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 VNAA2014061500013Carbon Seal · leakingCREW REPORTED LT ENGINE OIL PRESSURE RED WARNING MESSAGE AT FL320. DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND IDG CARBON SEAL LEAKING. MAINTENANCE R & R LT ENGINE IDG CARBON SEAL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FORSDR VNAA2014061300011Pump · failedCREW REPORTED, NR 1 HYD SYSTEM FAILED IN FLIGHT WITH NO PRESSURE AND NO FLUID LEVELS. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED REPAIR TO PRESSURE LINE FROM NR 1 ENGINE DRIVEN PUMP AFTER FINDING LINE CHAFED THROUGH AT CLSDR SWIA201438062Connector · brokenLT SIDE WINDSCREEN EXIT LIGHT HAS BROKEN CONNECTOR. C-CHECK, INSTALLED CONNECTOR AND CONTACT TO EXIT LIGHT WIRE IAW ESPM AND AMM.SDR CA140606004Apu · fire(CAN) DUE TO DIFFICULTIES TO START APU SOMETIMES, OPERATOR DECIDED TO DO AN APU RUN TO CHECK IF HE CAN REPLICATE FAULT. HE COULD NOT REPLICATE FAULT. APU RAN FOR 45 MINUTES WHILE DURING COMPRESSOR WASH. AFTER COMPRESSOR WASH, ACFT WAS SHUTDOWN TO TRY TO REPRSDR SWIA201437927Bushing · galledRIGHT ENGINE FWD MOUNT LINK AND CLAMP-UP BUSHING GALLED. REMOVED RT ENGINE FWD MOUNT LINK AND CLAMP-UP BUSHING AND REPLACED WITH A SERVICEABLE LINK AND CLAMP-UP BUSHING IAW AMM.SDR CA140527001Not Reported · not reported(CAN) THE ACFT WAS STRUCK BY LIGHTNING WHILE PERFORMING FLIGHT INSPECTIONS ON THE VOR. THE WEATHER WAS VFR, BUT THERE WAS CUMULUS CLOUDS AND RAIN SHOWERS IN THE AREA. THE ACFT LANDED WITHOUT FURTHER INCIDENT. THE ACFT WAS INSPECTED IAW THE OEM MANUALS, WHICSDR CA140521001Battery · deformed(CAN) DURING UNRELATED MAINTENANCE, AN AME FOUND THE APU BATTERY CASE DISTORTED, SWOLLEN. BATTERY WAS REPLACED WITH SERVICEABLE UNIT. ACFT CYCLES:18725, ACFT HOURS:24248.SDR SWIA201437682Mount · galledRIGHT ENGINE FWD MOUNT LINK ASSY AND CLAMP UP BUSHING HAVE GALLING. INSTALLED SERVICABLE MOUNT LINK ASSY AND CLAMP UP BUSHING ONTO MOUNT YOKE IAW AMM.SDR SWIA201437684Bushing · galledRIGHT ENGINE FOUND GALLING ON OTBD BUSHING OF AFT ENGINE MOUNT. INSTALLED A SERVICEABLE RT ENGINE AFT SPHERICAL BUSHING IAW AMM.SDR CA140521005Gauge · failed(CAN) AFTER REPLACEMENT OF A NR 3 BRAKE ACCUMULATOR FOR A PARK BRAKE PRESSURE DECAY DEFECT, THE ASSOCIATED PRESSURE GAUGE FAILED, CATASTROPHICALLY. THE ACCUMULATOR AND GAUGE WERE REPLACED WITH SERVICEABLE UNITS AND THE AC RETURNED TO SERVICE. AC HOURS:23865SDR VNAA2014051700011Engine · surgesCREW REPORTED LT ENGINE BEGAN TO SURGE IN POWER IMMEDIATELY AFTER TAKEOFF, DROPPING AND SPIKING UP TO 5 PERCENT N1. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED GROUND ENGINE RUN AND FOUND LT ENGINE N1 SURGING ABOVE 80 PERCENT N1SDR SWIA201437639Housing · galledRT ENGINE AFT MOUNT HOUSING SHOWING SIGNS OF GALLING. R & R RT ENGINE AFT MOUNT HOUSING IAW AMM.SDR SWIA201437640Bushing · galledRIGHT ENGINE AFT ENGINE MOUNT SPHERICAL BUSHING SHOWING SIGNS OF GALLING. R & R RT ENGINE MOUNT SPHERICAL BUSHING IAW AMM.SDR VNAA2014051600010Throttle Cable · brokenCREW REPORTED F/O REDUCED BOTH THRUST LEVERS ON DESCENT AND IMMEDIATELY IDENTIFIED NO N1 CHANGE. ATTEMPTED TO MOVE THRUST LEVER AND FOUND NO CHANGE TO N1 FOR LT ENGINE. CREW FOLLOWED QRH, SHUTDOWN LT ENGINE, DECLARED AN EMERGENCY AND LANDED SAFELY. MAINTENANSDR SWIA201437456Link · damagedLEFT ENGINE, FWD YOKE LINK HAS CORRODED BUSHINGS. RT & LT ENGINE FWD YOKE LINK IAW AMM.SDR SWIA201437457Bushing · damagedLEFT AFT MOUNT BUSHING IS CORRODED AND NICKED. R & R LT AFT MOUNT BUSHING IAW AMM.SDR VNAA2014050200004Sensor · failedCREW REPORTED LT N1 PLUS OR MINUS 5 PERCENT UNCOMMANDED POWER ADJUSTMENTS DURING FLIGHT, N1, ITT, N2 AND FUEL FLOW ALL UNCOMMANDED MOVEMENT. UNABLE TO SET AND MAINTAIN POWER SETTING AT HIGHER SETTING. NO ISSUES AT IDLE. CREW RETURNED TO FIELD AND LANDED WITSDR CA140502006Servo · failed(CAN) DURING CLIMB, WHILE THE ACFT WAS EXECUTING A LT BANK TURN WITH THE AUTOPILOT ENGAGED, FLIGHT CREW RECEIVED A BOXED "A" YELLOW INDICATION ON THE PRIMARY FLIGHT DISPLAY (PFD) INDICATING A SIGNIFICANT MISTRIM CONDITION ASSOCIATED WITH AN AP TRIM IS LWD CAUTSDR CA140421001Oil System · leaking(CAN) JUST AFTER DEPARTURE, THE CREW NOTICED SMOKE IN THE CABIN AND RETURNED TO THE DEPARTURE AIRPORT FOR AN UNEVENTFUL LANDING. IT WAS DETERMINED THAT THE SMOKE WAS CAUSED BY RESIDUAL OIL, RESIDUE IN THE ECS SYSTEM DUE TO A PRIOR APU FAILURE, LARGE OIL LEAK SDR CA140414009Cable · unserviceable(CAN) CREW REPORT NR 2 POWER LEVER IS PHYSICALLY BLOCKED AND THEY ARE UNABLE TO ACHIEVE MAX POWER. ACFT DESCENDED TO 30000 FEET AND STAGGER REPORTED 2.5 KNOBS , FOUND AUTO THROTTLE RETARDER CABLE FOUND SEVERELY STIFF. ATR CABLE INSTALLED IN POSITION IAW AMSDR VNAA2014040800007Unknown · vibrationCREW REPORTED RT ENGINE FAN VIBRATION DURING CLIMB. CREW FOLLOWED QRH, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED RT FAN BLADES AND PERFORMED CHECKS IAW AMM. NO DEFECTS NOTED. ACFT RELEASED FOR SERVICE.SDR CA140408003Case · delaminated(CAN) QTY-35 FAN CONTAINMENT CASES FROM CF34-3B1 ENGINES HAVE BEEN FOUND WITH DELAMINATION ON THE ABRADABLE RUB STRIP AREA. THE CYCLES SINCE SHOP REPAIR ON THESE INCIDENTS RANGE FROM 183 CYCLES TO 11171 CYCLES. THESE WERE REPAIRED BETWEEN 2009 AND 2012. FOR SDR CA140409002Restrictor · damaged(CAN) AFTER ARRIVAL THE FLIGHT CREW COMPLAINED THAT THE NOSE WHEEL STEERING WAS SLOW TO RESPOND, THERE WERE NO CAUTION MESSAGES. THE ACFT HAS A RECENT HISTORY OF THIS DEFECT WITH EXTENSIVE TROUBLESHOOTING HAVING BEEN CARRIED OUT INCLUDING GEAR REPLACEMENT. DSDR REXA2014040300342Priority Valve · failedWHEN SELECTING GEAR DOWN GOT GEAR DISAGREE & NOSE DOOR OPEN WARNING MSG. MSG CAME ON 3 - 5 SEC AFTER GEAR SELECTION, WE RAN THE QRH & AFTER CYCLING THE GEAR WITH ALL PUMPS ON, THE GEAR CAME DOWN & LOCKED NORMALLY. TROUBLE SHOT LG SYS IAW PA 05-018 REV K SCENSDR CA140320005Solenoid · faulty(CAN) DURING INITIAL CLIMB FLIGHT CREW RECEIVED A LT REV UNLOCK CAUTION MSG. DECISION WAS TAKEN TO RETURN & LAND. THE ACFT LANDED WITHOUT FURTHER INCIDENT. IT WAS THE FOURTH SIMILAR PROBLEM REPORTED WITHIN A FEW DAYS. THE THRUST REVERSER WAS DEACTIVATED & SDR SWIA201436673Bushing · corrodedDURING C-CHECK, LEFT ENGINE MOUNT LINK BUSHINGS FOUND PITTED AND WORN. , REPLACED LT ENGINE MOUNT LINK BUSHINGS IAW AMM.SDR CA140312007Fairing · damaged(CAN) DURING ROUTINE MAINTENANCE, THE LT ENGINE UPPER STANG FAIRING WAS FOUND PARTIALLY MISSING. IT IS NOT KNOWN WHEN OR WHERE THE PART DEPARTED THE ACFT. THERE WAS EVIDENCE OF THE SUPPORT BRACKETS CRACKING. THIS PART IS KNOWN TO HAVE ISSUES AND IS ROUTINELY SDR CA140310008Windscreen · arced(CAN) AFTER TAKEOFF, IN THE CLIMB PHASE OF FLIGHT, THE CAPTAIN`S WINDSCREEN STARTED ARCING ON THE LOWER, RT CORNER AND CONTINUED ALONG THE LOWER PORTION OF THE WINDSCREEN. HEAT WAS TURNED OFF, THE ARCING STOPPED AND THE FLIGHT DIVERTED. HOURS: 23646:16. CYCLESDR VNAA2014030700007Union · leakingCREW REPORTED HYDRAULIC 1 LOW PRESSURE MESSAGE AT 600 FEET AGL. QUANTITY WAS ZERO. CREW RAN QRH, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND UNION LEAKING ON ENGINE DRIVEN PUMP. MAINTENANCE R & R NR 1 ENGINE EDP AND PERFORSDR CA140314011Scavenge Pump · defective(CAN) WE HAVE PURCHASED A NEW C SUMP SCAVENGE & DRAIN TUBE, PN 5054T31G03 FROM AVIALL IN AUGUST OF 2013. THE PART WAS PURCHASED UNDER KACM PO P52 & SHIPPED UNDER AVIALL SHIPMENT NR 8161821. IT WAS USED DURING A SCAVENGE TUBE REPLACEMENT IAW CF34 ENG SHOP MANSDR VNAA2014030500005Drive Unit · failedCREW REPORTED RT THRUST REVERSER MESSAGE IN FLIGHT. CREW RAN QRH, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT THRUST REVERSER POWER DRIVE UNIT (PDU), AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.SDR A6WA201441219Engine · contaminatedCABIN & COCKPIT FILLED WITH SMOKE & FUMES ONCE BLEEDS WERE TRANSFERRED TO ENGINES.
SWAPPED BLEEDS BACK TO APU & SMOKE & FUMES STOPPED. CONTACTED MX & CONFIRMED THIS
WAS 1ST FLIGHT AFTER COMPRESSOR CLEANING. SUSPECT RESIDUAL CHEMICALS FROM COMPRESSOR WASH. RSDR CA140304006Floor Panel · cracked(CAN) THIS AREA IS COVERED BY RECURRENT INSPECTIONS BUT WE DECIDED TO SUBMIT AN SDR SINCE THEY ARE SOMEWHAT DIFFICULT TO DETECT. A CRACK WAS FOUND IN THE PRESSURE FLOOR DURING INSPECTION. THE PRESSURE FLOOR IS A KNOWN AREA FOR CRACKS, HOWEVER THIS CRACK WOULSDR CA140306008Sensor · failed(CAN) SMOKE IN THE CABIN ON THE GROUND AT ENGINE START PLACE. DURING APU COMPARTMENT INSPECTION MAINTENANCE PERSONNEL FOUND THE RT ACM TEMP SENSOR DESTROYED, MISSING OF 2 BOLTS AND LOOSING ON ACM FLANGE. THE UNCONTROLLED TEMP RISING HAS BEEN NOTICED DURING OSDR SWIA201436475Carbon Seal · failedSLOW LOSS OF OIL PRESS IN FLIGHT. COMPLETED QRH PROCEDURE. IN FLIGHT ENGINE SHUTDOWN. FLT 5561 REPLACED HYD ENG DRIVEN PUMP, AIR TURBINE STARTER & IDG CARBON SEALS ON RT ENG. PERFORMED OIL CONSUMPTION CHECK IAW AMM.SDR VNAA2014021200011Pump · leakingCREW REPORTED HYD SYSTEM NR 1 PRESSURE LOW AND QUANTITY READING ZERO DURING FLIGHT. DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND LEAK ON HYD EDP NR 1 AND HYD NR 1 PRESSURE MANIFOLD LINE. R & R NR 1 EDP, R & R NR 1 HYDRAULIC PRESSURE MSDR ASOA2014020609910Engine · shutdownRIGHT ENGINE SHUTDOWN IN FLIGHT DURING CRUISE AT FL 300. ATTEMPED TWO STARTS, NO HELP. ACFT DIVERTED. EMERGENCY DECLARED. RIGHT ENGINE ASSY REPLACED, ALL OPS & FUNCTIONAL TEST GOOD, NO DEFECTS NOTED AT THIS TIME.SDR CA140203020Pdu · failed(CAN) RIGHT THRUST REVERSER UNLOCK MESSAGE DURING FLIGHT. EMERGENCY DECLARED. R & R RT PDU IAW AMM 78-32-03.SDR CA140203024Oxygen Bottle · failed(CAN) PRIOR TO DEPARTURE, THE CREW REPORTED OBSERVING THE CREW OXYGEN LEVEL WAS READING 1660 PSI. AFTER DEPARTURE, DURING THE CLIMB AT 14,000 FT, THE EICAS MESSAGE OXY LOW PRESSURE" ILLUMINATED. AT THIS TIME THE CREW NOTICED THE CREW OXYGEN SUPPLY PRESSURE DRSDR CA140207004Rod · broken(CAN) AFTER DEPARTURE, CREW WAS UNABLE TO PRESSURIZE THE ACFT. MAIN CABIN DOOR (MCD) FLAPPER FOUND OPEN. INVESTIGATION REVEALED BROKEN ROD INSIDE DOOR. ROD REPLACED ,THE PASSENGER DOOR SPRING ROD ASSY REPLACED IAW 52-11-15 OF THE AMM. OPS TEST OF THE PAX DOSDR CA140131007Window · cracked(CAN) RT WINDSHIELD CRACKED DURING CLIMBOUT. ACFT AIR TURN BACK TO DEPARTURE AIRPORT.SDR A6WA201441085Plate · crackedLEFT EXHAUST FAIRING INBD NUTPLATE MOUNT PLATE CRACKED. R & R PN 228-50181-833 IAW CMM 20-42-06.SDR REXA2014012800148Warning System · activatedOIL PRESS GAUGE SHOWING ZERO INBOUND ABE. QRH FOLLOWED, ENG. WAS SHUT DOWN. EMERGENCY WAS DECLARED. FLT LANDED WITHOUT INCIDENT & TAXIED TO GATE.SDR CA140127008Line · leaking(CAN) DURING FLIGHT, THE NR 1 HYDRAULIC SYSTEM FLUID LEVEL DEPLETED TO ZERO. AIRPORT CFR SERVICES WERE PLACED ON STANDBY FOR THE LANDING WHICH WAS UNEVENTFUL. SUBSEQUENT MAINTENANCE INVESTIGATION FOUND A CHAFED HYDRAULIC LINE AT THE NR 1 SYS PRESSURE MANIFOLSDR CA140128002Flap System · failed(CAN) THE FLIGHT CREW EXPERIENCED A "FLAP FAIL" CAUTION INDICATION WHEN THE FLAPS WERE SELECTED FOR APPROACH INTO. FLAPS REMAINED AT ZERO DEGREES. AN EMERGENCY WAS DECLARED AND A FLAP ZERO APPROACH AND LANDING WAS CARRIED OUT WITHOUT FURTHER INCIDENT. THE ASDR REXA2014012600135Warning System · false activationAFTER TAKEOFF FROM CMH AT ABOUT 26000 FT, LT ENG OIL PRESS WARNING MESSAGE ILUMINATED. OIL PRESS WAS FLUCTUATING BETWEEN 23 - 32 PSI, APPROXIMATELY 4 - 5 MIN LATER PRESS FELL BELOW 25 & STAYED IN THE RED. COMPLETED QRH & SHUT DOWN LT ENG. DIVERTING TO DTW DSDR CA140124013Mount · cracked(CAN) WHILE PERFORMING THE VISUAL INSPECTION OF THE RT PYLON IAW MM, TASK 000-54-420-500. A CRACK WAS DETECTED ON THE FORWARD ENGINE MOUNT SPAR. THE CRACK WAS FOUND ON THE AFT FACE OF THE SPAR AT FUSELAGE BS FS 625.30 APPROXIMATELY 2" INBD OF THE FUSELAGE SKSDR A6WA201441066Control Rod · misriggedAFTER TOUCH DOWN & STOWING T/R RECEIVED LT ENG OIL PRESS MASTER WARNING. OIL PRESS READ 2PSI & ENG SHUT ITS SELF-DOWN ON ITS OWN. COMPLIED WITH QRH, DECLARED EMERGENCY & REQUESTED SPECIAL SERVICE VEHICLES INSPECT AC & ESCORT TO GATE. FOUND THROTTLE CONTROL SDR REXA2014011200114Engine · contaminatedON CLIMB OUT STRONG BURNING ACRID SMELL IN COCKPIT & CABIN. FLIGHT ATTENDANT REPORTED PAX COMPLAINING OF A BURNING SMELL & PAX IN BACK OF ACFT WERE COMPLAINING OF ACRID CHOKING SMELL. VERIFIED WITH CREW, NO SMOKE VISIBLE. VERIFIED FIRST FLIGHT SINCE ENG COMSDR CA140113005Tire · burst(CAN) DURING TAXI TO ASSIGNED GATE AFTER AN UNEVENTFUL LANDING, FLIGHT CREW FELT TAXI WAS VERY BUMPY. TAXI WAS ABORTED ON TAXI WAY A M. CREW REPORTED BOTH RT TIRES NR 3 & NR 4 FLAT. PAXS OFFLOADED & BUSSED TO TERMINAL. NO EMER RESPONSE WAS REQUIRED. REMOV
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