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 VNAA0510009Hose · rupturedCLIMBING THRU FL120, THE CREW HEARD A HISSING SOUND AND REPORTED THAT THE CREW OXYGEN QUANTITY WAS DEPLETED. THE QRH WAS FOLLOWED AND THE FLIGHT DIVERTED TO PIT. MAINTENANCE FOUND THE OXYGEN HOSE UNDER THE FIRST OFFICER'S MASK STOWAGE BOX RUPTURED. THE HOSESDR VNAA0510008Warning Light · false activationTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED DURING LANDING APPROACH. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING. THE CREW REPORTED THAT THE FLAP SELECTOR WAS NOT IN THE DETENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM IAW CRJSDR CA060211003Turnbuckle · separated(CAN) WHEN STARTING APPROACH, THROTTLES WERE PULLED BACK, A LOUD BANG WAS WITNESSED AND FELT IN A/C. ENG NR 1 STARTED TO LOSE POWER IMMEDIATELY, FOLLOWED BY LOW OIL PRESSURE WARNING. ITT ROSE UP TO 1230 DEG CELSIUS AND HIGH ENGINE VIBRATION WERE FELT. ENG WASDR CA060211004Blades · damaged(CAN) FLIGHT CREW REPORTED SEEING HIGH NR 1 ENGINE ITT > 900 DEG CELSIUS, TOGETHER WITH ENGINE VIBRATION. N1 STARTED TO SPOOL DOWN AND FLUCTUATING N2 WAS SEEN. CREW SHUTDOWN THE ENGINE AND RETURNED TO DEPARTURE. SUCCESSFUL SINGLE ENGINE LANDING WAS PERFORMED.SDR VNAA0510007Proximity Switch · intermittentTHE PAX DOOR OUT HANDLE CAUTION MESSAGE ILLUMINATED SEVERAL TIMES DURING THE FLIGHT. THE AIRCRAFT WAS FERRIED TO CLT WHERE MAINTENANCE REMOVED & REPLACED THE PAX DOOR OUTER HANDLE PROXIMITY SWITCH IAW CRJ200 AMM 52-70-04-000(400)-803. AN OPERATIONAL CHECK FLSDR VNAA0510006Warning Light · false activationCLIMBING THRU 5000 FT WITH THE LT PACK DEFERRED, THE RT PACK HI PRESS CAUTION MESSAGE ILLUMINATED. DUCT PRESSURE WAS REPORTED >80 PSI. THE FLIGHT RETURNED TO CLT AND LANDED. MAINTENANCE COMPLIED WITH AN OPERATIONAL CHECK OF THE RT AIR CONDITIONING SYSTEM ANSDR VNAA0510005Door · openSHORTLY AFTER TAKEOFF THE CREW REPORTED A LOUD POPPING NOISE NEAR THE NOSE OF THE AIRCRAFT. THE FLIGHT RETURNED TO CLT AND LANDED SAFELY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE EXTERNAL SERVICES PANEL DOOR OPEN AND A HEADSET PLUG ADAPTOR PLUGGED INSDR VNAA0510004Computer · malfunctionedTHE CREW ABORTED TAKEOFF WHEN THE EFIS COMP MON CAUTION MESSAGE ILLUMINATED AND BOTH HEADING INDICATORS RED FLAGGED. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE CYCLED THE AHARS SYSTEM POWER. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS SDR CA051011001Relay · melted(CAN) THE FLIGHT CREW WAS ON THE GROUND WITH THE APU ON (NO PASSENGERS ON BOARD). JUST AFTER TRANSFERING FROM APU TO EXTERNAL POWER, SMOKE STARTED TO FILL THE COCKPIT. POWER WAS REMOVED FROM THE AIRCRAFT. THE MECHANICS DETERMINED THAT THE SOURCE OF THE SMOKSDR VNAA0510003Warning Light · false activationTHE STEERING INOP CAUTION MESSAGE ILLUMINATED AFTER TAKEOFF FROM DCA. THE CREW FOLLOWED THE QRH, DIVERTED TO BTV, AND MADE AN UNEVENTFUL LANDING. THE STEERING SYSTEM OPERATED NORMAL ON LANDING. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE NOSE WHEEL STESDR REXA200500129Bracket · unsecureON CLIMBOUT, ATTEMPTED TO REDUCE CLIMB POWER FL250. CAPTAIN CONFIRMED THE THRUST LEVER WAS JAMMED. COMPLIED WITH THE QRH CHECKLIST, AND DECLARED AN EMERGENCY. THE FLIGHT WAS CLEARED DIRECT TO MEMPHIS (MEM). AT THIRTY MILES OUT AND ON THE ILS TO RUNWAY 18C,SDR REXA200500130Scavenge Pump · failedEN ROUTE TO DTW FROM GSP THE RT ENGINE MASTER WARNING ILLUMINATED FOLLOWED BY THE FLUCTUATION OF THE OIL PRESSURE GAUGE. THE FLIGHT CREW EXECUTED THE QRH AND SHUT DOWN THE ENGINE. DECLARED AN EMERGENCY. ATC CLEARED THEM DIRECT TO AVL WHERE AN OTHERWISE UNEVSDR VNAA0510001Steering Sys · warning lightTHE STEERING INOP CAUTION MESSAGE ILLUMINATED AFTER DEPARTURE. THE NWS SWITCH WAS CYCLED BUT THE SYSTEM WOULD NOT RESET. THE CREW FOLLOWED THE QRH AND MADE A PRECAUTIONARY LANDING WITH EQUIPMENT AT DESTINATION. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF TSDR VNAA0510002Wire Harness · failedTHE STEERING INOP CAUTION MESSAGE ILLUMINATED AFTER DEPARTURE. THE NWS SWITCH WAS CYCLED BUT THE SYSTEM WOULD NOT RESET. THE CREW FOLLOWED THE QRH AND RETURNED TO PIT AND LANDED SAFELY. THE AIRCRAFT WAS FERRIED TO CAK WHERE AFTER TROUBLESHOOTING, MAINTENANSDR MASA200500764Engine · overtempASH 6110 PHX. RED FLASHING ITT ON LT ENGINE DURING TAKE OFF ROLL. TEMPERATURE EXCEEDED 900 DEGREES. MX R2 ENGINE.SDR A6WA200540312Control Panel · inoperativeADG INADVERDENTLY DEPLOYED DURING CLIMBOUT, PERFORMED QRH AMBER CAS MESSAGE FOR L WINDOW HEAT, L AOA HEAT, PITOT BASE HEAT ILLUMINATED. ADG POWERED AC ESS BUS. EMERGENCY LIGHTS ILLUMINATED BEFORE ADG DEPLOYMENT. REMOVED AND REPLACED AUTO DEPLOY CONTROL PANESDR A6WA200540311Idg · lack of lubeIDG NR 1 CAUTION MESSAGE AT TAKEOFF THRUST ABORTED TAKEOFF BELOW 40 KNOTS BTMS INDICATES 3, 3, 4, 4 LIGHT BRAKING. NO HIGH ENERGY STOP INSPECTION REQUIRED IAW 05-51-27 P601. COMPLIED WITH (M) ACTION FOR MEL 24-11-01-01 PLACARDED. SERVICED IDG NR 1 WITH OIL SDR VNAA0509014Fcu · malfunctionedTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH WITH THE FLAPS AT 20 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE CLEARED CODES FROM THE FECU AND RESET THE SYSTEM IAW CRJ200 FIM 27-50-00. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOSDR A6WA200540310Access Door · corrodedRT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT PANEL 650 GB WING STA 274.319 HAS MINOR CORROSION .006 INCH DEEP AND 2 INCH LONG. MAINTENANCE REMOVED MINOR CORROSION IAW REO. MATERIAL REMOVED WAS LESS THAN .010 INCH IAW REINSPECT IS DUE OF HOLE NR 14 AT 386SDR ASOA05794Cargo Track · corrodedDURING A C-CHECK IN MCN, CORROSION WAS FOUND ON THE TIE DOWN FITTINGS AND TIE DOWN TRACKS. AFTER MAINTENANCE REMOVED CORROSION ON THE TIE DOWN FITTINGS AND THE TIE DOWN TRACKS, THEY WERE FOUND TO BE WITHIN LIMITS. (M)SDR ASOA05789Floorbeam · corrodedDURING A C-CHECK IN MCN, THE FLOORBEAM CAP AT FS 559 PLUS 112 THRU 621.00, LBL 27 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FLOOREAM CAP AT FS 559 PLUS 112 THROUGH 621.00, LBL 27. (M)SDR ASOA05788Skin · crackedDURING A C-CHECK IN MCN, THE RADIUS OF FUSELAGE SKIN FORWARD OF THE NOSE LANDING GEAR DOOR WAS SUSPECTED OF BEING CRACKED BEYOND LIMITS. S/D - MAINTENANCE REPAIRED THE FUSELAGE SKIN RADIUS RH AND LHS, AT FS 235, IAW ASA EO 600-53-0122. (M)SDR A6WA200540309Drag Angle · crackedPASSENGER DOOR DRAG ANGLE IS CRACKED 1.0 INCH IN RADIUS ABOVE POWER ASSIST CABLE SUPPORT PULLEY BRACKET. MAINTENANCE REPAIRED PAX DOOR ANGLE IAW MDG REO. (K)SDR ASOA05779Rib · crackedDURING A C-CHECK IN MCN, THE RIGHT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-0039B. (M)SDR VNAA0509012Warning Light · false activationDURING TAKEOFF ROLL CONFIG AILERON WARNING MESSAGES ILLUMINATED AND SOUNDED. A REJECTED TAKEOFF WAS PERFORMED. THE CREW RESET THE CONTROLS AND REPORTED THE TAKEOFF CONFIG SYSTEM OPERATIONALLY CHECKED GOOD. AFTER THE BRAKES COOLED, THE CREW CONTINUED THE FLISDR A6WA200540305Floorbeam · crackedRIGHT FS 621 FLOORBEAM ANGLE CRACKED. REPAIRED RT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (M)SDR A6WA200540306Floor Support · crackedLT FS 621 FLOOR SUPPORT ANGLE CRACKED. MAINTENANCE LT FS 621.00, FLOOR SUPPORT ANGLE IAW REO. (M)SDR A6WA200540307Angle · crackedRIGHT FS 484 AT RBL 36 ANGLE CRACKED. MAINTENANCE REPAIRED CRACKED ANGLE BY REMOVING CRACKS FLANGE AND INSTALLING A REPAIR FLANGE BRAS AND REO. (M)SDR A6WA200540308Angle · crackedFOUND LT FS 484 AT LBL 36 ANGLE CRACKED. MAINTENANCE REPAIRED CRACKED ANGLE BY REMOVEING CRACKED FLANGE AND INSTALLING REPAIRED FLANGE IAW SRM AND REO. (M)SDR CA050920002Oxygen System · failed(CAN) DURING SCHEDULED MM DEPLOYMENT OF THE PASSENGER OXYGEN MASKS WAS ATTEMPTED. THE CONTROLLER WAS SWITCHED TO THE OVERRIDE POSITION BUT ALL OF THE PASSENGER OXYGEN MASKS FAILED TO DEPLOY. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THERE WAS INSUFICIESDR A6WA200540304Intercostal · crackedFOUND RT SIDE FS 621 TO 625.3 INTERCOSTAL AT STRINGER 142 IS CRACKED NEAR RADIUS APPROX .80 INCH LONG. MAINTENANCE REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM. (M)SDR VNAA0509011Pitot Head · damagedAS THE JETWAY WAS BEING PULLED BACK, THE AUTO LEVELER CONTACTED AND DAMAGED THE STANDBY PITOT PROBE. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE REMOVED & REPLACED THE STANDBY PITOT PROBE IAW CRJ200 AMM 34-11-02-000(400)-801. OPERATIONAL AND LEAK CHECKSDR VNAA0509010Access Panel · puncturedA BELT LOADER HIT THE LT ENGINE NOSE COWL LOWER ACCESS PANEL. DAMAGE AT THE 5 O'CLOCK POSITION WAS A 6 X 2 HOLE. AFTER INSPECTION AND TEMPORARY REPAIR THE AIRCRAFT WAS FERRIED TO CKB WHERE MAINTENANCE REMOVED & REPLACED THE PANEL WITH A SERVICEABLE UNIT IAW SDR A6WA200540303Skin · damagedAIRCRAFT DAMAGED BY IMPACT FROM BELT LOADER, LT LOWER SKIN AFT OF CARGO DOOR. REPAIRED FUSELAGE SKIN BY CUTTING OUT DAMAGE AND FABRICATING AND INSTALLING SHIM FILLERS AND EXTERNAL DOUBLER IAW EO. (M)SDR ASOA05803Carbon Seal · wornFLT 4514 - DURING CLIMB-OUT FROM ATL, AT APPROXIMATELY 2000 FEET, A `RIGHT ENGINE OIL PRESSURE` WARNING WAS RECEIVED. THE WARNING WENT OUT AND RETURNED APPROXIMATELY 5 SECONDS LATER WITH OIL PRESSURE READING 20 PSI. THE QRH WAS COMPLIED WITH AND AN EMERGENCYSDR ASOA05758Lamp · inoperativeDURING AN OVERNIGHT INSPECTION IN VPS, AN EMERGENCY CEILING LIGHT AT ROW 4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)SDR ASOA05757Handle · bindingDURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE. MAINTENANCE REMOVED AND REPLACED THE ROLLER ON THE INNER DOOR HANDLE OF THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)SDR VNAA0509009Warning Light · false indicationTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS SELECTED TO 20 DEGREES AND INDICATING 8 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE PERFORMED FAULT ISOLATION AND RESET PROCEDURES IAW CRJ200 FIM 27-50-00. THE SYSTEM RESET AND NO FSDR VNAA0509008Fcu · failedAFTER TAKEOFF FROM DCA WITH FLAPS AT 20 DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND DIVERTED TO PHL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW CRJ200 AMM 27-51-05-000(400)-801.SDR MASA200500716Fuel Control · malfunctionedASH 2763 GRR. ABORTED TAKEOFF DUE TO THE NR 1 ENG NOT MAKING TAKEOFF POWER. CONTRACT MAINTENANCE PERFORMED A PERFORMANCE RUN OF THE ENGINE AND COULD NOT FIND A FAULT. FERRIED THE PLANE TO PHL WHERE MX REMOVED AND REPLACED NR 1 FUEL CONTROL.SDR VNAA0509006Fcu · malfunctionedWITH FLAPS AT 45 DEGREES ON APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW MADE A NORMAL LANDING. MAINTENANCE RESET THE FECU IAW CRJ200 SL-00-001. OPERATIONAL CHECKS WERE PERFORMED 5 TIMES AND WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICESDR VNAA0509005Fcu · malfunctionedWITH FLAPS AT 20 DEGREES ON APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND MADE A FLAPS 20 DEGREES LANDING. MAINTENANCE RESET THE FECU IAW CRJ200 SL-00-001. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERSDR A6WA200540298Angle · crackedLT FS621.0 FLOOR SUPPORT ANGLE HAS A 1 INCH CRACK. MAINTENANCE CUT OUT AND REMOVED DAMAGED ANGLE AT FS 621 LT FITTED AND DRILLED NEW ANGLES AND STRAP AND INSTALLED IAW REO. (K)SDR A6WA200540299Floorbeam · crackedRT FS 621.0 FLOOR SUPPORT ANGLE HAS A 1 INCH CRACK. CUT OUT AND REMOVED DAMAGED ANGLE. FITTED AND DRILLED UP NEW ANGLE AND STRAP, COUNTER SUNK HOLES. TREATED ALL REPAIR PARTS. INSTALLED PARTS AND PAINTED IAW REO. (K)SDR VNAA0509001Warning Light · illuminatedDURING CLIMBOUT, WITH THE LT PACK MEL'D, THE RT PACK HIGH PRESS MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETURNED TO DCA. MAINTENANCE OPERATIONALLY CHECKED THE RT PACK IAW CRJ200 AMM 21-51-00-710-801 AND WAS UNABLE TO DUPLICATE THE DISCREPANCY. NOSDR VNAA0509002Fcu · malfunctionedWITH FLAPS AT 45 DEGRESS ON FINAL APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW REPORTED NO ASYMMETRY AND MADE A NORMAL LANDING. MAINTENANCE RESET THE FECU IAW CRJ200 SL-00-001. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SESDR VNAA0509003Tire · failedAFTER LANDING INSPECTION REVEALED NR 2 MLG TIRE TREAD SEPARATION AND DAMAGE TO THE LT INBOARD FLAP. MAINTENANCE REPLACED THE WHEEL/TIRE ASSY IAW CRJ200 AMM 32-41-01-000(400)-801. THE AIRCRAFT WAS THEN FERRIED TO DAY WHERE MAINTENANCE REMOVED AND REPLACED THESDR A6WA200540300Flange · crackedMWC 138, UNDERFLOOR INTERCOSTAL ATTACHED FLANGE IS CRACKED AT LBL 36, BS 484, WL73. REPAIRED UNDERFLOOR INTERCOSTAL AT LBL 36 IAW 601R-53-41-059 AND 601R-53-0030 BY CUTTING OUT CRACKED ANGLE AND INSTALLING REPAIR ANGLE. (K)SDR A6WA200540302Intercostal · crackedRT FS621-625.3 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.2 INCHES LONG. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM. (K)SDR MASA200500689Engine · malfunctionedASH 2828 CLE. ABORTED TAKEOFF DUE TO THE NR 1 ENG WOULD NOT ACCELERATE PAST 70 PERCENT N1. CONTRACT MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE FAN AND ENGINE AREAS AND FOUND NO DEFECTS. PERFORMED ENGINE RUNS AND THE DISCREPANCY COULD NOT BE DUPLICATED
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