# Service difficulty reports: N106CK, cancelled Sep 2, 2009

A list on [N106CK, cancelled Sep 2, 2009](https://openairdocs.org/deregistered/N106CK-2009-09-02.md).

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

Page 1 of 2 · 77 reports

- [SDR K4HA99088](https://openairdocs.org/sdr/K4HA99088.md): Control Cable · failed · Jun 16, 1999 · N106CK · Lkheed 1011385115 · Landing Gear Position and Warning
  > UNSAFE GEAR INDICATION. REPLACE CABLE.
- [SDR CKSA99058](https://openairdocs.org/sdr/CKSA99058.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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 PARTS IAW SRM 53-21-00. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-21-00 FIG 802. WO
- [SDR CKSA99057](https://openairdocs.org/sdr/CKSA99057.md): Seat Track · cracked · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage, Seat/Cargo Attach Fittings
  > 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. WORK PERFORMED AT AIA MAINTENANCE FACILITY OSCODA. WORK ORDER NUMBER 106-206, SOURCE DOCUMENT CPC
- [SDR CKSA99056](https://openairdocs.org/sdr/CKSA99056.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-21-00 FIG 804 SHEET 2. WORK PERFORMED AT AIA MAIN
- [SDR CKSA99055](https://openairdocs.org/sdr/CKSA99055.md): Stringer · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Longeron/Stringer
  > 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 TO BE OUT OF LIMITS IAW SRM 53-13-00. FABRICATED REPAIR IAW SRM 53-13-00. INSTALLED REPAIR IAW
- [SDR CKSA99054](https://openairdocs.org/sdr/CKSA99054.md): Longeron · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Longeron/Stringer
  > 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 & 51-40-0. FOUND TO BE OUT OF LIMITS IAW SRM 53-13-00 FIG 801. FABRICATED NEW PARTS IAW AIA ENGINEERING
- [SDR CKSA99053](https://openairdocs.org/sdr/CKSA99053.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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 REPAIR PARTS IAW SRM 53-21-00 FIG 807. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-21-
- [SDR CKSA98744](https://openairdocs.org/sdr/CKSA98744.md): Web · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Cargo/Baggage Doors
  > 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 AREAS OUT OF LIMITS IAW SRM 52-11-00. FABRICATED REPAIR PARTS IAW AIA DRAWING EDR-L106044. TREATE
- [SDR CKSA98743](https://openairdocs.org/sdr/CKSA98743.md): Angle · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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 53-12-00. TREATED AND PRIMED IAW SRM 51-21-02 AND MM 20-51-09. INSTALLED REPAIR ANGLE IAW SRM 5
- [SDR CKSA98742](https://openairdocs.org/sdr/CKSA98742.md): Tie · cracked · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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.md): Longeron · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Longeron/Stringer
  > 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. REMOVED CORRODED AREA AND FABRICATED DOUBLERS IAW SRM 53-31-00 FIG 804. ALODINED AND PRIMED IA
- [SDR CKSA98740](https://openairdocs.org/sdr/CKSA98740.md): Web · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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 BE OUT OF LIMITS IAW SRM 53-23-00 FIG 801. REPAIRED FLOORBEAM UPPER CAP IAW SRM 53-23-00 FIG 802
- [SDR CKSA98739](https://openairdocs.org/sdr/CKSA98739.md): Stringer · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Longeron/Stringer
  > 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 REPAIR IAW SRM 53-13-00 FIG 803. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT
- [SDR CKSA98738](https://openairdocs.org/sdr/CKSA98738.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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 53-27-00 FIG 804. FABRICATED REPAIR PARTS IAW SRM 53-20-00 FIG 802. INSTALLED REPAIR IAW SRM 53-23-00
- [SDR CKSA98737](https://openairdocs.org/sdr/CKSA98737.md): Seat Track · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage, Seat/Cargo Attach Fittings
  > 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 LIMITS IAW SRM 53-21-00. REPLACED SEAT TRACK IAW L1011 SRM 51-40-01. FOUND DURING SCHEDULED C-CH
- [SDR CKSA98736](https://openairdocs.org/sdr/CKSA98736.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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. REMOVED DAMAGED AREA IAW SRM 51-50-02. TREATED AND PRIMED IAW SRM 51-21-02. INSTALLED REPAIR PE
- [SDR CKSA98735](https://openairdocs.org/sdr/CKSA98735.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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 51-21-02 AND 20-51-09. INSTALLED REPAIR PER L1011 SRM 53-21-00 FIG 803. FOUND DURING SCHEDULED C-CH
- [SDR CKSA98734](https://openairdocs.org/sdr/CKSA98734.md): Bulkhead · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Bulkhead
  > 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 REPLACEMENT PARTS IAW SRM 51-10-01. TREATED AND PRIMED IAW SRM 51-21-02 AND MM 20-51-09. INSTALLED R
- [SDR CKSA98733](https://openairdocs.org/sdr/CKSA98733.md): Web · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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 51-21-01. TREATED IAW SRM 51-20-02, PRIMED IAW SRM 51-09-01, INSTALLED REPAIR IAW SRM 53-31 FIG 805
- [SDR CKSA98732](https://openairdocs.org/sdr/CKSA98732.md): Bulkhead Angle · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Bulkhead
  > 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 51-40-01. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACIL
- [SDR CKSA98731](https://openairdocs.org/sdr/CKSA98731.md): Web · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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 PARTS IAW SRM 53-12-00 FIG 805. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-12-00 FIG 805
- [SDR CKSA98730](https://openairdocs.org/sdr/CKSA98730.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN O
- [SDR CKSA98729](https://openairdocs.org/sdr/CKSA98729.md): Stringer · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Longeron/Stringer
  > 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 51-10-01. TREATED, PRIMED AND INSTALLED IAW SRM 51-21-01. FOUND DURING SCHEDULED C-CHECK AND CPCP W
- [SDR CKSA98728](https://openairdocs.org/sdr/CKSA98728.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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 REPAIR PARTS IAW L1011 SRM 53-21-00 FIG 807. TREATED, PRIMED AND INSTALLED IAW SRM 53-21-00 FIG 804.
- [SDR CKSA98727](https://openairdocs.org/sdr/CKSA98727.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN
- [SDR CKSA98726](https://openairdocs.org/sdr/CKSA98726.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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 ACCOMODATE REPAIR ANGLE IAW L1011 SRM 51-40-01. CORROSION FOUND OUT OF LIMITS IAW SRM 53-21-00. FABRIC
- [SDR CKSA98725](https://openairdocs.org/sdr/CKSA98725.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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. REMOVED FASTENERS AND FABRICATED REPAIR PART IAW L1011 SRM 51-40-01 AND 53-21-00. INSTALLED REPAIR
- [SDR CKSA98724](https://openairdocs.org/sdr/CKSA98724.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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 53-23-00 FIG 801. FABRICATED REPAIR PARTS IAW SRM 53-23-00 FIG 802. TREATRED, PRIMED AND INSTALLED IAW
- [SDR CKSA98723](https://openairdocs.org/sdr/CKSA98723.md): Shear Tie · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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 PARTS IAW SRM 53-12-00 FIG 804. TREATED, PRIMED AND INSTALLED REPAIR IAW L1011 SRM 51-21-02. FOUND
- [SDR CKSA98722](https://openairdocs.org/sdr/CKSA98722.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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 INSTALLED IAW SRM 53-21-00 FIG 802. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT
- [SDR CKSA98721](https://openairdocs.org/sdr/CKSA98721.md): Shear Tie · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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 51-40-01. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACI
- [SDR CKSA98720](https://openairdocs.org/sdr/CKSA98720.md): Skin · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Plate/Skin
  > 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. REPAIRED IAW SRM 51-50-01. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT
- [SDR CKSA98719](https://openairdocs.org/sdr/CKSA98719.md): Web · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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 L1011 SRM 51-40-01, EDR L106152 AND SKETCH AIA-E2530. FOUND DURING SCHEDULED C-CHECK AND CPCP WO
- [SDR CKSA98718](https://openairdocs.org/sdr/CKSA98718.md): Floorbeam · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Floor Beam
  > 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 53-21-00 FIG 802. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINT
- [SDR CKSA98717](https://openairdocs.org/sdr/CKSA98717.md): Shear Tie · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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 PARTS IAW SRM 53-12-00 FIG 806. INSTALLED IAW SRM 51-40-01. FOUND DURING SCHEDULED C-CHECK AND CP
- [SDR CKSA98716](https://openairdocs.org/sdr/CKSA98716.md): Bulkhead Patch · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Bulkhead
  > 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 REPAIR PATCH IAW L1011 SRM 53-11-00 FIG 805. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACC
- [SDR CKSA98715](https://openairdocs.org/sdr/CKSA98715.md): Stringer · corroded · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Longeron/Stringer
  > 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 IAW SRM 53-13-00 FIG 804. INSTALLED IAW SRM 51-40-01. FOUND DURING SCHEDULED C-CHECK AND CPCP W
- [SDR CKSA98714](https://openairdocs.org/sdr/CKSA98714.md): Seat Track · cracked · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage, Seat/Cargo Attach Fittings
  > 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 WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-206, NON
- [SDR CKSA98713](https://openairdocs.org/sdr/CKSA98713.md): Frame · damaged · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Frame
  > 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 PRIMED IAW SRM 51-21-02. INSTALLED REPAIR IAW L1011 SRM 53-12-00 FIG 805. FOUND DURING SCHEDULED C-CH
- [SDR CKSA98712](https://openairdocs.org/sdr/CKSA98712.md): Strap · cut · Dec 16, 1998 · N106CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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 SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WOR
- [SDR CKSA98029](https://openairdocs.org/sdr/CKSA98029.md): Skin · damaged · Feb 10, 1998 · N106CK · Lkheed 1011385115 · Fuselage Main, Plate/Skin
  > 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 2/10/98.
- [SDR CKSA97609](https://openairdocs.org/sdr/CKSA97609.md): Skin · corroded · Dec 12, 1997 · N106CK · Lkheed 1011385115 · Fuselage Main, Plate/Skin
  > 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 AND FIG 820. CORROSION TASK CARD NUMBER C53-120-04-01. NON-ROUTINE TASK CARD NUMBER 14064.
- [SDR CKSA97608](https://openairdocs.org/sdr/CKSA97608.md): Stringer · corroded · Dec 12, 1997 · N106CK · Lkheed 1011385115 · Fuselage Main, Longeron/Stringer
  > 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. CORROSION TASK CARD NUMBER C53-120-04-02. NON-ROUTINE TASK CARD NUMBER 14062.
- [SDR CKSA97607](https://openairdocs.org/sdr/CKSA97607.md): Support · corroded · Dec 12, 1997 · N106CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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 AIR DUCT. REMOVED CORROSION IAW L1011 SRM 51-21-01. FOUND TO BE OUT OF LIMITS IAW L1011 SRM 53-21-
- [SDR CKSA97606](https://openairdocs.org/sdr/CKSA97606.md): Angle · corroded · Dec 12, 1997 · N106CK · Lkheed 1011385115 · Fuselage Miscellaneous Structure
  > 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 51-21-01. FOUND TO BE OUT OF LIMITS IAW 53-21-00. REPLACED MAIN CARGO FLOOR SUPPORT UPPER ANGLE IA
- [SDR CKSA97605](https://openairdocs.org/sdr/CKSA97605.md): Longeron · corroded · Dec 12, 1997 · N106CK · Lkheed 1011385115 · Fuselage Main, Longeron/Stringer
  > 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 51-21-01. FOUND TO BE OUT OF LIMITS IAW 53-11-00 FIG 801. INSTALLED REPAIR IAW LOCKHEED L1011 SR
- [SDR CKSA97604](https://openairdocs.org/sdr/CKSA97604.md): Frame · corroded · Dec 12, 1997 · N106CK · Lkheed 1011385115 · Fuselage Main, Frame
  > 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 BE OUT OF LIMITS IAW L1011 SRM 53-12-00 FIG 801. INSTALLED REPAIR IAW L1011 SRM 53-12-00 FIG 805.
- [SDR CKSA97603](https://openairdocs.org/sdr/CKSA97603.md): Frame · corroded · Dec 12, 1997 · N106CK · Lkheed 1011385115 · Fuselage Main, Frame
  > 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 OUT OF LIMITS IAW L1011 SRM 53-12-00 FIG 801. INSTALLED REPAIR IAW L1011 SRM 53-12-00 FIG 805.
- [SDR CKSA97602](https://openairdocs.org/sdr/CKSA97602.md): Skin · corroded · Dec 12, 1997 · N106CK · Lkheed 1011385115 · Fuselage Main, Plate/Skin
  > DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: CORROSION AROUND AFT WASTE COMPT HYD LINE BULKHEAD BOX (LT) APPROX FS1819 ABOVE S41. REMOVED CORROSION IAW L1011 SRM 51-21-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-00 FIG 801. INSTALLED REPAIR IAW S
- [SDR CKSA97601](https://openairdocs.org/sdr/CKSA97601.md): Skin · corroded · Dec 12, 1997 · N106CK · Lkheed 1011385115 · Fuselage Main, Plate/Skin
  > 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 IAW L1011 SRM 51-21-01. FOUND OUT OF LIMITS IAW L1011 SRM 53-31-00 FIG 801. REPAIRED IAW L1011 SRM

Next page: https://openairdocs.org/deregistered/N106CK-2009-09-02/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N106CK' AND deregistration_id = 'N106CK-2009-09-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N106CK-2009-09-02/reports

---
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, except the copies of manufacturers’ service documents, which belong to their rights holders.
