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 engine_model_key = 'CF343B1' 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 engine_model_key = 'CF343B1' 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 CHQA200800011Handle · not closedIAH TO BTR - AFTER TAKEOFF CREW RECEIVED AN"OVBD COOL" EICAS MESSAGE. THE CREW NOTICED THAT THE CABIN PRESSURE WAS ABNORMAL AND PROCEEDED TO THE UNPRESSURIZED FLIGHT PROCEDURE. WITH THE AIRCRAFT AT 4,000FT AND THE CABIN ALTITUDE AT 2,300FT THE "EMER DEPRESS SDR VNAA0801006Engine · failedCREW REPORTED A SMOKE TOILET CAUTION MESSAGE 5 SECONDS AFTER TAKEOFF. CREW ELECTED TO RETURN TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE RIGHT HAND ENGINE. MAINTENANCE FOUND EXTERIOR OIL LEAKAGE AT STAGES 2-5 OF THE SDR VNAA0801007O-Ring · faultyCREW REPORTED ON TAKEOFF ROLL THE EICAS, STATUS DISPLAY AND PFD-MFD ON THE FIRST OFFICERS SIDE WENT DARK. IN ADDITION, A GEN 2 OFF CAS MESSAGE DISPLAYED AFTER EICAS CAME BACK ON. CREW ELECTED TO ABORT THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MSDR CHQA200800010Position Sensor · malfunctionedIAH TO CMH - ON DOWNWIND LEG TO LAND AT CMH, THE FLAPS FAILED AT ZERO DEGREES. CREW FOLLOWED QRH AND MADE AN UNEVENTFUL LANDING AT CMH. MAINTENANCE TROUBLESHOT THE FLAP SYSTEM DOWN TO THE RIGHT FLAP BRAKE POSITION SENSOR. AFTER REPLACING THE POSITION SENSORSDR A6WA200840017Flap · failedON APPROACH, WHEN FLAPS SELECTED, THE FLAPS FAILED TO MOVE AND (FLAPS FAIL) EICAS MESSAGE APPEARED, DIVERTED TO PIT, LANDED WITHOUT INCIDENT. (K)SDR REXA200800003Engine · leakingON CLIMB-OUT OF MSP THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. THE FLIGHT CREW PERFORMED QRH PROCEDURES, DECLARED AN EMERGENCY AND REQUESTED TO RETURN TO MSP. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT MSP. THIS AIRCRAFT HAD PREVIOUSLY HAD ISDR A6WA20080014Flap · failedFLAPS FAILED AT 0 DEGREES ON APPROACH. (K)SDR A6WA200840030Separator · corrodedQTY 1 SEPARATOR HAS FRETTING ON LT PYLON ACCESS PANEL 421DB. (K)SDR CA080126001Windshield · broken(CAN) (CAPTAINS WINDSHIELD SHATTERED IN FLIGHT. PRESSURIZATION STAYED NORMAL AND THE AC CONTINUED. MAINT IS GOING TO CHANGE THE WINDSHIELD). REPLACED THE WINDOW WINDSHIELD, MAIN PILOT, NP-139321-13 01355H5650 TSO: 14906.50 CSO: 12838 (TC NR 20080126001)SDR AA6WA200840030Separator · damagedQTY 1 SEPARATOR HAS FRETTING ON LT PYLON ACCESS PANEL 412DB. QTY (1) SEPARATOR REPLACED ON LT PYLON ACCESS PANEL 412DB IAW SRM 51-42-06. (K)SDR CHQA200800009Pressure Valve · stuckIAH TO MOB - WHILE CLIMBING THROUGH 1,500 FEET, CREW RECEIVED RIGHT PACK HIGH PRESSURE CAUTION MESSAGE ACCOMPANIED BY FAULT LIGHT INDICATION ON RIGHT PACK BUTTON. CREW FOLLOWED QRH AND MESSAGE REMAINED. THE PACK WOULD NOT RECYCLE AND THE AIRCRAFT WOULD NOT PSDR VNAA0801005Pressure Switch · failedCREW REPORTED A RIGHT HAND ANTI ICE DUCT FAIL RED MASTER WARNING ON TAKEOFF. CREW ELECTED TO RETURN TO GNV AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE WING ANTI ICE AND CONTROL INDICATION SYSTEM ALONG WITH THE BLEED AIR LEAK SDR A6WA200840032Frame · dentedDENT EXIST ON SKIN FS 700 STR L 22 TO L 23. REMOVED FRAME IAW REO 601R-53-61-2482. NEW FRAME INSTALLED IAW SRM 51-42-06. (K)SDR A6WA20084018ABracket · unknownRT ENGINE UPPER CORE COWL STA ROD PIN AND BRACKET (SPRING CLIP) FOUND. RT ENGINE UPPER CORE COWL STAY ROD PIN REPLACED AND BRACKET (SPRING CLIP) REPLACED IAW SRM 51-42-06. (K)SDR REXA200800001Engine · leakingON CLIMB-OUT OF SGF,ON 01/15/08, THE CREW WAS ALERTED BY THE "SMOKE TOILET" WARNING. QRH PROCEDURES WERE COMPLETED, AN EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO SGF WHERE AN OTHERWISE NORMAL APPROACH AND LANDING WERE MADE. MAINTENANCE INSPECTED THE AIRSDR A6WA200840041Structure · crackedCRACK FOUND ON FLOOR STRUCTURE ON FS 280, LBL 9. DAMAGE ON FLOOR STRUCTURE AT FS 280, LBL 9 REPAIRED IAW REO 601R-53-11-171. (K)SDR CA080117010Bpsu · failed(CAN) DURING DESCENT, CREW REPORTED A FLAP FAIL CAUTION MESSAGE WITH NO FLAP SELECTION. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL FLAPLESS LANDING WAS CARRIED OUT. THE AC WAS FERRIED TO MAINTENANCE BASE WERE THE LT BRAKE POSITION SENSOR UNIT (BPSU) WAS REPLASDR CA080117011Window · failed(CAN) LT COCKPIT SIDE WINDOW SHATTERED IN DESCENT. THE CREW DID NOT REPORT ANY IMPACT OR PROBLEM WITH THE WINDOW PRIOR TO INCIDENT. VISUAL INSPECTION OF THE WINDOW INDICATES THAT ONLY THE OUTER PLY WAS DAMAGED. THE SIDE WINDOW WAS REPLACED, TESTED AND THE AC SDR A6WA200840016Bpsu · failedREF 183967/2 DUE TO RECENT FLAP HISTORY AND CRJ AMM TEMP REVISION 05-035, AIRCRAFT REQUIRES FURTHER FLAP TROUBLESHOOTING AND RECTIFICATION CW CRJ AMM TR 05-035. REMOVED AND REPLACED LT BPSU, OPS TEST GOOD IAW AMM 27-51-10. (K)SDR A6WA200840013Flap System · failedFLAPS FAIL AT ZERO ON APPROACH, DURING FLAP EXTENSION. (K)SDR A6WA200840031Support Angle · crackedANGLE CRACK ON RT HEAT EXCHANGE SUPPORT STRUCTURE BTW FS 700 AND FS 718. ANGLE REPLACED ON RT HEAT EXCHANGER SUPPORT STRUCTURE BTW BS 700 AND BS 718 IAW SRM 51-24-16 AND SRM 51-42-06. (K)SDR A6WA200840039Fitting · gougedPAX DOOR SURROUND STRUCTURE CAM FITTING GOUGE ON FS 349, STR 5L. REPLACED IWA SRM 51-42-21. (K)SDR A6WA200840044Bracket · gougedPAX DOOR SURROUND STRUCTURE ROLLER BRACKET GOUGED ON FS 349, STR 6L. SURROUND STRUCTURE NEW ROLLER BRACKET INSTALLED ON PAX DOOR AT FS 349, STR 6 IAW SRM 51-41-04. (K)SDR CA080118003Adg · unwanted deploy(CAN) WHILE AC WAS IN CRUISE AT 30000 FT, ADG DEPLOYED UN-COMMANDED. ALL ELECTRICAL SYSTEMS WERE POWERED. TRIED SWITCHING BACK TO IDG POWER. ADG WOULD NOT SWITCH OVER. MAINTENANCE REPLACED ADG AUTO DEPLOYMENT CONTROLLER AND ADG RESTORE PUMP. (TC NR 2008011800SDR A6WA200840012Cooler · vibrationAIRFRAME VIBRATION FELT AF VIBES FELT FROM T/O, TO DESCENT , WENT AWAY ON FINAL APPROACH. FELT IN REAR ON LT SIDE OF THE AC EVIDENT AT ROW 13 BUT NOT EVIDENT IN LAV. REMOVE AND REPLACED HYDRAULIC COOLER REF AMM 29-11-42, OPS CHECK GOOD. (K)SDR A6WA200840011Handle · lack of lubeSERVICE DOOR WILL NOT OPEN FROM OUTSIDE. CLEANED AND LUBED OUTER HANDLE AND OPS CK NORMAL IAW 52-41-00. (K)SDR A6WA200840021Floorbeam · crackedANGLE CRACK ON IB SIDE OF FLOORBEAM AT FS 280, RBL 9. NEW ANGLE INSTALLED ON IB SIDE OF FLOORBEAM AT FS 280, RBL 9, SRM 51-42-20. (K)SDR A6WA200840022Intercostal · crackedCRACK EXIST ON INTERCOSTAL RBL 27, FS 484. BRACKET ON INTERCOSTAL RBL 27, FS 484, REPLACED IAW SRM 51-42-06. (K)SDR A6WA200840023Floor Support · crackedCRACK EXIST ON FLOOR SUPPORT STRUCTURE FS621, LBL 41. CRACK REMOVED ON FLOOR SUPPORT STRUCTURE FS 621, LBL 41 IAW REO 601R-53-61-117. (K)SDR A6WA200840024Intercostal · crackedCRACK EXIST ON INTERCOSTAL LBL 27 AND LBL 36, FS 484. BRACKET REPLACED ON INTERCOSTAL LBL 27 AND LBL 36, FS 484. (K)SDR A6WA200840027Attach Fitting · crackedFS621.0 AT REAR PRESSURE BULKHEAD AND CARGO DOOR STRUCTURE JUNCTION, ONE CLIP CRACKED. LT FS 621.00 AT REAR PRESSURE BULKHEAD AND CARGO DOOR STRUCTURE INTERCOSTAL QTY (1) ONE CLIP REPLACED IAW SRM 51-24-16 AND SRM 51-42-21. (K)SDR A6WA200840028Bulkhead · corrodedFRETTING FOUND ON AFT OF FLIGHT COMPARTMENT OF BULKHEAD RBL 9, WL 97.50 (250 X 300) .002 DEEP. FRETTING REMOVED IAW SRM 51-12-00. SURFACE FINISH APPLY IAW SRM 51-25-16. (K)SDR A6WA200840040Floor Support · crackedCRACK ON FLOOR SUPPORT STRUCTURE FS 280, RBL 9. REPAIRED IAW REO 61R-53-11-171, REV D. (K)SDR A6WA200840042Angle · crackedONE ANGLE IS CRACKED ON LT PYLON ACCESS PANEL 412BT. ANGLE ON LT PYLON ACCESS PANEL 412BT, REPLACED IAW SRM 51-42-06. (K)SDR A6WA200840018Bulkhead · gougedGOUGE FOUND ON AFT OF FLIGHT COMPARTMENT BULKHEAD RBL9, WL 97.50 (.250 X 300). (K)SDR CHQA200800008Flap System · malfunctionedRDU TO CLE - ON DOWNWIND TO LAND AT CLE, FLAPS WERE SELECTED TO 8 AND CREW RECEIVED A FLAP FAIL MESSAGE WITH THE FLAPS FAILED AT ZERO. THE CREW RAN THE APPROPRIATE QRH CHECK LISTS AND LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE FECU AND MDC FOR FAUSDR VNAA0801003Lock · dirtyCREW REPORTED A LEFT HAND THRUST REVERSER UNLOCKED CAS MESSAGE AFTER TAKEOFF. CREW FOLLOWED THE QRH AND RETURNED TO CAK WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED THE FLEX SHAFT LOCK UNIT. MAINTENANCE OPS CHECKED THE LEFT HAND THRUST REVERSER IN ACSDR A6WA200840038Stringer Clip · crackedBTW FS 621.00 AT RT STR 14 STRINGER CLIP CRACKED. NEW STRINGER CLIP INSTALLED IAW SRM 51-42-20. (K)SDR CA080115010Latch · stuck(CAN) ON SHORT FINAL A PASSENGER GOT STUCK INTO LAVATORY COMPARTMENT. THE F/A TRIED TO UNLOCK THE DOOR LATCH BUT THE PASSENGER ELECTED TO KICK THE DOOR OFF. IMPORTANT DAMAGES WERE DONE TO THE DOOR HINGE AND LOCKING MECHANISM. AT THIS TIME, INVESTIGATION COULDSDR A6WA200840033Bracket · gougedBRACKET ASSY FWD AND AFT OF CARGO STEP PLATE FOUND GOUGED. BRACKET ASSY FWD AND AFT ON CARGO STEP PLATE REPLACED IAW SRM 51-42-21. (K)SDR A6WA200840034Nose Cowl · wornLT ENGINE UPPER NOSE COWL (432AT) AFT CORNER WORN THIN. REPLACED ON LT ENG UPPER NOSE COWL (432AT) AFT CORNER IAW CMM 71-14-01-300-814-A01. (K)SDR A6WA200840036Nose Cowl · wornLT ENGINE LOWER NOSE COWL (432AB) AFT CORNER WORN THIN.. (K)SDR A6WA200840037Bulkhead · crackedCRACK SUSPECTED ON LT FWD PRESSURE BULKHEAD FS 202.75 AT PARKING BRAKE FITTING CUTOUT. REPAIR PERFORMED ON FWD PRESSURE BULKHEAD FS 202.75 AT PARKING BRAKE CUTOUT IAW REO 601R-53-11-563. (K)SDR A6WA200840035Support Bracket · crackedMLG BAY LT HYDRAULIC SUPPORT BRACKET FOUND CRACKED. MLG BAY LT NEW HYDRAULIC SUPPORT BRACKET INSTALLED IAW SRM 51-42-06. (K)SDR A6WA200840043Support Fitting · damagedLT HANDRAIL SUPPORT FITTING CHAFED AND BENT ON PAX DOOR. REPLACED LT HANDRAIL SUPPORT FITTING ON PAX DOOR. (K)SDR A6WA200840045Handle · crackedHANDLE ASSY CRACKED ON AVIONIC BAY DOOR. HANDLE ASSY REPLACED ON AVIONIC BAY ACCESS DOOR IAW SRM 51-42-06 IAW AMM 52-41-03-400-801. (K)SDR A6WA200840029Hinge · damagedPASSENGER DOOR VERTICAL FOLDING STEP HINGE REPLACED IAW SRM 51-42-06. (K)SDR CA080112001Adg · unwanted deploy(CAN) A/C RETURNED DUE TO ADG UNCOMMANDED DEPLOYMENT ON T/O. PRESENTLY THE AUTO DEPLOYMENT SYS IS UNDER MEL UNTIL MAINT PERMITS. UPDATE FURTHER WHEN T/S HAS BEEN C/O. (TC NR 20080112001)SDR CA080117001Engine · flamed out(CAN) FLIGHT,IN CRUISE, LT ENGINE FLAMED OUT WITH NO PREVIOUS WARNINGS. FLIGHT CREW TRIED TO RESTART LT WITHOUT SUCCESS. AC LANDED. NO ENGINE EXCEEDANCES FOUND. NO EVIDENCE OF WATER CONTAMINATION IN MAIN FUEL TANKS AND FUEL FILTER HOUSING. PERFORMED A VISUAL SDR A6WA200840076Floor Support · corrodedFLOOR SUPPORT CORRODED AT FS 589.0 TO 605.0 NL 73.50 LBL 10.0. (K) REPAIRED IAW REO 601R-53-00-027 REV C. (M)
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