# N106CK: 1981 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: 293C-1211
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: December 24, 1995
- Certificate issued: December 19, 2002
- Last registry action: December 16, 2008
- Mode S code: A01B3A
- 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/N106CK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=106CK
- Page: https://openairdocs.org/deregistered/N106CK-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 (77, newest 50)

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

- [SDR K4HA99088](https://openairdocs.org/sdr/K4HA99088), Jun 16, 1999: CONTROL CABLE. FAILED. UNSAFE GEAR INDICATION. REPLACE CABLE.
- [SDR CKSA99058](https://openairdocs.org/sdr/CKSA99058), Dec 16, 1998: FLOORBEAM. CORRODED. DURING ROUTINE C CHECK AND CPCP, FOUND CORROSION ON LOWER FLOORBEAM CAP AT MAIN DECK STA 789, LBL 4. CORROSION OUT OF LIMITS PER SRM 51-21-00. FABRICATED REPAIR
- [SDR CKSA99057](https://openairdocs.org/sdr/CKSA99057), Dec 16, 1998: SEAT TRACK. CRACKED. DURING ROUTINE C CHECK AND CPCP, FOUND CRACK ON SEAT TRACK, FWD CARGO COMPT, STA 629 TO 630, LBL94. TREATED, PRIMED AND INSTALLED REPLACEMENT IAW SRM 51-40-01. 
- [SDR CKSA99056](https://openairdocs.org/sdr/CKSA99056), Dec 16, 1998: FLOORBEAM. CORRODED. DURING ROUTINE C CHECK AND CPCP, FOUND CORROSION ON LOWER FLOOR BEAM CAP AT MAIN DECK STA 1465, STR 35. FABRICATED REPAIR PARTS IAW SRM 53-21-00 FIG 804. TREATE
- [SDR CKSA99055](https://openairdocs.org/sdr/CKSA99055), Dec 16, 1998: STRINGER. CORRODED. DURING ROUTINE C CHECK AND CPCP, FOUND CORROSION AROUND FASTNERS ON STRINGER 35, STA 1783, C-3 CARGO PIT. REMOVED CORROSION AND FASTNERS IAW SRM 51-21-01. FOUND
- [SDR CKSA99054](https://openairdocs.org/sdr/CKSA99054), Dec 16, 1998: LONGERON. CORRODED. DURING ROUTINE C CHECK AND CPCP, FOUND CORROSION AROUND FASTNERS ON LONGERON 29, STA 1515, C-2 CARGO PIT. REMOVED CORROSION AND FASTNERS IAW SRM 51-21-01 & 51-4
- [SDR CKSA99053](https://openairdocs.org/sdr/CKSA99053), Dec 16, 1998: FLOORBEAM. CORRODED. DURING ROUTINE C CHECK AND CPCP FOUND CORROSION ON LOWER FLOORBEAM CAP AT MAIN DECK STA 789, STR 4, LBL 38. CORROSION OUT OF LIMITS PER SRM 51-21-00. FABRICATED
- [SDR CKSA98744](https://openairdocs.org/sdr/CKSA98744), Dec 16, 1998: WEB. CORRODED. C-1 DOOR INTERNAL WEB FRAME HAS CORROSION AROUND ANCHOR NUT HOLES IN FOUR AREAS. REMOVED CORROSION IAW SRM 51-21-01. COMPLIED WITH THICKNESS CHECK, FOUND FOUR A
- [SDR CKSA98743](https://openairdocs.org/sdr/CKSA98743), Dec 16, 1998: ANGLE. CORRODED. IN NR 2 H/E BAY FOUND CORROSION AT LOWER END OF ANGLE ON I/B AFT CORNER OF H/E BAY FS 378. REMOVED CORROSION IAW SRM 51-21-01. FOUND TO BE OUT OF LIMITS IAW SRM
- [SDR CKSA98742](https://openairdocs.org/sdr/CKSA98742), Dec 16, 1998: TIE. CRACKED. IN C-3 CARGO COMPARTMENT AT FS 1790, THE TENSION TIE BETWEEN LONGERON 30 AND 31 IS CRACKED AND CORRODED.
- [SDR CKSA98741](https://openairdocs.org/sdr/CKSA98741), Dec 16, 1998: LONGERON. CORRODED. IN C-2 CARGO PIT AT STA 1455 THE LONGERON 30 STRINGER SKIN HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-00 FIG 801
- [SDR CKSA98740](https://openairdocs.org/sdr/CKSA98740), Dec 16, 1998: WEB. CORRODED. IN C-3 CARGO COMPT FS 1665 BETWEEN STRINGERS 33 AND 28 THE WEB TOP SURFACE AND ALL NUT PLATES FOUND CORRODED. REMOVED CORROSION IAW L1011 SRM 51-21-00. FOUND TO
- [SDR CKSA98739](https://openairdocs.org/sdr/CKSA98739), Dec 16, 1998: STRINGER. CORRODED. FOUND IN C-1 CARGO COMPT AT STA 619, THE S-30 STRINGER HAS CORROSION. REMOVED IAW SRM 51-21-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-13-00 FIG 801. INSTALLED RE
- [SDR CKSA98738](https://openairdocs.org/sdr/CKSA98738), Dec 16, 1998: FLOORBEAM. CORRODED. FOUND AT C-1 CARGO COMPT, STA 649, RBL 42 TO RBL 55, UPPER FLOORBEAM CHORD CORRODED. REMOVED CORROSION IAW SRM 51-21-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-27
- [SDR CKSA98737](https://openairdocs.org/sdr/CKSA98737), Dec 16, 1998: SEAT TRACK. CORRODED. SEAT TRACK AT FS 649 TO 669, RBL 56, CORROSION FOUND UNDER SEAT TRACK FLANGE. REMOVED SEAT TRACK IAW L1011 SRM 51-40-01. CORROSION FOUND TO BE BEYOND ALLOWABLE 
- [SDR CKSA98736](https://openairdocs.org/sdr/CKSA98736), Dec 16, 1998: FLOORBEAM. CORRODED. CORROSION FOUND AT MAIN DECK FLOORBEAM LOWER CHORD/CAP AT FS 669, RBL 78. REMOVED CORROSION IAW L1011 SRM 51-21-01. FOUND TO BE OUT OF LIMITS IAW SRM 51-50-02. 
- [SDR CKSA98735](https://openairdocs.org/sdr/CKSA98735), Dec 16, 1998: FLOORBEAM. CORRODED. CORROSION FOUND AT MAIN DECK FLOORBEAM LOWER CHORD/CAP AT FS 569, LBL 15. FABRICATED REPAIR PARTS IAW L1011 SRM 53-21-00 FIG 803. TREATED AND PRIMED IAW SRM 51-
- [SDR CKSA98734](https://openairdocs.org/sdr/CKSA98734), Dec 16, 1998: BULKHEAD. CORRODED. FOUND AFT PRESSURE BULKHEAD CIRCUMFERENTIAL BETWEEN STRINGERS 33 AND 38 CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 51-21-01. FABRICATED REPL
- [SDR CKSA98733](https://openairdocs.org/sdr/CKSA98733), Dec 16, 1998: WEB. CORRODED. IN C-3 PIT, BETWEEN FS 1775 AND 1790 STRINGERS 29 AND 30 THE PLATE AND WEB FOUND TO BE CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW L1011 SRM 5
- [SDR CKSA98732](https://openairdocs.org/sdr/CKSA98732), Dec 16, 1998: BULKHEAD ANGLE. CORRODED. IN C-1 CARGO PIT, FS 943 BULKHEAD HAS FLOOR SUPPORT EXTRUSION CORRODED. REMOVED DISCREPANT EXTRUSION IAW L1011 SRM 51-40-01. INSTALLED REPAIR ANGLE IAW SRM 51-4
- [SDR CKSA98731](https://openairdocs.org/sdr/CKSA98731), Dec 16, 1998: WEB. CORRODED. FOUND IN C-1 CARGO PIT, ZONE 130, STA 903, WEB BETWEEN STRINGER 27 AND 28 CORRODED. REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-12-00. FABRICATED REPAIR PA
- [SDR CKSA98730](https://openairdocs.org/sdr/CKSA98730), Dec 16, 1998: FLOORBEAM. CORRODED. IN C-1 PIT, ZONE 130, STA 549 TO 669, RBL 55, FLOORBEAM FOUND CORRODED. CORROSION FOUND TO BE OUT OF LIMITS. FLOORBEAM REMOVED AND REPLACED IAW SRM 51-40-01. FO
- [SDR CKSA98729](https://openairdocs.org/sdr/CKSA98729), Dec 16, 1998: STRINGER. CORRODED. IN C-2 CARGO PIT FOUND AT STA 1405 TO 1425 STRINGER 34 HAD CORROSION. FOUND TO BE OUT OF LIMITS IAW L1011 SRM 51-21-01. FABRICATED NEW SUPPORT ANGLE IAW SRM 51-
- [SDR CKSA98728](https://openairdocs.org/sdr/CKSA98728), Dec 16, 1998: FLOORBEAM. CORRODED. IN C-1 PIT, FS 789, LBL 48, FOUND CORROSION ON LOWER CAP OF FLOORBEAM. REMOVED CORROSION IAW SRM 51-21-00, FOUND OUT OF LIMITS IAW SRM 53-21-00. FABRICATED REPA
- [SDR CKSA98727](https://openairdocs.org/sdr/CKSA98727), Dec 16, 1998: FLOORBEAM. CORRODED. IN C-1 PIT, ZONE 130, STA 709, RBL 48, FOUND AREA OF CORROSION. CORROSION OUT OF LIMITS IAW L1011 SRM 53-21-00. INSTALLED REPAIR IAW SRM 53-21-00 AND 51-40-01. 
- [SDR CKSA98726](https://openairdocs.org/sdr/CKSA98726), Dec 16, 1998: FLOORBEAM. CORRODED. IN C-1 PIT, ZONE 130, FS 829, BETWEEN LBL 48 AND LBL 52, FOUND AN AREA OF CORROSION ON LOWER CAP OF MAIN DECK FLOORBEAM. REMOVED ALL EXISTING FASTENERS TO ACCOM
- [SDR CKSA98725](https://openairdocs.org/sdr/CKSA98725), Dec 16, 1998: FLOORBEAM. CORRODED. IN C-1 PIT, ZONE 130, STA 901, BETWEEN RBL 10 AND 15, FOUND AN AREA OF CORROSION. REMOVED CORROSION IAW SRM 51-21-01, FOUND TO BE OUT OF LIMITS IAW 53-21-00. RE
- [SDR CKSA98724](https://openairdocs.org/sdr/CKSA98724), Dec 16, 1998: FLOORBEAM. CORRODED. FOUND IN C-1 PIT, FS 923 AT STRINGER 41, THE TOP OF FLOORBEAM, INSIDE THE PLASTIC SUPPORT BLOCK IS CORRODED. CORROSION OUT OF LIMITS IAW SRM 51-21-01 AND 53-23-
- [SDR CKSA98723](https://openairdocs.org/sdr/CKSA98723), Dec 16, 1998: SHEAR TIE. CORRODED. IN C-2 PIT FS 1485 BETWEEN STRINGERS 35 TO 36 FOUND SHEAR TIE CORRODED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-21-01 AND 53-23-00. FABRICATED REPAIR PAR
- [SDR CKSA98722](https://openairdocs.org/sdr/CKSA98722), Dec 16, 1998: FLOORBEAM. CORRODED. IN C-1 PIT FS 789, RBL 4, FOUND LOWER CAP OF FLOORBEAM TO BE CORRODED BEYOND LIMITS. FABRICATED REPAIR PARTS IAW L1011 SRM 53-21-00. TREATED, PRIMED AND INSTALL
- [SDR CKSA98721](https://openairdocs.org/sdr/CKSA98721), Dec 16, 1998: SHEAR TIE. CORRODED. FOUND SHEAR TIE CORRODED IN C-3 PIT, FS 1790 BETWEEN STRINGERS 29 AND 30. OUT OF LIMITS IAW L1011 SRM 51-21-01 AND 53-12 FIG 801. REPLACED SHEAR TIE IAW SRM 51-
- [SDR CKSA98720](https://openairdocs.org/sdr/CKSA98720), Dec 16, 1998: SKIN. CORRODED. CORROSION FOUND ON SKIN PANEL AT FS 1107 BETWEEN STRINGERS 29 TO 30. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-00. TREATED PRIMED IAW SRM 51-21-02 AND MM 20-51-09
- [SDR CKSA98719](https://openairdocs.org/sdr/CKSA98719), Dec 16, 1998: WEB. CORRODED. BETWEEN FS 1645 AND 1665 WEB FOUND CORRODED BEYOND LIMITS. REMOVED CORRODED WEB IAW SRM 51-40-01. FABRICATED NEW WEB IAW L1011 SRM 51-10-01. INSTALLED WEB IAW L
- [SDR CKSA98718](https://openairdocs.org/sdr/CKSA98718), Dec 16, 1998: FLOORBEAM. CORRODED. FLOORBEAM AT FS 1445, RBL 14 LOWER CHORD/CAP CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-23-00. FABRICATED REPAIR PARTS IAW SRM 53-21-00. INSTALLED IAW SRM 5
- [SDR CKSA98717](https://openairdocs.org/sdr/CKSA98717), Dec 16, 1998: SHEAR TIE. CORRODED. AT FS 1790 BETWEEN STRINGERS 33 TO 34 AFT SIDE SHEAR TIE HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW L1011 SRM 51-21-01. FABRICATED REPAIR P
- [SDR CKSA98716](https://openairdocs.org/sdr/CKSA98716), Dec 16, 1998: BULKHEAD PATCH. CORRODED. FOUND REPAIR PATCH CORRODED ON AFT PRESSURE BLKHD BETWEEN STRINGERS 35 AND 37 FS APPROX 1824. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-01. REMOVED AND REPLACED R
- [SDR CKSA98715](https://openairdocs.org/sdr/CKSA98715), Dec 16, 1998: STRINGER. CORRODED. BETWEEN FS 1645 AND 1665 STRINGER 33R CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW L1011 SRM 51-21-01 & 53-13-00 FIG 801. FABRICATED REPAIR PIECES
- [SDR CKSA98714](https://openairdocs.org/sdr/CKSA98714), Dec 16, 1998: SEAT TRACK. CRACKED. FOUND SEAT TRACK FLANGE CRACKED AT FUSELAGE STATION 629, LBL 94. REMOVED AND REPLACED SEAT TRACK IAW L1011 SRM 51-40-01. FOUND DURING SCHEDULED C-CHECK AND CPCP
- [SDR CKSA98713](https://openairdocs.org/sdr/CKSA98713), Dec 16, 1998: FRAME. DAMAGED. FS 903 AFT SIDE OF FRAME HORIZONTAL LEG DAMAGED BETWEEN STRINGER 27 AND 28. REPAIRED DAMAGE AND FABRICATED PART IAW L1011 SRM 53-12-0 FIG 805. TREATED AND PRIME
- [SDR CKSA98712](https://openairdocs.org/sdr/CKSA98712), Dec 16, 1998: STRAP. CUT. FS 1393 RBL 2 SKIN TEAR STRAP HAS LEVEL 1 CORROSION. TITANIUM TEAR STRAP CUT TO FACILITATE CORROSION REMOVAL. REPAIRED IAW L1011 SRM 53-31-00. FOUND DURING SCHE
- [SDR CKSA98029](https://openairdocs.org/sdr/CKSA98029), Feb 10, 1998: SKIN. DAMAGED. FUSELAGE SKIN DAMAGE FS 593 TO FS 603 LT STR 49. REPAIRED SKIN DAMAGE IAW AIA EA NR L1-53-013 MARSHALLS DWG NR MT2-05-0282. FAA APPROVED ON FORM 8110-3 DATED 2/
- [SDR CKSA97609](https://openairdocs.org/sdr/CKSA97609), Dec 12, 1997: SKIN. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: EXTERNAL SKIN CORROSION OUT OF LIMITS AT FS789 TO 769 S36-37. INSTALLED REPAIRS IAW SRM 51-31-00 FIG 802
- [SDR CKSA97608](https://openairdocs.org/sdr/CKSA97608), Dec 12, 1997: STRINGER. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: STRINGER CORRODED OUT OF LIMITS FS1645 TO 1625 STR 30. INSTALLED REPAIR IAW SRM 53-13-00 FIG 804 SHEET 2
- [SDR CKSA97607](https://openairdocs.org/sdr/CKSA97607), Dec 12, 1997: SUPPORT. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: CORROSION ON MAIN CARGO FLOOR SUPPORT LAST ONE ON LT SIDE JUST FWD OF AFT PRESS BULKHEAD JUST ABOVE APU 
- [SDR CKSA97606](https://openairdocs.org/sdr/CKSA97606), Dec 12, 1997: ANGLE. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: CORROSION ON MAIN CARGO FLOOR SUPPORTS JUST FWD OF AFT PRESS BULKHEAD. REMOVED CORROSION IAW L1011 SRM 5
- [SDR CKSA97605](https://openairdocs.org/sdr/CKSA97605), Dec 12, 1997: LONGERON. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: CORROSION ON AFT PRESS BULKHEAD LONGERON FWD PART FS1809 BEHIND S17-S18. REMOVED CORROSION IAW L1011 SRM
- [SDR CKSA97604](https://openairdocs.org/sdr/CKSA97604), Dec 12, 1997: FRAME. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: CORROSION ON RING FRAME STA 1809 FROM S33 UP TO S22. REMOVED CORROSION IAW L1011 SRM 51-21-01. FOUND TO 
- [SDR CKSA97603](https://openairdocs.org/sdr/CKSA97603), Dec 12, 1997: FRAME. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: CORROSION ON RING FRAME AT FS1809 FROM S37 TO S42. REMOVED CORROSION IAW L1011 SRM 51-21-01. FOUND TO BE
- [SDR CKSA97602](https://openairdocs.org/sdr/CKSA97602), Dec 12, 1997: SKIN. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: CORROSION AROUND AFT WASTE COMPT HYD LINE BULKHEAD BOX (LT) APPROX FS1819 ABOVE S41. REMOVED CORROSION I
- [SDR CKSA97601](https://openairdocs.org/sdr/CKSA97601), Dec 12, 1997: SKIN. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: BETWEEN BS1778 AND BS1792; FROM S26 TO S35 BARE METAL AREAS WITH SIGNS OF CORROSION. REMOVED CORROSION I

All 77: https://openairdocs.org/deregistered/N106CK-2009-09-02/reports.md

## 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 CHI99IA100](https://openairdocs.org/ntsb/CHI99IA100), Mar 2, 1999: Lockheed L-1O11-385-1-15 (N106CK), Salina, KS, incident, no damage. Probable cause: The ARTCC personnel failed to maintain radio communications with both airplanes and failed to maintain IFR separation standards. Factors relating to the incident were the FAA does not require cargo…

## Other aircraft with N106CK

- [Registered now](https://openairdocs.org/aircraft/N106CK): Dassault FALCON 900EX, S/N 214, built 2008

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