# N733DS: 1981 Lockheed L-1011-385-1, registration cancelled 2013-02-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 27, 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) - Data sheets: [TCDS A23WE](https://openairdocs.org/tcds/A23WE) (OpenAirDocs) - Serial number: 193C-1224 - Year built: 1981 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: November 25, 1981 - Last registry action: May 13, 2004 - Mode S code: A9D68C - 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/N733DS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=733DS - Page: https://openairdocs.org/deregistered/N733DS-2013-02-27 From the FAA registry file of November 3, 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 (40) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DLL10010487](https://openairdocs.org/sdr/DLL10010487), Mar 25, 2001: CONTROL UNIT. DISCONNECTED. ON CLIMB OUT OVER HEAD BIN SEAT ROW 28 ABC OPENED IN CTR SECTION CAUSING BAG TO FALL OUT STRIKING PASSENGER IN HEAD. SNUBBER ASSY BECAME DISCONNECTED FROM OVERH - [SDR DLL10002204](https://openairdocs.org/sdr/DLL10002204), Nov 10, 2000: COVER. LEAKING. OIL QTY ON NR 1 ENGINE WENT TO ZERO AND OIL PRESS DROPPED INTO RED. SHUT DOWN ENG AT 1925Z. (ENG SHUT DOWN 18 MIN PRIOR TO LANDING). OIL TEMP REMAINED THE SAME - [SDR DLL10001966](https://openairdocs.org/sdr/DLL10001966), Oct 9, 2000: BATTERY. DISCHARGED. EMERGENCY FLASHLIGHT BATTERY LOW AT ATTENDANT SEAT L-1. REPLACED SAME. - [SDR DLL10001648](https://openairdocs.org/sdr/DLL10001648), Aug 25, 2000: SEAL. BLOWN. ON APPROACH INTO ATL, HEAVY OIL SMELL IN COCKPIT. CREW PUT O2 MASKS ON. REPLACED NR 2 ACM FOR BLOWN SEAL ON HOUSING. - [SDR DLL10000735](https://openairdocs.org/sdr/DLL10000735), Apr 17, 2000: ENGINE. VIBRATION. NR 2 ENGINE HIGH VIBES EGT EXCEEDED WITH LOUD BANG. REPLACED ENGINE. - [SDR DLL10000590](https://openairdocs.org/sdr/DLL10000590), Mar 27, 2000: WARNING LIGHT. ILLUMINATED. AFTER GEAR RETRACTION DOOR AND TRANS LIGHTS ON PILOTS PANEL,LT GEAR OR DOOR LIGHT ON SECOND OFFICERS PANEL. DUMPED FUEL RETURNED TO LAX. FOUND LEFT MAIN GEAR DO - [SDR DLL10992231](https://openairdocs.org/sdr/DLL10992231), Oct 5, 1999: ENGINE. MALFUNCTIONED. SHUT DOWN NR 2 ENGINE IN CRUISE DUE TO FILTER PRESSURE LIGHT ON S/O PANEL AS WELL AS LOW OIL QUANTITY, QUANTITY DECREASING. REPLACED NR 2 ENG GEARBOX HIGHSPEED - [SDR DLL10991796](https://openairdocs.org/sdr/DLL10991796), Aug 11, 1999: FIRE LOOP. FAILED. 'B' LOOP PREVIOUSLY BAD. NR 2 ENG FIRE HANDLE AND NR 2 'A' LOOP ILLUMINATED IN FLIGHT. NR 2 ENG SHUT DOWN AND BOTH FIRE BOTTLES DISCHARGED POM PROCEDURES COMPLE - [SDR DLL10991329](https://openairdocs.org/sdr/DLL10991329), Jun 12, 1999: GCU. FAILED. FLIGHT STATION BUS FAILURE NR 2 ON TAKEOFF. NR 2 BUS TIE BREAKER TRIP OPEN AND NR 2 BREAKER FAILED, OPEN NR 2 FIELD REMAINED CLOSED. REPLACED NR 2 GCU, RAN ENGS - [SDR DLL10990831](https://openairdocs.org/sdr/DLL10990831), Apr 13, 1999: BULKHEAD WEB. CRACKED. FUSELAGE BULKHEAD FS 1212 RBL 6, WEB CRACK REPAIR. THE FS 1212 BULKHEAD WEB WAS FOUND WITH A CRACK AT RBL 6. THE CRACK IS TYPICAL TO THOSE COVERED IN LAC S/B 09 - [SDR DLL10990404](https://openairdocs.org/sdr/DLL10990404), Feb 25, 1999: PUMP. BYPASSING. EXCESSIVE OIL CONSUMPTION, NR 1 ENGINE BEGAN FLT WITH FULL OIL QTY. AT TOP OF CLIMB, NR 1 ENG QTY WAS 15 QTS. CONSUMED 2.5 QTS IN THE NEXT 1 HR 15 MIN, INDICATE - [SDR DLL10981343](https://openairdocs.org/sdr/DLL10981343), Jun 25, 1998: SKIN. CRACKED. A 4 INCH LONG CRACK WAS FOUND EXTENDING FROM THE AFT EDGE OF LOWER SKIN PANEL AT IWS 450. THE CRACK RAN FWD, TERMINATING UNDER THE AFT EDGE OF THE LOWER SPAR CA - [SDR DLL10981223](https://openairdocs.org/sdr/DLL10981223), Jun 5, 1998: SPAR. CRACKED. TWO CENTER WING INTERMEDIATE SPAR UPPER CAPS WERE FOUND WITH CRACKS BEYOND TYPICAL SRM REPAIR. CRACKS WERE LOCATED IN THE RT O/B END OF THE STA 1043 SPAR AND TH - [SDR DLL10981222](https://openairdocs.org/sdr/DLL10981222), Jun 5, 1998: FRAME. CRACKED. THE STA 1163 FUSELAGE FRAME WAS FOUND WITH THE FRAME TO SKIN ATTACH ANGLE CRACKED AT WL 201 JUST ABOVE PASSENGER FLOOR LEVEL ON THE LT SIDE OF THE FUSELAGE. THE - [SDR DLL10980634](https://openairdocs.org/sdr/DLL10980634), Mar 23, 1998: MAGNA STICK. INOPERATIVE. IN FLT HAD 2 RT BOOST PUMPS 1/2 LOW PRESS LIGHTS ON WITH CORRESPONDING LOW QTY LEVEL LIGHT. FLT DIVERTED INTO BHM FOR ADDITIONAL FUEL. DURING FUELING FOUND NR 1 - [SDR DLL10980597](https://openairdocs.org/sdr/DLL10980597), Mar 17, 1998: BULB. FAILED. EXTERIOR EMERGENCY EXIT LIGHTS AT DOOR 3L 3R AND 4R ARE INOP. - [SDR DLL10972670](https://openairdocs.org/sdr/DLL10972670), Dec 18, 1997: ACM. REQD SERVICE. NR 3 PACK OVHT AT TOUCHDOWN. CABIN FILLED WITH SMOKE AND BURNING SMELL THROUGHOUT A/C. INSPECTED NR 3 PACK, FOUND NO OIL IN NR 3 ACM. LOCKED PACK VLV OUT PER ME - [SDR DLL10972596](https://openairdocs.org/sdr/DLL10972596), Dec 10, 1997: LOGIC CARD. FAILED. GEAR RETRACTED ON CLIMB-OUT, RED DOOR INTRANSIT AND S/O RT GEAR OR DOOR LIGHT REMAINED ILLUMINATED. AFTER FOLLOWING PROCEDURES WITH ATL MAINT, TRUCK LIGHT REMAI - [SDR DLL10971156](https://openairdocs.org/sdr/DLL10971156), Jun 12, 1997: PRESSURE DECK. CORROSION. CORROSION WAS FOUND ON THE FWD PRESSURE DECK AT FS 348 AND RBL 20. THE RESULTING CUTOUT MEASURED 1.625 INBD/OUTBD BY 2.625 FWD/AFT. A DOUBLER WAS PLACED OVER TH - [SDR DLL10971145](https://openairdocs.org/sdr/DLL10971145), Jun 11, 1997: SKATE ANGLE. CRACKED. A CRACK WAS FOUND IN ON OF THE OUTBOARD SKATE FWD ATTACH HOLES ON THE LT WING PYLON. THIS CRACK WAS LOCATED IN THE UPPER MOST FORWARD ROW OF FASTENERS AND EXTEN - [SDR DLL10971143](https://openairdocs.org/sdr/DLL10971143), Jun 11, 1997: SPAR CAP. MISDRILLED. THE LT SPAR TO UPPER WEB ATTACH FASTENER HOLES WERE OVERSIZED AT TWO LOCATIONS. THE FIRST LOCATION IS AT APPRX. IWS 306. THE SECOND LOCATION IS AT APPROX IWS 37 - [SDR DLL10971142](https://openairdocs.org/sdr/DLL10971142), Jun 11, 1997: SKIN. DENTED. THE SKIN AT STA 360 BETWEEN STR 51 AND THE FLOOR LONGERON WAS FOUND WITH A DENT WHICH WAS CUTOUT ALONG WITH THE FAIL/SAFE STRAP THAT WAS BONDED TO IT. THE FAIL/ - [SDR DLL10971320](https://openairdocs.org/sdr/DLL10971320), Jun 9, 1997: SKIN. DAMAGED. THE FUSELAGE SKIN BELOW THE L3 DOOR CUTOUT WAS DAMAGED BY TOOLING SURROUNDING A FASTENER HOLE. THE HOLE WAS ENLARGED TO REMOVE THE TOOLING DAMAGE. DURING OVERSI - [SDR DLL10971150](https://openairdocs.org/sdr/DLL10971150), Jun 6, 1997: SKIN. DENTED. SEVERAL DENTS WERE FOUND BETWEEN STR 21 AND THE EDGE OF THE PANEL BTWEEN THE FORWARD EDGE AND APPROX FS 735. SEVERAL REPAIR DOUBLERS WERE INSTALLED. THIS REPAIR - [SDR DLL10971151](https://openairdocs.org/sdr/DLL10971151), Jun 5, 1997: PRESSURE DECK. CRACKED. THE FUSELAGE HORIZONTAL PRESSURE DECK PANEL WAS FOUND WITH A 1.0 LONG CRACK. THE CRACK IS LOCATED AT RBL 102, JUST AFT OF FS 378 AND EXTEND DIAGONALLY INBOARD A - [SDR DLL10971091](https://openairdocs.org/sdr/DLL10971091), Jun 4, 1997: PRESSURE DECK. CORRODED. THE UPPER SURFACE OF THE NOSE LANDING GEAR PRESSURE DECK WAS FOUND CORRODED BEYOND LIMITS. THE DAMAGE IS LOCATED AT FS 350, RBL 42 DIRECTLY ABOVE AN INTEGRAL ST - [SDR DLL10970991](https://openairdocs.org/sdr/DLL10970991), May 20, 1997: SKIN. CRACKED. THE LOWER FUSELAGE BELLY SKIN WAS FOUND WITH CORROSION AND CRACKS AT FS 914 JUST O/B OF STR 34. REMOVAL OF DAMAGE IN THE SKIN ONLY RESULTED IN A CUT OUT SIZED A - [SDR DLL10970990](https://openairdocs.org/sdr/DLL10970990), May 20, 1997: SPAR WEB. CRACKED. WHILE ACCOMPLISHING DAL SPECIAL INSP 7-55740-12AD, REAR SPAR WEB INSPECTION FOR FATIGUE CRACKS, ONE FASTENER HOLE WAS OVERSIZED BEYOND THE MAX LIMITS DICTATED O - [SDR DLL10970579](https://openairdocs.org/sdr/DLL10970579), Mar 30, 1997: BATTERY PACK. DISCHARGED. FUSE LT ILLUM ON R1 EMERG LIGHT PACK. REPLACED PACK, OPN NORMAL. - [SDR DLL10970356](https://openairdocs.org/sdr/DLL10970356), Feb 24, 1997: BATTERY. DISCHARGED. EXT EMERG LIGHT AT R2 DOOR INOP. REPLACED EMERG LIGHT PWR PACK FWD OF R2 DOOR. EMERG LIGHTS CK OK. - [SDR DLL10970208](https://openairdocs.org/sdr/DLL10970208), Feb 4, 1997: TIRE. FAILED. NR 2 REAR TIRE BLEW ON TAKEOFF ROLL. UNABLE TO RAISE THE LEFT MAIN LANDING GEAR. FUEL DUMPED A/C RETURNED TO LAX. A/C REMOVED TO HGR FOR IN DEPTH INSP. INITIAL - [SDR DLL10962686](https://openairdocs.org/sdr/DLL10962686), Dec 12, 1996: BATTERY. DISCHARGED. F/A FLASHLIGHT AT DOOR 2R INOP. - [SDR DLL10962018](https://openairdocs.org/sdr/DLL10962018), Aug 31, 1996: POWER SUPPLY. INOPERATIVE. POWER SUPPLIES DO NOT INDICATE AMBER LIGHT CHARGING COND DURING TEST. REPLACED POWER SUPPLIES, TEST OK. LOC ADJ R1 AND L4 DOORS. - [SDR DLL10960191](https://openairdocs.org/sdr/DLL10960191), Jan 25, 1996: FITTING. DAMAGED. BOTH THE FWD AND AFT FITTINGS ON THE FWD FRAME FS 792 ARE REQUIRED TO BE MFG'D TO ACCOMMODATE A FRAME REPAIR INSTALLED BY ER/A 271917-14. SUBJECT FITTINGS ARE M - [SDR DLL10960101](https://openairdocs.org/sdr/DLL10960101), Jan 16, 1996: BUSHING. NOT INSTALLED. ON GEAR RETRACTION, RED DOOR AND INTRANS WITH LEFT GEAR OR DOOR ON S/O PANEL. CYCLED GEAR, SAME INDICATIONS. FOUND PHASE CONTROL VALVE INCORRECTLY INSTALLED DUE - [SDR DLL10960082](https://openairdocs.org/sdr/DLL10960082), Jan 13, 1996: CONTROL VALVE. MALFUNCTIONED. AFTER T/O RAISED GEAR HANDLE, ON PILOTS PANEL RSD DOOR AND INTRANSIT LIGHT ON, ALL GREEN LIGHTS OUT. ON S/O PANEL LT GEAR OR DOOR LIGHT ON. CYCLED GEAR, NO CHAN - [SDR DLL10954628](https://openairdocs.org/sdr/DLL10954628), Nov 29, 1995: SPAR CAP. CRACKED. DURING ACCOMPLISHMENT OF SI 7-63370-12AD, A CRACK WAS NOTED AT HOLE NR 10A BETWEEN IWS 319.83 AND IWS 346.109 IN THE RT WING REAR SPAR UPPER CAP. THE WING SKIN - [SDR DLL10953714](https://openairdocs.org/sdr/DLL10953714), Sep 16, 1995: EEL BATTERY PACK. DISCHARGED. ON LAYOVER, FOUND FWD CABIN EMERGENCY EXIT PATH LIGHTS FAILED TEST. REPLACED BATTERY AND POWER SUPPLY, OPERATION NORMAL. - [SDR DLL10953230](https://openairdocs.org/sdr/DLL10953230), Jul 29, 1995: EEL BATTERY PACK. DISCHARGED. DURING LAYOVER, EMERGENCY LIGHT INOP FWD CABIN RT SIDE. REPLACED BATTERY PACK, OPERATION NORMAL. - [SDR DLL10953200](https://openairdocs.org/sdr/DLL10953200), Jul 25, 1995: EEL POWER SUPPLY. FAILED. ON LAYOVER, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP IN FWD CABIN. REPLACED POWER SUPPLY, OPERATION NORMAL. ## Other aircraft with N733DS - [Registered now](https://openairdocs.org/aircraft/N733DS): Flight Design General Avn F2-LSA, S/N T-21-01-03, built 2021 - [Cancelled 1979-03-27](https://openairdocs.org/deregistered/N733DS-1979-03-27): Cessna U206G, S/N U20604759. Exported to Netherlands. Owner: [Cavico Aircraft Sales Inc](https://openairdocs.org/faa-owner/CAVICO%20AIRCRAFT%20SALES%20INC), [Ft Lauderdale, FL](https://openairdocs.org/faa-place/FL/Ft%20Lauderdale) --- 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.