs.org/sdr/DLL10954420), Nov 16, 1995: DUCT. RUPTURED. AT FL 370 HEARD LOUD BANG, POSSIBLY PNEU IN NATURE. CABIN PRESSURE NORMAL, ENGINE BLD CONT PANEL PSIG NORMAL. SUBSEQUENTLY C/D ZONES TURNED ICE COLD, WAS ABLE T
- [SDR DLL10953619](https://openairdocs.org/sdr/DLL10953619), Sep 5, 1995: STRINGER SPLICE. CRACKED. THE AFT PRESSURE BULKHEAD STRINGER SPLICE FITTING PER SI 7- 66332-12 AT STR 58 FITTING, WAS FOUND TO BE CRACKED. THE FITTING WILL BE RELEASED ON A TIME LIMITED 
- [SDR DLL10953618](https://openairdocs.org/sdr/DLL10953618), Sep 5, 1995: STRINGER SPLICE. CRACKED. DURING ACCOMPLISHMENT OF AN INSPECTION OF THE AFT P-DOME STR SPLICE FITTING PER SI 7-66332-12 AND VA 30620, STRINGER 10 FITTING WAS FOUND TO BE CRACKED. THE SUB
- [SDR DLL10953242](https://openairdocs.org/sdr/DLL10953242), Jul 11, 1995: SKIN. CORROSION. THE FORWARD LOWER BELLY SKIN WAS FOUND WITH EXTENSIVE CORROSION BETWEEN FS 529 AND FS 983, STR 29 TO STR 42. ALSO, THERE ARE NUMEROUS EXISTING EXTERNAL REPAIRS 
- [SDR DLL10952902](https://openairdocs.org/sdr/DLL10952902), Jul 2, 1995: FAIL-SAFE STRAP. DISBONDED. FAIL-SAFE STRAP DISBONDED AT FS 1555 STR 36 TO 37 AND AT FS 1575 BTWEEN STR 40 TO 41, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 830.
- [SDR DLL10952901](https://openairdocs.org/sdr/DLL10952901), Jul 2, 1995: FAIL-SAFE STRAP. DISBONDED. FAIL-SAFE STRAPS DISBONDED AT FS 1565 TO 1585 STG 30 TO 29. FAIL-SAFE STRAPS DISBONDED AT FS 1615 STR 30 TO 29. FAIL-SAFE STRAPS DISBONDED AT FS 1575 STR 36 TO 
- [SDR DLL10952900](https://openairdocs.org/sdr/DLL10952900), Jul 2, 1995: FLOORBEAM. CORRODED. FLOOR SUPPORT CAP CORRODED C2 BB FS 1480 RBL 4. REPAIRED PER SRM 53-23-00 PG 803 TO 804, FOUND AT HMV.
- [SDR DLL10953244](https://openairdocs.org/sdr/DLL10953244), Jun 27, 1995: SKIN. CORROSION. FUSELAGE SKIN BETWEEN FS 1453 AND FS 1655 BETWEEN STR 24 AND STR 37 REQUIRES REPLACEMENT, DUE TO EXTENSIVE CORROSION AND NUMEROUS REPAIRS. ACCOMPLISHED REPAIRS 
- [SDR DLL10952783](https://openairdocs.org/sdr/DLL10952783), Jun 25, 1995: STRINGER. CORRODED. STRINGER 29 CORRODED FS 1475, FS 1523 TO 1545, FS 1585, FS 1565 TO 1585, FS 1585 TO 1605. FOUND AT HMV, CORROSION SAMPLE INSP. REPLACED STRINGER PER SRM 53-13-0
- [SDR DLL10953245](https://openairdocs.org/sdr/DLL10953245), Jun 22, 1995: SILL. CORROSION. C-2 DOOR SURROUND STRUCTURE LOWER SILL OUTER CAP WAS FOUND CORRODED ON THE OUTBOARD HORIZONTAL FLANGE OF THE CAP AT STATION 1625. ACCOMPLISHED REPAIRS PER DL ER
- [SDR DLL10953246](https://openairdocs.org/sdr/DLL10953246), Jun 21, 1995: SPAR CAP. CRACKED. THE CENTER WING FS 1163 INTERMEDIATE SPAR UPPER CAP HAS A CRACK IN THE FWD LEFT AND RIGHT OUTBOARD ENDS. ACCOMPLISHED REPAIRS PER DL ERA 271114-14.
- [SDR DLL10952736](https://openairdocs.org/sdr/DLL10952736), Jun 21, 1995: FLOORBEAM. CORRODED. FLOORBEAM AT STA 1523 CORRODED 0 BL TO 30 LBL. FOUND DURING HMV CORROSION INSP. REPAIRED PER SRM 53-23-00 FIG 802.
- [SDR DLL10952684](https://openairdocs.org/sdr/DLL10952684), Jun 19, 1995: STRINGER. CORRODED. STRINGER 39 CRACKED AND CORRODED AT FS 1770, FOUND AT HMV. SPLICED IN SECTION OF NEW STRINGER PER SRM 53-13-00 PG 806.
- [SDR DLL10953247](https://openairdocs.org/sdr/DLL10953247), Jun 14, 1995: TRIPLER. CRACKED. A CRACK WAS FOUND IN THE AFT EDGE OF THE R-1 DOOR SURROUND TRIPLER BELOW WL 220. ACCOMPLISHED REPAIRS PER DL ERA 271153-14.
- [SDR DLL10952838](https://openairdocs.org/sdr/DLL10952838), Jun 14, 1995: DOUBLER. CRACKED. DURING SHOP INSPECTION, A DOUBLER WAS FOUND TO BE CRACKED AT THE AFT EDGE OF THE ELEVATOR TIP. A REPAIR WAS INSTALLED PER SRM 55-22-00 FIG 802.
- [SDR DLL10952837](https://openairdocs.org/sdr/DLL10952837), Jun 14, 1995: RIBS. CRACKED. DURING HMV, SHOP INSPECTION, RT ELEVATOR WAS FOUND WITH CRACKING IN VERTICAL AND DIAGONAL TRUSS MEMBERS OF ELEVATOR RIBS. REPAIRS WERE ACCOMPLISHED PER L011 SB 
- [SDR DLL10952775](https://openairdocs.org/sdr/DLL10952775), Jun 14, 1995: L/E SKIN. CRACKED. DURING SHOP INSPECTION, A GOUGE AND CRACK WAS FOUND IN A LEADING EDGE PANEL OF THE RT ELEVATOR. REPAIRED PER SRM 55-22-00 FIG 802.
- [SDR DLL10952663](https://openairdocs.org/sdr/DLL10952663), Jun 14, 1995: FRAME. DOUBLE DRILLED. AT HMV, FUSELAGE FRAME FS 569 AT STR 36 AND FS 589 AT FS 33 FOUND WITH DOUBLE DRILLED HOLE. REPAIRED PER SRM 53-31-00 FIG 818.
- [SDR DLL10952623](https://openairdocs.org/sdr/DLL10952623), Jun 14, 1995: FRAME. DOUBLE DRILLED. AT HMV, FUSELAGE FRAME FS 629 AT STR 32 AND FS 649 AT STR 32 FOUND WITH DOUBLE DRILLED HOLE. ACCOMPLISHED REPAIR PER SRM 53-31-00.
- [SDR DLL10952667](https://openairdocs.org/sdr/DLL10952667), Jun 13, 1995: STRINGER. CRACKED. AT HMV, STR 39 FS 1750 CRACKED. REPAIRED PER SRM 53-13-00 FIG 804.
- [SDR DLL10952641](https://openairdocs.org/sdr/DLL10952641), Jun 13, 1995: STRINGER. MISDRILLED. AT HMV, STRINGER FOUND MISSDRILLED, STR 40 FS 690. ROUTED OUT DAMAGE, WITHIN LIMITS PER SRM 53-13-00 PG 801, TREATED AND PAINTED.
- [SDR DLL10952640](https://openairdocs.org/sdr/DLL10952640), Jun 13, 1995: TEAR STRAP. DISBONDED. AT HMV, TEAR STRAP DISBONDED FS 1750 BETWEEN STR 35 TO 36. PEELED BACK TEAR STRAP AND FOUND NO CORROSION. REPAIRED PER SRM 53-31-00 FIG 816 NOTE 6.
- [SDR DLL10954211](https://openairdocs.org/sdr/DLL10954211), Jun 12, 1995: REAR SPAR. OVERSIZED HOLES. DURING ACCOMPLISHMENT OF PART 5 OF EO 7-56199-3AD, HOLES WERE OVERSIZED IN SEVERAL LOCATIONS, DUE TO REMOVAL OF EXISTING LOOSE FORCE MATE BUSHINGS. WING REAR SP
- [SDR DLL10952720](https://openairdocs.org/sdr/DLL10952720), Jun 10, 1995: FLOOR BEAM. CORRODED. AT HMV, CORRODED FLOOR BEAM UNDER T-CAP 2 LT OF B/L 0.0 C-2 B/B STA 1545. REPAIRED PER SRM 53-23-00, FIG 802.
- [SDR DLL10952624](https://openairdocs.org/sdr/DLL10952624), Jun 8, 1995: TEAR STRAP. CORRODED. AT HMV, FUSELAGE SKIN TEAR STRAP WITH CORROSION AND DISBONDED AT FS 897 BETWEEN STRINGES 40, 41 AND 42. REPAIRED PER SRM 53-31-00 PG 830.
- [SDR DLL10953144](https://openairdocs.org/sdr/DLL10953144), Jun 6, 1995: FITTING. CRACKED. DURING ACCOMPLISHMENT OF THE FLAP VANE FITTING REWORK PER DELA S.I. 7-65988-12AD, THE NR 3 FLAP VANE INBOARD FITTING LUG WAS FOUND CRACKED. IN ACCORDANCE WITH A
- [SDR DLL10952487](https://openairdocs.org/sdr/DLL10952487), Jun 5, 1995: STRINGER. CRACKED. STRINGER 34 HAS CRACK JUST BELOW FORMER STA. 789. FOUND HMV. REPAIRED PER SRM 53-13-00. SPLICED IN NEW STRINGER SECTION.
- [SDR DLL10952475](https://openairdocs.org/sdr/DLL10952475), Jun 5, 1995: DOUBLER. DAMAGED. INTERNAL DOUBLER HAS 2 INCH CUT BETWEEN STRINGER 41 AND 42 FS 1363, FOUND DURING HMV. REPAIRED PER SRM 53-31-00 FIG 836.
- [SDR DLL10952474](https://openairdocs.org/sdr/DLL10952474), Jun 5, 1995: TEAR STRAP. DISBONDED. TEAR STRAP DISBONDED FS 1695 BETWEEN STRINGER 29 AND 30, FOUND AT HMV. REPAIRED PER SRM 53-31-00 FIG 804.

All 153: https://openairdocs.org/deregistered/N721DA-2013-02-20/reports.md

## NTSB investigations (2)

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 NYC92IA086](https://openairdocs.org/ntsb/NYC92IA086), Apr 23, 1992: Lockheed L-1011-385 (N721DA), Flushing, NY, incident, minor damage. Probable cause: THE CAPTAIN'S IMPROPER AIRCRAFT CONTROL WHICH RESULTED IN AN EXCESSIVE NOSEWHEEL RATE OF SINK AND SUBSEQUENT OVERLOAD FAILURE OF THE NOSE GEAR TIRES.
- [NTSB ATL89FA161](https://openairdocs.org/ntsb/ATL89FA161), Jun 16, 1989: Lockheed L1011-385-1 (N721DA), Jacks Creek, TN, no damage. Probable cause: FAILURE OF THE PASSENGERS TO REMAIN SEATED WITH THEIR SEAT BELTS FASTENED AS THE AIRPLANE ENCOUNTERED UNFORECAST SEVERE CLEAR AIR TURBULENCE.

## 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 19920620025369I](https://openairdocs.org/incident/19920620025369I), Jun 20, 1992: Lkheed 10113851 (N721DA), Los Angeles, CA. Captain experienced an illness. Flight engineer occupied left seat and assisted first officer. Landed safely.
- [Incident 19920423022529I](https://openairdocs.org/incident/19920423022529I), Apr 23, 1992: Lkheed 10113851 (N721DA), New York, NY, Minor damage. Pilot made a hard landing. Fire on nose wheel assembly. Airport closed.
- [Accident 19890616016959A](https://openairdocs.org/incident/19890616016959A), Jun 16, 1989: Lkheed 10113851 (N721DA), Jacks Creek, TN, Minor damage. Encountered severe turbulence in descent. Unbelted passengers injured. 14 miles from a thunderstorm.
- [Incident 19790620016029I](https://openairdocs.org/incident/19790620016029I), Jun 20, 1979: Lkheed 10113851 (N721DA), Boston, MA. Wheel transducer cap found missing. Replaced brake, tire and wheel, sensor, spacer and transducer
- [Incident 19780728036719I](https://openairdocs.org/incident/19780728036719I), Jul 28, 1978: Lkheed 1011/ (N721DA), Boston, MA. Tower advised of fire in center engine during pushback, returned to gate. No evidence of fire found.

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