N332CK
Service difficulty reports · 57
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 = 'N332CK' 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 = 'N332CK' 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 K11A2025091800342Floor Support · corrodedFLOOR SUPPORT IN FWD PIT AT STA 485 LBL 18.2 CORRODEDSDR K11A2025091900347Floorbeam · corrodedFLOORBEAM LOWER CHORD AT STA 767 APPROX RBL 34 HAS CORROSION.SDR K11A2025091900346Floorbeam · corrodedFLOORBEAM LOWER TEE AT BS 747 AT APPROX RBL 24 TO RBL 45 IS CORRODED.SDR K11A2025091800344Stringer · corrodedEVIDENCE OF CORROSION ON STRINGER 21R AT STA 890.SDR K11A2025091800343Stringer · corrodedEVIDENCE OF CORROSION ON STRINGER 22R AT STA 880.SDR K11A2025091700341Skin · cracked#1 PYLON PANEL 5724L OPENING ON I/B SIDE OF #1 PYLON HAS EVIDENCE OF POSSIBLE CRACK EXTENDING PAST STOP DRILL ON PYLON SKIN AND DOUBLER.SDR K11A2025080800338Stiffener · corrodedEVIDENCE OF CORROSION ON BOTTOM SECTION OF VERTICAL STIFFENER ON FWD SIDE OF STA 227 BULKHEAD BL0SDR K11A2025092200351Stringer · corrodedEVIDENCE OF CORROSION ON STRINGER 26L AT STA 907SDR K11A2025080800337Stiffener · corrodedEVIDENCE OF CORROSION ON STIFFENER IN FWD ACCESSORY COMPARTMENT STA 219 - 227 BL-0.SDR K11A2025091900345Skin · corrodedSTATION 226 RBL 7 TO LBL 2 EVIDENCE OF CORROSION UNDER LEVELING COMPOUND ON A/C SKIN.SDR K11A2025091700340Stiffener · corrodedSTIFFENER AT STATION 352 BETWEEN STRINGER 27R AND 26R HAS EVIDENCE OF CORROSIONSDR K11A2025073000334Frame · corrodedFRAME IN FWD PIT STA 520 BETWEEN STR 26R-27R HAS EVIDENCE OF CORROSION ON LWR LEG.SDR K11A2025071800328Keelbeam · corrodedKEEL BEAM FOUND TO HAVE EVIDENCE OF CORROSION IN FWD PIT AT APPROX STA 500D STR-28R.SDR K11A2025070900333Intercostal · corrodedINTERCOSTAL ASSY HAS EVIDENCE OF CORROSION ON AFT SIDE OF FWD GALLEY DOOR SURROUND STRUCTURE AT APPROX STA 332-344 STR 16RSDR K11A2025070900332Intercostal · corrodedINTERCOSTAL ASSY HAS EVIDENCE OF CORROSION ON AFT SIDE OF FWD GALLEY DOOR SURROUND STRUCTURE AT APPROX STA 332-344 ABOVE STR 13RSDR K11A2025070300330Door · corrodedWEB HAS EVIDENCE OF CORROSION ON AFT SIDE OF FWD GALLEY DOOR SURROUND STRUCTURE AT APPROX STA 332 - 344 STR 7.SDR K11A2025091900348Floorbeam · damagedDAMAGED ANGLE ON FWD SIDE OF STA 1016 BBL 0.00 FLOOR BEAM AT AFT CARGO COMPARTMENTSDR K11A2025080400335Floor Support · corrodedL/H AFT CARGO FLOOR SUPPORT AT LBL 12 HAS CORROSION UNDER NUTPLATE APPROX 6 INCHES AFT OF STA 727D.SDR K11A2025092200350Stringer · corrodedEVIDENCE OF CORROSION ON STRINGER S25L STA 927 AT AFT CARGO COMPARTMENT.SDR K11A2025061300329Skin · corroded#3 SLAT HAS EVIDENCE OF CORROSION ON UPPER SURFACESDR K11A2025071800326Skin · corrodedEVIDENCE OF CORROSION ON FUSELAGE SKIN NEAR STA 520 STR 0SDR K11A2025080700336Floorbeam · corrodedFLOOR BEAM IN AFT PIT CEILING AT STATION 727B HAS CORROSION AROUND FASTENER HOLES FROM LBL 4 TO LBL 58SDR K11A2025021800299Autopilot Sys · faultedAUTO PILOT CMD IN A AND B WILL NOT ENGAGE. PERFORMED DFCS BITE CHECK IAW B737 AMM 22-11-34. OPS CHECK GOOD NO FAULTS STORED. COULD NOT DUPLICATE ON GROUND, THIS CLEARS DMI 33200051 PLACARDS REMOVED.SDR K11A2024070800265Connector · brokenCABIN ALTITUDE WARNING HORN AND LIGHT CAME ON DURING FLIGHT @ FL 360. LEFT BLEED WAS SHOWING 12 PSI AND RIGHT BLEED WAS SHOWING 38 PSI. REMOVED AND REPLACED CONNECTOR D1208 IAW SWPM 20-61-11. PERFORMED ENGINE RUN IAW AMM 71-00-00. EGT SYSTEM OPS CHECKS GOOD ISDR K11A2024062800064Cabin Pressure · faultedCABIN ALTITUDE WARNING HORN AND LIGHT CAME ON DURING FLIGHT @ FL 360. LEFT BLEED WAS SHOWING 12 PSI AND RIGHT BLEED WAS SHOWING 38 PSI.SDR K11A2024050600356Controller · defectiveWHILE ON DESCENT LOST CABIN PRESSURE AT 33,000 FEET MADE EMERGENCY DECENT BOTH PACKS OPERATED NORMAL NO PACK TRIP. CORRECTIVE ACTION: REMOVED AND REPLACED CABIN PRESSURE CONTROLLER OPS CHECK GOOD.SDR 2024FA0000351Cabin Pressure · failedWHILE ON DECENT LOST CABIN PRESSURE AT 33,000 FEET MADE EMERGENCY DECENT BOTH PACKS OPERATIONAL NORMAL NO PACK TRIP.SDR K11A20240212000Sense Line · unsecureAIRSPEED INDICATOR F/O SIDE ROSE TO 62 KTS AND STOPPED. FAILED 80 KTS CHECK. CORRECTIVE ACTION: RESECURED FIRST OFFICERS AIR DATA COMPUTER Q.D. SENSE LINE IAW B737 AMM 34-12-11. OPS CHECK GOOD.SDR K11A2023101090035Unknown · unknownDURING CLIMB ENGINE 1 WOULD NOT ACHIEVE COMMAND POWER SETTING AFTER INITIAL THRUST REDUCTION FROM TAKEOFF POWER ENGINE 1N HUNG BELOW 70% WHILE N2 INCREASED TO LIMITS.SDR K11A2021122100107None · nonePROBLEM DESCRIPTION: RIGHT PACK TRIP UNABLE TO CONTROL CABIN PRESSURE UNTIL 10,000 FEET. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: REMOVED DEBRIS FROM AFT PIT DOOR, PERFORMED CABIN PRESSURIZATION CHECK IAW B737 AMM 21-31-00 OPS CHECK GOOD NO DEFECTS NOTSDR K11A2021082400067Controller · intermittentINTERMITTENT CONTROL OF PRESSURIZATION. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: R&R CABIN PRESSURE CONTROL PANEL IAW B737 AMM 21-31-21 OPS CHECK GOOD IAW B737 AMM 21-31-00 NO DEFECTS NOTEDSDR K11A2021030100046Unknown · vibrationDURING FUNCTIONAL FLIGHT FOR FLAP REMOVAL EXPERIENCED HIGH FREQUENCY BUFFET CLIMBING THROUGH FL 240 @ 280 KIAS, CLEAN WING. INSPECTED AND OPS CHECK TRAILING EDGE FLAPS, LEADING EDGE FLAPS AND KRUEGER FLAPS IAW AMM 27-51-00, 27-81-00 NO DEFECTS NOTED. AIRCRAFTSDR K11A2020091540011Window · crackedL5 WINDOW CRACKED IN FLIGHT. AIRCRAFT RETURNED TO KSAT. R & R L5 WINDOW, IAW AMM 56-11-31.SDR K11A20200105325Skin · damagedSKIN DAMAGED STA 1080 FWD OF APU ACCESS DOORSDR K11A20200105313Structure · crackedAT STA 291.5 STR 14R R1 DOOR LOWER HINGE CUTOUT HAS CRACK INDICATIONSDR K11A20200105324Fitting · corrodedLT HORIZONTAL STAB FWD LOWER FITTING CORRODEDSDR K11A20200105323Tee Fitting · crackedAT STATION 277-360 STR 20L OUTER "T" CHORD IS CRACKEDSDR K11A20200105322Floorbeam · corrodedMAIN DECK FLOOR BEAM STA 312 LBL 12 HAS CORROSION AT INTERSECTIONSDR K11A20200105321Stringer · corrodedR/H TORQUE BOX STRINGER STA 1088-1156 IS CORRODEDSDR K11A20200105320Stringer · corrodedR/H TORQUE BOX STRINGER STA 1088-1130 IS CORRODEDSDR K11A20200105319Skin · crackedCRACK INDICATION AT STA 500 = 11" STR 14RSDR K11A20200105318Support Fitting · crackedL/H WING @ THE MAIN LANDING GEAR SUPPORT BEAM SUPPORT FITTING REAR SPAR STA 224.14 @ UPPER CHORD CRACKED INDICATIONSDR K11A20200105317Stiffener · crackedCRACK FOUND ON STIFFNER LBL 6.15 ON THE WING CENTER SECTION REAR SPARSDR K11A20200105316Stiffener · crackedCRACK FOUND ON STIFFNER RBL 6.15 ON THE WING CENTER SECTION REAR SPARSDR K11A20200105315Support Fitting · crackedRIGHT WING AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM IS CRACKEDSDR K11A20200105314Support Fitting · crackedLEFT WING AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM IS CRACKEDSDR K11A20200105312Seat Track · corrodedAT STA 636-663 LBL 60MAIN DECK SEAT TRACK HAS AREAS OF CORROSIONSDR K11A20200105311Cusp Web · crackedCUSP WEB CRACKED FWD OF BS 639 RBL 70SDR K11A20200105310Cusp Web · crackedCUSP WEB CRACKED AFT OF BS 616 RBL 64SDR K11A20200105309Cusp Web · crackedCUSP WEB CRACKED AFT OF BS 616 LBL 64 & LBL 70
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