# N720DA: 1976 Lockheed L-1011-385-1, registration cancelled 2013-06-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 13, 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 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-1136
- Year built: 1976
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 1994
- Last registry action: July 20, 2004
- Mode S code: A9A3D8
- 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/N720DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=720DA
- Page: https://openairdocs.org/deregistered/N720DA-2013-06-13

From the FAA registry file of October 28, 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 (42)

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

- [SDR DLL10992431](https://openairdocs.org/sdr/DLL10992431), Nov 3, 1999: THROTTLE. WORN. WHILE IN CRUISE NR 2 ENGINE POWER DECREASED AS THROTTLE WAS IN STATIONARY POSITION DURING APPROACH AT FL 100 THROTTLE WAS RETURNED TO IDLE STOP, BUT FUEL FLOW R
- [SDR DLL10992155](https://openairdocs.org/sdr/DLL10992155), Sep 24, 1999: STRINGER. CRACKED. THE LBL 25.5 KEELSON STRINGER WAS FOUND WITH A 1.5 INCH LONG CRACK RUNNING FWD-AFT IN THE HORIZONTAL FLANGE AT FS 1357. THE STRINGER WAS CUT AT FS 1357 AND THE 
- [SDR DLL10992016](https://openairdocs.org/sdr/DLL10992016), Sep 10, 1999: AIR DIST. ODOR. AFTER TAKEOFF ATL, A VERY NOXIOUS ODOR CAME FROM THE AIR CONDITIONING SYSTEM IT SET OFF THE AFT SMOKE DET IN AFT LAVS. ODOR REDUCED AND SEEMED SPENT AS A/C PRES
- [SDR DLL10991443](https://openairdocs.org/sdr/DLL10991443), Jun 27, 1999: SEAL. FAILED. DURING FLT, USUALLY AT REDUCED POWER, CABIN FILLED WITH A BLUE HAZE AND LAV SMOKE DETECTORS IN FWD AND AFT LAVS WENT OFF FOR SEVERAL MINUTES. REPLACED NR 3 ENGI
- [SDR DLL10990563](https://openairdocs.org/sdr/DLL10990563), Mar 11, 1999: SKIN. CRACKED. A CRACK WAS FOUND IN SKIN ASSY OF THE UPPER FORWARD CORNER OF THE L3 DOOR CUTOUT. THE CRACK IS IN THE SKIN, DOOR SURROUND DOUBLER, AND TRIPLER. THE SKIN ASSY WA
- [SDR DLL10990550](https://openairdocs.org/sdr/DLL10990550), Mar 11, 1999: SKIN. CRACKED. THE UPPER AFT CORNER OF THE R1 DOOR CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE SKIN ASSY AND TRIPLER. THE AREA WAS X-RAYED TO DETERMINE THE EXACT END OF THE C
- [SDR DLL10982623](https://openairdocs.org/sdr/DLL10982623), Dec 25, 1998: HYD LINE. BROKEN. AFTER TAKEOFF, COULD NOT RETRACT LANDING GEAR ALSO GOT TRUCK LIGHT ON, PERFORMED POM PROCEDURES AND RETUNED TO AIRPORT. MTC FOUND HYD FUSE SET AND FLEX LINE ON 
- [SDR DLL10981625](https://openairdocs.org/sdr/DLL10981625), Aug 8, 1998: POWER SUPPLY. INOPERATIVE. EMERGENCY EXTERIOR LIGHTS INOP LEFT FWD. REPLACED BATTERY AND PWR SUPPLY, SYS NOW CKS OK.
- [SDR DLL10980740](https://openairdocs.org/sdr/DLL10980740), Apr 5, 1998: GEARBOX. FAILED. BEGINNING DESCENT, -A- SYSTEM PRESSURE 0, QUANTITY REMAINED. IDG LOW OIL PRESSURE LIGHT ON, GEN DISCONNECTED. DISCONNECTED IDG. ON APPROACH NR 1 OIL QTY DROPPED
- [SDR DLL10980683](https://openairdocs.org/sdr/DLL10980683), Mar 28, 1998: SKIN. CORRODED. THE FUSELAGE SKIN AT FS 759 AND STRINGER 38 WAS FOUND CRACKED DUE TO CORROSION. THE CORRODED AREA WAS TRIMMED OUT AND AN EXTERNAL ALUMINUM DOUBLER WAS INSTALLED
- [SDR DLL10980685](https://openairdocs.org/sdr/DLL10980685), Mar 27, 1998: SKIN. CRACKED. THE LT LOWER WING SKIN WAS FOUND CRACKED AT IWS 477 AND STRINGER 17. THE CRACK IS SUBJECT TO THE SID AD 95-20-04. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A
- [SDR DLL10980672](https://openairdocs.org/sdr/DLL10980672), Mar 27, 1998: COUNTERBALANCE. BROKEN. R-4 DOOR DOES NOT OPEN WHEN USING EMERGENCY HANDLE. ITEM FOUND DURING E-LETTER CHECK INITIAL INSP, OPN 58131. ITEM CLEARED BY REPLACING DR COUNTERBALANCE. OPS C
- [SDR DLL10980481](https://openairdocs.org/sdr/DLL10980481), Feb 26, 1998: POWER SUPPLY. INOPERATIVE. COCKPIT AND L1 DOOR EMERG EXIT SIGNS INOP. REPLACED POWER SUPPLY UNIT, CKD NML.
- [SDR DLL10980359](https://openairdocs.org/sdr/DLL10980359), Feb 10, 1998: LIGHT. BROKEN. EMERGENCY LIGHT STRIP AT MID GALLEY CROSS-AISLE INOP. REPAIRED BROKEN WIRE AT SPLICE.
- [SDR DLL10972043](https://openairdocs.org/sdr/DLL10972043), Oct 11, 1997: CIRCUIT BOARD. BROKEN. EMERGENCY EXIT SIGN LIGHT INOP. FOUND TERMINAL POST ON LIGHT CIRCUIT BOARD BROKEN LOOSE ON EMERGENCY EXIT SIGN.
- [SDR DLL10971289](https://openairdocs.org/sdr/DLL10971289), Jul 3, 1997: PROX CARD. INOPERATIVE. AFTER GEAR RETRACTION, THE RED IN TRANSIT LIGHT ALONG WITH THE LEFT GEAR DOOR LIGHT ON S/O PANEL ILLUMINATED. ACCOMPLISHED POM PROCEDURES LIGHTS REMAINED ILLUMI
- [SDR DLL10971068](https://openairdocs.org/sdr/DLL10971068), Jun 2, 1997: CONTROL VALVE. CRACKED. UPON LOWERING GEAR HANDLE LOST C-SYSTEM PRESSURE AND FLUID TO BELOW HALF. APPLIED BRAKES AT 120 KNOTS. REPLACED CRACKED C-SYSTEM LEFT MAIN PHASE CONTROL VALVE. 
- [SDR DLL10970686](https://openairdocs.org/sdr/DLL10970686), Apr 11, 1997: SKIN. CRACKED. LT UPPER WING SKIN FOUND CRACKED OVER THE IWS 319.8 RIB JUST FWD OF THE REAR SPAR. THE CRACK IS APPROX 1.5 LONG AND RUNS DIAGONALLY THROUGH A RIB SHEAR CLIP ATT
- [SDR DLL10970284](https://openairdocs.org/sdr/DLL10970284), Feb 15, 1997: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT POWER SUPPLY AT L4 DOOR INOP.
- [SDR DLL10970169](https://openairdocs.org/sdr/DLL10970169), Dec 23, 1996: BULKHEAD WEB. CRACKED. BS 1212 BULKHEAD WEB FOUND CRACKED AT RBL 6. CRACK IS 2 INCHES. THE RBL 6 LOCATION REQUIRES A CHANGE TO THE DOUBLER PROFILE TO ACCOMMODATE A CABLE PASS-THROUGH.
- [SDR DLL10961535](https://openairdocs.org/sdr/DLL10961535), Jun 26, 1996: PBE. BUTTON POPPED. PBE IN LOWER GALLEY HAS BUTTON POPPED. REPLACED PBE, OK FOR SERVICE.
- [SDR DLL10961169](https://openairdocs.org/sdr/DLL10961169), May 7, 1996: LOWER SILL. CORROSION. CORROSION WAS FOUND ON THE C2 DOOR SURROUND LOWER SILL OUTER CAP STA 1625. THE CORROSION WAS CUT OUT, FILLED AND REINFORCED, REV A ADDS FAA APPROVAL.
- [SDR DLL10961101](https://openairdocs.org/sdr/DLL10961101), May 6, 1996: SKIN. DENTED. A DENT WAS DISCOVERED AT FS 189 LBL 30.6. THE DENT WAS CUT OUT, FILLED AND REINFORCED.
- [SDR DLL10961100](https://openairdocs.org/sdr/DLL10961100), May 6, 1996: SKIN. DENTED. AT FS 717 AND 719 BETWEEN STRINGERS 23 AND 24, TWO DENTS WERE FOUND JUST AFT OF THE LOWER AFT CORNER OF THE C-1 CARGO DOOR. THE DENTS WERE CUT OUT, FILLED AND R
- [SDR DLL10961139](https://openairdocs.org/sdr/DLL10961139), Apr 22, 1996: RIB CAPS. CRACKED. THE RT WING IWS 503 RIB UPPER AND LOWER CAPS HAVE CRACKS IN THE TYPICAL LOCATION AT THE ATTACH TABS. THE CAPS ARE TO BE REPLACED PER EO 7-59208-3AD, BUT THE COM
- [SDR DLL10961137](https://openairdocs.org/sdr/DLL10961137), Apr 22, 1996: SKIN. DENTED. THE SKIN SECTION BETWEEN FS 158 AND 267 AT WL 198 WAS FOUND TO HAVE FURTHER DAMAGE THAN THAT WHICH WAS REPAIRED BY ER/A 266918-14. THE NEW DAMAGE CONSISTED OF S
- [SDR DLL10961138](https://openairdocs.org/sdr/DLL10961138), Apr 18, 1996: SKIN. CORROSION. THE FUSELAGE SKIN BETWEEN FS 887, 940 AND STR 42 AND 2 BELOW STR 40 REQUIRES REPLACEMENT, REV B TO ER/A PROVIDES FAA APPROVAL.
- [SDR DLL10960969](https://openairdocs.org/sdr/DLL10960969), Apr 15, 1996: ACT ATTACH FTG. CORROSION. THE LEFT MLG ATTACH RIB FITTING WAS CORRODED AT THE MLG RETRACT ACTUATOR ATTACH FITTING LOCATION. THE DAMAGE WAS CLEANED UP AND INSPECTED PER DL ERA 273650-14.
- [SDR DLL10960593](https://openairdocs.org/sdr/DLL10960593), Mar 16, 1996: POWER SUPPLY. INOPERATIVE. BLINKING AMBER LIGHT ON LOWER GALLEY EMERGENCY LIGHT POWER SUPPLY. REPLACED POWER SUPPLY, OPERATION NORMAL.
- [SDR DLL10960240](https://openairdocs.org/sdr/DLL10960240), Jan 23, 1996: WEB. CRACKED. AT LAYOVER IN ATL WHILE PERFORMING SI 7-70645-12, THE FS 1212 CANTED BULKHEAD WAS FOUND WITH VERTICAL CRACKS AT RBL 22.5 LBL 10 AND LBL 30. THEY MEASURE 9, 8 AN
- [SDR DLL10954124](https://openairdocs.org/sdr/DLL10954124), Oct 27, 1995: BULB. FAILED. EMERGENCY PATH LIGHT AT SEAT 23HJ IS BROKEN. REPLACED LAMP HOLDER AND BULB, CKS GOOD.
- [SDR DLL10953966](https://openairdocs.org/sdr/DLL10953966), Oct 11, 1995: COWL. CRACKED. NR 2 ENGINE LOWER LT HINGED COWL, 6 INCH CRACK IN LOWER EDGE OF COWL, AFT OF 2ND LATCH FROM FORWARD EDGE. REPAIRED PER SRM 51-50-02 PAGE 3.
- [SDR DLL10953851](https://openairdocs.org/sdr/DLL10953851), Sep 28, 1995: EEL POWER PACK. INOPERATIVE. DURING L/O CK, FOUND EMERGENCY LIGHTS OUT AT MID GALLEY, CROSS AISLE. REPLACED POWER PACK PS9.
- [SDR DLL10953645](https://openairdocs.org/sdr/DLL10953645), Aug 31, 1995: FITTING. CRACKED. COMPLYING WITH INSPECTION SI 7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTINGS CRACKED AT STRINGERS NR 8, 10 AND 58. THE FITTINGS WERE S
- [SDR DLL10953166](https://openairdocs.org/sdr/DLL10953166), Jul 6, 1995: TORQUE TUBE. CORROSION. HORIZONTAL STABILIZER RT UPPER TORQUE TUBE SUPPORT BRACKET WAS FOUND WITH CORROSION ON THE LWR SURFACE OF THE UPPER LUG. CORROSION DOES NOT EXTEND INTO THE PART
- [SDR DLL10953103](https://openairdocs.org/sdr/DLL10953103), Jul 6, 1995: FITTING. CORRODED. AT LETTER CHECK ATL, FOUND SUPPORT FITTINGS ON THE GALLEY DOOR WERE CORRODED. THE FITTINGS WERE REPLACED IN ACCORDANCE WITH FAA FORM 8110-3, DATED 07-06-95 TO A
- [SDR DLL10953002](https://openairdocs.org/sdr/DLL10953002), Jun 29, 1995: BLKHD FRAME. CRACKED. AT B-LETTER CHECK, FOUND BULKHEAD FRAME CRACKED, AT FS 1363 HORZ LEG LT SIDE WL160. REPAIRED PER SRM 53-11-00, PG 932-933
- [SDR DLL10952920](https://openairdocs.org/sdr/DLL10952920), Jun 27, 1995: TRUNNION FTG. CORROSION. OUTBOARD SIDE OF RT TRUNNION FITTING WEB WAS FOUND WITH NUMEROUS AREAS OF SURFACE RUST. REPAIRED PER SRM 51-21-01.
- [SDR DLL10952905](https://openairdocs.org/sdr/DLL10952905), Jun 27, 1995: FORMER. CRACKED. FLOOR PANEL SUPPORT RAIL CRACKED IN RADIUS AT STA 1163 FORMER LBL 104. REPAIRED PER SRM 53-21-00.
- [SDR DLL10952884](https://openairdocs.org/sdr/DLL10952884), Jun 27, 1995: FRONT SPAR. CRACKED. LT ELEV, FRONT SPAR CRACKED THROUGH BOTH LAYERS OF SKIN AT LIGHTENING HOLE, JUST INBD OF NR 8 ELEV HINGE. REMOVED REPAIR SECTION OF WEB, FABRICATED NEW WEB PIEC
- [SDR DLL10952835](https://openairdocs.org/sdr/DLL10952835), Jun 27, 1995: SUPPORT. CRACKED. FLOOR PANEL SUPPORT RAIL CRACKED IN RADIUS AT STA 1163 FORMER, LBL 104. REPAIRED PER SRM 53-21-00.
- [SDR DLL10950041](https://openairdocs.org/sdr/DLL10950041), Jan 4, 1995: SWITCH. BURNED. DURING DESCENT, CAPTAIN TURNED ON OVERHEAD PANEL AND EYE BROW PANEL LIGHTS AND A BURNING ODOR WAS NOTICED. AFTER LANDING INSPECTION, DISCOVERED THE RIGHT WING L

## 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 ATL87FA240](https://openairdocs.org/ntsb/ATL87FA240), Aug 25, 1987: Lockheed L-1011-385-1 (N720DA), Atlanta, GA, substantial damage
- [NTSB MIA78DA096](https://openairdocs.org/ntsb/MIA78DA096), Jun 11, 1978: Lockheed L-1011 (N720DA), Atlanta, GA, no damage

## 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 19940814033089I](https://openairdocs.org/incident/19940814033089I), Aug 14, 1994: Lkheed 10113851 (N720DA), Dallas-Ft Worth, TX. Turned off on high speed taxiway. Missed turn off taxiway onto asphalt. Wheel broke thru and stopped aircraft.
- [Accident 19870825052189A](https://openairdocs.org/incident/19870825052189A), Aug 25, 1987: Lkheed 10113851 (N720DA), Atlanta, GA, Substantial damage. Unstabilized approach and late leveloff caused aircrafts tail to hit runway on touchdown.
- [Incident 19830221007679I](https://openairdocs.org/incident/19830221007679I), Feb 21, 1983: Lkheed 10113851 (N720DA), Boston, MA. Pilot had high vibration and overheat light on #3 engine came on. Returned. Found faulty vibration harness.
- [Incident 19790611014999I](https://openairdocs.org/incident/19790611014999I), Jun 11, 1979: Lkheed 10113851 (N720DA), Ft Lauderdale, FL. Aircrafft hijacked while en route to Ft Lauderdale, ordered to cuba. Flight fueled and returned.
- [Incident 19781101023879I](https://openairdocs.org/incident/19781101023879I), Nov 1, 1978: Lkheed 1011/ (N720DA), Dallas, TX. Engine failed during climb. Found metal in tail pipe, replaced engine.

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