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 A6WA200540339Skin · nickedNUMEROUS NICKS IN PAIR AND/OR SKIN ON AFT FUSELAGE RT SIDE FS 589 TO 605 BETWEEN STRINGERS 21R TO 26R. REPAIRED DAMAGED AREA IAW EO BY CUTTING AWAY DAMAGE AND INSTALLING FILLERS AND EXTERNAL DOUBLERS. (K)SDR A6WA200540345Skin · damagedTHE FUSELAGE 5 KM BETWEEN VS 55.625 PERCENT AND VS 67.5 PERCENT. SPAR DATUM BETWEEN STRINGER 2R AND 4R HAS A DENT 1.5 INCH LONG X 1.875 INCH WIDE X .109 INCH DEEP. REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN VS 55.625 AND VS 67.5 SPAR DATUM BETWEEN STRINGERS 2RSDR A6WA200540346Floor Support · crackedRT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED. PERFORMED REPAIR TO RT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K)SDR VNAA0511009Pedal · obstructedTHE TAKEOFF WAS REJECTED DUE TO BINDING IN THE RUDDER PEDALS. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE FOUND A COCKPIT SUN VISOR JAMMING THE RT RUDDER PEDALS. THE SUN VISOR WAS REMOVED AND THE RUDDER SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ200 AMSDR A6WA200540344Skin · crackedLT FS640 BONDED SKIN CRACKED. REPAIRED LT BONDED DOUBLER AT FS 640 BY FABRICATING ANGLE AND INSTALLING BETWEEN STR6L AND 14L. (K)SDR VNAA0511007Flap System · malfunctionedDURING APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 8° SELECTED TO 20°. THE CREW FOLLOWED THE QRH, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM PER THE CRJ FIM. THE FLAP SYSTEM WAS RESET IAW BOMSDR VNAA0511008Unknown · noneTHE CREW REPORTED ENCOUNTERING SEVERE TURBULENCE DURING DESCENT BETWEEN FL230 AND FL210. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE PERFORMED AN EXTREME TURBULENCE / MANEUVER INSPECTION IAW CRJ200 AMM 05-51-03-210-801. NO DEFECTS WERE FOUND. THE AIRCSDR CA051112001Window · cracked(CAN) CAPTAINS SIDE WINDOW CRACKED, WINDOW REPLACED.SDR VNAA0511006Striker · damagedTHE CREW REPORTED A LOUD SQUEAL FROM THE PASSENGER DOOR DURING CLIMBOUT. THE AIRCRAFT RETURNED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DAMAGE TO THE PASSENGER DOOR FORWARD AND AFT SEAL STRIKERS. A TEMPORARY REPAIR WAS PERFORMED IAW BOMBARDIER SDR VNAA0511005Skin · lightning strikeTHE CREW REPORTED A LIGHTNING STRIKE ON DESCENT INTO YYZ. MAINTENANCE COMPLIED WITH AN EN ROUTE LIGHTNING STRIKE INSPECTION AND FOUND DAMAGE TO THE LEFT WINGLET. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE COMPLIED WITH DETAILED LIGHTNING STRIKE INSPECSDR A6WA200540321Angle · crackedOB CLIP AT FS 280, LBL 9.0, IS CRACKED IN RADIUS AT TOP OF CLIP CRACK APPROX .5 INCH LONG. REMOVED AND REPLACED FS 280, LBL 9.0 FLOORBEAM TO BULKHEAD ATTACHMENT ANGLE IAW SRM (OB CLIP). (K)SDR A6WA200540322Angle · crackedIB CLIP AT FS280, RBL 9.0, IS CRACKED IN RADIUS AT TOP OF CLIP, APPROX .5 INCH LONG. REMOVED AND REPLACED FS 280, RBL 9.0 FLOORBEAM TO BULKHEAD IB ATTACHMENT ANGLE IAW SRM. (K)SDR A6WA200540336Attach Angle · crackedOB CUP AT FS280, RBL 9.0 IS CRACKED IN RADIUS AT TOP OF CUP, APPROX .50 INCH LONG. REMOVED AND REPLACED FS280, RBL 9.0 FLOORBEAM TO BULKHEAD ATTACHMENT ANGLE IAW SRM (OB CLIP). (K)SDR A6WA200540337Attach Angle · crackedOB CLIP AT FS 280, RBL 9.0 IS CRACKED IN RADIUS AT TOP OF CUP, APPROX .50 INCH LONG. REMOVED AND REPLACED FS 280, RBL 9.0 FLOORBEAM TO BULKHEAD ATTACHMENT ANGLE IAW BRAS SRM (OB CLIP). (K)SDR A6WA200540338Angle · crackedOB CLIP AT FS 280, LBL 9.0 IS CRACKED IN RADIUS AT TOP CLIP, CRACK APPROX .50 INCH LONG. REMOVED AND REPLACED FS 280, LBL 9.0 FLOORBEAM TO BULKHEAD ANGLE IAW SRM (OB CLIP). (K)SDR A6WA200540341Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED APPROX 1.0 INCH LONG AT DOOR SUPPORT CABLE PULLEY. CUT AWAY DAMAGED SECTION OF DRAG ANGLE AND INSTALLED REPAIR ANGLE AND SPLICES IAW REO. (K)SDR A6WA200540342Angle · crackedWO 87925, MWC 214, FS484, LBL 36 IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCH LONG. REPAIRED CRACKED ANGLE AT FS 484, LBL 36 BY REMOVING AND REPAIRING ANGLE WITH FABRICATED ANGLE IAW REO. (K)SDR A6WA200540343Angle · crackedWO 87925, MWC 213, FS484, RBL36 IB ANGLE OF INTERCOSTAL IS CRACKED .5 INCH LONG. REPAIRED CRACKED ANGLE AT FS 484, RBL36 BY REMOVING AND REPLACING ANGLE WITH FABRICATED ANGLE IAW REO. (K)SDR VNAA0511004Skin · lightning strikeAFTER LANDING THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE ON THE NOSE OF THE AIRCRAFT. MAINTENANCE PERFORMED AN EN ROUTE LIGHTNING STRIKE INSPECTION AND FOUND EVIDENCE OF LIGHTNING DAMAGE ON THE RT HORIZONTAL STABILIZER TIP FAIRING. THE AIRCRAFT WAS FERRIESDR VNAA0511003Warning Light · noneTHE ANTI-ICE DUCT WARNING MESSAGE ILLUMINATED WHEN WING ANTI-ICE WAS SELECTED ON. THE CREW FOLLOWED THE QRH AND RETURNED TO PIT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE WING ANTI-ICE SYSTEM IAW CRJ200 AMM 30-12-00-710-801. THE SYSTEM OPERATIONALLY CSDR CA051129003Apu · failed(CAN) WHILE AT THE GATE AND PRIOR TO DEPARTURE, THE FLIGHT CREW HAD AN APU FIRE WARNING INDICATION. THE CREW FOLLOWED THE QRH PROCEDURE AND DICHARGED THE APU FIRE BOTTLE. LINE MAINTENANCE INSPECTED THE APU AND FOUND NO EVIDENCE OF FIRE. THEY ALSO FOUND THE FUESDR ASOA05949Sill · corrodedDURING A C-CHECK, THE SERVICE DOOR SILL AREA WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINT REMOVED LIGHT CORROSION IN 2 PLACES OF SERVICE DOOR SILL AREA. CLEANED, TREATED, PRIMED AND PAINTED AREAS IAW SRM. (K)SDR ASOA05948Flashlight · inoperativeDURING A GROUND INSPECTION, THE CAPTAINS FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE CAPT FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)SDR 05134Guide Vane · brokenFLIGHT LEFT SBN ON A FERRY FLIGHT TO THE TYS MAINTENANCE BASE DUE TO A MISSING RIGHT HAND ENGINE THRUST REVERSER BLOCKER DOOR. AT FL230 AND 80 MILES OUT OF KNOXVILLE, THE RIGHT HAND ENGINE FLAMED OUT. THE FLIGHT CREW EXECUTED THE SINGLE ENGINE OPERATION QRH SDR REXA200500134Guide Vane · brokenTHE AIRCRAFT DEPARTED, ON A FERRY FLIGHT TO THE MAINTENANCE BASE, DUE TO A MISSING RT THRUST REVERSER BLOCKER DOOR. AT FL230 AND 80 MILES OUT, THE RT ENGINE FLAMED OUT. THE FLIGHT CREW EXECUTED THE SINGLE ENGINE OPERATION PORTION OF THE QRH AND DECLARED AN EMESDR VNAA0511001Pitot Head · bird strikeAFTER LANDING THE CREW REPORTED A BIRD STRIKE TO THE RT SIDE OF THE RADOME AND RT PITOT TUBE. MAINTENANCE COMPLIED WITH A BIRD STRIKE INSPECTION. THE RT PITOT TUBE WAS FILLED WITH BIRD DEBRIS. NO OTHER DAMAGE WAS FOUND. THE AIRCRAFT WAS FERRIED TO DAY WHERSDR ASOA05943Support Beam · crackedDURING AN A-CHECK, THE RT SIDE ENGINE SUPPORT BEAM, AT BL36.20, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RT SIDE ENGINE SUPPORT BEAM, AT BL 36.20, IAW EO. (K)SDR CA051112002Thrust Reverser · broken(CAN) AC WAS BEING FERRIED SOUTH TO BASE WITH MISSING BLOCKER DOOR, WITH T/R BEING DEFERRED IAW MEL IN ORDER TO BE REPAIRED, DIDN'T HAVE BLOCKER DOOR IN STOCK. ON ITS WAY TO DESTINATION, CREW HEARD A LOUD BANG DURING DESCENT, RT ENGINE FLAMED OUT ON ITS OWN. SDR VNAA0510023Flap System · malfunctionedDURING APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 20 DEGREES SELECTED TO 30 DEGREES. THE CREW ABORTED THE APPROACH, RECONFIGURED THE AIRCRAFT, AND LANDED WITHOUT INCIDENT. MAINTENANCE RECORDED FECU LRU & FAULT LOG CONTENTS PER THE FIM.SDR ASOA05917Clip · crackedDURING A C-CHECK, THE LT IB CLIP AT FS 484, LBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT IB CLIP AT FS 484, LBL 27 IAW EO 600-53-0098.SDR AMTA200500944Terminal · looseLOOP ONE EICAS MSG LT ENG. FOUND TERMINAL LOOSE AT LOOP TS5033. TIGHTENED AS REQUIRED. FIRE LOOP OPS CHECK NORMAL IAW AMM. (K)SDR COMA0560568Actuator · unreliableFLAPS FAIL CAUTION. CND REPLACED THE RT WING FLAP ACTUATORS.SDR VNAA0510022Striker · damagedDURING AN FAA RAMP CHECK, THE INSPECTOR DISCOVERED DAMAGE TO THE PASSENGER DOOR SEAL STRIKER. THE AIRCRAFT WAS FERRIED TO CAK. MAINTENANCE PERFORMED A TYPE II REPAIR IAW REO 601R-53-22-033. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR VNAA0510020Skin · lightning strikeDURING AN FAA RAMP CHECK, THE INSPECTOR DISCOVERED EVIDENCE OF LIGHTNING STRIKE DAMAGE ON THE TRAILING EDGE OF THE RT AILERON AND RT OUTBOARD FLAP. MAINTENANCE COMPLIED WITH AN EN ROUTE LIGHTNING STRIKE INSPECTION AND FOUND EVIDENCE OF LIGHTNING DAMAGE ON THSDR VNAA0510021Skin · undamagedDURING AN FAA RAMP CHECK, THE INSPECTOR DISCOVERED EVIDENCE OF LIGHTNING STRIKE DAMAGE ON TOP OF THE LT AILERON. THE AIRCRAFT WAS FERRIED TO CAK. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION AND FOUND NO LIGHTNING DAMAGE TO THE AIRCRAFT. SDR AMTA200500936Card · unserviceableEICAS MSG (L ENG OH LLP1). REMOVED AND REPLACED LT ENG AUTO FIRE HEAT DET CARD IAW MM. RAN LT ENG, OPS CHECKED OK. (K)SDR A6WA200540315Ecu · faultyIN LEVEL FLIGHT AT 240, RECEIVED SPOILERON FAULT, ALSO RECEIVED ROLLING MOVEMENT 5-8 DEGREES TO THE RT. AIRCRAFT RETURNED TO NORMAL FLIGHT CHARACTERISTICS, SPOILERON FAULT EXTINGUISHED ON GROUND. REMOVED AND REPLACED SECU NR 2 IAW AMM, OPS CHECCK GOOD AT THISDR ASOA05895Cover · brokenDURING A GROUND INSPECTION, THE FORWARD RT SIDE EMERGENCY EXIT LIGHT COVER WAS FOUND TO BE BROKEN. MAINT REMOVED AND REPLACED THE FORWARD RT SIDE EMERGENCY EXIT LIGHT COVER. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)SDR ASOA05894Step · disconnectedDURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP TIE ROD WAS FOUND DISCONNECTED FROM THE PASSENGER DOOR BOTTOM STEP. MAINT REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)SDR ASOA05786Intercostal · crackedDURING A C-CHECK IN MCN, THE FS 280 INTERCOSTAL, AT RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE FS 280 INTERCOSTAL, AT RBL 9, IAW REO 601R-53-11-638. (M)SDR CA051104017Skin Panel · damaged(CAN) DURING DESCENT, AIRCRAFT HIT GOOSE. AIRCRAFT LANDED NORMALLY. DAMAGE FOUND ON IB RT LE (DENT .7500 INCH DEEP 4.5 INCH WIDE AND 8.5 INCH LONG). MFG AUTHORIZED FERRY FLIGHT WITH THIS DAMAGE TO MAINTENANCE BASE. MAINTENANCE REMOVED LEADING EDGE FOR INSPESDR COMA0560561Actuator · failedFLAPS FAIL. CND REPLACED 4 FLAP ACTUATORS ON LT WING.SDR COMA0560559Drive Assy · dirtyFLAPS FAIL CAUTION. CND, FOUND NO DEFECTS IN FLAP SYSTEM, CLEANED AND GREASED FLEX DRIVE CABLES.SDR A6WA200540314A/C Pack · contaminatedUPON CLEANING OIL RESIDUE FROM APU, FOUND LT PACK SMOKING SLIGHTLY FROM EXHAUST. FOUND OIL CAME FROM APU OIL COOLER RESIDUE. OPERATED LT PACK IAW AMM, NO FUMES OR SMOKE NOTED FROM AIR CONDITIONING SYSTEM OR EXHAUST. (K)SDR VNAA0510014Servo · failedTHE CREW REPORTED STAB TRIM MOVEMENT WITHOUT PILOT INPUT IN FLIGHT. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE FOUND A FAILED AUTOPILOT ELEVATOR SERVO. THE SERVO WAS REMOVED & REPLACED IAW CRJ200 AMM 22-11-24-000(400)-801. OPERATIONAL TESTS OF AUTOPISDR VNAA0510013Flap System · malfunctionedON APPROACH WITH FLAPS AT 20 DEGREES, THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WHEN SELECTING FLAPS 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM IAW CRJ200 AMM 27-54-00-710-801. OPS CSDR CA051019000Exhaust Pipe · detachedEN ROUTE LOST THE LT ENGINE EXHAUST NOZZLE DURING CRUISE. THE FLIGHT CREW REPORTED A SLIGHT YAW WHEN THE EXHAUST NOZZLE DETACHED, AND THE FLIGHT ATTENDANT REPORTED A CHANGE IN ENGINE NOISE. THE EXHAUST NOZZLE HAS NOT BEEN RECOVERED. SHORTS BROTHERS SERVICE SDR VNAA0510012Bolt · failedAFTER POST FLIGHT INSPECTION THE CREW REPORTED THE LEFT ENGINE EXHAUST NOZZLE AND FAIRING WERE MISSING. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED ALL 31 ATTACH BOLTS HAD FAILED AND WERE ALSO MISSING. ALL MISSING AND DAMAGED PARTS WERE REPLACED WITH SSDR VNAA0510010Flap System · malfunctionedTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH WITH FLAPS 20 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE INSPECTED THE FLAP SYSTEM AND RESET THE FECU IAW CRJ200 FIM 27-50-00. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELESDR A6WA200540313B-Nut · looseWHILE APU RUNNING HEARD LOUD BANG NOISE FROM REAR OF AIRCRAFT. APU RPM DROPPED BY 10 PERCENT. FLIGHT ATTENDANT NOTICED SMELL OF FUEL IN REAR OF AIRCRAFT. NO INDICATION OF FIRE. SHUTDOWN APU. INSPECTED APU, FOUND LOOSE B-NUT ON FUEL SOLENOID. RETORQUED B-
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