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 CA040613001Idg · inoperative(CAN) NR 1 IDG CAUTION MESSAGE CAME ON DURING TAKEOFF ROLL AND CREW ELECTED TO REJECT TAKEOFF. ON WEEK PRIOR OR(JUNE 5), THE CREW RECEIVED A CAUTION MESSAGE (DURING CRUISE AT 31000 FEET) ON EICAS FOR APPROX 30 SECONDS WITH SYNOPTIC CHANGING FROM GREEN TO YELLSDR VNAA0406006Warning Light · intermittentDURING FLT, THE CREW RECEIVED A RT EMERGENCY EXIT DOOR CAS MESSAGE, THE PRESSURE WAS NORMAL AND THE INDICATION EXTINGUISHED BY ITSELF ON DESCENT. MAINTENANCE DEFERRED WITH THE CREW USING MEL 52-70-03 CODE-C.SDR REX2004F00002Engine · malfunctionedAT LEVEL CRUISE AT FL310 AND MACH .74, THE FIRST OFFICER NOTICED A FLUXUATION IN THE RT ENGINE OIL PRESSURE. WITHIN FIVE MINUTES THE FLUXUATION BEGAN TO INCREASE. THE CAPTAIN ALSO NOTICED AN ASSOCIATED INCREASE IN OIL TEMPERATURE. THE FLIGHT CREW PERFORMED SDR SWIA200413396O-Ring · leakingCREW HAD TO SHUT DOWN NR 2 ENGINE DUE TO LOW OIL PSI. REMOVED AND REPLACED O-RINGS FOR IDG, STARTER, HYDRAULIC PUMP IAW CRJ MM CHAPTERS 80-11-01, 24-11-01, 29-11-00. OPERATIONAL CHECK GOOD.SDR SWIA200413390Pcu · malfunctionedSPOILERON FAULT MESSAGE. REPLACED HYDRAULIC NR 1 PRESSURE SWITCH, LEFT SPOILERON PCU AND NR 2 SECU. OPS CHECK GOOD IAW MM CH 27-62-01. P/N 49-164-06, S/N OFF 01598.SDR SWIA200413458Clip · crackedFUSELAGE FLOORBEAM ATTACH CLIPS ARE CRACKED (2) INBOARD AND OUTBOARD FS 280.00 RBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-42-13, 51-25-16, 51-21-11.SDR SWIA200413459Clip · crackedFUSELAGE FLOORBEAM ATTACH CLIP IS CRACKED INBOARD LOCATION FS 280.00 LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-25-16, 51-21-11SDR SWIA200413460Floor Support · crackedCARGO PIT FLOOR SUPPORT ANGLE IS CRACKED FS 621.00 RBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV. B.SDR SWIA200413461Clip · crackedAFT EQUIPMENT BAY CLIP CRACKED AT FS 621.00 - 625.00 STR 14R. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-41-06, AND 51-25-16.SDR CA040623006Bolt · seized(CAN) PILOT REPORTED MAIN PASSENGER DOOR DIFFICULT TO OPEN FROM OUTSIDE, HAD TO ENTER FROM SERVICE DOOR TO ACCESS AIRCRAFT. TRIED TO OPEN DOOR AND HANDLE WAS DIFFICULT TO TURN. MAINTENANCE FOUND AIRSTAIR PIVOT FITTING ASSEMBLY WAS SEIZED. UPON DISMANTLING THSDR SWIA200413406Control Unit · malfunctionedMACH TRIM DISENGAGED WOULD NOT RESET. REMOVED AND REPLACED HSTCU WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD PER MM 27-41-01.SDR VNAA0406003Transmitter · failedDURING FLIGHT, THE CREW RECEIVED A FLAP DEGRADE STATUS MESSAGE AND DIVERTED TO BTV. MAINTENANCE WAS SENT TO BTV. MAINTENANCE THEN INSPECTED AND REPLACED THE LEFT HAND FLAP POSITION TRANSMITTER ASSEMBLY IN ACCORDANCE WITH DORNIER MAITNENANCE MANUAL 27-00-00. SDR VNAA0406004Seal · failedTHE CREW REPORTED THAT AT THE RT EMERGENCY EXIT, THERE WAS SOME OF THE SEAL MISSING AROUND THE WINDOW. MAINTENANCE INSPECTED AND PLACED THE SEAL ON THE CDL LIST, CDL 51-23. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.SDR CA040602004Valve · gouged(CAN) THE LOW LIMIT VALVE WAS OBSERVED TO STICK IN AN OPEN POSITION AND WOULD NOT MODULATE. AFTER REMOVAL OF THE VALVE THE BUTTERFLY WAS FOUND TO BE SCRAPING AGAINST THE BODY OF THE VALVE.ANOTHER VALVE WITHTHIS CONDITION HAD PREVIOUSLY BEEN FOUND TO SHEAR THE SDR CA040602005Turbine · seized(CAN) DURING INITIAL START AN UNUSUAL NOISE WAS HEARD FROM THE APU. THE UNIT WAS RUN FOR APPROXIMATELY ONE HOUR WITH NO ABNORMAL INDICATIONS. UPON FURTHER INVESTIGATION OF THE NOISE IT WAS DISCOVERED THAT IT WAS NOT POSSIBLE TO ROTATE THE TURBINE WHEEL BY HANDSDR ASOA04392Wire · brokenDURING A GROUND INSPECTION, THE AFT EMERGENCY FLOOR LIGHT POWER CABLE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLOOR LIGHT POWER STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.SDR ASOA04391Lamp · burned outDURING HANGER MAINTENANCE, THE NR 3 EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.SDR ASOA04387Carbon Seal · leakingDURING CLIMB OUT, WHEN PASSING THROUGH 14,500 FEET THE CREW NOTICED A DROP IN THE LT ENGINE OIL PRESSURE TO 27 PSI, IT THEN BEGAN FLUCTUATING BETWEEN 27 PSI AND 40 PSI. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO AIRPORT, LANDING SAFELY. MAINTENANSDR CA040528001Transmitter · failedDURING FLIGHT, UPON SELECTION OF WEATHER RADAR, THE BLUE 'RADAR FAULT' AND AMBER 'RADAR CONTROL FAULT' MESSAGES APPEARED ON THE MFD DISPLAY, CREW CYCLED ON AND OFF WITH NO SUCCESS, CREW DETERMINED TO RETURN AIRCRAFT WHERE MAINTENANCE ENGINEERS UPON TESTING THESDR CA040615008Tire · separated(CAN) NR 2 MLG TIRE SEPARATION/ RUPTURE ENGINE VIBRATION (N1) WAS DEPICTED ON EICAS AND FELT THROUGHOUT THE AIRCRAFT. THE FLIGHT CREW RETARDED THE POWER LEVERS TO REDUCE N1 VIB. TO WITHIN LIMITS. (FYI:AT 42 PERCENT N1 = 3.9 MILS). A/C DIVERTED. FLIGHT CREW POSDR ASOA04383Lever · bindingDURING A GROUND INSPECTION, THE PASSENGER DOOR WAS HARD TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR RELEASE LEVER AND OPEN LOCK MECHANISM. OPERATIONAL CHECKS GOOD AIRCRAFT OK FOR SERVICE.SDR ASOA04388Clip · crackedDURING A C-CHECK, THE LT AND RT CLIPS BELOW THE BOX BEAM AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT CLIPS BELOW THE BOX BEAM AS FS621.SDR ASOA04386Clip · crackedDURING A C-CHECK, THE FLOOR SUPPORT CLIP AT FS 484, LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT CLIP AT FS 484, LBL 36 IAW EO 600530098.SDR ASOA04385Floor Support · crackedDURING A C-CHECK, THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT OB ANGLES AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT OB ANGLES ON THE LT AND RT SIDES IAW EO 600SDR ASOA04384Clip · crackedDURING A C-CHECK, THE OB CLIP AT FS 280, LBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OB CLIP AT FS 280, LBL 9 IAW SRM 51-42-21.SDR ASOA04382Clip · crackedDURING A (C) CHECK, THE OB CLIP AT FS 280, RBL 9 IN THE AVIONICS EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE OB CLIP AT FS 280, RBL9 IN THE AVIONICS EQUIPMENT BAY.SDR ASOA04381Clip · crackedDURING A C-CHECK, THE IB CLIPS AT FS280, LBL9 AND RBL 9 IN THE FORWARD AVIONICS EQUIPMENT BAY WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE IB CLIPS AT FS280, LBL9 AND RBL9 IN THE FORWARD AVIONICS EQUIPMENT BAY.SDR SWIA200413349Trim Panel · inoperativeAILERON TRIM INOP. REMOVED AND REPLACED AILERON/RUDDER TRIM PANEL. OPS CHECK GOOD.SDR ASOA04380Windshield · brokenDURING DESCENT, OUT OF 25,000 FT, THE F/O`S WINDSHIELD SHATTERED. THE QRH WAS COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT LANDED SAFELY.SDR CA040528002Windshield · crackedFLIGHT EN ROUTE WHILE DESCENDING OUT OF 25,000 FT, FIRST OFFICER'S WINDSHIELD CRACKED. WINDSHIELD REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR VNAA0405013Warning Light · illuminatedTHE CREW REPORTED RECEIVING A RT EMERGENCY DOOR CAUTION MESSAGE. MAINTENANCE CONTROL DEFERRED THE EMERGENCY DOOR INDICATION WITH THE CREW IN ACCORDANCE WITH 52-70-03 CODE C.SDR ASOA04376Scavenge Pump · cloggedDURING CRUISE, AT APPROXIMATELY 35,000 FEET THE CREW RECEIVED A RED RT ENGINE OIL PRESSURE MESSAGE AND ASSOCIATED AURAL WARNING. OIL PRESSURE FLUCTUATED BETWEEN THE HIGH TEENS AND LOW TWENTIES. THE CREW REDUCED THE RT ENGINE TO IDLE THROUGH DESCENT. THE QRHSDR SWIA200413444Floor Support · crackedFS 621 LEFT FLOOR SUPPORT ANGLE LBL 41 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV A AND RII53-401.SDR SWIA200413445Floor Support · crackedFS 621 RIGHT FLOOR SUPPORT ANGLE RBL 41 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601RR-53-61-117 REV A AND RII53-401.SDR SWIA200413446Attach Angle · crackedCARGO PIT TRANSVERSE BEAM TO LANDING PLATE ATTACH ANGLE IS CRACKED FOR DOOR STOP FITTING FS 589.00 LBL 43.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-42-02, AND RII53-401.SDR CA040615010Tire · separated(CAN) ON LANDING VIBRATION DETECTED. PILOTS' POST FLIGHT INSPECTION NOTICED NR 3 MLG TIRE HAD SEPARATED AND RUPTURED. RT IB FLAP WAS DAMAGED AS A RESULT.SDR VNAA0405009Warning Light · illuminatedDURING TAKEOFF, THE CREW RECEIVED A CONFIG FLAP RED WARNING MESSAGE AND ABORTED TAKEOFF. THE CREW RESET THE CONFIG AND THE MESSAGE CLEARED. FLIGHT 2377 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT.SDR VNAA0405010Adc · failedDURING TAKEOFF, THE CREW RECEIVED A CONFIG FLAP RED WARNING MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE AIR DATA COMPUTER IN ACCORDANCE WITH 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR CA040531006Engine · bird ingestionSHORTLY AFTER TAKEOFF A BIRD STRIKE OCCURRED ON THE RIGHT ENGINE. CREW CONTINUED CLIMB-OUT AND REDUCED POWER TO IDLE. FLIGHT CONTINUED AND MADE AN UNEVENTFUL LANDING. POST FLIGHT INSPECTION REVEALED SEVERAL FAN BLADES DAMAGED BEYOND LIMITS AND DAMAGE TO THESDR CA040531007Engine · bird ingestionSHORTLY AFTER TAKEOFF, A BIRD STRIKE OCCURRED ON THE RIGHT ENGINE. CREW CONTINUED CLIMB-OUT AND REDUCED POWER TO IDLE. FLIGHT CONTINUED TO AND MADE AN UNEVENTFUL LANDING. POST FLIGHT INSPECTION REVEALED SEVERAL FAN BLADES DAMAGED BEYOND LIMIT AND DAMAGE TO SDR CA040514001Shaft · sheared(CAN) AFTER ENGINE START CREW WAS UNABLE TO OBTAIN COLD AIR-CONDITIONED AIR OUT OF THE LT AIR CONDITIONING PACK. ENGINES WERE SHUTDOWN AND MAINTENANCE WAS NOTIFIED OF THE SNAG. MAINTENANCE DISCOVERED THAT THE LOW LIMIT VALVE, BUTTERFLY VALVE WAS NO LONGER ATTSDR CA040615009Tire · separated(CAN) DURING PASSENGER DEPLANING, A RAMPER REPORTED THE LT IB TIRE SHOWN TIRE SEPARATION (TREAD MISSING) AND THE CORD SECTION WAS SHREDDED AND THE TIRE HAD POPED OUT IN SEVERAL AREAS. UPON A CLOSURE LOOK, THE FLIGHT CREW NOTICED THE LT IB FLAP SURFACE HAD SUSSDR VNAA0405008Adc · failedDURING TAKEOFF, THE CAPTAIN'S SIDE AIR SPEED INDICATOR, VERTICAL SPEED INDICATOR, AND MACH TRIM HAD NO INFORMATION DISPLAYED. MAINTENANCE THEN REPLACED THE NR 1 AIR DATA COMPUTER IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 34-00-00. OPERATIONALSDR VNAA0405007Pump · failedAPPROXIMATELY 20 MINUTES FROM PHL, THE CREW RECEIVED A FUEL IMBALANCE INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND SHUTDOWN THE LEFT HAND ENGINE AND LANDED AT PHL. MECHANICS WERE SENT FROM DAY. MAINTENANCE THEN INSPECTED AND REPLACED THE ASDR CA040604016Tire · separated(CAN) THE NR 2 MLG TIRE HAD SEPARATED THAT INCURRED DAMAGE TO THE IB FLAP SURFACE, FLAP STUB FAIRING AND 3 FAN BLADES..SDR CA040511001Drain · contaminated(CAN) ON TAKE-OFF ROLL , THE PILOT NOTICED THAT STANDBY ALTIMETER-AIR SPEED INDICATOR NOT SHOWING ANY AIRSPEED THUS REJECTING TAKEOFF. MAINTENANCE REPLACED THE INSTRUMENT AND NOTED THERE WAS EXCESSIVE AMOUNT OF MOISTURE DRAINED FROM THE PITOT DRAIN PLUG .SDR VNAA0405006Door · failedTHE CREW RECEIVED A RIGHT HAND OVERWING EMERGENCY EXIT CAS MESSAGE AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REINSTALLED THE RIGHT HAND OVERWING EMERGENCY DOOR IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WSDR CA040515001Trim Switch · failed(CAN) RUDDER TRIM GOES FULL RT WITHOUT INPUT COMMAND. WITH NOSE LT SELECTED, TRIM MOVES FURTHER RT. AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED RUDDER TRIM PANEL AND OPS CHECKED. NO FURTHER DEFECTS NOTED.SDR VNAA0405005Amplifier · failedAFTER TAKEOFF, THE LT ENGINE SURGED 10 PERCENT AND THE CREW RETURNED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE NR 1 CONTROL AMPLIFIER IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 72-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFTSDR CA040615011Window · damaged(CAN) SMOKE IN COCKPIT DUE TO LT WINDOW HEATER. EMERGENCY DECLARED DUE TO DAMAGED INSULATION BLOCK, REPLACEMENT OF LT SIDE WINDOW AND CONTINUITY CHECK OF SUPPLY WIRES NECESSARY. TROUBLESHOOTING POINTS TO INTERNAL FAULT OF THE HEATER ELEMENT TERMINAL BLOCK AT
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