# N718DA: 1974 Lockheed L-1011-385-1, registration cancelled 2005-06-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 13, 2005 - Exported to: Thailand - Status when cancelled: Valid registration - 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-1097 - Year built: 1974 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 24, 1974 - Certificate issued: February 10, 2005 - Last registry action: April 8, 2005 - Mode S code: A99A11 - Owner when cancelled: [Jet Midwest Inc](https://openairdocs.org/faa-owner/JET%20MIDWEST%20INC) - Location: [Kansas City, KS](https://openairdocs.org/faa-place/KS/Kansas%20City) - Owner type: Corporation - 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/N718DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=718DA - Page: https://openairdocs.org/deregistered/N718DA-2005-06-13 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 (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DLL10991808](https://openairdocs.org/sdr/DLL10991808), Aug 11, 1999: SKIN. CRACKED. WING LT UPPER SKIN, IWS 395, CRACK REPAIR. AN EXISTING CRACK IN THE LEFT UPPER WING SKIN AT IWS 395 PROGRESSED BEYOND THE ALLOWABLE SRM LIMIT. THE CRACK STARTED - [SDR DLL10991806](https://openairdocs.org/sdr/DLL10991806), Aug 11, 1999: SKIN. CRACKED. WING RT LOWER AFT SKIN IWS 425.7, STRINGER 3, CRACK REPAIR. THE LOWER AFT SKIN OF THE RT WING WAS FOUND WITH A 4.5 LONG CRACK AT THE STRINGER 3 RUNOUT AT IWS 42 - [SDR DLL10991805](https://openairdocs.org/sdr/DLL10991805), Aug 11, 1999: FRAME. CRACKED. FUSELAGE FRAME FS 1183, WL 280.6, CRACK REPAIR. A TYPICAL CRACK WAS FOUND IN THE FS 1183 FUSELAGE FRAME AT WL 280.6. THE CRACK WAS STOP DRILLED AND REPAIRED PER - [SDR DLL10991804](https://openairdocs.org/sdr/DLL10991804), Aug 11, 1999: FRAME. CRACKED. FUSELAGE FRAME FS 1645, STRINGER 14L, CRACK REPAIR. THE FS 1645 FRAME WAS FOUND WITH A TYPICAL CRACK AT WL 280.6 AND AN ADDITIONAL CRACK AT STRINGER 14L ABOVE T - [SDR DLL10991484](https://openairdocs.org/sdr/DLL10991484), Jun 29, 1999: BULKHEAD WEB. CRACKED. WHILE ACCOMPLISHING HFEC INSPECTIONS OF THE UPPER GORE WEB OF THE AFT P-DOME, A 2.5 INCH CRACK WAS FOUND IN THE WEB AT LBL 10. THE CRACK IS TYPICAL OF LAC S/B 0 - [SDR DLL10991136](https://openairdocs.org/sdr/DLL10991136), May 21, 1999: PANEL. CRACKED. CRACK IN SHEET METAL ON TOP OF LEFT WING SECOND CANOE FITTING OUTBOARD FROM WING ROOT. REPAIRED PER ERA OR SRM AS APPLICABLE. - [SDR DLL10991100](https://openairdocs.org/sdr/DLL10991100), May 18, 1999: FIRE LOOP. INOPERATIVE. NR 1 ENG LOOP A ON MCO, LOOP B FLICKERED THEN CAME ON STEADY. CREW SHUTDOWN NR 1 ENG PER POM. REPLACED UPPER GEARBOX LOOP. - [SDR DLL10990434](https://openairdocs.org/sdr/DLL10990434), Mar 2, 1999: BATTERY. DISCHARGED. F/C EMER LIGHTS INOP. REPLACED BATTERY PACK AND POWER SUPPLY. - [SDR DLL10982393](https://openairdocs.org/sdr/DLL10982393), Nov 18, 1998: POWER SUPPLY. INOP. LWR GALLEY EMER LIGHT INOP. REPLACED PWR SUPPLY, OP CK NORMAL. - [SDR DLL10981430](https://openairdocs.org/sdr/DLL10981430), Jul 9, 1998: CHIP DETECTOR. NOT INSTALLED. NR 1 ENG OIL LOSS IN EXCESS OF 4 QTS HR. DIVERTED SLC. ENG WAS NOT SHUTDOWN AND NO LOSS OF OIL PRESS. FOUND NR 1 ENG FINE SCAVAGE CHIP DET NOT IN HOUSING AND LA - [SDR DLL10981158](https://openairdocs.org/sdr/DLL10981158), May 31, 1998: LIGHT. INOPERATIVE. ON LAYOVER, FOUND FLASHLIGHT AT L-2 FLT ATTN SEAT INOP. RED IND NOT FLASHING. RELAMPED INDICATOR LIGHT. CKS OK. - [SDR DLL10980632](https://openairdocs.org/sdr/DLL10980632), Mar 22, 1998: LIGHT. INOPERATIVE. LOWER GALLEY LEFT SIDE EMERGENCY FLASHLIGHT INOP. FOUND MAGNET MISSING FROM HOLDER CAUSING LIGHT TO REMAIN ON WHEN STOWED. REPLACED HOLDER AND BATTERY. - [SDR DLL10980264](https://openairdocs.org/sdr/DLL10980264), Jan 30, 1998: BALLAST. FAILED. BURNING ELECTRICAL SMELL 1ST CLASS LAV CAPT'S SIDE. REPLACED BALLAST, CHECK NORMAL. - [SDR DLL10970636](https://openairdocs.org/sdr/DLL10970636), Apr 6, 1997: BULKHEAD WEB. CRACKED. DURING INSPECTION PER DAL EO 7-69959-12AD, THE FS 1363 BULKHEAD WEB SECTION I/B OF OF LBL 42.5 WAS FOUND WITH TWO CRACKS AT APPROX WL 133. THE SUBJECT WEB SECTI - [SDR DLL10961360](https://openairdocs.org/sdr/DLL10961360), Jun 4, 1996: LIGHT. INOPERATIVE. AFT CABIN EMERGENCY TRACK LIGHTS WILL NOT COME ON DURING TEST. FOUND FUSES BLOWN IN AFT RT CONTROL MODULE. REPLACED FUSES, TRACK LIGHTS CKS GOOD. - [SDR DLL10960786](https://openairdocs.org/sdr/DLL10960786), Apr 7, 1996: SEAL. TORN. LOUD BEATING NOISE ABOVE FWD CARGO DOOR AND LOUD AIR NOISE IN LOWER GALLEY. FLIGHT RETURNED TO ATL. FOUND SECTION OF C-1 DOOR SEAL BLOWN. REPLACED SECTION OF SE - [SDR DLL10960497](https://openairdocs.org/sdr/DLL10960497), Mar 5, 1996: CHIP DETECTOR. LEAKING. NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED - GAUGE SHOWED LOW OIL QUANTITY. ENGINE NR 1 SHUT DOWN IAW POM AND EMERG PROCEDURES ON FINAL APPROACH. N3 WENT TO - [SDR DLL10960335](https://openairdocs.org/sdr/DLL10960335), Feb 13, 1996: BULB. FAILED. FLIGHT ATTENDENT REPORTED IN CDL THAT THE EXIT SIGN BETWEEN FIRST CLASS AND COACH ON RIGHT SIDE OF CABIN INOP. RELAMPED, OPERATION NORMAL. - [SDR DLL10960197](https://openairdocs.org/sdr/DLL10960197), Jan 25, 1996: MACH FEEL WIRE. BROKEN. DURING CLIMB, NR 1 MACH FEEL FAIL LIGHT CAME ON, WOULD NOT RESET. THEN 30 MINS LATER, DURING CRUISE THE NR 2 MACH FEEL FAIL LIGHT CAME ON AND WOULD NOT RESET. R - [SDR DLL10954631](https://openairdocs.org/sdr/DLL10954631), Dec 6, 1995: EEL POWER SUPPLY. INOPERATIVE. L-2 DOOR EMERGENCY EXIT LIGHT POWER SUPPLY INOP. REPLACED SAME, OPERATION NORMAL. - [SDR DLL10954161](https://openairdocs.org/sdr/DLL10954161), Oct 27, 1995: ATTACH FITTING. CORROSION. RIGHT MLG ATTACH RIB FITTING WAS CORRODED AT THE MLG RETRACT ACTUATOR ATTACH FITTING LOCATION. ATTACH RIB UPPER AND LOWER ACTUATOR ATTACH PAD FASTENER HOLES WER - [SDR DLL10954500](https://openairdocs.org/sdr/DLL10954500), Oct 26, 1995: RIB TABS. CRACKED. THE RT/LT WINGS IWS 503 AND IWS 529 RIB UPPER/LWR CAP ATTACH TABS ARE CRACKED. ACCOMPLISHED REPAIRS PER DL ERA 272012-14AD. - [SDR DLL10961591](https://openairdocs.org/sdr/DLL10961591), Oct 18, 1995: STIFFENER. CRACKED. DURING HMV, THE NLG PRESSURE DECK INTEGRAL STIFFENER ALONG RBL 40 WAS FOUND CRACKED. THE CRACK WAS TRIMMED OUT AND A FILLER/DOUBLER REPAIR WAS INSTALLED. - [SDR DLL10954174](https://openairdocs.org/sdr/DLL10954174), Oct 6, 1995: RIB. CRACKED. THE RT WING IWS 503 RIB UPPER CAP ATTACH TAB IS CRACKED IN THE TYPICAL LOCATION BETWEEN STR 18 AND 19. ACCOMPLISHED REPAIRS PER DL ERA 272012-14AD. - [SDR DLL10954172](https://openairdocs.org/sdr/DLL10954172), Oct 6, 1995: RIB. CRACKED. THE LT WING IWS 555 RIB UPPER AND LOWER CAP WERE FOUND WITH CRACKS IN THE ATTACH TABS AT TYPICAL LOCATIONS. ACCOMPLISHED REPAIRS PER DL ERA 272011-14AD. - [SDR DLL10954177](https://openairdocs.org/sdr/DLL10954177), Oct 5, 1995: DECK. DENTED. THE PRESSURE DECK WAS FOUND DAMAGED AT FS 409 AND RBL 80 ON BOTH THE HORIZONTAL LEG AND THE LOWER SURFACE. THE DAMAGE WAS BLENDED OUT PER DL ERA 268387-14. - [SDR DLL10953994](https://openairdocs.org/sdr/DLL10953994), Sep 29, 1995: RIB. CRACKED. NR 6 L/E SLAT RIB CRACKED. REPAIRED PER SRM 57-51-00 FIG 812, FOUND AT LETTER CHECK. - [SDR DLL10953644](https://openairdocs.org/sdr/DLL10953644), Aug 31, 1995: FITTINGS. CRACKED. COMPLYING WITH DL INSPECTION SI7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTINGS AT STRINGERS NR 5, 10 AND 61 CRACKED. THE FITTINGS WERE - [SDR DLL10952494](https://openairdocs.org/sdr/DLL10952494), Jun 6, 1995: GEARBOX. FAILED. AT FLT LEVEL 330, NR 3 OIL PRESSURE WENT TO ZERO FOLLOWED BY LOSS OF THRUST. NR 3 ENG SHUT DOWN, OIL QTY AND TEMP NORMAL. FOUND NR 3 GEARBOX FAILED. REPLACED GE - [SDR DLL10960486](https://openairdocs.org/sdr/DLL10960486), May 12, 1995: BLKHD CAP. CRACKED. TWO CRACKS WERE FOUND IN BLKHD CAP AT LBL 42.5 AND 74.5. THE CRACKS ARE LOCATED IN THE VERTICAL BLKH ATTACH FLANGE AND EMANATES FROM FASTENER HOLES. THE CRACKS - [SDR DLL10952104](https://openairdocs.org/sdr/DLL10952104), May 6, 1995: STRINGER. DAMAGED. DURING SERVICE CHECK FOUND TOOLING DAMAGE ON STR 14 RT AT STA 1023. REPAIRED PER SRM 53-13-00 PG. 806. - [SDR DLL10950084](https://openairdocs.org/sdr/DLL10950084), Jan 2, 1995: FLAP VANE. CRACK. DURING SHOP INSPECTION, CRACKING WAS FOUND IN THE LEFT WING NR 3 FLAP VANE TOP SKIN DOUBLER AT 35 INCHES FROM THE INBOARD EDGE. INSTALLED SPLICED SKIN REPAIR PE ## 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 ATL92IA113](https://openairdocs.org/ntsb/ATL92IA113), Jun 2, 1992: Lockheed L-1011-1 (N718DA), Atlanta, GA, incident, no damage. Probable cause: THE OVERHEATING OF THE NUMBER 2 AIR CYCLE MACHINE WHICH RESULTED IN AN EMERGENCY EVACUATION VIA SLIDES; THE FAILURE OF THE FLIGHT ATTENDANTS TO SECURE THE SLIDE GIRT BARS. ## FAA accident and incident reports (6) 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 19960709022459I](https://openairdocs.org/incident/19960709022459I), Jul 9, 1996: Lkheed 10113851 (N718DA), Salt Lake City, UT. Narrative: delta flt 706, a Lockheed L-1011, N718DA, departed seattle int'l, WA at approx. 0830 PDT under VFR conditions. While enroute to atlanta, ga and… - [Incident 19920602021499I](https://openairdocs.org/incident/19920602021499I), Jun 2, 1992: Lkheed 10113851 (N718DA), Atlanta, GA. Smoke in cabin on climb. Returned. Landed safely. Evacuation. Some slides did not deploy. Air cycle machine faulty. - [Incident 19860331052889I](https://openairdocs.org/incident/19860331052889I), Mar 31, 1986: Lkheed 10113851 (N718DA), West Palm Beach, FL. During taxi after runup following an aborted takeoff the right gear left hard surface and became mired in the sand. - [Incident 19800602052569I](https://openairdocs.org/incident/19800602052569I), Jun 2, 1980: Lkheed 10113851 (N718DA), Chicago, IL. #2 Engine would not develop more than idle power. High pressure fuel shutoff valve frozen. - [Incident 19780818049119I](https://openairdocs.org/incident/19780818049119I), Aug 18, 1978: Lkheed 10113851 (N718DA), Dallas, TX. Diverted due to loss of NR1 generator. NR2 generator already inoperative. Integrated drive generator no 708542N. - [Incident 19780410009789I](https://openairdocs.org/incident/19780410009789I), Apr 10, 1978: N718DA, San Diego, CA, Minor damage. Crew unable to fully extend flaps for landing. Found flap track had separated from aircraft. ## Other aircraft with N718DA - [Registered now](https://openairdocs.org/aircraft/N718DA): Aea Research PTY EXPLORER 350R, S/N 350-001 --- 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.