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 = 'CF348E5A1' 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 = 'CF348E5A1' 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 CA190809017Bushing · worn(CAN) FLIGHT CREW ADVISED MTCE THE THE #1 ENGINE WAS PERSISTENTLY APPROACHING (BUT NOT EXCEEDING) ITT LIMITS DURING STARTS. MOC REQUESTED AN INSPECTION OF THE VGV SYSTEM. AN UNUSUAL AMOUNT OF PLAY WAS FOUND IN ONE OF THE ACTUATORS (MASTER) ON REMOVAL THE ATTASDR CA190604019Pcu · corroded(CAN) SPOILER FAULT EICAS MESSAGE AFTER TOUCH DOWN ,FLIGHT CONTROL NO DISPATCH MESSAGE FOLLOWED SHORTLY AFTER . AIRCRAFT OUT OF SERVICE, AOG. WAS TOWED TO HANGAR DURING T/S FOUND L/H WING O/B PCU CONNECTOR HEAVILY CORRODED AND ALSO CONNECTOR AIRFRAME SIDE MFS SDR CA190502003Rod · broken(CAN) DURING SERVICE CHECK, LEFT WING INB FLAP WAS FOUND LOWER THAN OTHER FLAP. INB AFT FLAP OUTB ROD WAS FOUND SHORTER THAN THE INB ROD. ROD WAS FOUND BROKEN IN HALF. REF: AIPC: 57-54-00-10 P/N: 171-03779-901. TRAX DEFECT 145287. THIS IS NOT THE FIRST TIME THSDR CA190304017Duct · failed(CAN) #1 ENGINE PRE-COOLER INLET DUCT ASSY PART NUMBER 171-03352-405 FOUND CRACKED AND BLOWN OUT DURING A SCHEDULED INSPECTION. COMPOSITE PANEL FOUND BRITTLE DUE TO AGE, PANEL 170-03352-405 HAS BEEN REPLACED AND AC HAS BEEN RETURNED TO SERVICE.SDR CA160215001Bracket · out of alignment(CAN) DURING CLIMB OUT THE "DOOR UNLOCKED" LIGHT ILLUMINATED AT 1500 AGL. RETURN TO BASE AND UNEVENTFUL LANDING COMPLETED. DOOR UNLOCK ANNUNCIATION EXTINGUISHED DURING DESCENT. MAINTENANCE WAS NOT ABLE TO DUPLICATE CONDITION. MOST SUSPECT PART REPLACED - EXTERSDR CA160205010Line · leaking(CAN) AFTER ENGINE SHUTDOWN CREW REPORTED THAT NR 2 ENGINE OIL QUANTITY READS 4.1. THE CREW CARRIED OUT A WALK AROUND FOUND A PUDDLE OF OIL UNDER NR 2 ENGINE. MAINTENANCE WAS ADVISED AND ASKED TO INVESTIGATE/SERVICE OIL AS REQUIRED. CONTRACT MAINTENANCE FOUND SDR CA151203005Wire Harness · damaged(CAN) ON CLIMB OUT AT APPROXIMATELY 15000 FEET THE ENGINE NR 1 FIRE EICAS MESSAGE CAME ON ALONG WITH THE ALARM. #1 ENGINE SET TO IDLE AND MAYDAY DECLARED. CHECKLIST PERFORMED AND ENGINE WAS SHUT DOWN. BOTH EXTINGUISHERS WERE DISCHARGED. MAINTENANCE CARRIED OUTSDR CA150731006Brake · failed(CAN) DISPATCH REPORTED A FLIGHT INCIDENT THAT ON LANDING THE RT OUTBOARD BRAKE SHATTERED. ON TAXI IN TO GATE THE RT INBOARD BRAKE OVERHEATED. MAINTENANCE FOUND THE NR 4 BRAKE SHATTERED WITH SIGNIFICANT DAMAGE TO THE PISTONS AND LARGE SECTIONS OF A ROTOR AND PSDR CA150703007Wire · shorted(CAN) PILOT REPORTED THAT FUEL 2 LOW LEVEL - EICAS WARNING MESSAGE CAME ON. MEL 28-44-00 APPLIED ALLOWED THE AIRCRAFT TO RETURN TO SERVICE PROVIDED THAT ASSOCIATED FUEL QUANTITY INDICATIONS ON EICAS AND MFD ARE AVAILABLE AND ARE MONITORED THROUGHOUT FLIGHT. SDR CA150616008Insulation · unsecure(CAN) AFTER B CHECK, DURING A FLIGHT, THERE WAS A PRESS AUTO FAULT MSG. THIS WAS RESET IAW THE FAULT ISOLATION MANUAL. DURING A FLIGHT THERE WAS ANOTHER PRESS AUTO FAIL MSG. WHILE TROUBLESHOOTING & INSPECTING, AN INSULATION BLANKET WAS FOUND STUCK IN THE OUSDR CA150312004Stop · cracked(CAN) WHILE DOING SCHEDULED INSPECTION TASKS ON "B" CHECK, A CRACK WAS FOUND IN THE RT AILERON UPPER TORQUE TUBE BEARING STOP. REPLACED WITH A NEW ONE.SDR CA150209008Wire Harness · failed(CAN) THE LANDING GEAR WOULD NOT RETRACT. CREW USED THE DOWNLOCK RELEASE BUTTON TO RETRACT THE GEAR AND THEN RETURNED FOR MAINTENANCE TO TROUBLESHOOT. THE FAULT CODE 32612301PSS DIRECTED MAINTENANCE TO THE RT MLG NR 2 WEIGHT ON WHEEL (WOW) SENSOR. THE SENSOR HSDR CA150207002Bearing · damaged(CAN) CREW REPORTED AILERONS STIFF. UPON FURTHER INSPECTION, MAINTENANCE FOUND UPPER BEARING REF IPC 27-11-07-06 ON LH FUSELAGE SECTOR TORQUE TUBE BEARING ASSY STIFF (METAL TO METAL CONTACT) REF IPC 27-11-07-01. MAINTENACE ALSO FOUND LH WING STUB AILERON FEEL SDR CA141007006Relay · burned(CAN) 1 COFFEMAKER IN THE FWD GALLEY HAD ELECTRICAL FLASHES AND ARCING EMANATING FOR THE RELAY AT THE BACK OF THE UNIT. A CLOUD OF BLACK SMOKE AND A BIG BLUE/YELLOW FLASH WAS SEEN BY THE CABIN CREW. THEY DISCHARGED A FIRE EXTINGUISHER ON BOTH COFFEMAKERS ANDSDR CA140916004Connector · broken(CAN) THIS AIRCRAFT HAS HAD NUMEROUS REPORTS OF WING ANTI-ICE LEAK FROM THE LTSLAT 2 SENSOR CAUSING MANY OPERATIONAL INTERRUPTIONS AND DELAYS. ALL THE RECOMMENDED TROUBLESHOOTING WAS CARRIED OUT IAW THE FAULT ISOLATION MANUAL (FIM) WITHOUT ANY SUCCESS. BECAUSESDR CA140710004Line · chafed(CAN) FLIGHT CREW REPORTED NR 1 HYDRAULIC SYSTEM FLUID QUANTITY DEPLETING IN FLIGHT. AN EMERGENCY WAS DECLARED AND AIRCRAFT HAD AN UNEVENTFULL LANDING. POST LANDING INSPECTION BY MAINTENANCE FOUND CUSHION CLAMP MIGRATED AND CHAFFED SMALL PIN HOLE IN PRESSURESDR CA140508002Sensor · failed(CAN) A "SLAT FAIL" EICAS MESSAGE ON THE GROUND. ON THE 3RD A LT WING OTBD SLAT SKEW SENSOR WAS REPLACED. ALSO, RIGGING CHECKS WERE CARRIED OUT AND FAULT CLEARED. THE FOLLOWING DAY FLYING THE SAME MESSAGE APPEARED AND MAINTENANCE WAS SENT TO FIX THE FAULT.SDR CA140421006Pump · damaged(CAN) FUEL 2 LO LEVEL WARNING EICAS MESSAGE WITTH LOTS OF FUEL IN TANK. EJECTOR ENGINE FEED PUMP REMOVED TO INSPECT FOR DEFECTS. CLAMP FLANGE ON FORWARD SIDE FOUND DAMAGED. IAW FIM TASK 28-21-00-810-8B-A, FUEL MAIN EJECTOR PUMP REPLACED IAW AMM 28-21-13-400SDR CA140423001Wire Harness · chafed(CAN) A "LANDING GEAR NO DISPATCH" MESSAGE WAS DISPLAYED. IT HAD OCCURRED EARLIER THAT DAY BUT WAS RESETTABLE IAW THE FIM 32-00-00-810-801-A. ANOTHER RESET WAS ATTEMPTED BUT THE CONDITION RETURNED SHORTLY AFTER PUSHBACK. TROUBLESHOOTING REVEALED A WIRE BROKSDR CA140421003Duct · cracked(CAN) AFTER T/O BLEED 2 OVERPRESS AMBER EICAS ALERT. CHECKLIST PROCEDURE CARRIED OUT WITH NO RELIEF. EMERGENCY DECLARED AND ACFT RETURNED TO DEPARTURE IAW CHECKLIST. MECHANIC ON RAMP DISCOVERED CRACKED T-DUCT. NR 2 ENGINE BLEED "T-DUCT" REPLACED IAW AMM 36SDR CA140421005Duct · cracked(CAN) RT ENGINE T-DUCT FOUND CRACKED, PN 170-14806-401, MECHANIC ON RAMP NOTED SOUND OF BLEED AIR LEAK DURING REGULAR SCHEDULED ENGINE OIL SERVICE CHECK. RT ENG T-DUCT, BLEED, REPLACED IAW AMM 36-11-04. OPS CHECK SERVICEABLE.SDR CA140331008Sensor · failed(CAN) DURING CRUISE A "SLAT FAIL" FAILURE WARNING OCCURRED. BECAUSE OF THE ABNORMAL LANDING CONFIGURATION, SLATS UP, AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT IAW THE FIM 27-83-00-810-814-A AND FOUND THE SDR CA140227002Attach Fitting · broken(CAN) RUDDER LOWER ATTACHMENT FITTING BROKEN, DISCOVERED DURING ROUTINE INSPECTION. CAUSE OF DAMAGE UNKNOWN AT THIS TIME.SDR CA140225009Sensor · failed(CAN) AFTER TAKEOFF THE LANDING GEAR LEVER WOULD NOT GO UP. RETURNED FOR LANDING. CONTRACT MAINTENANCE DISCOVERED A FAULTY NLG WOW SENSOR. THIS WAS REPLACED AND ADJUSTED IAW AMM 32-62-01AND THE GEAR SWUNG SEVERAL TIMES SUCCESSFULLY. ACFT RELEASED FOR SERVICESDR CA140128011Sensor · failed(CAN) AFTER T/O DEPARTING, THE LANDING GEAR COULD NOT BE SELECTED UP. CREW PERFORMED THE CHECKLIST AND RETURNED. MOC WAS CONTACTED AND A SPECIAL FERRY PERMIT WAS APPLIED FOR AND GRANTED FOR A GEAR DOWN, NON-STOP FERRY FLIGHT. MAINTENANCE FOUND A DEFECTIVE NLSDR CA140121002Landing Gear · lack of lube(CAN) AFTER T/O THE LT MLG WOULD NOT RETRACT. THE ACFT RETURNED. MAINTENANCE FOUND THE MID PIVOT POINT OF THE SIDE BRACE STIFF AND NEEDING LUBRICATION. AFTER LUBRICATION THE RETRACTION WAS TESTED SERVICEABLE. SINCE THIS IS A KNOWN HISTORICAL PROBLEM ON THESDR CA131231001Landing Gear · frozen(CAN) INSTANCES OF LANDING GEAR DISAGREE LIGHTS AFTER TAKEOFF ON 17TH, 25TH AND 26TH OF DECEMBER 2013. ON THE 17TH A LOT OF ICING ACCUMULATION WAS FOUND, CLEANED AND GEAR SWINGS CARRIED OUT SUCCESSFULLY. NO FURTHER OCCURRENCES UNTIL THE 25TH DECEMBER ON THE SDR CA131001005Wire · chafed(CAN) SMOKE ODOR IN CABIN IN INITIAL CRUISE. ACFT DIVERTED FOR INVESTIGATION. POWER CONTROL BOARD FOUND BURNED. AFFECTED SEAT AND OTHERS, AS A PRECAUTION, PUT ON MEL. ON A SUBSEQUENT FLIGHT THE CHIMES WERE GOING OFF AGAIN SO DUE TO HISTORY OF CHIMES AND BURSDR CA130805018Module · failed(CAN) MAYDAY DECLARED FOR A MAU 1 FAULT. MAYDAY DECLARED. MAU 1 POWER, MOD 1 REPLACED IAW AMM 31-41-02 PB401. MAU 1 NIC-PROCESSOR 1 REPLACED IAW AMM 31-41-04, PB401. MAU 1 MAIN BRAKE CONTROL MOD 1 REPLACED IAW AMM 32-41-07, PB401. CHECKED SERVICEABLE. REMSDR CA131125014Torque Tube · chafed(CAN) RUDDER PEDAL TORQUE TUBE GOUGED FROM PANEL COVER. TORQUE TUBE REPLACED, COVER PANELS REWORKED OR VERIFIED CLEARANCE.SDR CA130625005Panel · out of position(CAN) DURING PRIMARY INSPECTION, IT WAS NOTED THAT PANEL 221 EZ WAS CHAFING AGAINST THE PILOTS RT RUDDER PEDAL TORQUE TUBE.SDR CA130524007Module · overheated(CAN) ON ARRIVAL , APU WAS IN OPERATION WHEN CREW SELECTED APU GENERATOR AND BLEED THERE WAS A BURNING ELECTRICAL SMELL, GPU WAS HOOKED UP BUT FAILED SHORTLY THEREAFTER , CREW THEN NOTICED A BLUISH HAZE THROUGHOUT THE CABIN AND THE BURNING SMELL WAS STRONGER.SDR CA130411001Shroud · corroded(CAN) AFTER FINDING CORROSION ON 2 OTHER AIRCRAFT. THE FUEL SHROUDS AND FUEL LINES WERE REMOVED FORM THIS ACFT, CURRENTLY BEING PARTED OUT, TO SERVICE THE FIRST ACFT. THE INSIDES OF THESE COMPONENTS WERE COVERED WITH A BLACK SUBSTANCE, ONCE CLEANED OFF THE CSDR CA130409002Flap System · failed(CAN) ON APPROACH THE CREW REPORTED THE FLAPS HAD FAILED. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER COMPLICATIONS. BY CMC FAULT CODE - 27512014ACE. FIM TASK- 27-51-00-810-802-A. FAULT ISOLATION PROCEDURE CARRIED OUT. TRANSITORY CONDISDR CA130318018Actuator · leaking(CAN) OVERWEIGHT LANDING DUE TO AIRBORNE RETURN ACCOUNT OF STRONG IRRITATING DIRTY SOCK ODOR EMANATING THROUGHOUT CABIN/FLIGHT DECK. SEQUENCED PACKS, UNABLE TO ELIMINATE ODOR. ACFT LANDED APPROXIMATELY 600 KGS OVER MAXIMUM LANDING WEIGHT. BOROSCOPE INSP C/OSDR CA130204001Duct · punctured(CAN) UNABLE TO PRESSURIZE AIRCRAFT. RETURNING TO DEPARTURE. NO EMERGENCY DECLARED BY CREW. CABIN ALT HI EICAS WARNING MESSAGE ON WHILE CLIMBING THROUGH FL250, PACK 2 APPEARED NORMAL, OFV SHOWING FULLY CLOSED. PACK NR 2 AIR SUPPLY DUCT FOUND WITH HOLE IN SDR CA130129005Gasket · leaking(CAN) WHEN FLIGHT WAS ENROUTE, ACFT EXPERIENCED A NR 1 BLEED FAILURE FOLLOWED BY NR 1 BLEED LEAK MESSAGE. WITH THUNDERSHOWERS FORECAST, THE CREW ELECTED TO RETURN. NR 1 ENGINE PRECOOLER AFT INTERFACE GASKET REPLACED IAW AMM 36-11-08 PB401.SDR CA130114009Filter · failed(CAN) THE FLIGHT CREW ENCOUNTERED FUMES IN THE COCKPIT AFTER TAKEOFF. THERE WAS ALSO A POSSIBLE HAZE ASSOCIATED. THERE WERE SIMILAR FUMES REPORTED IN THE FWD & AFT CABIN. THE FLIGHT CREW DIVERTED BACK AND DID DECLARE AN EMERGENCY AND LANDED RUNWAY WITHOUT FSDR CA121217004Control Valve · failed(CAN) ENCOUNTERED HOT BRAKES AT THE THRESHOLD OF R23 WARNING AMBER, REQUESTED TO BE TOWED TO GATE. REPLACED INBD MAIN BRAKE CONTROL VALVE IAW AMM 32-41-09 PB 401. OPS TEST SERVICABLE.SDR CA121211015Fitting · collapsed(CAN) BOTH LT AND RT PYLON TORQUE MOTOR CONTROLLER FITTING AIR FILTERS HAVE COLLAPSED. ACFT WAS DUE FOR N1 VISIT, AND TASK CARD 37-36-11-06-001AC-01 CALLED FOR THE CLEANING OF BOTH FILTERS. UPON DISCOVERING THEIR CONDITIONS, THEY WERE BOTH REPLACED. THESE FSDR CA121128001Engine · power loss(CAN) ENGINE SHUTDOWN AFTER T/O, RETURNED TO DEPARTURE. NR 2 ENGINE SUFFERED AN IFSD SHORTLY AFTER TAKEOFF. AT THE TIME, THE THROTTLES WERE AT HIGH POWER SETTING WHILE CLIMBING THROUGH 15,000 FT, A LOUD AUDIBLE BANG WAS REPORTED BY THE CREW, FOLLOWED SHORTLSDR CA121009006Flap System · failed(CAN) ON, SHORT FINAL, THE FLIGHT CREW RECEIVED A FLAP DISAGREE MESSAGE. A GO-AROUND WAS INITIATED. DURING THE SECOND APPROACH, NO MESSAGES WERE RECEIVED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. AS A PRECAUTION, CFR WAS CALLED AND MET THE FLIGHT ON ASDR CA121009005Transponder · failed(CAN) AFTER TAKEOFF THE CREW WAS ADVISED BY ATC THEY WERE NOT RECEIVING TRANSPONDER INFO FROM THE FLIGHT. THE FLIGHT RETURNED AND LANDED NORMALLY. THE CREW DID NOT DECLARE ANY EMERGENCY BUT THE EMERGENCY RESPONSE VEHICLES ATTENDED THE LANDING. MRC1 NIM REPSDR CA121009002Duct · cracked(CAN) FOUND DURING SCHEDULED MAINTENANCE, T-DUCT BELOW PRE-COOLER ON RT PYLON SIDE IS CRACKED. IPC ATTACHED, PN 170-14806-401.SDR CA120921003Shutoff Valve · failed(CAN) ON DEPARTURE PASSING 14,000 FT THE SERVICE DIRECTOR REPORTED AN ODOR RESEMBLING DIRTY SOCKS THROUGHOUT THE CABIN. THE FLIGHT CREW SWITCHED OFF THE NR 1 PACK AND THE ODOR DISSIPATED. TROUBLESHOOTING COMPLETED IAW FMR M2028728. NO FAULTS FOUND. IAW FMRSDR CA120914006Indicator · malfunctioned(CAN) DEPARTING ON THE TAKE OF ROLL, THE FLIGHT EXPERIENCED AN EGT EXCEEDENCE ON THE NR 1 ENGINE AT 110 KNOTS FOLLOWED BY A REJECTED TAKEOFF AT 120 KNOTS. THE ACFT PULLED OF THE RUNWAY AND STOPPED TO ENSURE BRAKE TEMPERATURES DIDN`T EXCEED LIMITS. ONCE THE BSDR CA120911004Flap System · failed(CAN) DURING THE APPROACH, IN SHORT FINAL WHEN SELECTING FULL FLAPS FROM FLAPS 3 CONFIGURATION THE CREW RECEIVED A FLAPS FAIL INDICATION. THEY EXECUTED A GO- AROUND, AND TRIED A RE-SET. THE SECOND APPROACH WAS THE SAME INDICATION BUT THEY WERE ABLE TO CONITSDR CA120904009Sensor · failed(CAN) ON DEPARTURE, ACFT YAWED TO THE LT, NUMBER 1 SIDE, CREW ELECTED TO LEAVE GEAR DOWN AS THEY THOUGHT POSSIBLE BLOWN TIRE. ATC HAD THEM CLIMB TO 7000FT, AT THAT TIME THE NR 1 ENGINE HAD HIGH OIL TEMP 180C. THE CREW THEN ELECTED TO RETURN. WITH THE TEMP TSDR CA120828007Circuit Card · failed(CAN) AIRCRAFT WAS OSCILLATING WHILE THE AUTOPILOT WAS ENGAGED AT APPROXIMATELY 10000 FT, AUTOPILOT WAS DISENGAGED, THE OSCILLATING WENT AWAY FLT RETURNED. THE ACFT CONDUCTED AN OVERWEIGHT LANDING. PILOT TALKED WITH MTCE AFTER THE LANDING. CAPTAIN WILL FILSDR CA120828008Oil System · low pressure(CAN) ENGINE 2 LOW OIL PRESSURE, ENGINE 2 SHUTDOWN, DIVERTED, EMERGENCY DECLARED.
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