# N107CK: 1980 Lockheed L-1011-385-1-15, registration cancelled 2009-09-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 2, 2009 - Status when cancelled: Triennial form not returned - Airframe: [Lockheed L-1011-385-1-15](https://openairdocs.org/model/lockheed-l-1011-385-1-15) (registry code 5265015) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Data sheets: [TCDS A23WE](https://openairdocs.org/tcds/A23WE) (OpenAirDocs) - Serial number: 193N-1182 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, normal - Airworthiness date: April 16, 1980 - Certificate issued: December 19, 2002 - Last registry action: December 16, 2008 - Mode S code: A01EF1 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%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/N107CK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=107CK - Page: https://openairdocs.org/deregistered/N107CK-2009-09-02 From the FAA registry file of November 5, 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-1011-385-1-15: https://openairdocs.org/model/lockheed-l-1011-385-1-15.md ## Service difficulty reports (19) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CKSA99018](https://openairdocs.org/sdr/CKSA99018), Mar 15, 1999: SKIN. CRACKED. DURING ACCOMPLISHMENT OF C-CHECK INSPECTION, FOUND CRACK 4 INCHES LONG AT SLAT NR 7 RT I/B UPPER CORNER WITH 4 RIVETS SHEARED. STOP DRILLED CRACK AS PER SRM 51- - [SDR CKSA99017](https://openairdocs.org/sdr/CKSA99017), Mar 15, 1999: BLKHD STIFFENER. CRACKED. DURING ACCOMPLISHMENT OF C-CHECK INSPECTION, FOUND FWD BULKHEAD RT SIDE I/B STIFFENER BOTTOM CORNER PREVIOUSLY REPAIRED CRACK EXTENDING APPROX 1.5. REMOVED PREV - [SDR CKSA99016](https://openairdocs.org/sdr/CKSA99016), Mar 15, 1999: SKIN. CRACKED. DURING ACCOMPLISHMENT OF C-CHECK INSPECTION, FOUND AFT PRECONDITION AIR CONNECTOR FUSELAGE CUT OUT CRACKED. REMOVED RIVETS IN REPAIR AREA AS PER SRM 51-40-01. S - [SDR CKSA99015](https://openairdocs.org/sdr/CKSA99015), Mar 15, 1999: DOUBLER. CRACKED. DURING ACCOMPLISHMENT OF C-CHECK, FOUND RT ELEVATOR TIP, TOP ON/OFF PLATE CRACKED AND HAVING SHEARED RIVETS. REMOVED CRACKED DOUBLER ON/OFF PLATE AS PER SRM 51- - [SDR CKSA99014](https://openairdocs.org/sdr/CKSA99014), Mar 15, 1999: FITTING. CRACKED. DURING ACCOMPLISHMENT OF C-CHECK, FOUND C2 CARGO DOOR LT STEPPED PANEL SUPPORT FITTING AT FS 1565 CRACKED. REMOVED CRACK TEE GUIDE SUPPORT BRACKET AS PER SRM 51 - [SDR CKSA99013](https://openairdocs.org/sdr/CKSA99013), Mar 15, 1999: FITTING. CRACKED. DURING ACCOMPLISHMENT OF C-CHECK, FOUND C2 CARGO DOOR LT STEPPED PANEL SUPPORT FITTING AT FS 1605 CRACKED. REMOVED CRACK TEE GUIDE SUPPORT BRACKET AS PER SRM 51 - [SDR CKSA99012](https://openairdocs.org/sdr/CKSA99012), Mar 15, 1999: SKIN. GROOVED. DURING ACCOMPLISHMENT OF C-CHECK, FOUND RT WING NR 2 FLAP VANE LEADING EDGE IS GROOVED 20 I/B FROM VANE O/B END. CUT OUT DAMAGED AREA AS REQUIRED PER SRM 51-53- - [SDR CKSA99011](https://openairdocs.org/sdr/CKSA99011), Mar 15, 1999: SKIN. CRACKED. DURING ACCOMPLISHMENT OF C-CHECK INSPECTION CARD 57-00-100, FOUND APPROX 4 INCH LONG CRACK AT RT NR 1 SLAT INNER SKIN FWD OF O/B TRACK. CUT OUT DAMAGED AREA AS - [SDR CKSA99010](https://openairdocs.org/sdr/CKSA99010), Mar 15, 1999: SKIN. CRACKED. DURING C-CHECK INSPECTION, FOUND LT WING NR 3 SLAT INNER SURFACE CRACKS AT 4 PLACES. TRIMMED OUT CRACK AREA AND REMOVED SMALL NUMBER OF RIVETS TO FACILITATE REP - [SDR CKSA99009](https://openairdocs.org/sdr/CKSA99009), Mar 15, 1999: MOUNT. FAILED. DURING C-CHECK INSPECTION, FOUND LT WING NR 2 SLAT SCREW JACK SHEARED OFF FROM UPPER MOUNT. REMOVED NR 2 SLAT ACTUATOR IAW MM 27-81-00. DURING INSPECTION, FOUND - [SDR CKSA99008](https://openairdocs.org/sdr/CKSA99008), Mar 15, 1999: RIB. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARD, FOUND ON LT SIDE, NR 4 L/E SLAT RIBS NR 3 AND 23 TO BE CRACKED. REMOVED NR 4 SLAT, ROUTED TO S/M SHOP IAW MM 27-8 - [SDR CKSA99007](https://openairdocs.org/sdr/CKSA99007), Mar 15, 1999: RIB. CRACKED. DURING ACCOMPLISHMENT OF ROUTINE C-CHECK INSPECTION WORK CARD NR 05-57-1006, FOUND LT SIDE NR 7 LEADING EDGE SLAT RIBS NR 4 AND 21 TO BE CRACKED. REMOVED LT SLA - [SDR CKSA99006](https://openairdocs.org/sdr/CKSA99006), Mar 15, 1999: SKIN. CRACKED. LT WING NR 1 SLAT FOUND CRACKED, I/B LOWER EDGE AREA. REPAIR OF CRACK COMPLIED WITH IAW AIA EA L1-057-058 REVISION ORIGINAL DATED 02-28-99 AND AIA DRAWING AIA/E - [SDR CKSA99005](https://openairdocs.org/sdr/CKSA99005), Mar 15, 1999: SKIN. CRACKED. MESC DOOR CUTOUT, BOTTOM AREA SKIN FOUND CRACKED AT 2 LOCATIONS (REFERENCE GAMCO NRC NR 5082). FOUND CRACK TO BE CAUSED BY CORROSION. REMOVED CORROSION AND INST - [SDR CKSA99004](https://openairdocs.org/sdr/CKSA99004), Mar 15, 1999: BOLTS. SHEARED. DURING C-CHECK INSPECTION, FOUND LT WING NR 2 SLAT ACTUATOR MOUNT BOLTS, (3 OF 4) SHEARED. FOUND O/B TORQUE TUBE RESTING ON TORQUE TUBE GUIDE. REPLACED MOUNT BO - [SDR CKSA98540](https://openairdocs.org/sdr/CKSA98540), Oct 2, 1998: AIR DISTR. ODOR. ELECTRICAL ODOR COMNG FROM FEDC AREA. ODOR DIMINISHED WHEN FLT STATION COURIER AND AFT CABIN TEMP CONTROLS WERE UNLATCHED. INSPECTED FLIGHT DECK, FWD AND AFT FE - [SDR CKSA98539](https://openairdocs.org/sdr/CKSA98539), Sep 27, 1998: AIR DISTR. ODOR. A STRONG ELECTRICAL SMELL WAS NOTICED IN THE COCKPIT AT 10,000 FT. WHEN STARTING THE APU. RAN APU AND APPLIED ELECTRICAL POWER AND OPERATED PACKS. CHECKED LOWER - [SDR CKSA97071](https://openairdocs.org/sdr/CKSA97071), Mar 13, 1997: CONTROL UNIT. SHORTED. ENGINE NR 1B LOOP COMES ON DURING FLIGHT. FOLLOWED ABNORMAL PROCEDURE 3-3-3 AFM (FOM). REMOVED AND REPLACED DETECTOR CONTROL UNIT IAW MM 26-11-08, OPS CHECKS NO - [SDR CKSA97010](https://openairdocs.org/sdr/CKSA97010), Feb 6, 1997: SENSOR. OUT OF ADJUST. CARGO DOOR (C-4) WARNING LIGHT ILLUMINATED INFLIGHT AT 33,000 FT. ALSO, AFT MID SPAN LOCK INDICATED UNSAFE. DESCENDED TO 27,000 FT; INCREASED CABIN ALTITUDE TO ## Other aircraft with N107CK - [Registered now](https://openairdocs.org/aircraft/N107CK): Keyes Charles R HELISQUITO, S/N 5-21, built 2021 --- 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.