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 jasc_code = '2810' 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 jasc_code = '2810' 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 DJFA2005103Relief Valve · leakingSHORTLY AFTER T/O, TOWER REPORTED FUEL SPRAYING FROM RT WING. CREW VISUALLY VERIFIED, RETURNED AND LANDED WITHOUT INCIDENT. INSP FOUND FUEL LEAKING FROM RT WING VENT. WING FUEL PRESSURE RELIEF VALVE FOUND TO BE OPEN. EXTENDED REFUELING TEST WAS PERFORMEDSDR UPS05844701Fuel Tank · damagedRT AUX TANK UPPER SURFACE FASTENER HOLE ELONGATED AT XW 208. FABRICATED REPAIR DOUBLER, INSTALLED CONICAL WASHERS AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-1 FIG 37, 51-1-26, 51-1-20D, AND 51-1-21.SDR CED2006F00006Fuel Tank · leakingON TAKEOFF ROLL AND INITIAL CLIMBOUT, FUEL WAS OBSERVED LEAKING FROM THE LT WING TIP. INFORMED THE CREW OF THE LEAK AND INSTRUCTED THEM TO COME AROUND AND LAND. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LT FUEL VENT AND FOUND NO DISDR ANCF200400050Tank · leakingDURING FLIGHT A FUEL LEAK WAS DETECTED ON LEFT MAIN FUEL TANK. ALL FUEL FLOW NORMAL AND ENGINE CONSUMPTION WAS NORMAL. PER AMM 72-00-04 P 197 ACCOM T/S FOUND FUEL PUMP DUCT CORK. ADJ IAW 73-34-01PG 201. RUN UP TEST NORMALLY IAW 72-44-0 PAG 532 , NO LEAKS FSDR ABXA050107Fuel Cap · defectiveAFTER TAKEOFF, TOWER ADVISED FUEL VENTING FROM LEFT WING. AIR TURNBACK, MADE RETURN TO ILN. LOST 1000 LBS OF FUEL IN FLIGHT. EMERGENCY DECLARED BY TOWER. FOUND LEFT OVER THE WING FILL CAP POPPED. CAP FOUND TO BE NOT LOCKING. REMOVED AND REPLACED LEFT OVESDR RAIA00505002Valve · defectiveFLT-5697 - STL - TOWER REPORTED SMOKE OR VAPOR COMING FROM RIGHT WING TIP. MAINTENANCE REMOVED AND REPLACED RT TANK FLAP VALVE.SDR DXTA200500704O-Ring · cutWING TANK OVERFULL R AMBER CAS MESSAGE CAME ON IN FLIGHT. DID NOT STOP OVERVENTING FUEL UNTIL DESCENDING THRU +/- 17000 FEET AND RIGHT FUEL GAUGE 3010 LBS, LEFT GAUGE 3290 LBS. - (M2B) FOUND FUEL COMING FROM RT AILERON BELCRANK DRY BAY. FOUND ONE CROSS OVER SDR GTIA050145Valve · openCAE - CENTER TANK PUMP NR 1 FAULTED DURING CLIMB-OUT. FOUND CENTER TANK REFUEL VALVE LEFT MANUALLY OPEN AT FUELING PANEL, PUT VALVE SWITCH TO NORMAL AND IT CLOSED, OPS CHECK NORMAL. (M)SDR ASAA0510088Fuel Tank · corrodedYXX - FOUND FUEL CENTER TANK CORRODED AT UPPER STRUCTURE AT BS 578 LBL 67. CORROSION REMOVED IAW EA 5710-01119. (M)SDR ASAA0510072Fuel Tank · corrodedYXX - FUEL CENTER TANK CORRODED AT UPPER SURFACE BS 578 RBL 67. REPAIRED IAW EA 5710-01118. (M)SDR CHQA200500083Flapper Valve · leakingAT CRUISE ALTITUDE FLT ATTENDANT LOOKED OUT THE WINDOW AT ROW 13 TO THE RT AND NOTICED THAT SOMETHING WAS NOT RIGHT. THE OTHER FLT ATTENDANT LOOKED AND SAW SOMETHING WAS GUSHING OUT OF THE RT WING IN LARGE QUANTITIES. THE PILOT REQUESTED FLT ATTENDANT TO COMSDR 2005FA0000575Placard · failedDEBRIS (PLASTIC RIB AND MANHOLE DOOR IDENTIFICATION DECALS) FOUND ON THE INLET STRAINER OF THE LT AND RT WING FUEL TANK, NR 2 MAIN FUEL PUMP AFT SCREENS DURING C-CHECK. OIT ISSUED BY AIRBUS AND IS APPLICABLE TO MSN1136. (K)SDR 2005FA0000496Fuel Tank · mismanufacturedDURING INSTALLATION OF NEW TANK, IT WAS DISCOVERED THAT THE BUNGS FOR INSTALLING THE FUEL STRAINER ASSEMBLIES HAVE BEEN BRAZED TO THE TANK INVERSELY. THE BUNG THAT SHOULD HAVE BEEN BRAZED AT THE AFT LOCATION WAS BRAZED IN THE FORWARD MOUNT WAS BRAZED IN THE ASDR COMA0570031Ejector · crackedFLIGHT 5285 FUEL TRANSFERRING FROM RIGHT TANK TO CENTER TANK. REPLACED THE PRIMARY EJECTOR.SDR VNAA0503008Cap · unsafetiedEN ROUTE (CLT TO GSO) A FLIGHT ATTENDANT NOTICED A NOISE COMING FROM THE RIGHT SIDE OF THE AIRCRAFT AT THE WING AREA. THE CREW WAS NOTIFIED. THE CREW OF FLIGHT 2249 HAD NO INDICATION OF MALFUNCTIONS AND CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. SDR CA050315012Vent · failed(CAN) DURING REFUELING, A LOUD BANG WAS HEARD FROM CABIN OF AIRCRAFT. FUEL WAS THEN SEEN LEAKING RAPIDLY FROM AIRCRAFT. PILOTS NOTED FUEL INSIDE CABIN SECTION BUT NOT IN COCKPIT. ENGINES WERE SHUT DOWN, ELECTRICAL SYSTEMS TURNED OFF AND PILOTS EXITED AIRCRAFTSDR QXEA200500296Valve · leakingPDX - MAINTENANCE FOUND THE SINGLE POINT REFUELING VALVE ADAPTER ASSEMBLY LEAKING AND REPLACED SAME. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CA050216004Fuel Tank · leaking(CAN) RECEIVED A COUPLE OF FUEL RUBBER TANKS REPAIRED FROM MFG THAT WE HAVE PROBLEM WITH. EACH TIME THAT WE DO RECEIVE NOW, WE TEST THEM BEFORE THE INSTALLATION ON THE A/C TO MAKE SURE THEY DON'T LEAK. SOMETIMES THEY LEAK FROM THE REPAIR PATCH OR THE JOINT. SDR QXEA200500430Line · chafedYYC - TWO FUEL LINES IN THE LEFT FUEL TANK HAVE BEEN CHAFING, LINES ARE LOCATED IN THE FORWARD TANK SECTION UNDER PANEL 523AT. REPAIRED IAW DHC-8 400 SRM SUB TASK 28-11-06-400-801 AND 28-11-06-420-001.SDR QXEA200500150O-Ring · leakingPDX - FLIGHT 2268 - THERE WAS A FUEL LEAK NOTED BY THE SINGLE POINT REFUELING DOOR. MAINTENANCE INSPECTED THE AREA AND REPLACED THE MASTER REFUEL/DEFUEL VALVE O-RINGS. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CA050119010Vent Line · leaking(CAN) DURING INSPECTION, FUEL WAS NOTICED LEAKING FROM THE LT WING. THERE WAS A FUEL STAIN AROUND THE VENT TUBE. WHEN THE TUBE WAS MOVED IT BROKE OFF AT THE TANK END OF THE TUBE. BOTH IB AND OB TANKS WERE REMOVED FOR INSPECTION. THEY BOTH SHOWED SIGNS OF SDR 2005FA0000377Fuel Cell · damagedDURING A SCHEDUALED 12 MONTH FUEL SYSTEM INSPECTION IAW MM, THE DEFECT WAS NOTED ON A CUSTOMERS AIRCRAFT. THE BOTTOM INSIDE OF THE AFT FUEL CELL WAS BLISTERED WITH .2500 INCH BLISTER IN DIAMETER, SPACED FROM .5000 INCH TO .2500 INCH APART. THE BLISTERS CONTISDR QXEA200500008Fitting · leakingPDX - A FUEL LEAK WAS NOTED BY MAINTENANCE AFT OF THE NR 2 WHEEL WELL. THE SYSTEM WAS INSPECTED AND THE WIGGINS FITTING OF THE MASTER REFUEL VALVE WAS REPLACED. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR DXTA200400488Fuel Sys · malfunctionedREPEAT - AMBER WING TANK -O FULL R- CAS ON IN FLIGHT. FUEL SPILLING FROM RIGHT WING WITH ONLY 3000 LBS IN WING TANK, SPILLING STOPPED THEN STARTED AGAIN WITH 2700 LBS IN WING TANK AND SAME CAS MESSAGE. ITEM IS UNDER INVESTIGATION.SDR 2004FA0000934Fuel Cell · leakingDURING TROUBLESHOOTING A FUEL LEAK FOUND THAT WHEN THE FUEL CELL WAS FLEXED, FUEL WOULD WEEP FROM EXTERIOR SURFACE. REMOVED FUEL CELL AND SENT OUT FOR TEST AND REPAIR. EVALUATION RESULTS SHOWED WEEPING/ POROUS CONDITION OVER 80 PERCENT OF THE CELL AND CELL TO SDR QXEA200400877Line · chafedPDX - EJECTOR MOTIVE FLOW LINE INSIDE LEFT WING PANEL 523AT CHAFED BY FUEL FEED LINE. REPAIRED IAW HORIZON AIR EA 6-28-19 AND SRM TASK 28-21-06-000-801.SDR CA041208003Fuel Cell · contaminated(CAN) WHILE TROUBLE SHOOTING A FUEL INDICATION PROBLEM, TWO RED PLASTIC PROTECTIVE CAPS WERE FOUND IN THE LT UPPER AFT TANK.SDR QXEA200400845Packing · leakingFUEL WAS NOTED LEAKING FROM THE NR 2 ENGINE COWLING BEHIND THE ENGINE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE PACKING FOR THE RIGHT WING SPAR CONNECTOR RECEPTACLE. THE LEAK CHECK AND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SDR RU3A0419Seal · deterioratedAFTER TAKEOFF FUEL WAS SEEN STREAMING OUT OF LT OVERWING FUEL CAP DURING CLIMB. REPLACED FUEL CAP.SDR DXTA200400459Check Valve · failedWING TANK OVERFILL RT CAS MESSAGE FOLLOWED BY FUEL VENTING OUT OF RIGHT WING TIP, 6000 LBS OF FUEL TOTAL IN AIRCRAFT. FOUND RT WING SURGE TANK CHECK VALVE TO EXCESSIVE SIDE PLAY. REMOVED AND REPLACED CHECK VALVE WITH NEW. CLOSED ACCESS PANELS AND FUELED A/CSDR FCPR200400020Retaining Ring · dislodgedFUEL CELL RETAINING RING AND CLIP HAD DISLODGED AND MIGRATED TO THE FORWARD SIDE OF THE FUEL CELL, THEN PUNCTURED CELL RESULTING IN A FUEL LEAK.SDR GLBA20030762Panel · leakingFUEL SEEP RT LOWER I/B PANEL. REPAIRED FUEL LEAK IAW EO 04-71GL-02.SDR DXTA200400440Flapper Valve · failedINFLIGHT THE WING TANK OVERFILL L CAS MESSAGE CAME ON. THE LEFT WING TANK SHOWED 3200 LBS OF FUEL IN IT AND FUEL STARTED TO VENT OVERBOARD, VENTING STOPPED AT ABOUT 2970 LBS INDICATED IN L WING TANK. AFTER LANDING (20 MIN LATER) CREW NOTICED THE UNDERSIDE OFSDR CHQA000572Flapper Valve · leakingDURING CLIMB-OUT ON FLIGHT 3098 FROM PHL TO CMH, FUEL WAS SEEN LEAKING OUT OF THE LEFT WING. STREAM WAS APPROXIMATELY 8 INCHES WIDE AND IT WAS COMING OUT AT A STEADY RATE UNTIL THE AIRCRAFT LEVELED OFF. THE STREAM WAS LOCATED APPROXIMATELY 6 TO 8 FEET FROM TSDR AALA20041053Cap · leakingMIA - INFLIGHT T671/17 RIGHT HAND WING FUEL LEAK. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED CAP AND O-RING FOR RIGHT HAND FUEL TANK. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR CA041014007Reservoir · damaged(CAN) UPON 1000 HR FUEL SYSTEM INSPECTION AS REQUIRED BY CESSNA, THE FUEL WAS COMPLETELY DRAINED FROM THE AIRCRAFT.UPON REMOVING THE LOWER R/H RESEVOIR QUICK DRAIN,IT WAS REVEALED IT WAS QUITE LOOSE BUT NOT LEAKING. UPON REINSTALLATION OF QUI CK DRAIN VALVE ISDR CA041014006Reservoir · cracked(CAN) COULD SMELL STRONG FUEL ODOR IN COCKPIT AND ALSO NOTED FUEL STAIN ON BELLY OF AIRCRAFT DURING INSPECTION. SUSPECTED RESEVOIR QUICK DRAIN LEAKY BUT FURTHER INVESTIGATION REVEALED A 1 INCH CRACK ON FORWARD LOWER WELD SEAM ON RESEVOIR. RESEVOIR REMOVED, RSDR DXTA200400411Vent · malfunctionedAT FL280 APPROXIMATELY 25 MINUTES INTO FLIGHT LEFT WING BEGAN VENTING FUEL STARTING AT 2900 LBS IN WING (NO FUEL IN CENTER TANK), VENTING CONTINUED THROUGH DESCENT. OPENED LEFT WING FUEL BAY PANELS 552AB, 542DB, 541DB, 551AB, 511CB, & 511AB. INSPECTED SURGE SDR 2004FA0000744Cap · cloggedPILOT EXPERIENCED FUEL INTERUPTION. MADE EMERGENCY LANDING IN SOYBEAN FIELD. NO INJURIES OR DAMAGE TO AC. REMOVED AC FROM FIELD TO LOCAL AIRPORT. DRAINED ALL FUEL FROM WING TANKS. FOUND WHILE DRAINING FUEL WITH FUEL CAPS ON THAT DRAINING FUEL WAS SLOW. REMOVSDR 2004FA0000783Cap · cloggedPILOT EXPERIENCED FUEL INTERRUPTION TO ENGINE WHILE ENROUTE. SWITCHED FUEL TANKS AND ENGINE QUIT. MADE EMERGENCY LANDING. NO INJURIES OR DAMAGE TO AIRCRAFT. REMOVED AC FROM FIELD TO LOCAL AIRPORT (N75). DRAINED ALL FUEL FROM WING TANKS. FOUND WHILE DRAINING FSDR 2004FA0000782Cap · cloggedPILOT EXPERIENCED FUEL INTERRUPTION TO ENGINE WHILE ENROUTE. SWITCHED FUEL TANKS AND ENGINE QUIT. MADE EMERGENCY LANDING. REMOVED AC FROM FIELD TO LOCAL AIRPORT (N75). DRAINED ALL FUEL FROM WING TANKS. FOUND WHILE DRAINING FUEL WITH FUEL CAPS ON THAT DRAININGSDR 2004FA0000873Fuel Cell · mismanufacturedDURING CRUISE FLIGHT, THE ROTAX ENGINE EXPERIENCED POWER LOSS AND PILOT PERFORMED EMERGENCY LANDING. AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE AND PILOT WAS SERIOUSLY INJURED. SUBSEQUENT INVESTIGATION REVEALED THAT WATER WAS IN BOTH CARBURETOR FUEL BOWLS, THE FUSDR CA041109007Check Valve · unserviceable(CAN) UPON TROUBLESHOOTING FOR STARTING SNAG, FOUND THAT FUEL WASN'T BEING DELIVERED TO THE FUEL NOZZLE. REPLACED CHECK VALVE. THE REMOVED VALVE WAS FOUND TO HAVE A CRACKING PRESSURE OF APPROXIMATELY 15 PSI.SDR 2004UALA00793Cap · wrong partFLIGHT DIVERTED DUE TO POSSIBLE FUEL LEAK. INCORRECT CAP ASSEMBLY INSTALLED. REPLACED CAP WITH CORRECT PART NUMBER.SDR FGQ2004F00002Fuel Cap · crackedBOTH FUEL CAPS PN 39824-803 FOUND CRACKED AT LATCH PIVOT WHERE ROLL PIN RETAINS LATCH LEVER TO CAP BODY.SDR 0401389609Fuel Tank · leakingFLIGHT CREW NOTICED A FUEL IMBALANCE OF 1200 LBS BETWEEN LEFT AND RIGHT MAIN WING FUEL TANKS WHILE AT CRUISE. CREW HAD TO MANUALLY CROSSFEED THE FUEL AND ELECTED TO DIVERT TO ALTERNATE. THE LANDING AT GRB WAS UNEVENTFUL BUT NO MENTION OF COM PROCEDURES OR IFSDR 04FDEA02435Fuel Tank · crackedAT BLOCK IN, FOUND LT OUTER WING FUEL TANK LEAKING FROM BOTTOM OF WING JUST OUTBD OF RIB NR 20, JACK 05, TRACK 08. FUEL COMING OUT OF DRAIN HOLE ON BOTTOM OF WING JUST FWD OF OVAL ACCESS PANEL. MX FOUND LT NR 8 SLAT TRACK CANISTER TO HAVE APPROX 1 - 2 INCH CSDR UIEA200400138Fuel Tank · corrodedFOUND DURING D-CHECK, AT SIN, CORROSION AT WING CENTER SECTION UPPE SKIN AT REAR SPAR BETWEEN BL 0 AND RBL 11.33. CORROSION WAS BLENDED USING A 20:1 RATIO, 125 RHR OR BETTER AND REMAINING THICKINESS TO BE .381 INCH OR GREATER. BLENDED AREA WAS SHOP/FLAP PEENSDR 20040720Housing · crackedMFG PN 6-2255-44 CHECK VALVE IN FUEL LINE WAS LEAKING. THE HOUSING OF THE CHECK VALVE WAS CRACKED.SDR CA040812006Angle · corroded(CAN) DURING IMPORT INSPECTION, RT FUEL CELL CAVITY AFT CAP ANGLE FOUND BADLY CORRODED (EXFOLIATION). PART REPLACED.
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