# N15017: Lockheed L-1011-385-1, registration cancelled 1998-05-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 14, 1998 - Status when cancelled: Valid registration - 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: 193B1063 - Type of aircraft: Fixed wing multi engine - Certificate issued: April 29, 1998 - Last registry action: April 29, 1998 - Mode S code: A0CCCA - Owner when cancelled: [First Security Bank Na Owner Trustee](https://openairdocs.org/faa-owner/FIRST%20SECURITY%20BANK%20NA%20OWNER%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N15017 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=15017 - Page: https://openairdocs.org/deregistered/N15017-1998-05-14 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 (24) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TWAA9781001](https://openairdocs.org/sdr/TWAA9781001), Jul 19, 1997: OIL FILTER. DIRTY. LAX - FLT 442 - DURING CLIMB, NR 2 ENGINE, SN 4816, LOST OIL INDICATION. DRAINED GEARBOX, CHANGED MAIN OIL SCREEN AND SCAVENGE SCREEN. SERVICED GEARBOX AND RAN - [SDR TWAA9752010](https://openairdocs.org/sdr/TWAA9752010), Mar 20, 1997: SKIN. CORRODED. LAX - DURING CHECK 'C', FOUND FUSELAGE SKIN CORROSION WITH HI-LOK HEADS PULLED AT STR 38, FS 1615. REMOVED CORROSION PER SRM 51-21-01 AND REPAIRED STRINGER PER - [SDR TWAA9752009](https://openairdocs.org/sdr/TWAA9752009), Mar 20, 1997: FRAME. CORRODED. LAX - DURING CHECK 'C', FOUND CORROSION , 3 INCH BY 3 INCH CORROSION HOLE BETWEEN STRINGERS 40 AND 41, FS 1625 FRAME. INSTALLED FRAME REPAIR PER SRM 53-12-00, F - [SDR TWAA9752008](https://openairdocs.org/sdr/TWAA9752008), Mar 19, 1997: INTERCOSTAL. CRACKED. LAX - DURING CHECK 'C', FOUND STR 42 INTERCOSTAL CRACKED, FS 1705. STOP DRILLED CRACK AND INSTALLED DOUBLER WITH SEALANT PER SRM 51-50-02, PAGE 4, FIGURE 2. AIR - [SDR TWAA9752007](https://openairdocs.org/sdr/TWAA9752007), Mar 19, 1997: SKIN. CORRODED. LAX - DURING CHECK 'C', FOUND FUSELAGE SKIN CORROSION WHICH POPPED TWO BLIND FASTENERS AND CRACKED RIVET HEAD, STRINGER 37, FS 1615. REPAIRED BY REMOVAL OF CORR - [SDR TWAA9752006](https://openairdocs.org/sdr/TWAA9752006), Mar 18, 1997: SKIN. CORRODED. LAX - DURING CHCK 'C', FOUND FUSELAGE SKIN CORROSION AT FOUR BLIND FASTENERS, STR 29, FS 1732. REMOVED CORROSION AND REPAIRED PER SRM 53-30-07, PAE 20. AIRCRAFT - [SDR TWAA9752004](https://openairdocs.org/sdr/TWAA9752004), Mar 17, 1997: STRINGER. CORRODED. LAX - DURING CHECK 'C', FOUND CORROSION AT STRINGERS 37 AND 40, FS 1715. REMOVED CORROSION AND REPAIRED PER SRM 53-30-02. AIRCRAFT TOTAL TIME: 62,400 HOURS; 23, - [SDR TWAA9752003](https://openairdocs.org/sdr/TWAA9752003), Mar 17, 1997: SKIN. CORRODED. LAX - DURING CHECK 'C', FOUND FUSELAGE SKIN CORROSION BELOW STR 30, FS 839.5. REPAIRED PER SRM 53-03-02. AIRCRAFT TOTAL TIME: 62,400 HOURS; 23,718 CYCLES. (X) - [SDR TWAA9752002](https://openairdocs.org/sdr/TWAA9752002), Mar 17, 1997: SKIN. CORRODED. LAX - DURING CHECK 'C', FOUND FUSELAGE SKIN CORROSION ABOVE STR 30, FS 816.5. REPAIRED PER SRM 53-30-02. AIRCRAFT TOTAL TIME: 62,400 HOURS; 23,718 CYCLES. (X) - [SDR TWAA9752005](https://openairdocs.org/sdr/TWAA9752005), Mar 1, 1997: SKIN. CORRODED. LAX - DURING CHECK 'C', FOUND FUSELAGE SKIN CORROSION BETWEEN STRINGERS 29 AND 30, FS 822. REPAIRED PER SRM 53-30-02. AIRCRAFT TOTAL TIME: 62,400 HOURS; 23,718 - [SDR TWAA9720001](https://openairdocs.org/sdr/TWAA9720001), Feb 10, 1997: BRACKET. FAILED. MCO - FLT 264 - DURING LANDING, RIGHT INBOARD ELEVATOR GAP FAIRING SEPARATED FROM THE AIRCRAFT DUE TO BRACKET FAILURE. REPLACED FAIRING, MFG P/N 1554958-104. VI - [SDR TWAA9703002](https://openairdocs.org/sdr/TWAA9703002), Jan 3, 1997: FOOD CART. FAILED. LAX - FLT 443 - DURING CRUISE SINGLE SERVE FOOD CART NR 1479, P/N 88801-1 SMOKED WHEN TURNED ON. REMOVED AND REPLACED CART NR 1479, WITH A SERVICEABLE CART. (M) - [SDR TWAA9616002](https://openairdocs.org/sdr/TWAA9616002), Aug 4, 1996: ENGINE. MALFUNCTIONED. LAX - DURING CLIMB, NR 3 ENGINE, S/N 4456 EXPERIENCED HIGH AVM. ENGINE WAS SHUT DOWN. INLET AND EXHAUST WERE CHECKED, CHIP DETECTORS CHECKED, AND GEARBOX WAS DR - [SDR 96ZZZX3031](https://openairdocs.org/sdr/96ZZZX3031), May 10, 1996: RIB. CRACKED. MCI - DURING SPECIAL CHECK FOUND CRACK IN RIB CASTELLATION AT FORWARD SIDE OF STR 9, BOTTOM IWS 555. REPAIRED PER SRM 51-10-01. AIRCRAFT TOTAL TIME: 60,229 HOUR - [SDR 96ZZZX3030](https://openairdocs.org/sdr/96ZZZX3030), May 10, 1996: RIB. CRACKED. MCI - DURING SPECIAL CHECK FOUND CRACKS IN TOP WING RIB CASTELLATION OF RT WING, IWS 503, STRINGERS 18, 19, AND 21. REPAIRED PER SB 093-57-207 AND LOCKHEED DWG - [SDR 96ZZZX3029](https://openairdocs.org/sdr/96ZZZX3029), May 10, 1996: RIB. CRACKED. MCI - DURING SPECIAL CHECK, FOUND CRACK IN RIB CASTELLATION AT FORWARD SIDE OF STR 13 AND STR 19, TOP IWS 555. REPAIRED PER SB 093-57-207 AND SRM 51-10-01. AIRC - [SDR 96ZZZX3027](https://openairdocs.org/sdr/96ZZZX3027), May 10, 1996: ANGLE. CRACKED. MCI - DURING SPECIAL CHECK, FOUND A 2 INCH CRACK AT TOP OF CLOSURE RIB ATTACH ANGLE IN RIGHT WING, IWS 503. REPAIRED BY INSTALLING NEW ATTACHED ANGLE PER SB 093 - [SDR 96ZZZM892](https://openairdocs.org/sdr/96ZZZM892), Apr 24, 1996: ENGINE. VIBRATION. MCI - FLT 5034 - DURING CRUISE, SHUT DOWN NR 2 ENGINE DUE TO INCREASE OF VIBRATION ON BOTH A AND B CHANNELS. FOUND FAN OUT OF TRIM BALANCE. PERFORMED ENGINE TRI - [SDR 96ZZZM896](https://openairdocs.org/sdr/96ZZZM896), Apr 18, 1996: RIB. CRACKED. MCI - DURING SPECIAL CHECK, FOUND SEVEN CRACKS IN LEFT WING TOP RIB CASTELLATION, STATION 555. REPAIRED PER SERVICE BULLETIN 093-57-207, PARA 2B. (M) - [SDR 96ZZZM895](https://openairdocs.org/sdr/96ZZZM895), Apr 18, 1996: RIB. CRACKED. MCI - DURING SPECIAL CHECK, FOUND 1.25 INCH CRACK IN LEFT WING RIB CASTELLATION FORWARD SIDE OF STRINGER 19, TOP CHORD, WS 503. REPAIRED PER SERVICE BULLETIN 09 - [SDR 95ZZZM293](https://openairdocs.org/sdr/95ZZZM293), Jul 21, 1995: OIL FILTER. DIRTY. DURING DESCENT SHUT DOWN NR 2 ENGINE, S/N 4806, DUE TO OIL FILTER DIFFERENTIAL PRESSURE LIGHT ILLUMINATION. FOUND CARBON IN OIL FILTER. REPLACED OIL FILTER, DRA - [SDR 95ZZZW441](https://openairdocs.org/sdr/95ZZZW441), Mar 31, 1995: CONTROL VALVE. MALFUNCTIONED. JFK - DURING APPROACH LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. USED MECHANICAL LANDING GEAR EXTENSION. REPLACED LANDING GEAR CONTROL SWITCH, MFG P/N 450-100 - [SDR 95ZZZW440](https://openairdocs.org/sdr/95ZZZW440), Mar 31, 1995: CONTROL SWITCH. MALFUNCTIONED. JFK - DURING APPROACH LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. USED MECHANICAL LANDING GEAR EXTENSION. REPLACED LANDING GEAR CONTROL SWITCH, MFG P/N 450-100 - [SDR 95ZZZW224](https://openairdocs.org/sdr/95ZZZW224), Feb 13, 1995: SKIN. CRACKED. MCI - DURING CHECK C-6C, FOUND 1.5 INCH CRACK IN FUSELAGE SKIN, WITH AREA BULGED OUTWARD AND WITH RIVET HEAD MISSING, STATION 649, STRINGER 36-37. REPAIRED PER ## 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 19891109057939I](https://openairdocs.org/incident/19891109057939I), Nov 9, 1989: Lkheed 10113851 (N15017), St Louis, MO. Flaps would not completely retract after takeoff. Returned. Found 3 sheared bolts on left inboard flap latch roller - [Incident 19860213008749I](https://openairdocs.org/incident/19860213008749I), Feb 13, 1986: Lkheed 10113851 (N15017), St Louis, MO. Controlled descent due to fire in lower lobe of galley. Landed and found 4 sausages on a saucer burning. - [Incident 19850423018839I](https://openairdocs.org/incident/19850423018839I), Apr 23, 1985: Lkheed 10113851 (N15017), St Louis, MO, Minor damage. Heavy vibration from R3 door area on climbout. Returned for landing. Panel mising aft main gear wheel well. - [Incident 19800707059989I](https://openairdocs.org/incident/19800707059989I), Jul 7, 1980: Lkheed 10113851 (N15017), St Louis, MO. Due to missing plastic guard, crewmember accidently depleted crew oxygen supply. Landed to replace. - [Incident 19800115013849I](https://openairdocs.org/incident/19800115013849I), Jan 15, 1980: Lkheed 10113851 (N15017), St Louis, MO. Trailing edge flaps inoperative. Changed flap asymmetry comparator and sticking left flap indicator. ## Other aircraft with N15017 - [Registered now](https://openairdocs.org/aircraft/N15017): Firefly Balloons FIREFLY 8B-15, S/N F8B-2003, built 2001 - [Cancelled 1937-04-01](https://openairdocs.org/deregistered/N15017-1937-04-01): Brush Joseph BRUSH A, S/N 1, built 1935. Owner: [Brush Joseph](https://openairdocs.org/faa-owner/BRUSH%20JOSEPH), [Riverdale, NJ](https://openairdocs.org/faa-place/NJ/Riverdale) --- 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.