# N104CK: 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: [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: 193N-1193
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 11, 1995
- Certificate issued: December 19, 2002
- Last registry action: December 16, 2008
- Mode S code: A013CC
- 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/N104CK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=104CK
- Page: https://openairdocs.org/deregistered/N104CK-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 (11)

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

- [SDR K4HA99074](https://openairdocs.org/sdr/K4HA99074), Aug 18, 1999: STRINGER. CORRODED. STR 29 BS 943 WEB AT STR/SKIN ATTACH CORRODED. REMOVED CORROSION FROM WEB, FOUND TO BE WITHIN LIMITS IAW L1011 SRM 51-21-01 AND 53-12-00. FOUND STRINGER OUT OF 
- [SDR K4HA99073](https://openairdocs.org/sdr/K4HA99073), Aug 18, 1999: LONGERON. CORRODED. LOWER AFT CORNER OF MESC DOOR CUTOUT FRAME CORRODED. REMOVED CORRODED AREA ON FRAME AND KEELSON LONGERON. MANUFACTURED LONGERON REPAIR PARTS IAW L-1011 SRM 53-1
- [SDR CKSA98500](https://openairdocs.org/sdr/CKSA98500), Jun 21, 1998: FIRE LOOP. OUT OF ADJUST. DURING CLIMB, B FIRE LOOP LIGHT NR 2 ENGINE CAME ON STEADY. TEST SHOWED A LOOP OK. A FIRE LOOP SELECTED. AFTER ABOUT 2 MIN, A FIRE LOOP CAME ON. SELECTED BOTH, 
- [SDR CKSA98342](https://openairdocs.org/sdr/CKSA98342), Jun 15, 1998: SKIN. DAMAGED. C1A CARGO DOOR AFT LOWER CORNER IS DEFORMED/DAMAGED. DAMAGED AREA IS APPROX 7 IN LENGTH ALONG RIM OF DOOR SKIN. (REF: GAMCO NON-ROUTINE CARD NUMBER 4114). CUT A
- [SDR CKSA98097](https://openairdocs.org/sdr/CKSA98097), Mar 8, 1998: STRINGER. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, STRINGER 32 HAS CORROSION AT STA 970. REMOVED CORRODED STRINGER DAMAGE AND FOUND OUT OF LIMITS IAW L1011
- [SDR CKSA98096](https://openairdocs.org/sdr/CKSA98096), Mar 8, 1998: ANGLE. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, KEELSON SUPPORT ANGLE CORRODED RBL45 STA 969. INSTALLED REPAIR DOUBLERS IAW AIA SKETCH AIA/E/2765 REV OR
- [SDR CKSA98095](https://openairdocs.org/sdr/CKSA98095), Mar 8, 1998: SKIN. BULGING. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, SKIN BULGING AT LONG 30 BETWEEN FS 963 AND FS 983. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLERS IAW AIA
- [SDR CKSA98094](https://openairdocs.org/sdr/CKSA98094), Mar 8, 1998: BULKHEAD CAP. CRACKED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: BULKHEAD CAP 6:00 POS AT STA 1792 PREVIOUS REPAIR CRACKED. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER IAW
- [SDR CKSA98093](https://openairdocs.org/sdr/CKSA98093), Mar 8, 1998: JAMB. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION AFT PIT DOOR JAM SILL, CORROSION AT FWD LOWER CORNER. REMOVED AND REPLACED CORRODED FILLER IAW L1011 SRM
- [SDR CKSA98092](https://openairdocs.org/sdr/CKSA98092), Mar 8, 1998: STRINGER. CRACKED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, STRINGER 32 AT STA 1792 CRACKED. INSTALLED STRINGER REPAIR IAW L1011 SRM 53-13-00 PG 806. CORROSION TASK
- [SDR CKSA97587](https://openairdocs.org/sdr/CKSA97587), Dec 6, 1997: SKIN. DAMAGED. PRE-DEPARTURE FOUND HOLE ON RIGHT SIDE OF AIRCRAFT, 53 AFT OF C1 DOOR. REPAIRED STRUCTURE DAMAGE TO SKIN, STRINGER AND FRAME IAW 53-13-00 FIG 804, 51-50-03 FIG 

## Other aircraft with N104CK

- [Registered now](https://openairdocs.org/aircraft/N104CK): Mark Krotky CH750 STOL, S/N 75-11445, built 2023

---
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.