N107CK, cancelled Sep 2, 2009
Service difficulty reports · 19
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CKSA99018Skin · crackedDURING 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. INSTSDR CKSA99017Blkhd Stiffener · crackedDURING 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 OUTSDR CKSA99016Skin · crackedDURING 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 8SDR CKSA99015Doubler · crackedDURING 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 CKSA99014Fitting · crackedDURING 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 STANDASDR CKSA99013Fitting · crackedDURING 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 STANDASDR CKSA99012Skin · groovedDURING 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. INSTALLESDR CKSA99011Skin · crackedDURING 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 TRISDR CKSA99010Skin · crackedDURING 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 ANSDR CKSA99009Mount · failedDURING 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 ACTUASDR CKSA99008Rib · crackedDURING 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 CKSA99007Rib · crackedDURING 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 27SDR CKSA99006Skin · crackedLT 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 CKSA99005Skin · crackedMESC 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-CHECSDR CKSA99004Bolts · shearedDURING 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 BSDR CKSA98540Air Distr · odorELECTRICAL 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 DEFECTSSDR CKSA98539Air Distr · odorA 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 NOSDR CKSA97071Control Unit · shortedENGINE 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 CKSA97010Sensor · out of adjustCARGO 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
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