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 = 'CF343A1' 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 = 'CF343A1' 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 CA011128004Support · cracked(CAN) DURING INSPECTION PER SB A601R-53-059, ONE CRACK ON THE SUPPORT BEAM LOWER WEB INBOARD FORWARD CORNER (BL 36) WAS FOUND ON THE R/H SIDE AND THE L/H SIDE. REPAIR PER REO 601R-53-61-358 WAS CARRIED OUT.SDR CA011123007Support · cracked(CAN) CRACKS FOUND AT ONE LOCATION WHILE PERFORMING REPEAT INSPECTION: FS 640, BL 0.0 (UPPER WEB).THIS WAS FOUND WHILE PERFORMING THE SB A601R-53-059.DISCREPANCIES WILL BE REPAIRED USING BOMBARDIER DISPOSITIONS.SDR CA011122012Support · cracked(CAN) CRACKS FOUND AT THREE LOCATIONS WHILE PERFORMING REPEAT INSPECTION. FS 640, BL 0.0 TO LBL 9.50, WL 199.6 DISCREPANCIES WILL BE REPAIRED.SDR CA011122002Floor Support · cracked(CAN) MAINTENANCE DISCOVERED A CRACK ON TWO FRAME STATIONS IN THE AFT CARGO FLOOR LANDING PLATE AT FS589 AND FS605, WL73. GENERIC REO 601R-53-61-433 PROVIDED TO OPERATOR FOR REPAIR.SDR CA011122001Floor Support · cracked(CAN) MAINTENANCE DISCOVERED CRACK ON THE RT AND LT SIDE OF THE FLOOR SUPPORT ANGLE FOR THE COCKPIT FLOOR. THE CRACKS RUN FROM A RADIUS CUT OUT TO THE FIRST ADJACENT RIVET IN THE HORIZONTAL FLANGE. CRACK IS JUST FORWARD OF THE POST AT FS280 IN THE COCKPIT ENTRSDR CA011119010Link · broken(CAN) DURING 1200 HOURS INSPECTION, FOUND LINK P/N 228-50765-105 BROKEN. BLOCKER DOOR NR 9, P/N 228-50219-108 AND THE 6 O'CLOCK DIVERTER FAIRING P/N 228-50691-109 DAMAGED (PRESUMABLY BY LINK).SDR CA011113020Floor Panel · cracked(CAN) A 8 INCH CRACK WAS REPORTED AT FS 520. LBL 36 IN THE PRESSURE FLOOR SKIN 601R31146.SDR CA011113018Support · cracked(CAN) CRACK FOUND AT FS 630, BL: LET BL 36. FOUND DURING REPEAT INSPECTION.SDR CA011113019Support · cracked(CAN) FOUND DURING '96 MONTH' INSPECTION CHECK; CRACKED AT FS 640 & BL 00.SDR CA011113009Support · cracked(CAN) ONE CRACK FOUND ON ENGINE SUPPORT BEAM AT THE LOWER WEB FS 630, BL 0 WHILE PERFORMING SB A601R-53-059.DISCREPANCIES WILL BE REPAIR USING BOMBARDIER DISPOSITIONS.SDR CA011113010Support · cracked(CAN) CRACKS FOUND AT THREE LOCATIONS ON REPEAT INSPECTION: FS 630, LBL 36 & BL 0 WHILE PERFORMING SB A601R-53-059.DISCREPANCIES WILL BE REPAIR USING BOMBARDIER DISPOSITION.SDR CA011113011Support · cracked(CAN) CRACKS FOUND AT TWO LOCATIONS ON REPEAT INSPECTION: FS 630, LBL 36, RBL 36 WHILE PERFORMING SB A601R-35-059.DISCREPANCIES WILL BE REPAIR USING BOMBARDIER DISPOSITIONS.SDR CA011113012Support · cracked(CAN) CRACKS FOUND AT THREE LOCATIONS ON REPEAT INSPECTION: FS 630, LBL 36, RBL 36 & BL 0 WHILE PERFORMING SB A601R-53-059. DISCREPANCIES WILL BE REPAIR USING BOMBARDIER DISPOSITIONS.SDR CA011113014Support · cracked(CAN) CRACK FOUND AT ONE LOCATION ON REPEAT INSPECTION: FS 630, BL 0 WHILE PERFORMING SB A601R-53-059.DISCREPANCIES WILL BE REPAIR USING BOMBARDIER DISPOSITIONS.SDR CA011113008Bypass Valve · failed(CAN) LT ACM UNCONTROLLABLE IN AUTO OR MANUAL, AFT EQUIPMENT BAY FILLED WITH SMOKE. MCO MAINTENANCE REMOVED AND REPLACED DUEL BYPASS VALVE, DUCT SLEEVE AND COUPLING. ALSO HEAT EXCHANGES WAS REPLACED ON OVERNIGHT IN CVG. AIRCRAFT RETURNED TO SERVICE.SDR CA011121015Bearing · failed(CAN) CREW REPORTED AILERON JAMMED IN FLIGHT, QRH CARRIED OUT SYSTEM CHECK SERVICEABLE ON THE GROUND BUT THE AIRCRAFT WAS FERRIED BACK TO MONTREAL FOR FURTHER INVESTIGATION. AN FMR TO REMOVE THE LEFT END AFT AILERON QUADRANT WAS ORDERED DUE TO THE FACT THAT A SDR CA011101014Window · cracked(CAN) LT SIDE WINDOW SHATTERED IN CRUISE AT 29,000 FT. LT SIDE WINDOW REMOVED AND REPLACED. AIRCRAFT BACK IN SERVICE.SDR CA030922001Window · failed(CAN) CAPT'S SIDE WINDOW SHATTERED AT 29000 FT. LANDED AT SCHEDULED DESTINATION. WINDOW REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR CA011101006Web · cracked(CAN) FOUND CRACK ON ENGINE SUPPORT BEAM WHILE PERFORMING SB A601R-53-059. FOUND CRACKS AT THREE LOCATIONS ON LOWR WEB AT LBL 36, RBL 36 AND BL 0.SDR CA011114009Connector · corroded(CAN) FLAP FAIL AMBER CAUTION MESSAGE APPEARED DURING APPROACH (SPEED 250 KNOTS, 5000 FT FLAPS SET 0 DEGREES) FOUND CIRCUIT BREAKER 2-F4 TRIPPED. QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT AND UNEVENTFUL FLAPLESS LANDING COMPLETED. NOTE: THIS IS LAST OF A SDR SWIA200110221Rotor Shaft · brokenLEFT ENGINE N2 GAUGE FLUCTUATES BETWEEN NORMAL INDICATIONS AND ZERO. LEFT ENGINE REMOVED DUE TO N2 ROTOR SHAFT BROKEN. INSTALLED LEFT ENGINE WITH SERVICEABLE UNIT PER RII 71-401.SDR CA011005007Engine · failed(CAN) DURING CRUISE, NR 2 ENGINE LOW OIL PRESSURE INDICATOR ILLUMINATED AND VERTICAL SCALE SHOWED NO OIL PRESSURE. ENGINE WAS SHOWING HIGH VIBE INDICATIONS. FLIGHT CREW SECURED ENGINE. MADE UNEVENTFUL LANDING. INVESTIGATION IN PROGRESS.SDR CA011019007Relay · faulty(CAN) AFTER TAKEOFF UNABLE TO POWER AC ESSENTIAL BUS EITHER BY AC BUS NR 1 OR AC BUS NR 2 AIRCRAFT RETURN TO TORONTO. FOUND TO BE THE ESSENTIAL BUS SENSE RELAY AT FAULTY.REPLACED AC ESSENTIAL RELAY, POWER AVAILABLE FROM BOTH BUSES. OPERATIONAL TEST 24-51-27-71SDR COMA0160674Fan Blade · damagedFLIGHT #5775. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DECLARED AN EMERGENCY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE.SDR COMA0160675Fan Blade · damagedFLIGHT #5775. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DELCARED AN EMERGENCY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFETY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE.SDR COMA0160676Fan Blade · damagedFLIGHT #5775. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERD MULTIPLE BIRD STRIKES ON #1 ENIGNE, CREW DECLARED AN EMERGENCY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE.SDR COMA0160677Fan Blade · damagedFLIGHT #5575. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DECLARED AN EMERGENCY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE.SDR COMA0160678Fan Blade · damagedFLIGHT #5575. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DECLARED AN EMERGENCY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE.SDR COMA0160679Fan Blade · damagedFLIGHT #5775. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DECLARED AN EMERGENCY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ONT HE LEFT ENGINE.SDR CA010627046Support Bracket · cracked(CAN) BOMBARDIER AEROSPACE HAS JUST RECEIVED A REPORTALE SDR EVENT WHICH WE ARE REQUIRED TO REPORT ON. DURING INSPECTION OF ENGINE SUPPORT BEAM IAW SB A601R-53-059, MAINTENANCE FOUND CRACKS. REPAIR ENGINEERING ORDER PROGRESS, SHOULD BE PROVIDED TO THE OPERATORSDR CA010627047Support Bracket · cracked(CAN) DURING INSPECTION OF ENGINE SUPPORT BEA IAW SB A601R-53-059, MAINTENANCE FOUND CRACKS. REPAIR ENGINEERING ORDER PROVIDED, REPAIR IN PROGRESS.SDR CA010627048Support Bracket · cracked(CAN) DURING INSPECTION OF ENGINE SUPPORT BEAM IAW SB A601R-53-059, MAINTENANCE FOUND CRACKS. REPAIR ENGINEERING ORDER PROVIDED, REPAIR IN PROGRESS.SDR JBXA000292Screen · cokedFLIGHT 215 RDU TO PVD ON APPROACH HAD RIGHT ENG OIL PRESSURE LOW MASTER WARNING. DRAINED ADG OIL, INSPECTED CHIP DETECTOR FOUND C SUMP FWD SCAVENGE DRAIN SCREEN COKED UP. REMOVED COKED UP OIL RESIDUE IAW ALERT SVC BULLETIN 79-00-12. C-SUMP SCAVENGE SCREEN CSDR CA010626050Transmitter · failed(CAN) ON APPROACH AFTER SELECTING FLAP DOWN, CREW NOTICED THAT THE FLAP INDICATION WAS DIFFERENT FROM LEFT TO RIGHT. MAINTENANCE INSPECTED FLAP SYSTEM AMD FOUND FUNCTIONING NORMALLY. RT FLAP POSITION TRANSMITTER WAS DEFERRED PER MEL.SDR CA010626043Sump · coked(CAN). NR 2 ENGINE SHUT WITHOUT PILOT'S INPUT DURING THE APPROACH PHASE OF THE FLIGHT, APPROX 3500 FEET. UPON INSPECTION, MAINTNANCE NOTED: OIL DETECTED IN THE TAILPIPE, ENGINE QUANTITY CHECKED AND FOUND DEPLETED, AND SUMP B SCREEN COKED UP. ENGINE REPLACED ANSDR CA010706018Windshield · cracked(CAN) LEFT WINDSHIELD CRACKED. WINDSHIELD REPLACED.SDR CA010510019Control Unit · failed(CAN) AFTER TAKEOFF, UNABLE TO TRIM AIRCRAFT HORIZONTAL STABILIZER, AIRCRAFT RETURN TO OTTAWA, UNDER QRH PROCEDURE. RESET ATTEMPTED WITH NO SUCCESS. FOUND TO BE THE HORIZONTAL STAB TRIM CONTROL UNIT AT FAULT. REPLACED THE HORIZONTAL STAB TRIM CONTROL UNIT. OPESDR CA010511018Beam · cracked(CAN) DURING C-CHECK SEVEN CRACKS WERE FOUND IN THE ENGINE SUPPORT BEAM. TWO CRACKS WERE LOCATED ON THE LOWER WEB AT FS 640.0 NAR LBL9.0. FIVE CRACKS WERE LOCATED ON THE UPPER WEB AT FS640.0 BETWEEN LBL9.0 AND RB122.0.REPAIR ONGOING IAW REO 601R-53-61-340.SDR CA010511019Window · cracked(CAN) ON LANDING COPILOTS SIDE WINDOW CRACKED.REPLACED COPILOTS SIDE WINDOW. AIRCRAFT RETURNED TO SERVICE.SDR CA010531003Drive Unit · faulty(CAN) FLAP FAIL CAUTION MESSAGE DISPLAY ON EICAS (ENGINE INDICATIONS AND CREW AL ERT SYSTEM), QRH PERFORM WITH A NORMAL LANDING. RESET DONE AND FOUND SERVICEABLE BUT DEFECT RE-OCCURRED. FECU (FLAP ELECTRONIC CONTROL UNIT) CHANGED AS A PREVENTIVE MEASURE WITHOUSDR CA010510021Windshield · cracked(CAN) ON TAXI IN YYZ THE CAPTAINS WINDSCREEN CRACKED. WINDSHIELD AND HEAT CONTROLLER REPLACED AS PER MAINTENANCE MANUAL TASKS 56-11-01-000-801 AND 56-11-01-400-801.HEAT CONTROLLER P/N 1659-1SDR SWIA972482Adc · failedADC NR 1 INOP. IAS/ALT/VS BLANK FOR 20 MINS QRH. RETURNED TO SLC. REMOVED AND REPLACED NR 1 ADC IAW 34-12-01. OPS CHECK GOOD.SDR CA010510020Isolation Valve · failed(CAN) EICAS CAUTION MESSAGE FOR GEAR DISAGREE WHEN GEAR SELECTED, ALL INDICATION TO NORMAL AFTER SEVERAL SECONDS. AFTER TROUBLESHOOTING AND AFTER THE REPLACEMENT OF 3A AND 3B HYDRAULIC PUMPS WITH A NIL FIX, THEY ISOLATED THE PROBLEM TO BE THE MAIN LANDING GEARSDR CA010410009Apu · failed(CAN) APU SELECTED DURING DESCENT, FIRST TIME DID NOT START, PILOT RESELECT APU START. SECOND TIME APU START WITHOUT ANY INCIDENT. AIRCRAFT PULLED UP TO THE GATE, MAINTENANCE MET PILOT AT THE AIRCRAFT, ENGINE HAD BEEN SHUTDOWN WITH THE APU RUNNING. MAINTENANCESDR CA010410012Idg · damaged(CAN) DURING CRUISE, CREW NOTED AN IDG NR 1 FAULT MESSAGE, FOLLOWED BY OIL PRESSURE FLUCTUATIONS, OIL PRESSURE WARNING. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT MADE AN UNEVENTFUL SINGLE ENGINE LANDING. MAINTENANCE INVSTIGATION SUGGEST THAT IDG DISCONNECT DIDSDR CA010430002Actuator · failed(CAN) FLAP FAIL CAUTION MESSAGE WHEN FLAP SELECTED TO 30 DEGREES FOR LANDING (FLAP LOCK OUT). REPLACED NR 4 RT FLAP ACTUATOR AND NR 1 & 2 LT FLAP ACTUATORS ALSO REPLACED RT NR 4 FLEX SHAFT CABLE AND NR 1 & 5 LT FLEX SHAFT. WINTERIZATION OF THE SYSTEM ALSO COMPSDR CA010430004Psu · failed(CAN) FLAP FAIL CAUTON MESSAGE ON LANDING ROLL OUT AT 70 KNOTS. RESET ATTEMPTED WITHOUT ANY SUCCESS, FLAP TWIST INSPECTION CARRIED OUT AND FOUND R/H END BPSU BREAK AWAY TORQUE BEYOND LIMITS.REPLACED AND RIGGED BOTH B.P.S.US.PSU P/N 855100-9S/N 147 (R/H) AND 35SDR CA010403006Apu · fire(CAN) APU CAUGHT FIRE ON THE GROUND AFTER LANDING.FIRE WAS EXTINGUISHED BUT RELIT. FIRE DEPARTMENT EXTINGUISHED IT FOR GOOD. APU WAS REPLACED.SDR CA010320013Handle · failed(CAN) DURING CLIMBOUT LANDING GEAR WOULD NOT RETRACT, ANTI-SKID FAIL MESSAGE SHOW ON EICAS. MAINTENANCE REPLACED LANDING GEAR HANDLE AND AIRCRAFT BACK IN SERVICE.SDR CA010307030Engine · failed(CAN) ENGINE VIBRATION DURING CLIMB OUT AND LEVEL FLIGHT (FL230). MAXIMUM VALUE WAS 3.3 MILS. LATER FLUCTUATION BETWEEN 2.3 AND 3.3 MILS. ENGINE SHUT DOWN IN FLIGHT. SINGLE ENGINE OPERATION AS PER QRH. CHANGE LEFT ENGINE. REASON: HIGH N1 VIBRATION.
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