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 CA070205002Vane · failed(CAN) DURING CLIMB OUT STALL FAIL CAUTION MESSAGE ILLUMINATED. CREW UNABLE TO RESET DURING FLIGHT. CREW ELECTED TO LAND AT ENROUTE MAINTENANCE BASE. MAINTENANCE REPLACED RT AOA VANE, FUNCTION CHECKED AND AIRCRAFT RETURNED TO SERVICE (TC NR 20070205002)SDR CA070205003Actuator · failed(CAN) ON APPROACH, CREW SELECTED FLAP 8 AND RECEIVED A (FLAP FAIL) MESSAGE. FLAP FAILED AT 0. CREW ADVISED ATC AND DECLARED EMERGENCY. LANDING WAS UNEVENTFUL. (TC NR 20070205003)SDR VNAA0702002Idg · failedCREW REPORTED AN IDG CAS MESSAGE ON TAKEOFF ROLL. CREW REJECTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 IDG IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.SDR CA070202018Wheel · damaged(CAN) DURING ROTATION THE A/C PULLED TO THE LT ON CLIMB OUT , ASSOCIATED WITH SEVERE VIBRATION. THE FLIGHT CREW DECIDED TO DIVERT THE A/C. UPON LANDING THE ROB TIRE DEFLATED. UPON INVESTIGATION, THE FOLLOWING WAS FOUND . THE INNER RT MAIN WHEEL CORD WAS DAMAGSDR REXA200700013Unknown · unknownAFTER ESTABLISHING CRUISE ALTITUDE OUT OF DTW, THE FLIGHT CREW WAS ALERTED TO HIGHER THAN NORMAL N1 VIBRATION ON THE LEFT ENGINE. WHEN VIBRATION LEVELS CONTINUED TO INCREASE, THE QRH CHECKLIST WAS COMPLETED AND THE ENGINE WAS SHUT DOWN. THE FLIGHT CREW DECLASDR VNAA0701011Handle · unsecureCREW REPORTED A CARGO DOOR CAS MESSAGE ON TAKEOFF ROLL. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE RESECURED THE CARGO DOOR HANDLE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 52-70-02-710-801. AIRCRAFT WAS RELEASESDR VNAA0701010Outflow Valve · failedCREW REPORTED A LEFT & RIGHT HAND PACK HIGH PRESSURE MESSAGE ALONG WITH AN APU OVERTEMP MESSAGE ON CLIMBOUT. CREW FOLLOWED THE QRH AND RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE REGULATING VALVE IN ACCORDANCE WITH THE AIRSDR VNAA0701009Unknown · unknownCREW REPORTED A LOSS OF THE NR 2 GENERATOR ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PROPERLY SERVICED THE NR 2 IDG IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SESDR CA070126013Fan · dislodged(CAN) THE NR 1 ENGINE FAN DISLODGED ITSELF FROM THE ENGINE AND TORE OFF THE INLET AND FAN CASING. IT ALSO DID EXTENSIVE DAMAGE TO THE PYLON AND THE FUSELAGE. NTSB IS ON SITE FOR THE INVESTIGATION. MORE INFORMATIOON TO FOLLOW ONCE AVAILABLE. (TC NR 20070126013SDR MASA200700056Guide Vane · departedASH 2985 DEN - DURING CRUISE FLIGHT, THE CREW HEARD A LOUD POP FOLLOWED BY A LOUD BANG THEN RECEIVED A NR 1 ENGINE OIL PRESS WARNING. THE CREW THEN ISOLATED THE ENGINE, DECLARED AND EMERGENCY AND RETURNED TO THE FIELD. MX FOUND THE FAN SECTION FWD OF THE BY-SDR CA070128001Bearing Seal · leaking(CAN) REPORTS OF LAV SMOKE CAUTION MSG COMING ON. PROBLEM APPEARS TO HAVE BEGUN ON DEC 5,2006 FLT. 8620, ON CLIMB-OUT, CREW RECEIVED A LAV SMOKE DETECT CAUTION LIGHT, FA CHECKED LAV NO SMOKE WAS EVIDENT, FLIGHT RETURNED TO DEPARTURE. A/C WAS DE-ICED PRIOR TO DSDR VNAA0701008Unknown · unknownCREW REPORTED A FLAPS FAIL AT 20 DEGREES MESSAGE AFTER TAKEOFF. CREW RETURNED TO DCA AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CYCLED CIRCUIT BREAKERS IN ACCORDANCE WITH THE SERVICE LETTER. AIRCRAFT WAS RELEASED FOR SERVICE.SDR CA070131005Landing Gear · inoperative(CAN) THE AIRCRAFT LANDED WITH ALL LANDING GEAR UP. BA FSR ON SITE. FSR REPORTED THAT THE ADG WAS DEPLOYED, AND FLAPS RETRACTED. AIRPORT AUTHORITIES ARE PRESENTLY IN THE PROCESS OF LIFTING THE A/C IAW THE AIRCRAFT RECOVERY MANUAL USING CRANES. AIRCRAFT CONDITISDR CA070122006Bushing · lack of lube(CAN) CREAKING NOISE HEARD WHEN THE HORIZONTAL STABILIZER WAS CYCLED THROUGH FULL RANGE. AFT FITTING ON THE HORIZONTAL STABILIZER DISASSEMBLED. BUSHING WAS FOUND DRY ( NO LUBRICATION ). PARTS CLEANED, INSPECTED, HAND LUBED AND RE-ASSEMBLED IAW MM TASK NR 00SDR CA070122005Bushing · lack of lube(CAN) CREAKING NOISE HEARD WHEN HORIZONTAL STABLIZER WAS CYCLED THROUGH FULL RANGE. HORIZONTAL STAB HINGE BUSHINGS.THEY WERE FOUND DRY. IPC REF:27-43-01-01, ITEM NR 60. PARTS HAND LUBED AND RE-ASSEMBLED IAW MM TASK NR 000-13-320-121. CURRENT INTERVAL FOR THISDR CA070118002Flap System · malfunctioned(CAN) THE CREW REPORTED A FLAP FAIL MESSAGE ON APPROACH. THE CREW SELECTED FLAP 8 AND FLAP FAIL MESSAGE CAME ON IMMEDIATELY AND THE FLAPS FROZE AT 0 DEGREES INDICATED. ON THE GROUND A CB RESET WAS CARRIED OUT AND THE CODES WERE OBTAINED . THE AIRCRAFT WAS FERRSDR CA070119001Window · cracked(CAN) SEVERAL CRACKS IN LT SIDEWINDOW INNER AND CENTER. A/C AOG LT SIDEWINDOW CHANGED ACC AMM. ALL TESTS SATISFIED (TC NR 20070119001)SDR VNAA0701003Door · unknownCREW REPORTED A LOUD SQUEAL FROM PASSENGER DOOR ON INITIAL CLIMBOUT. CREW ELECTED TO RETURN TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND SEAL WAS NOT INFLATING. MAINTENANCE CLEANED SEAL AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS SDR VNAA0701004Valve · failedCREW REPORTED A LEFT HAND COWL ANTI-ICE MESSAGE IN FLIGHT. CREW PERFORMED AN UNSCHEDULED LANDING IN TRI WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND COWL ANTI ICE VALVE. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SESDR VNAA0701005O-Ring · crackedCREW REPORTED THE NR 2 GENERATOR FAILED ON TAKEOFF ROLL. CREW ABORTED TAKEFOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED THE NR 2 IDG AND FOUND CRACKED O-RINGS AND OIL LEAKING FROM THE STANDPIPE OVERFILL. MAINTENANCE REPLACED DAMAGED O-RINGS AND SERVICED SDR CA070115003Flap System · jammed(CAN) FLAPS FAILED UPON SELECTION TO 8 DEGREES, THEY DID NOT MOVE FROM 0 DEGREES, OAT -46 AT ALTITUDE, - 15 DEGREES ON APPROACH. AIRCRAFT LANDED FLAPS ZERO. (TC NR 20070115003)SDR VNAA0701001Shaft · brokenCREW REPORTED A FLAPS FAIL CAUTION MESSAGE ON APPROACH. CREW ABORTED APPROACH, WENT AROUND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE FLEXIBLE DRIVE SHAFT BROKEN. MAINTENANCE REPLACED THE FLEXIBLE DRIVE SHAFT PER AMM 27-53-10. OPERATISDR VNAA0701002Connector · looseCREW REPORTED A GEAR DISAGREE WARNING MESSAGE ON APPROACH. CREW ABORTED THE APPROACH, FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND A LOOSE CONNECTOR TO THE MAIN LANDING GEAR SELECTOR VALVE. MAINTENANCE REINSTALLED THE CONNECTORSDR CA070111004Flap System · jammed(CAN) CREW REPORTED ON SHORT FINAL, WHEN SELECTING FLAPS TO 8 DEGREE THE FLAP FAIL MESSAGE APPEARED AND THE FLAPS DID NOT MOVE OUT OF 0 DEGREE. MAINTENANCE UNABLE TO GET CODES. A/C FERRIED FOR FURTHER INVESTIGATION AND TROUBLESHOOTING. (TC NR 20070111004)SDR CA070111005Flap System · jammed(CAN) FLAPS SELECTED TO 8 DEGREES, NO ISSUES, THEN SELECTED TO 20 DEGREES, NO ISSUES, FLAPS 30 SELECTED NO ISSUES, UPON SELECTION TO 45 DEGREES, FLAP FAIL AND THE FLAPS LOCKED AT 30 DEGREES, OAT -30 IN FLIGHT, - 15 DEGREES OPN APPROACH, TEMP WAS -15. HAS OBTAISDR 2007FA0000102Bracket · crackedWHILE PERFORMING A 96 MONTH AIRFRAME INSPECTION, DISCOVERED THE LT FLIGHT SPOILER TRANSMITTER BRACKET WAS CRACKED. UPON REMOVING BRACKET, DISCOVERED MATTING SURFACE WITH TRANSMITTER WAS CORRODED. DECIDED TO REMOVE TO INSPECT RT TRANSMITTER BRACKET AND FOUND SDR CA070108003Fairlead · worn(CAN) DURING MAINTENANCE INSPECTION, FOUND FAIRLEAD (CLAMP) ON NR 1 HYDRAULIC SYSTEM LINES FAIRLEAD IN AFT FUSELAGE (APU COMPARTMENT) WORN. [IPC 29-11-00 FIG 15 (H) ITEM 395. BLOCK HAS 3 HOLES FOR CLAMPING HYDRAULIC LINES AND CENTER HOLE (PRESSURE LINE) MATERISDR A6WA200740006Transducer · fluctuatesAT FL320, RECEIVED ENGINE NR 2 LOP PRESS FLUCTUATED 32-38 PSI, DIVERTED TO PIT, ENGINE WAS NOT SHUTDOWN, COMPLIED WITH QRH, OIL PRESSURE INCREASED AS ALTITUDE DECREASED (44 PSI MAX). REMOVED AND REPLACED OIL PRESSURE, RAN ENGINE NR 2 FOR OIL PRESSURE. NO DEFSDR CA070108005Fcu · leaking(CAN) DEC 28/06, AERO CALLOUT 061228/01, ON PUSHBACK, A RAMP AGENT NOTICED A PUDDLE OF FUEL ON THE GROUND AT THE BACK OF THE AIRCRAFT. APPARENTLY, FUEL WAS LEAKING FROM THE APU. THE CAPTAIN CHECKED THE LEAK AS F/O CALLED APRON. THE FIRE TRUCKS WERE CALLED ASDR VNAA0612012Static Wick · damagedCREW REPORTED A LIGHTNING STRIKE ON DESCENT. MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION. MAINTENANCE REPAIRED ALL DAMAGE AND REPLACED A STATIC DISCHARGER. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.SDR SWIA200617456Fuel Control · malfunctionedON DESCENT AT 8,000/250 KNOTS AT FLIGHT IDLE LEFT ENGINE WAS NOT RESPONDING FROM IDLE TO 71.9 POSITION. SHUT DOWN LEFT ENGINE AND DIVERTED FROM BUR TO LAX. REPLACED LEFT ENGINE FUEL CONTROL UNIT IAW 73-21-00 AND RII CARD 73-900-1000. OPERATIONAL CHECKS GOODSDR CA061221005Hose · ruptured(CAN) UPON SHUTDOWN ON THE RAMP, CREW NOTICED A STRONG SMELL OF FUEL WHEN MAIN CABIN DOOR WAS OPENED. LT MAIN GEAR WAS SITTING IN A PUDDLE OF FUEL. FOUND ENGINE FUEL FEED AUX TANK LINE RUPTURED. (IPC 28-21-16 NR 285) (TC NR 20061221005)SDR TRAX200601137Beam · crackedBOX BEAM CRACKED AT UPPER CENTER LOCATION. PERFORMED EDDY CURRENT INSPECTION OF UPPER BOX BEAM JUST FWD OF FIRE LOOP STAND OFF CLIP PER MTC REQUEST IAW CRJ 200 NDTM PART 1. 51-20-06. BOX BEAM IS CRACKED AT UPPER CENTER LOCATION. REMOVED UPPER FIRE BOTTLSDR TRAX200601140Frame · corrodedLOWER SEGMENT OF FRAME 333 IS CORRODED. FOUND LOWER FRAME SEGMENT CORROSION TO BE OUT OF LIMITS OF THE SRM, REMOVED FRAME SECTION REF CRJ200SRM 51-42-06 AND 53-00-15. DRILLED UP NEW SECTION OF FRAME AND TRANSFERED FAILSAFE ANGLE TO NEW FRAME REF CRJ 200 SRMSDR TRAX200601134Light · inoperativeFLOOR EMERG LIGHTING STRIP AT 8C INOP.SDR TRAX200601135Light · inoperativeFWD HALF OF CABIN LIGHTING INOP. (CABIN INTERIOR LIGHTS WITHOUT PHOTOLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM STRIP/TAPE).SDR VNAA0612010Idg · lowCREW REPORTED A NR 1 IDG CAUTION MESSAGE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE SAFELY. MAINTENANCE INSPECTED THE NR 1 IDG AND FOUND THE OIL LEVEL LOW. MAINTENANCE PROPERLY SERVICED THE OIL LEVEL AND PERFORMED OPERATIONAL CHECKS. AIRCRASDR CA070102004Actuator · excess play(CAN) ON APPROACH (FLAPS FAIL) CAUTION MESSAGE APPEARED WHEN THE CREW SELECTED FLAPS FROM 30 - 45 DEG. ON LANDING. MAINTENANCE INSPECTED THE A/C FLAP SYSTEM AND FOUND RT AND LT IB FLAP (O/B ACTUATORS HAD EXCESSIVE SIDE PLAY OVER 0.015) IAW AMM 27-53-01-400-80SDR TRAX200601132Connector · brokenFLOOR TRACK LIGHT EMERGENCY AT THE END HAS BROKEN CONNECTOR.SDR TRAX200601133Light · inoperativeLT EXT EMERGENCY LIGHT BEHIND EMERGENCY EXIT DOOR INOP.SDR VNAA0612007O-Ring · failedCREW REPORTED A NR 1 ENGINE LOW OIL PRESSURE CAS MESSAGE IN FLIGHT. THE CREW FOLLOWED QRH PROCEDURES, DIVERTED TO CHO AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND OIL COMING FROM THE ENGINE GANG DRAIN. MAINTENANCE REPLACED O-RINGS TO THE IDGSDR CA061218001Bpsu · failed(CAN) THE CREW REPORTED THAT CLIMBING THROUGH FL220 (FLAP FAILED) MESSAGE CAME ON. THE CREW ELECTED TO CONTINUE AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. LINE MAINTENANCE FOUND THE FOLLOWING FAULT CODES 1-12-2B RH BPSU. FECU TEST CARRIED OUT NFF. WIRINSDR A6WA200640413Bolt · looseINTERMITTENT VIBRATION IN AIRCRAFT, FLIGHT CONTROL AND ENGINE INDICATIONS NORMAL. INSPECTED ALL DOOR AND SEALS, PRIMARY AND SECONDARY FLIGHT CONTROLS, MLG AND NLG DOORS, ALL FAIRINGS, WHEEL BINS, RAM AIR SOV, APU INLET DOOR, ACM`S, RADOM, WING TO FUSELAGE MOUSDR VNAA0612005Wire · brokenCREW REPORTED A NR 2 GENERATOR CAS MESSAGE ON TAKEOFF. CREW RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 2 GENERATOR. MAINTENANCE PROPERLY SERVICED OIL LEVEL AND REPAIRED A BROKEN WIRE ON NR 2 IDG TEMP BULB. OPERATIONAL CHECKS WERE PERFORSDR A6WA200640407Smoke Detector · malfunctionedLAV SMOKE WARNING IN FLIGHT, COMPLIED WITH QRH, F/A REPORTS LAV SMOKE WARNING AND F/A REPORTS TEMPERATURE WARM IN CABIN, PACK AIR OUTPUT IN COCKPIT SMELLS OF DIRTY SOCKS. REMOVED AND REPLACED SMOKE DETECTOR, (CHANGING BOTH COALESCER BAGS). (K)SDR VNAA0612004Oil System · unknownCREW REPORTED AN IDG NR 1 CAUTION MESSAGE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED THE NR 1 IDG OIL LEVEL. MAINTENANCE PROPERLY SERVICED OIL LEVEL. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVISDR A6WA200640404Cover · dislodgedOXYGEN MASKS COVERS FELL FROM SEATS 4 AND 5 (A) AND (C). RESECURED PSU COVERS AT SEATS 4 AND 5 IAW AMM. (K)SDR A6WA200640405Flap System · malfunctionedFLAPS FAILED TO EXTEND WHEN SELECTED ON APPROACH. COMPLIED WITH SUPPLEMENT 98-018A, FLAP RESET AND OPERATE NORMALLY. (K)SDR CA070109001Tube · blocked(CAN) AUTO SHUTOFF DID NOT OCCUR DURING PRESSURE REFUELING OPERATIONS RESULTING IN FUEL SPILL ON RAMP. OPERATOR REPORTED SIMILAR PROBLEMS SINCE TAKING DELIVERY OF NEW AIRCRAFT. IT WAS FOUND THAT A NUMBER OF LT AND RT WING TRANSFER AND BALANCING PIPES (TUBES) HSDR A6WA200640412Bpsu · faultyFLAPS FAILED AT ZERO DEGREES WHEN SELECTED ON APPROACH. CROSS REFERENCE: A6WA200740030 - FOUND EVIDENCE OF WATER IN RT NR 3 AND NR 4 FLEX DRIVE SHAFT, CLEANED FLEX DRIVE SHAFTS NR 3 AND NR 4. (K) WHEN SELECTING FLAPS FROM 8 DEGREES TO 20 DEGREES, A FLAP CAUT
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