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 CA011123006Window · cracked(CAN) CLIMBING THROUGH 22,5000 FT, CAPTAINS SIDE WINDOW CRACKED. DIVERTED TO IND AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT FERRIED BACK TO CVG FOR WINDOW REPLACEMENT.CAPTAINS SIDE WINDOW REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR CA011123002Beam · cracked(CAN) THE ENGINE SUPPORT BEAM UPPER WEB CRACKED AT FS 640 RBL 9.5 AT 7.6 INCHES LONG AND ANGLE CRACKED AT 0.23 INCHES. THIS WAS FOUND WHILE PERFORMING THE SB A601R-53-059.DISCREPANCIES WILL BE REPAIR USING BOMBARDIER DISPOSITIONS.SDR CA011128001Connector · failed(CAN) APU CHARGER STATUS MESSAGE CIRCUIT BREAKER POPPED - ON TAXI OUT. WHEN MECHANIC RESET THE CIRCUIT BREAKER THE CONNECTOR PLUG ON TOP OF THE CHARGER CAUGHT FIRE. REPAIRED CONNECTOR PLUG BY REPINING ALL ASSOCIATED WIRES. REPLACED APU BATTERY & CHARGER. COMPOSDR SWIA200110359Wire · brokenSTAB TRIM CH2 WILL NOT ENGAGE. REPAIRED WIRE CD91A22 AT CONNECTOR J6CD IN CARGO BAY. STAB TRIM OPS CHECK GOOD IAW AMM 27-41-00.SDR CA011122003Window · cracked(CAN) DURING THE FIRST FLIGHT AT CRUISING ALTITUDE THE RIGHT SIDE COCKPIT WINDOW (OUTER PLY) CRACKED, THE PILOT DECIDED TO RETURN THE AIRCRAFT TO POINT OF DEPARTURE. THE RIGHT SIDE COCKPIT WINDOW REPLACED. AIRCRAFT RETURNED IN SERVICE.SDR CA011122004Windshield · cracked(CAN) DURNG CRUISE AT FL260, DELTA P 7.8 PSI, THE LT WINDSHIELD OUT PLY CRACKED. THE FLIGHT WAS COMPLETED UNEVENTFULLY AND THE WINDSHIELD WAS REPLACED IN MUNICH. AIRCRAFT RETURNED IN SERVICE.SDR CA011122007Fuel Control · leaking(CAN) NR 2 MFC FUEL LEAK THROUGH THE THROTTLE SHAFT BODY. NR 2 ENGINE FUEL LEAK DISCOVERED DURING ROUTINE INSPECTION. RT ENGINE COWLING OPENED. LEAK COMING FROM THE NR 2 MFC THROTTLE SHAFT BODY. EVIDENCE OF FIRE MARKS IN THE CORE COWL AND JET PIPE. NO FIRE WARSDR CA011122008Support · cracked(CAN) ENGINE SUPPORT BEAM CRACKED ON TOP WEB 7TH RIVET OUT TO LEFT OF BL 0 AT AFT ROW OF RIVETS. CRACK IS FROM RIVET TO AFT EDGE OF MATERIAL. AIRCRAFT FERRIED FROM CINCINNATI TO HOT SPRINGS FOR REPAIR.SDR CA011113022Charger · failed(CAN) APU CHARGER STATUS MESSAGE POSTED - CIRCUIT BREAKER POPPED - NO TAXI OUT. WHEN MECHANIC RESET THE C/B THE CONNECTOR PLUG ON TOP OF THE CHARGER CAUGHT FIRE.REPAIRED CONNECTOR PLUG BY REPINNING AND ASSOCIATED WIRES. REPLACED APU BATTERY & CHARGER. AFFECTEDSDR CA011113021Adc · failed(CAN) PRIMARY FLIGHT DISPLAY (PFD) NR 1 AND MULTIFUNCTION FLIGHT DISPLAY (MFD) NR 1, BOTH FLICKERED OFF FOR APPROXIMATELY 1-2 MINUTES THEN CAME BACK ON. FMS GETS FMS NAV INVALID ON GROUND. UNABLE TO GET COURSE UNTIL AIRCRAFT INFLIGHT. CAPTAINS PFD LOOSES DATA SDR CA011113023Support · cracked(CAN) FOUND ON REPAIR INSPECTION. 0.5 INCH CRACK FOUND AT ONE LOCATION ON TIP WEB 7TH RIVET TO THE RIGHT OUT FROM BL 0 (CLOSE TO RBL 9.50). AIRCRAFT FERRIED FROM CINCINNATI TO HOT SPRINGS FOR REPAIR. WHILE PERFORMING SB A601R-53-059.SDR CA011113001Pump · failed(CAN) ENGINE FLIGHT SHUT DOWN DUE TO "ENGINE OIL PRESS" MESSAGE AND "ENGINE OIL" AURAL MESSAGE ON THE LEFT ENGINE. THE AIRCRAFT WAS CRUISING AT FL410.OIL LEVEL CHECKED WITHOUT REMARKS, OIL FILTER AND CHIP DETECTOR CHECKED WITHOUT REMARKS, B SUMP SCAVENGES SCRESDR CA011113015Support · cracked(CAN) FOUND CRACK ON UPPER WEB OF ENGINE SUPPORT BEAM DURING SB A601R-53-059 AT FS 640 NEAR RBL 7.0. CRACK WAS 0.125 INCHES LONG. REPAIRED IAW REO 601R-53-345 (UPPER AND LOWER WEBS). ALSO CARRIED OUT REO 601R-53-61-366 (BOTH SIDES).SDR CA011113005Switch · failed(CAN) AFTER TAKEOFF DURING BLEEDS TRANSFER, LT PACK HI PRESSURE AND RT PACK HI TEMP APPEARED ON EDI.FLIGHT ABORTED. REMOVED AND REPLACED THE RT COMPRESSOR OUTLET TEMP SWTICH. AIRCRAFT RETURNED TO SERVICE.SDR CA011113004Switch · failed(CAN) DURING FLIGHT 5280 FROM WILKES-BARRE / SCRANTON, PA (AVP) TO CINCINNATI OH (CVG). STAB TRIM & MACH TRIM CAUTION MESSAGES ON CLIMBOUT. FOLLOWED QRH PROCEDURE AND TRIMS WOULD NOT RESET. DECALRED AN EMERGENCY AND MADE AN UNSCHEDULED LANDING AT PITTSBURGH, PSDR CA011101013Connector · failed(CAN) FOUND CONNECTOR P28EZ AT THROTTLE GEAR BOX SHORTED TO GROUND. REPLACED CONNECTOR AND OPS CHECKED SERVICEABLE. AIRCRAFT RETURNED TO SERVICE.SDR CA011101016Pump · failed(CAN) THE CREW REPORTED THAT, HYDRAULIC QUANTITY 3 DROPPED TO ZERO. AIRCRAFT LANDED INTO ZARAGOZA. FINDINGS: PUMP 3A WAS REPLACED AND SYSTEM 3 REPLENISHED.SDR CA011101017Windshield · cracked(CAN) PILOT REPORT DURING FLIGHT LT WINDSHIELD INNER PLY CRACKED. PILOT CARRIED OUT THEIR QRH. MAINTENANCE REMOVED AND REPLACED LT COCKPIT WINDOW.AIRCRAFT BACK IN SERVICE.SDR CA011101009Web · cracked(CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM AT THE LOWER WEB FS 630, BL R36. WHILE PERFORMING SB A601R-53-059.AREA TO BE REPAIRED IAW REO 601R-53-61-361.SDR CA011101010Web · cracked(CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM AT THE LOWER WEB FS 630, LBL 36, WHILE PERFORMING SB A601R-53-059.AREA TO BE REPAIRED IAW RBO 601R-53-61-361.SDR CA011101011Web · cracked(CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM AT THE LOWER WEB FS 630, LBL 36, RBL 36 WHILE PERFORMING SB A601R-53-059. AREA TO BE REPAIRED IAW REO 601R-53-61-361.SDR A6WA200100062Oil System · overservicedNR 2 ENGINE HIGH OIL TEMP, PRECAUTIONARY ENGINE SHUTDOWN, NR 2 ENGINE OIL TEMP 158 DEGREES, PSI 40. MAINTENANCE INSPECTED AND FOUND NR 2 ENGINE OIL OVERSERVICED. REMOVED EXCESS OIL, GROUND RAN AIRCRAFT, OPERATIONAL CHECK GOOD.SDR CA011101005Actuator · inoperative(CAN) ON APPROACH, WHEN EXTENDING THE FLAPS, THE FLAP FAIL MESSAGE APPEARED AT 23 DEGREES. THE RIGHT OUTBOARD FLAP TWISTED, (OUTBOARD ACTUATOR STOPPED TRAVELLING). FOUND THE RT OUTBOARD FLAP TWISTED AND ACTUATOR NR 4 NOT OPERATIONAL.SDR CA011101007Windshield · cracked(CAN) LT SIDE WINDOW CRACKED 35 CM. THE DETAILED INSPECTION SHOWED CRACKS IN THE INNER PLY IN THE LOWER PART OF THE WINDOW. REMOVED AND REPLACED THE WINDOW.SDR CA011101008Beam · cracked(CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM. ONE EACH AT THE CUT OUT FOR THE ACCESS PANELS.SDR CA011101002Seal · failed(CAN) DURING A FLIGHT IN CLIMB AT FL220, UN-COMMANDED DEPRESSURIZATION OF THE AIRCRAFT OCCURRED. THE CREW DID AN EMERGENCY DESCENT TO FL60 AND DIVERTED. THE FLIGHT ATTENDANT NOTICED A LOUD WHISTLE COMING FROM THE PAX DOOR AT THE TIME.AIRCRAFT LANDED WITH NO FUSDR CA011101003Line · leaking(CAN) PILOTS REPORTED HYD 1 LO PRESS CAUTION MESSAGE ON IN FLIGHT. PRESSURE AND QUANTITY AT ZERO. EXECUTED APPROPRIATE CHECK LISTS. ENGINE DRIVEN PUMP RAN DRY FOR 37 MINS. REMOVED AND REPLACED NR 1 EDP IAW 29-13-00 DUE TO BEING RAN DRY. REMOVED AND REPLACED NRSDR CA011101004Web · cracked(CAN) DURING C-CHECK ZONAL INSPECTION COMPLIED WITH SB 601R-53-059, FOUND A CRACK ON ENGINE SUPPORT BEAM AT THE UPPER WEB FS 640, RBL 18. AREA TO BE REPAIRED IAW REO 601R-53-61-439.SDR CA011101001Mount · cracked(CAN) FOUND CRACK ON ENGINE SUPPORT BEAM WHILE PERFORMING SB A601R-53-059. FOUND CRACKS ON UPPER WEB AT LBL 8 FROM THE FASTENER TO THE AFT EDGE. RBL 8 (1.5 INCHES LONG) AND LOWER WEB EXTENDING FROM EACH ACCESS PANELS CUTOUTS R/H INBOARD FORWARD RADIUS 0.25 INCSDR CA011019014Pump · failed(CAN) DURING CRUISE, NR 2 ENGINE OIL PRESSURE RAPIDLY ROLLED BACK FROM 65 TO 24 PSI. THE FLIGHT CREW THROTTLED BACK THE ENGINE TO IDLE AND OIL PRESSURE SLOWLY CLIMBED TO 45 PSI. CREW ADVANCED THROTTLE TO 90 PERCENT AND OIL PRESSURE AGAIN ROLLED BACK TO 25 PSI.SDR CA011019019Selector Valve · faulty(CAN) DURING APPROACH WHEN THE LANDING GEAR WAS SELECTED DOWN, THE NOSE LANDING GEAR (NLG) DID NOT COME DOWN AND THE WARNING MESSAGE "GEAR DISAGREE" WAS POSTED. THE CREW SELECTED THE MANUAL GEAR RELEASE HANDLE AND THE NLG CAME DOWN. THE AIRCRAFT LANDED WITH NOSDR CA011019017Web · cracked(CAN) DURING C-CHECK COMPLIED WITH SB A601R-53-059. FOUND CRACKS ON UPPER WEB AT LBL 8 (1.2IN ), RBL 8 (3.5IN) AND LOWER WEB AT LBL 8 (0.5").AREAS TO BE REPAIRED IAW REOS 601R-53-61-345 AND -366.SDR CA021002003Windshield · cracked(CAN) THE LT FRONT COCKPIT WINDSHIELD OUTER PANE CRACKED ON CLIMB. THE A/C RETURNED FOR REPLACEMENT OF THE WINDSHIELD. REMOVE AND REPLACED WINDSHIELDSDR CA011011005Control Unit · failed(CAN) PILOT REPORT: GROUND SPOILER DEPLOYED DURING TAKEOFF ROLL. MAINTENANCE FOUND SECU (SPOILER ELECTRONIC CONTROL UNIT), S/N 396, INTERNAL FAULT. REMOVED AND REPLACED.AIRCRAFT BACK IN SERVICE.SDR CA011011004Tire · failed(CAN) PILOT EPORT: AFTER TAKEOFF, THE TOWER NOTIFIED THEY HAD SEEN DEBRIS DEPART THE AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LT INBOARD TIRE ON MAIL LANDING GEAR. AIRCRAFT BACK IN SERVICE.SDR SWIA200110203Latch · malfunctionedCABIN DOOR DIFFICULT TO OPEN FROM INSIDE OR OUT.REPLACED TRIGGER ON MAIN PASSENGER HANDLE LATCH IAW CMM 52-11-03.SDR CA011019021Window · failed(CAN) PILOT REPORT DURING FLIGHT LT COCKPIT WINDOW INNER PLY SHATTERED. PILOT CARRIED OUT THEIR QRH. MAINTENANCE REMOVED AND REPLACED LT COCKPIT WINDOW.AIRCRAFT BACK IN SERVICE. SERIAL NUMBER: 9929H2174SDR CA011005010Smoke Detector · failed(CAN) PILOT REPORT "SMOKE CARGO" INDICATION IN FLIGHT. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR AND AIRCRAFT BACK IN SERVICE.SDR CA011005012Packing · broken(CAN) PILOT REPORT LT ENGINE IN FLIGHT SHUT DOWN WAS CARRIED OUT AS A PRECAUTIONARY MEASURE. MAINTENANCE FOUND PACKING ON HYDRAULIC PAD BROKEN. PACKING REMOVED AND REPLACED.AIRCRAFT BACK IN SERVICE.SDR CA011005009Pump · damaged(CAN) PILOT REPORT LOSS OF NR 3 HYDRAULIC PRESSURE IN CRUISE. MAINTENANCE REMOVED AND REPLACED EDP (ENGINE DRIVEN PUMP) 3A AND AIRCRAFT BACK IN SERVICE.SDR CA030417008Bushing · loose(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.SDR CA011005008Attach Fitting · failed(CAN) "ON TAKEOFF ROLL AT 80 KTS RT THRUST REVERSER "REV" ICON, "REV UNLOCK" MESSAGE AND UNLOCK LIGHT ON CENTRE PEDESTAL APPEARED".PILOT REPORTED YAW AT THE TIME OF OCCURRENCE.SDR CA010912015Web · cracked(CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM UPPER WEB AT FS 640 NEAR L & R BL 9.0 (1.25 AND 1.5 INCHES LONG). ONE CRACK FOUND ON LHS OF ACCESS PANEL LANDING CORNER ON LOWER WEB NEAR LBL 36.2 (0.5 INCHES LONG). REPAIRED IN ACCORDANCE WITH REO'S 601R-53-61-366SDR CA010912012Lever · failed(CAN) THE CREW REPORTED THAT ON FINAL, WHILE RETRACTING THE FLIGHT SPOILERS, THE AIRCRAFT ROLLED LEFT 1/4 DETENT. FULL RETRACTION OF THE FLIGHT SPOILER CORRECTED THE CONDITION.THE MAINTENANCE FOUND NO FAULTS LOGGED IN THE MDC OR SECUS. THE SPOILER RIGGING CHECSDR CA010912009Pump · leaking(CAN) SHORTLY AFTER TAKEOFF, THE FLT CREW REPORTED LOSS OF NR 3 HYDRAULIC PRESSURE. ALTRNATE LANDING GEAR EXTENSION CARRIED OUT IN ACCORDANCE WITH THE QRH. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. UPON FURTHER INVESTIGATION, A LEAK WASSDR CA010912010Web · cracked(CAN) DURING COMPLETION OF ASB 601R-53-61-059 FOUND UPPER WEB OF ENGINE SUPPORT BEAM CRACKED NEAR L & RBL 9.0 AT FS 640. ALSO FOUND HOLES IN SUPPORT ANGLE CRACKED AT RBL 7.5 AND 8.5 (FOUND BY NDT). ALSO FOUND 1/2 INCH CRACK IN LOWER WEB NEAR RBL 36.20 IN THE FSDR CA010912011Handle · cracked(CAN) GALLEY/SERVICE DOOR OUTER HANDLE CRACKED WHILE DOOR WAS BEING CLOSED BY CATERING PERSONNEL.SDR A6WA200100056Shutoff Valve · failedIN-FLIGHT WITH RIGHT PACK SELECTED ON AND RIGHT 10TH STAGE BLEED SELECTED ON, RIGHT PACK INOP ECS PAGE SHOWED RT PACK AND 10TH STAGE VALVE CLOSED. CABIN TEMP TOO HIGH, ACFT RETURNED TO DEN. MAINTENANCE REPLACED RIGHT 10TH STAGE BLEED VALVE.SDR CA011005005Brace · loose(CAN) AFTER TAKEOFF, AT 700 FEET AGL, CREW THROTTLED BACK & FOUND THAT LEFT THROTTLE WAS STIFF. THEY ATTEMPTED TO REDUCE POWER FURTHER, BUT IT COULD NOT BE REDUCED ANY LOWER THAN 90 PERCENT. THROTTLE COULD BE ADVANCED SLIGHTLY BUT WOULD ONLY OPERATE BETWEEN 90SDR JBXA000313Powerplant · making metalRH ENGINE CHIP DETECTOR LIGHT WAS FOUND DURING A SCHEDULED INSPECTION. METAL WAS FOUND ON DETECTOR AND WAS FOUND TO BE OUT OF LIMITS PER GE MAINTENANCE MANUAL.CORECTIVE ACTION: R&R RH ENGINE IAW CRJ AMM 71-00-00
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