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 CA000830026Engine · malfunctioned(CAN) AFTER TAKEOFF, THE RIGHT ENGINE OIL PRESSURE WAS FLUCTUATING RAPIDLY 55-42 PSI. THE PILOT DECLARED EMERGENCY, THE LANDING WAS UNEVENTFUL. MAINTENANCE CONTROL REPLACED THE RT ENGINE (THE EXACT CAUSE IS NOT KNOWN) (S/N OFF: 807100/S/N ON: 807432).SDR CA000830027Selector Valve · failed(CAN) AFTER TAKEOFF, WHEN SELECTING THE LANDING GEAR UP, THE NOSE DOOR OPEN WARNING APPEARED. MAINTENANCE REPLACED THE NOSE GEAR DOOR SELECTOR VALVE (P/N:55540-5, S/N OFF: 1131/S/N ON: 1197) AND THE PROX. SENSOR P/N: 8-648-07 & P/N: 8-648-08.SDR COMA0060678Engine · fluctuatesRIGHT HAND ENGINE OIL PRESSURE FLUCTUATING BETWEEN 42 AND 55 PSI. REPLACED RIGHT HAND ENGINE.SDR CA000830029Aileron · jammed(CAN) THE FLIGHT CREW REPORTED AFTER TAKEOFF THE RIGHT AILERON APPEARS TO BE JAMMED. ON DESCENT, THE AILERON CAME UN-JAMMED AND APPEARED TO BE NORMAL.AILERON SERVO REPLACED AS PRE-CAUTIONARY MEASURE.SDR CA001004020Bpsu · failed(CAN) FLAP FAIL MESSAGE ON (EICAS) ENGINE INDICATION AND CREW ALERT SYSTEM ON FINAL FAILED WHILE MOVING FROM TO 10 TO 20 DEGREES.CHANGED FLAP CONTROL UNIT AND LEFT AND RIGHT BRAKE POSITIONING UNIT.CF-98-14 CARRIED OUT OPERATION AND INDICATION FOUND SERVICEABLESDR COMA0060649Amplifier · malfunctionedLEFT ENGINE OVERSPEED WARNING. REPLACED THE N1 AMPLIFIER.SDR CA000918004Control Unit · failed(CAN) MACH TRIM FAULTY WITH STAB TRIM FAILURE. RE-RACKED OF THE HORIZONTAL STAB CONTROL UNIT (HSTCU) AND CARRIED OUT A BITE CHECK OF THE OPERATIONAL SYSTEM. NO FAULT FOUND, CONSIDERED SERVICEABLE.SDR CA000810017Line · burst(CAN) DESCRIPTION OF DEFECTS: AIRCRAFT AFTER TAKEOFF AND ON CLAIM RECEIVED HYD 3 PRESS EICAS WARNING MESSAGE. SYSTEM NR 3 HAD NO PRESSURE. AIRCRAFT DECLARED EMERGENCY LANDING AND EMERGENCY GEAR EXTENSION AND RETURN TO FIELD. MAINTENANCE ACTIONS: MAINTENANSDR COMA0060631Engine · leakingLEFT ENGINE LOW OIL PRESSURE WARNING. SERVICED ENGINE WITH 6 QUARTS OIL. C/W OIL CONSUMPTION CHECKS, NO FAULTS FOUND.SDR CA000918009Switch · loose(CAN) REJECTED TAKEOFF AT 100 KNOTS FOR A UNLOCKED LIGHT OF THE RIGHT END THRUST REVERSER.FOUND STOW SWITCH TO BE VERY LOOSE. SWITCH RE-ADJUSTED.SDR CA000810009Duct · cracked(CAN) DURING A PERIOD OF 4 DAYS, THE CREW REPORTED NUMEROUS INDICATION OF RT JET OVHT FAIL, CAUTION MESSAGE AND RT JET PIPE OVHT WARNING MESAGE. WHEN RETARDING THE THRUST AS PER QRH, THE MESSAGES WENT AWAY. THE PROBLEM WAS IDENTIFIED AS A 14TH STAGE DUCT LEAK SDR CA000918005Actuator · failed(CAN) TAKEOFF REJECTED AT 20 KNOTS FOR A HORIZONTAL STAB CHANNEL 1 FAULT MESSAGE ON THE ENGINE INDICATION CREW ALERT SYSTEM (EICAS), AIRCRAFT RETURNED TO GATE IN WASHINGTON. REPLACED HORIZONTAL TRIM UNIT (P/N 7060-8), HORIZONTAL STAB ACTUATOR (P/N 8396-3) AND SDR CA000830003Handle · unsecure(CAN) AIR TURN BACK TO YUL DUE TO A AVIONICS BAY DOOR CAUTION AT 2800 FEET. FOUND DOOR HANDLE NOT SECURED.DOOR HANDLE CYCLED AND LATCHED PROPERLY, FOUND OPERATIONAL.SDR CA001019030Ecu · failed(CAN) GEAR DISAGREE MESSAGE AFTER GEARS SELECTED DOWN,, AND ON LANDING NOSE GEAR STEERING NOT AVAILABLE. NECESSARY TO TOW AIRCRAFT TO GATE. REPLACED STEERING ELECTRONIC CONTROL UNIT, STEERING SOLENOID VALVE (MPN 16850-101), AND SELECTOR VALVE (MPN 750006000)SDR CA000830004Bearing · failed(CAN) RIGHT ENGINE IN FLIGHT SHUT DOWN AFTER LOSS OF OIL PRESSURE AND LOUD BANG HEARD. AIRCRAFT RE-ROUTED TO ST. LOUIS AND LANDED SAFELY. AIRCRAFT EXPERIENCED HIGH VIBRATION AFTER THE LOUD BANG NOISE. TO BE INVESTIGATED.ENGINE TO BE REPLACED AND SENT TO STRSDR CA000830006Bpsu · failed(CAN) FLAP LOCK OUT MESSAGE AT FLIGHT LEVEL OF 3,300 FEET.AIRCRAFT REMOVED FROM SERVICE DUE TO REPEATED DEFECT. REPLACED R/H AND L/H BRAKE POSITIONING SENSOR UNIT. REPLACED R/H OUTBOARD ACTUATOR. REPLACED THE FLAP CONTROL 5 POSITION LEVER. REPLACED THE FLAP ELSDR CA000830024Vane · failed(CAN) THE FLIGHT CREW ABORTED THE TAKEOFF WHEN THE STALL FAIL CAUTION MESSAGE APPEARED AT 70 TO 80 KNOTS. (ABORTED T/O).THE LEFT AOA VANE WAS REPLACED AND THE AIRCRAFT RETURNED IN SERVICE.SDR CA000830005Flap · malfunctioned(CAN) FLAP LOCK OUT MESSAGE AT 20,000 FEET WITH NO FLAP MOVEMENT, AIRCRAFT RETURNED TO OTTASA FOR INSPECTION. INSPECTION OF FLAPS FOR TWISTING, SQUEAKING AND DEFORMATION COMPLETED. A RESET OF THE FLAPS WAS DONE AND AN OPERATIONAL CHECK CARRIED OUT WITH NO FAULSDR CA000808024O-Ring · leaking(CAN) DURING A FERRY FLIGHT FROM MORLAIX TO CAEN, PILOTS REPORTED A LT ENGINE N2 FLUCTUATION FOLLOWED BY A LOW OIL PRESSURE WARNING MESSAGE. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT COMPLETED AN UNEVENTFUL LANDING IN MORLAIX. FINDINGS: OIL LEAK WAS FOUND ASDR CA000808022Pcu · leaking(CAN) WHILE PERFORMING FIRST FLIGHT OF THE DAY ELEVATOR SYSTEM CHECK USING NR 2 HYDRAULIC SYSTEM ONLY, ELEVATOR POSITION EICAS READINGS SHOWING SPLIT AS MUCH AS 15-24 DEGREES. LT ELEVATOR PCU NR 2 AND RT ELEVATOR PCU NR 3 REPLACED.SDR CA000918002Bpsu · failed(CAN) FLAP FAIL AT 27 DEGREES. BPSU AND MEN POWER SENT TO OTTAWA FOR REPAIR. REPLACED BRAKE POSITIONING SENSING UNIT (BPSU), RIGGED AND OPERATIONAL CHECK CARRIED OUT. FOUND SERVICEABLE.SDR CA000830007Bracket · deformed(CAN) WARNING MESSAGE GEAR DISAGREE AND NOSE DOOR OPEN DURING TAKEOFF.RECYCLING OF THE GEAR WAS TRIED UNSUCCESSFULLY, AIRCRAFT RETURNED TO YUL FOR LANDING. AFTER INVESTIGATION, FOUND PROXIMITY SENSOR BRACKET DEFORMED. BRACKET CHANGED AND PROXIMITY SENSOR ADJUSSDR COMA0060576Engine · overservicedLEFT ENGINE HIGH OIL TEMP. FOUND ENGINE TO BE OVERSERVICED. DRAINED OIL TO PROPER LEVEL AND AIRCRAFT RETURNED TO SERVICE.SDR CA000724008Turbine · failed(CAN) ON CLIMB OUT NR 2 ENGINE N2 EXCEEDED LIMITS, THEN SHUT DOWN. CREW DECLARED AN EMERGENCY AND MADE AN UNEVENTFUL LANDING. AFTER INVESTIGATION MAINTENANCE REPORT LPT (LOW PRESSURE TURBINE SECTION) CASE PENETRATION (PRIMARILY AT THE 7-8 OCLOCK POSITION). THESDR COMA0060563Engine · vibrationLEFT ENGINE VIB METER AT 3.4. C/W FAN TRIM BALANCE.SDR CA000802003Warning Light · illuminated(CAN) ON APPROACH TO WINNIPEG, FLAP FAIL MESSAGE APPEARED, STUCK AT 8 DEGREES.0 DEGREE LANDING PROCEDURE CARRIED OUT.CIRCUIT BREAKER RESET, SYSTEM FOUND SERVICEABLE.SDR COMA0060559Engine · failedRIGHT HAND ENGINE FAILED AFTER TAKE OFF. REPLACED THE RIGHT HAND ENGINE.SDR CA000802002Fuel Control · failed(CAN) RT POWER LEVER STUCK IN CRUISE AT FLT LEVEL 280-680 LB/RT FF & APPROXIMATELY. 91 PERCENT N1 92.5 N2. QRH 1.11 CARRIED OUT (ENGINE SHUTDOWN) LDG IN WINNIPEG.REPLACED FUEL CONTROL UNIT & THROTTLE CONTROL GEARBOX, SYS RIGGED AS PER MAINT MANUAL 7 6-11-17, 7SDR CA000714007Control Unit · failed(CAN) AFTER TAKE OFF, NOSE GEAR WOULD NOT RETRACT, WITH ASSOCIATED MSG, WOW INPUT, STEERING FAIL ETC. CREW DECLARED AN EMERGENCY AND COMPLETED AN UNEVENTFUL LANDING, RETURNING TO THEIR ORIGINATING BASE. MAINTENANCE REPLACED STEERING HARNESS P/N: DOWTY 17300-23SDR CA000802006Control Unit · failed(CAN) GROUND SPOILERS DEPLOYED UNCOMMANDED DURING TAXI OUT AFTER CONTROL. CHECK SPOILERS STOWED BY THEMSELVES SEVERAL SECONDS LATER. THIS REPEATED MOMENTS LATER WITH NO CONTROL WHEEL INPUT. AIRCRAFT RETURNED TO GATE.SWAPPED LT AND RT SPOILER ELECTRONIC CONTROSDR CA000720014Battery · wrong part(CAN) UPON ELT RECERTIFICATION, A NON TC APPROVED BATTERY WAS FOUND IN THE UNIT.ONLY THE DM U158-1 IS APPROVED BY TC (REF AWN BO14, EDITION 4) FOR USE IN THIS ELT. CORRECT BATTERY WAS INSTALLED AND ELT RECERTIFIED.SUPSDR CA000721002Lever · out of adj(CAN) PASSENGER DOOR HARD TO OPEN.ADJUSTED DOOR FORWARD, PUL IN LEVERS AND PUSH OUT STOP, AS PER AIRCRAFT MAINTENANCE MANUAL 52-11-02-820-801, CHECK SERVICEABLE.SDR COMA0060503Seal · leakingRIGHT HAND ENGINE LOST OIL PRESSURE. REPLACED THE DRIVE PAD OIL SEALS FOR THE AIR STARTER, HYDRAULIC PUMP AND IDG.SDR CA000714021Uplock Target · loose(CAN) EICAS (ENGINE INDICATION AND CREW ALERT SYSTEM) MESSAGE FOR DISAGREEMENT FOR LANDING GEAR RETRACTION, (FOR UP LOCK) AIRCRAFT RETURNED TO LAND IN PHILADELPHIA AFTER QRH PROCEDURE APPLIED.AFTER INSPECTION, FOUND THE UP LOCK TARGET TO BE LOOSE. RE-TIGHTENEDSDR CA000714018Aileron · failed(CAN) ON CLIMB OUT OF HALIFAX AT FL250 RIGHT HAND AILERON INDICATED PLUS 1 DEGREE AND JAMMED, CONTROL WHEEL STIFF TO OPERATE. AUTOPILOT TRIM MESSAGE, AUTOPILOT DISCONNECTED. ON DESCENT AILERON RETURNED TO NORMAL. LUBRICATED ALL ACCESSIBLE PIVOT POINTS AT POWERSDR COMA0060468Turbine Wheel · crackedAFTER REPLACEMENT OF THE NR 1 CARBON SEAL ON AIRCRAFT 7123 LEFT ENGINE 807393, A CRACK WAS DISCOVERED ON THE FAN DISK AT THE FORWARD 12:00 POSITION OF THE NR 21 FAN BLADE PIN RETAINING BORE. THE CRACK IS APPROXIMATELY 1.5 INCHES IN LENGTH AND EXTENDS FROM THESDR CA000714020Door · jammed(CAN) PASSENGER DOOR DIFFICULT TO CLOSE FROM INSIDE. UNABLE TO LATCH DOOR CLOSED EASILY BECAUSE IT SEEMS TO BE JAMMING AT BOTTOM OF DOOR. DOOR TESTED SEVERAL TIMES FROM BOTH SIDES AND FOUND TO FUNCTION NORMAL. AT NEXT HANGER VISIT GAS SPRING FUNCTIONAL TEST CASDR CA000621040Door · missing(CAN) ON ARRIVAL IN OTTAWA, GROUND AIR CONDITIONING CONNECTION DOOR FOUND MISSING. NEW DOOR INSTALLED AND OPERATION CHECKED SERVICEABLE.SDR CA000530055Transducer · inoperative(CAN) OIL PRESSURE TRANSDUCER WAS INOPERATIVE, GIVING FALSE LOW PSI READING. NO EICAS SYSTEM WARNING PRESENT.SDR CA000530064Sensor · overheated(CAN) ENGINE SHUT DOWN IN FLIGHT DUE TO 14TH STAGE DUCT OVERHEAT MESSAGE. MESSAGE APPEARED, BLEEDS CLOSED WITH NO SUCCESS.MESSAGE STILL APPEARED. EMERG LANDING DECLARED. 14 STAGE LOOP REPLACED.SDR CA000511032Warning System · false indication(CAN) CARGO SMOKE MESSAGE ON SHORT FINAL. FOLLOWED QRH AND BLEW BOTTLES.SDR CA000511035Panel · failed(CAN) ON SHORT FINAL FLT SPOILER DEPLOYED UNCOMMANDED ABOUT 25 DEG UP ON THE RT WING AND APPROX 10 DEGREES UP ON THE LT WING. SPOILER PANEL, INBOARD PCU AND O/B PCU REPLACED.SDR CA000511036Apu · overserviced(CAN) SMOKE TOILET MESSAGE APPEARED ON EICAS AFTER TRANSFERING PACKS TO APU BLEED AIR. APU FOUND OVERSERVICED BY APPROX. 1/2 QT.SDR CA000505029Actuator · seized(CAN) DURING FINAL APPROACH A/C HAD FLAP FAILURE AT 40 DEGREES.SDR CA000530068Actuator · failed(CAN) FLAP FAIL MESSAGE ON EICAS WHEN FLAP SELECTED TO 45 DEG AT 155 KNOTS. VISUAL CHECK CARRIED OUT AND FLAPS RESET. FLAPS CYCLED. REPLACED LT BPSU AND NR 3 ACTUATOR. COMPLETE RIGGING AND FUNCTIONAL CHECK CARRIED OUT.SDR CA000530067Bpsu · failed(CAN) FLAPS FAILED AT 42 DEG ON APPROACH. BITE CHECK CARRIED OUT. RT BPSU REPLACED.SDR COMA0060397Engine · overservicedRIGHT ENGINE OIL TEMP HIGH. FOUND OIL OVER SERVICED.SDR CA000530066Control Unit · failed(CAN) FLAP FAILED, FAULT CLEARED WITH A JOB CARD TO DO A VERIFICATION CHECK OF SYSTEM WAS ISSUED. FECU REPLACED. RIG CHECK CARRIED OUT.SDR CA000530063Engine · malfunctioned(CAN) NOT ABLE TO DUPLICATE SNAG, NO FAULT FOUND.SDR CA000530065Seal · leaking(CAN) FUEL SMELL IN TAIL COMPARTMENT ON THEIR TRIP CHECK BEFORE DEPT. A/C REMOVED FROM SERVICE. FUEL LEAK AT ELBOW OF FITTING AT THE FCU TO SOLENOID VALVE. SEAL REPLACED.
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