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 ASOA04908Scavenge Pump · cokedDURING CLIMB-OUT, AT APPROXIMATELY 31,800 FT, THE CREW RECEIVED AN ENGINE OIL PRESSURE MASTER WARNING AND AURAL. THE QRH WAS COMPLIED WITH AND THE CREW SHUTDOWN THE LT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED, LANDING SAFELY. MAINTENANCE SDR ASOA04909Step · crackedDURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.SDR ASOA04910Handle · crackedDURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE BASE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE MAIN AVIONICS BAY DOOR HANDLE ASSEMBLY.SDR ASOA04911Angle · crackedDURING C-CHECK, THE LT AND RT SIDE FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT AND RT SIDE FLOOR SUPPORT ANGLES AT FS 621 IAW EO 600-53-0105.SDR ASOA04912Plate · crackedDURING A C-CHECK, THE CARGO BAY FLOOR SILL AT FS 562.72-FS 589.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72- FS 589.00 IAW EO 600-53-0095.SDR VNAA0411004Tire · damagedPOST FLIGHT INSPECTION OF THE AIRCRAFT BY THE CREW OF FLIGHT 2293 REVEALED THE LEFT INBOARD MAIN LANDING GEAR RETREADED TIRE HAD SHED APPROXIMATELY HALF ITS TREAD DURING LANDING AT MSP. UPON FURTHER INVESTIGATION FOD WAS FOUND ON THE LEFT INBOARD FLAP AND ON SDR ASOA04903Clip · crackedDURING A C-CHECK, THE CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL 36, RBL36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL36 AND RBL 3SDR ASOA04904Floor Support · crackedDURING A C-CHECK, THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 IAW EO 600-53-0105.SDR ASOA04905Clip · crackedDURING C-CHECK, THE LT AND RT FS 625 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT AND RT FS625 CLIP.SDR ASOA04906Support Beam · crackedDURING A C-CHECK, THE LT AND RT LOWER ENGINE SUPPORT BEAMS AT BL 36.20 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT LOWER ENGINE SUPPORT BEAMS AT BL 36.20 IAW EO 600-53-0070.SDR ASOA04907Support Beam · crackedDURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW EO 600-53-0072.SDR ASOA04938Step · crackedDURING A C-CHECK, THE PASSENGER DOOR TOP STEP FORWARD IB CORNER WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP IAW MM 52-11.SDR REXA04031Controller · malfunctionedFLAP FAILS AT ZERO WHEN SELECTED TO 20 ON APPROACH. QRH FOLLOWED EMERGENCY DECLARED, UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01.SDR REXA04032Control System · malfunctionedFLAPS FAILED AT ZERO ON APPROACH WHEN SELECTED TO THIRTY. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01.SDR ASOA04902Structure · crackedDURING C-CHECK, THE EMERGENCY EXIT LIGHT NEAR THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSY NEAR THE SERVICE DOOR.SDR A6W2005F00000Bushing · migratedLT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .025 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 2ND OVERSIZED BUSHING IAW REO.SDR ASOA04901Connector · disconnectedDURING A GROUND INSPECTION, THE EMERGENCY FLOOR TRACK LIGHT BETWEEN ROWS 6 AND 7 OPERATIED INTERMITTENTLY. MAINTENANCE RESECURED THE CONNECTION TO THE EMERGENCY FLOOR TRACK LIGHT BETWEEN ROWS 6 AND 7 AND ALSO REMOVED AND REPLACED A SECTION OF THE FLOOR TRACK SDR A6WA200440215Angle · crackedLT FS 625.00 OBLIQUE ANGLE CRACKED.SDR ASOA04899Step · crackedDURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.SDR 04317684Engine · shutdownEVENT SUMMARY STATED RIGHT ENG SHUT DOWN IN FLT DUE TO LOW OIL PRESSURE. REMOVED AND REPLACED AGB CARBON SEALS FOR IDG, ATS AND HYDRAULIC PUMP IAW AMM 72-60-00. OIL CONSUMPTION RUNS COMPLIED WITH AMM 71-00-00.SDR 04317679Bleed Valve · malfunctionedEVENT SUMMARY STATED BLEED MISCONFIG, ABORTED TAKEOFF, RTG. REMOVED AND REPLACED LT ENG 10TH STAGE BLEED VALVE IAW MM 36-11-04. OPS CHECK GOOD.SDR A6WA200440186Strut · dischargedGEAR DISAGREE AFTER TAKEOFF, COMPLIED WITH QRH LANDING WEIGHT 47,000 LBS. JACKED AIRCRAFT AND OBSERVED NLG NOT SELF-CENTERING SERVICED HYDRAULIC FLUID IN STRUT AND NITROGEN CHARGE IAW MM 12-1232. JACKED AIRCRAFT AGAIN, NLG CENTERS ON ITS OWN. SWUNG ALL 3 GESDR ASOA04896Clamp · looseDURING CLIMB-OUT, AT APPROXIMATELY 25,000 FT, THE CREW RECEIVED AT RIGHT 14TH DUCT WARNING MESSAGE. THE QRH WAS COMPLIED WITH AND THE RT ENGINE THRUST LEVER BROUGHT BACK TO IDLE FOLLOWED BY THE WARNING MESSAGE EXTINGUISHING. AN EMERGENCY WAS DECLARED WITH THSDR COMA0460616Carbon Seal · unreliableFLIGHT 5912 RT ENGINE OIL PRESSURE AND TEMP DROPPING DURING FLIGHT. IFSD REPLACED THE ACCESSORY DRIVE GEARBOX CARBON SEALS AT AXIS BB, D AND F.SDR ASOA04895Loop · malfunctionedDURING CLIMB-OUT, AT APPROXIMATELY 9,500 FEET, THE CREW RECEIVED A TRIPLE CHIME RT 14TH DUCT MESSAGE AND AURAL WARNING. THE CREW LEVELED THE AIRCRAFT TO 12,000 FEET AND COMPLIED WITH THE QRH. THE RT ENGINE WAS PULLED TO FLIGHT IDLE AND THE MESSAGE EXTINGUISHSDR SWIA200414087Engine · power lossON DESCENT RT ENGINE N1, SPOOLED DOWN, ITT INCREASED TO 800 DEGREES, AND A BANG WAS HEARD. N1 DID NOT RESPOND TO THRUST LEVER ADVANCEMENT. ENGINE WAS LEFT AT IDLE UNTIL LANDING. REMOVED AND REPLACED RT ENGINE PER CRJ MM 71-00-00. OPERATIONAL CHECK GOOD.SDR REXA04030Flap · malfunctionedFLAPS FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. (NE02200500600)SDR ASOA04897Bpsu · malfunctionedDURING CLIMB-OUT, AT APPROXIMATELY 18,000 FEET, THE CREW RECEIVED A (FLAP FAIL) MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT BRAKE POSITION SENSOR UNIT (BPSU) AND ALSO SDR A6WA200440182Skin · dentedRT IB FLAP BOTTOM SKIN IS DENTED APPROX .7500 INCH LONG X .6250 INCH WIDE AND .040 DEEP WITH GOUGES IN CENTER OF DENT. DENT IS 1.7500 INCH FORWARD OF AFT EDGE AND 8 INCH OB FROM IB ENGINE. PERFORMED A MAJOR REPAIR BY CUTTING OUT DAMAGED SKIN AND INSTALLING DSDR REXA04029Flap · malfunctionedRECEIVED (FLAPS HALF-SPEED) MESSAGE ON BLOCK OUT. FLAP SYSTEM INSPECTED FECU CHECKED FOR CODES, NO CODES FOUND. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01.SDR ASOA04891Acm · malfunctionedDURING DESCENT, AT APPROXIMATELY 11,000 FEET, THE CREW NOTICED A STRONG BURNING SMELL IN THE COCKPIT AND CABIN WITH THE LT PACK GOING TO FULL HOT WHICH BECAME UNCONTROLLABLE IN EITHER AUTOMATIC OR MANUAL MODES. AN AUTOMATIC SHUTDOWN OF THE PACK OCCURRED. THESDR VNAA0411002Structure · bird strikeAFTER SHUTDOWN IN DAY EVIDENCE OF A BIRD STRIKE ON THE RT WING INBOARD LEADING EDGE WAS REPORTED BY THE CREW OF FLIGHT 2461. PSA MAINTENANCE INSPECTED THE AREA AND FOUND THE DAMAGE TO BE OUT OF LIMITS FOR CONTINUED SERVICE. PSA MAINTENANCE THEN REMOVED & REPSDR A6WA200440180Odor · detectedFUEL SMELL UPON START UP OF APU ON GROUND BEFORE BLEEDS ARE TRANSFERRED. MAINTENANCE VERIFIED NO FUEL OR OIL LEAKS IN APU BAY. TROUBLESHOT APU FUEL SYSTEM. RAN APU AND AIR CYCLE MACHINE. NO FUEL SMELL DETECTED AND NO LEAKS.SDR A6WA200440178Splice · wrong partFLOOR TRACK LIGHTING HAS WRONG SPLICES AT ROW NR 12. REMOVED AND REPLACED SPLICES AT ROW NR 12 IAW CRJ 200 WIRING MANUAL 20-17-10.SDR A6WA200440179Splice · brokenFLOOR TRACK LIGHTING HAS A BROKEN SPLICE AT ROW NR 8. REMOVED AND REPLACED SPLICE AT ROW NR 8 IAW CRJ 200 WIRING MANUAL 20-17-10.SDR A6WA200440177Bushing · migratedLT MAIN LANDING GEAR AFT TRUNNION BUSHING MIGRATED 0.005 INCH. REMOVED LT AFT MLG TRUNNION BUSHING IAW AMM 20-26-00-910-803. INSTALLED A NEW OVERSIZE (2ND) BUSHING PN 601R5721003-23. IAW REO 601R57-21-003B. REAMED INSIDE DIA TO 2.4384 IAW DWG 601R85007RWC.SDR A6WA200440176Odor · detectedFUEL SMELL UPON START UP OF APU ON GROUND BEFORE BLEEDS ARE TRANSFERRED. COMPLIED WITH (CM) ACTION PLACARDED AND PLACED ON MEL. TROUBLESHOT APU FUEL SYSTEM RAN APU AND ACM NO FUEL ODOR DETECTED. NO LEAKS DETECTED. RETURN TO SERVICE. REMOVED OFF MEL. (K)SDR MASA200400627Gearbox · making metalAIRCRAFT RETURNED TO THE FIELD. CREW REPORTED A LEFT FUEL SCAVENGE EJECTOR CAUTION AND A LEFT FUEL MAIN SCAVENGE CAUTION MESSAGES, FOLLOWED BY A LOW OIL PRESSURE WARNING MESSAGE. OIL PRESSURE WAS FLUCTUATING BETWEEN 25 TO 28 PSI AND WITHIN A MINUTE DROPPED TSDR ASOA04887Step · crackedDURING AN A-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.SDR REXA04028Potentiometer · out of rigFLAP FAILURE ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. PERFORMED RIGGING OF FLAP POTENTIOMETERS AND BPSU IAW AMM 27.SDR ASOA04884Control Panel · malfunctionedDURING CLIMB-OUT, AT APPROXIMATELY 10,000 FEET THE CREW EXPERIENCED A FULL SCALE NOSE LT RUDDER TRIM DEFLECTION. THE CAPTAIN CORRECTED FOR THE TRIM PROBLEM USING RUDDER AND AILERON INPUTS. AN EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES REQUESTED TO BE ON SSDR ASOA04885Charger · inoperativeDURING A GROUND INSPECTION, THE AFT EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHTS BATTERY PACK CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.SDR REXA04026G Switch · failedELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207.SDR ASOA04883Tire · blownDURING CRUISE, THE CREW WAS ADVISED BY TOWER THE AIRCRAFT MAY HAVE EXPERIENCED A TIRE BLOWING ON THE RT SIDE UPON TAKEOFF. AN EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY. MAINTENASDR ASOA04874Support Angle · crackedDURING A C-CHECK, THE FLOOR SUPPORT ANGLES AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLES AT FS 621 ON THE LT AND RT SIDES IAW EO 600-53-0105.SDR ASOA04875Lens · brokenDURING A C-CHECK, THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY ABOVE THE SERVICE DOOR.SDR ASOA04876Clip · crackedDURING A C-CHECK, THE CLIPS AT FS 280, LBL 9 IB AND OB WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS280, LBL 9 IB AND OB.SDR ASOA04877Clip · crackedDURING A C-CHECK, THE CLIPS AT FS280, RBL 9 IB AND OB WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS280, RBL 9 IB AND OB.SDR ASOA04878Clip · crackedDURING A C-CHECK, THE FLOOR SUPPORT CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT CLIPS AT FS 484, LBL 36 AND RBL 36 IAW EO 600-53-0098.SDR ASOA04880Handle · crackedDURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE MAIN AVIONICS BAY DOOR HANDLE ASSEMBLY.
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