# Service difficulty reports: N107CK, cancelled Sep 2, 2009 A list on [N107CK, cancelled Sep 2, 2009](https://openairdocs.org/deregistered/N107CK-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. - [SDR CKSA99018](https://openairdocs.org/sdr/CKSA99018.md): Skin · cracked · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Leading Edge Devices > 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 51-10-04. FABRICATED REPAIR DOUBLER, BACK DRILLED, TRIMMED AND PRE-PROTECT AS PER SRM 51-21-02. INST - [SDR CKSA99017](https://openairdocs.org/sdr/CKSA99017.md): Blkhd Stiffener · cracked · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Fuselage Main, Bulkhead > DURING ACCOMPLISHMENT OF C-CHECK INSPECTION, FOUND FWD BULKHEAD RT SIDE I/B STIFFENER BOTTOM CORNER PREVIOUSLY REPAIRED CRACK EXTENDING APPROX 1.5. REMOVED PREVIOUS REPAIR AND TRIMMED OUT PROPAGATED CRACK ON CITED AREA AS PER SRM 51-10-04. REPAIR CARRIED OUT - [SDR CKSA99016](https://openairdocs.org/sdr/CKSA99016.md): Skin · cracked · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Fuselage Main, Plate/Skin > 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. STOP DRILLED END OF CRACK AS PER SRM 51-10-04. FABRICATED REPAIR DOUBLER AS PER SRM 53-81-20 FIG 8 - [SDR CKSA99015](https://openairdocs.org/sdr/CKSA99015.md): Doubler · cracked · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Elevator Structure > 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 51-40-01. FABRICATED REPAIR DOUBLER, DEBUR AND PRE-PROTECT AS PER SRM 51-21-02. INSTALLED DOUBLER AS - [SDR CKSA99014](https://openairdocs.org/sdr/CKSA99014.md): Fitting · cracked · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Cargo/Baggage Doors > 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 51-40-01. PRE-INSTALLED FABRICATED PARTS TO FACILITATE BACK DRILLING OF EXISTING HOLES AS PER STANDA - [SDR CKSA99013](https://openairdocs.org/sdr/CKSA99013.md): Fitting · cracked · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Cargo/Baggage Doors > 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 51-40-01. PRE-INSTALLED FABRICATED PARTS TO FACILITATE BACK DRILLING OF EXISTING HOLES AS PER STANDA - [SDR CKSA99012](https://openairdocs.org/sdr/CKSA99012.md): Skin · grooved · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Trailing Edge Flaps > 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 51-53-00 FIG 812. FABRICATED REPAIR DOUBLERS, TRIMMED, DEBUR AND REPROTECTED IAW SRM 51-21-00. INSTALLE - [SDR CKSA99011](https://openairdocs.org/sdr/CKSA99011.md): Skin · cracked · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Leading Edge Devices > 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 PER SRM 51-10-04 TO FACILITATE REPAIR REQUIREMENTS. FABRICATE REPAIR DOUBLER, BACK DRILLED AND TRI - [SDR CKSA99010](https://openairdocs.org/sdr/CKSA99010.md): Skin · cracked · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Leading Edge Devices > 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 REPAIR REQUIREMENTS AS PER SRM 51-40-01. FABRICATED REPAIR DOUBLER, TRIMMED TO SIZE, DEBUR, PRIMED AN - [SDR CKSA99009](https://openairdocs.org/sdr/CKSA99009.md): Mount · failed · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Leading Edge Slat Actuator > 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 TORQUE TUBE O/B OF NR 2 SLAT ACTUATOR DAMAGED. REMOVED AND REPLACED IAW MM 27-81-18. SLAT ACTUA - [SDR CKSA99008](https://openairdocs.org/sdr/CKSA99008.md): Rib · cracked · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Leading Edge Devices > 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 27-81-26. S/M REPAIRED CRACKED RIBS IAW SRM 57-51-00. INSTALLED NR 4 SLAT IAW MM 27-81-26. SLAT OPS - [SDR CKSA99007](https://openairdocs.org/sdr/CKSA99007.md): Rib · cracked · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Leading Edge Devices > 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 SLAT NR 7 IAW MM 27-81-26, REPAIRED CRACKED RIBS IAW SRM 57-51-00, RE-INSTALLED LT NR 7 SLAT IAW MM 27 - [SDR CKSA99006](https://openairdocs.org/sdr/CKSA99006.md): Skin · cracked · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Leading Edge Devices > 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/2940 REV ORIG DATED 3-1-99. FOUND DURING SCHEDULED C-CHECK INSPECTION AT GAMCO, INC. - [SDR CKSA99005](https://openairdocs.org/sdr/CKSA99005.md): Skin · cracked · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Fuselage Main, Plate/Skin > 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 INSTALLED REPAIR IAW AIA EA L1-53-058 REVISION ORIGINAL DATED 03-02-99. FOUND DURING SCHEDULED C-CHEC - [SDR CKSA99004](https://openairdocs.org/sdr/CKSA99004.md): Bolts · sheared · Mar 15, 1999 · N107CK · Lkheed 1011385115 · Leading Edge Slat Actuator > 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 BOLTS IAW MM 27-81-21, REPLACED TORQUE TUBE IAW MM 27-81-18. PERFORMED NDT OF SLAT ACTUATOR MOUNT B - [SDR CKSA98540](https://openairdocs.org/sdr/CKSA98540.md): Air Distr · odor · Oct 2, 1998 · N107CK · Lkheed 1011385115 · Air Distribution System > 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 FESC AND MESC, COCKPIT LIGHTING AND ECS SYSTEM FOR ELECTRICAL MALFUNCTIONS AND SECURITY. NO DEFECTS - [SDR CKSA98539](https://openairdocs.org/sdr/CKSA98539.md): Air Distr · odor · Sep 27, 1998 · N107CK · Lkheed 1011385115 · Air Distribution System > 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 FESC AND MESC. NO DEFECTS NOTED. ALL ELECTRICAL LOAD INDICATORS NORMAL. NO ELECTRICAL ODOR NO - [SDR CKSA97071](https://openairdocs.org/sdr/CKSA97071.md): Control Unit · shorted · Mar 13, 1997 · N107CK · Lkheed 1011385115 · Fire Detection > 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 NORMAL. - [SDR CKSA97010](https://openairdocs.org/sdr/CKSA97010.md): Sensor · out of adjust · Feb 6, 1997 · N107CK · Lkheed 1011385115 · Door Warning System > 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 10,000 FT, DECREASED DIFFERENTIAL PRESSURE TO 6.5 PSI AND ALL WARNING LIGHTS EXTINGUISHED. PROCEE ## 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 = 'N107CK' AND deregistration_id = 'N107CK-2009-09-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N107CK-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.