N724CK
Service difficulty reports · 154
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 = 'N724CK' AND registry_match = 'registration' 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 = 'N724CK' AND registry_match = 'registration' 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 K11A2020013172401Floorbeam · corrodedCORROSION ON LOWER SURFACE OF UPPER CHORD OF FLOORBEAM STA 620 LBL 2SDR K11A2020020647402Floorbeam · corrodedCORROSION ON MAIN DECK FLOORBEAM @ STA 500 LBL 10 TO RBL 10SDR K11A2020020647401Seat Track · corrodedCORROSION ON MAIN DECK STA 500 BL 0SDR K11A2019091172406Intercostal · crackedINTERCOSTAL CRACKED @ STA 850-870 INBETWEEN STR 8 & 9R.SDR K11A2019091172405Skin · corrodedEVIDENCE OF CORROSION ON FUSELAGE SKIN @ STA 869 BETWEEN STR 8 & 9R.SDR K11A2019091172404Skin · corroded@ STA 1161, LAP SEAM STR 20L, EXTERNAL SKIN HAS AREA OF PULLING FASTENERS & PILLOWING SKIN.SDR K11A2019091172403Frame Splice · crackedULTRASONIC INDICATIONS FOUND @ STA 870 FRAMESPLICE @ STR 9L IN CENTER OF TERMINAL FITTING O/B FLANGE.SDR K11A2019091172402Frame Splice · crackedULTRASONIC CRACK INDICATION FOUND @ STA 870 FRAME SPLICE @ STR 9R IN CENTER OF TERMINAL FITTING O/B FLANGE.SDR K11A201991172401Web · crackedRT SIDE OF AIRSTAIRS LIGHTNING HOLE CRACKED @ STA 1293 RBL 20.5.SDR K11A2019011401Clamp · looseDURING THE CLIMB PHASE OF FLIGHT CABIN ALTITUDE CLIMBED AT 1500’/MIN AFTER CLIMBING THROUGH 20000 FEET CABIN PRESSURIZATION COULD NOT BE CONTROLLED, DECENT BELOW 10000 REQUIRED AND RETURNED TO KYIP. CORRECTIVE ACTION: UPON INVESTIGATION FOUND RT MOISTURE SEPARSDR K11A2018111672401Pitot Line · cloggedDURING THE CLIMB PHASE OF FLIGHT (THROUGH FL250) THE ELEVATOR FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED. NO OTHER INDICATIONS OCCURRED. PILOT CALLED FOR AND COMPLIED WITH CHECKLIST. PILOT THEN COORDINATED WITH OPS TO DIVERT TO KLRD
CORRECTIVE ACTION: FOUNSDR K11A2018112972402Stringer · crackedSTRINGER CRACKED AT STA 294.5 STR 15L @ UPPER & LOWER FASTENER HOLES COMMON TO FRAMESDR K11A2018112972401Stringer · crackedSTRINGER CRACKED AT STA 294.5 STR 14L @ UPPER & LOWER FASTENER HOLES COMMON TO FRAMESDR K11A2018112124013Beam · crackedVERTICAL STAB KICK LOAD BEAM WEB POST CRACKED.SDR K11A2018112124012Structure · corrodedINNER CHORD ABOVE #2 ENGINESDR K11A2018112124011Structure · corrodedINNER CHORD ABOVE #2 ENGINE RIGHT SIDE HAS AREAS OF CORROSION.SDR K11A2018112124010Structure · corrodedOUTER CHORD ABOVE #2 ENGINE HAS CORROSIONSDR K11A2018112124009Support Rib · corrodedFUSELAGE SKIN SUPPORT RIB ABOVE #2 ENGINE HAS CORROSION ON RIGHT SIDE.SDR K11A2018112124008Skin · crackedFUSELAGE SKIN, 1 INCH CRACK. UNDER ENGINE INLET FWD END OF CAVITY THROUGH ACCESS PANELS 9521 AND 9522, ON FUSELAGE.SDR K11A2018112124007Skin · corrodedFUSELAGE EXTERIOR CORROSION. #2 ENGINE RIGHT SIDE ABOVE COWLING.SDR K11A2018112124006Web · crackedWEB CRACK ON KICKLOAD BEAMSDR K11A2018112124005Shear Tie · crackedSHEAR TIE CRACK ON KICKLOAD BEAMSDR K11A2018112124004Floorbeam · corrodedFLOOR BEAM CORROSIONSDR K11A2018112124003Floorbeam · corrodedFLOOR BEAM CORROSIONSDR K11A2018112124002Support Angle · crackedSUPPORT ANGLE CRACKED IN RIGHT WHEEL WELLSDR K11A2018112124001Skin · crackedCRACK IN EXTERIOR SKIN ABOVE LEFT AFT EMERGENCY EXIT HATCH, ABOVE HANDLE.SDR K11A2018040372401Warning System · false activationCARGO FIRE BELL AND LIGHT ACTIVATED AT APPROXIMATELY 20,000 FT. DURING CLIMB OUT. WARNINGS CEASED AFTER APPROXIMATELY ONE MINUTE. ACCOMPLISHED EMERGENCY PROCEDURES AND RETURNED TO DEPARTURE. PERFORMED AN OPS CHECK OF THE CARGO SMOKE DETECTION SYSTEM. OPS CSDR K11A2017092072401Not Reported · malfunctionedAIRCRAFT WOULD NOT PRESSURIZE.SDR K11A2016090924001Shear Tie · corrodedSHEAR TIE CORRODED BS 720A BETWEEN STRINGERS 27 - 28R.SDR K11A2016062572401Drive Unit · defectiveOTBD FLAPS RETRACTED FROM 25 DEGREES TO 0 ON FINAL APPROACH UNCOMMANDED. LEADING EDGE DEVICES ALSO RETRACTED. REPLACED OUTBOARD FLAP DRIVE POWER UNIT.SDR K11A2016051072401Switch · failedGEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. REPLACED CONTROL LEVER POSITION SWITCH, OP'S CHECKED GOOD IAW AMM 32-61-12.SDR K11A2015121124002Spar · corrodedVERTICAL STABILIZER INTERIOR REAR SPAR CORROSION BS 1342, RBL 5.SDR K11A2015121124001Mount · corrodedNR 1 PYLON LOWER SIDE OF FWD MOUNT FITTING HAS CORROSION ON AND AROUND FASTENERS.SDR K11A2015121124006Trunnion · corrodedRIGHT UPPER NLG TRUNNION CAP EVIDENCE OF CORROSION ON OTBD FACE.SDR K11A2015121124009Skin · corrodedLAP SEAM AREA OF CORROSION BS 1101, STR 10L.SDR K11A2015121124008Frame · crackedFRAME WEB CRACKED BS 1303 OTBD END.SDR K11A2015121124005Trunnion · corrodedNLG LT UPPER TRUNNION CAP EVIDENCE OF CORROSION ON OTBD FACE.SDR K11A2015121124004Trunnion · corrodedTRUNNION CAP EVIDENCE OF CORROSION BOTH INBD AND OTBD FACE, NLG.SDR K11A2015121124007Fitting · corrodedSEVERAL CORRODED FASTENERS ON RIGHT SIDE OF S-DUCT FIREWALL FITTING.SDR K11A2015052172401Warning Light · illuminatedNR 2 ENGINE FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. PERFORMED PRECAUTIONARY SHUTDOWN IAW ABNORMAL PROCEDURES AND RETURNED TO DEPARTURE.SDR K11A2013062024001Pump · inoperativeAFTER TAKEOFF, LOST (B) SYSTEM HYDRAULICS, REPLACED RT (B) SYSTEM HYDRAULIC PUMP IAW AMM 29-12-11, SERVICED HYD IAW AMM 12-12-01, PERFORMED SYSTEM TEST IAW AMM 29-12-11, OPS CHECK GOOD, NO LEAKS NOTED.SDR K11A2012112924001Gyro · defectiveF/O'S HSI COMPASS CARD FAILED, RETURNED TO HOME BASE, NO EMERGENCY PROCEDURES TAKEN. PART RETURNED FROM VENDOR WITH THE FOLLOWING FINDINGS, HOUSING LOOSE, FOUND OPEN LAMPS, BACKPLATE LOOSE, BOTH POINTERS STICKING, MOTOR AND GEARS DIRTY. THIS REPORT IS A FOLLOSDR K11A2012062824001Tru · malfunctionedNR 2 GEN RT SYNC LIGHT REMAINED ILLUMINATED AFTER SYNCHRONIZING GEN WITH STANDARD BLEED CONFIGURATION AT 35,000 VISIBLE SMOKE IN COCKPIT CAME FROM AROUND PILOTS FEET, PACKS WERE FULL COLD COOLING DOOR HALF OPEN, 1 PACK TEMP IND RIGHT TEMP 50 DEGREES RAN A/C SMSDR K11A201151172402Stringer · corrodedSTRINGER CORROSION, 10 INCHES.SDR K11A2011052672407Shear Tie · corrodedSHEAR TIE CLIP CORROSION, 6 INCHES, STA 1130 STRINGER 20 TO 21 LEFT.SDR K11A2011051172401Pressure Panel · crackedNOSE WHEEL PRESSURE WEB CRACK.SDR K11A2011052672406Stringer · corrodedSTRINGER CORROSION, STA 950E PLUS 16 INCHES TO = 20 INCHES STRINGER 30, 20 INCH CORROSION.SDR K11A2011052672405Skin · corrodedSKIN CORROSION, STA 720B PLUS 8 INCHES STRINGER 28R, 2 X 3 INCHES.SDR K11A2011052672404Seat Track · corrodedSEAT TRACK CORROSION, 60 INCHES, STA 1010 TO 1070 LBL 46.SDR K11A2011052672403Floorbeam · corrodedFLOORBEAM CORROSION AT STA 1130 LBL 28 AND 43.
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