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 QXEA200400517Line · leakingSEA - FLIGHT 2104 - FUEL WAS NOTED LEAKING ON THE NUMBER 2 INBOARD NACELLE. MAINTENANCE INSPECTED THE NACELLE AND FOUND THE FUEL LINE CONNECTING THE FLOW DIVIDER AND PUMP VALVE TO FIREWALL LOOSE. THE LINE WAS TORQUED AND THE OPERATIONAL AND LEAK CHECKS WERE SDR CA041123012Fuel Cell · split(CAN) LOW FUEL LIGHT COMING ON WITH 250-300 LBS INDICATED IN LT LOWER FUEL CELL. INVESTIGATION FOUND SPLIT IN FUEL CELL INTERNALLY ACROSS BAFFLE, WHICH ACTED LIKE A ONE WAY VALVE. THIS WOULD PUMP FUEL AWAY FROM BOOST PUMP WHEN A/C IS IN UNUSUAL ATTITUDES (HOVSDR QXEA200400480Shutoff Valve · leakingPDX - FUEL DRIPPING FROM RIGHT NACELLE, BETWEEN FUEL DOOR AND GEAR DOOR. REMOVED AND REPLACED REFUEL/DEFUEL SHUTOFF VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 04FDEA01860Fuel Tank · corrodedCORROSION ON UPPER SURFACE OF CENTER WING TANK AT BS 821 RBL 13. *S/D* CORROSION ON UPPER SURFACE OF CENTER WING TANK AT BS 821, RBL 13 REPAIRED PER EA NR 7-5730-55326.SDR CA040712001Cap · leaking(CAN) LANDED BACK TO THE BASE, DUE TO FUEL LEAKAGE FROM FUEL CAP INTO THE CABIN. ON ARRIVAL FOUND SIGN OF FUEL LEAKAGE AT AFT TANK CAP TO THE ADJACENT PAX DOOR INTO THE CABIN. AFT TANK WAS FULL ON DEPARTURE, SUSPECT FUEL SEEPAGE FROM THE TANK CAP DUE TO SEALSDR 2004FA0000799Gasket · deterioratedFUEL TANK GASKETS MAY NOT BE COMPATABLE WITH AUTO FUEL. ENGINE IS APPROVED FOR AUTO FUEL. GASKETS WERE FOUND SEVERELY DETERIORATED. (WP11200403100)SDR 04FDEA01619Structure · corrodedCORROSION AT LOWER SURFACE OF CTR FUEL TANK, BS 830, RBL 26, WL 160, JUST ABOVE RT PRIMARY HEAT EXCHANGER. CORROSION AT LOWER SURFACE OF CENTER FUEL TANK - BS 830, RBL 26, WL 160 ABOVE PRIMARY HEAT EXCHANGERS FOUND TO BE OUT OF LIMITS PER SRM 57-30-1. REPAISDR CED2004F00003Fuel Sys · leakingON TAKEOFF ROLL AND INITIAL CLIMB OUT, FUEL WAS OBSERVED LEAKING FROM THE LEFT WING TIP. ATC 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 FOUNSDR 2004FA0000652Reservoir · leakingRESERVOIR FUEL TANKS BELOW FUEL SELECTOR WAS LEAKING FUEL FROM A SEEM WELD THAT HAD CRACKED. FOUND DURING ROUTINE WALK AROUND INSPECTION. THE LEAK WHEN FIRST NOTICED WILL INDICATE THE FUEL PEDCOK IS LEAKING UNDER THE BELLY OF THE AIRCRAFT FURTHER INSPECTION SDR AUS20040371Tank · corroded(AUS) LT WING FUEL SYSTEM COLLECTOR TANK CONTAINED LEVEL 3 CORROSION ON LOWER INTERNAL SURFACE.SDR AUS20040370Tank · corroded(AUS) RT WING FUEL SYSTEM COLLECTOR TANK CONTAINED LEVEL 3 CORROSION ON LOWER INTERNAL SURFACE.SDR CA040518005Line · restricted(CAN) DURING CRUISE FLIGHT, PILOT SELECTED CROSSFEED FOR RT ENGINE. SHORTLY AFTERWARDS, THE RT ENGINE LOST POWER/FUEL FLOW. SELECTOR WAS RETURNED TO NORMAL, AND ENGINE CONTINUED TO RUN NORMALLY. MAINTENANCE DISCOVERED UPON INSPECTION THAT THERE WERE 2 LONG SDR USAASA04042Disc · rupturedONT - FLT 46 - LAX-PHL, AFTER TAKEOFF, A FUEL IMBALANCE DEVELOPED, ACCOMPANIED BY A 'FUEL AUTO TRANSFER FAULT' MESSAGE. BY ABOUT FL180, THE IMBALANCE HAD REACHED 3,000 LBS, WITH THE LEFT WING LOSING FUEL. MANUAL FEED WAS SELECTED, BUT DID NTO HAVE ANY AFFECTSDR GTIA040340Vent · unsecureFOUND RIGHT OUTBOARD WING LEAKING FUEL FROM WEEP HOLE. FOUND FASTENER TO VENT PORT NOT PROPERLY SECURED. (M)SDR QXEA200400281O-Ring · missingA LEAK WAS NOTED COMING FROM THE CENTER FUEL TANK DURING THE POST FLIGHT WALK AROUND. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE O-RING MISSING ON THE FUEL MANIFOLD TUBE FITTING. A NEW O-RING WAS INSTALLED, OPERATIONAL AND LEAK CHECKS WERE PERFORMED, ANDSDR AWXA200400375Valve · faultyCMH - FUEL - FLT 0794 - WHILE TAXIING TO RUNWAY FOR DEPARTURE FUEL WAS REPORTED LEAKING FROM THE RIGHT WING, RETURNED TO GATE. MAINTENANCE FOUND FUEL LEAK COMING FROM RIGHT WING OUTBOARD SURGE TANK NACA INTAKE VENT. REMOVED AND REPLACED FUEL LEVEL SENSING COSDR AUS20040275Fuel Tank · leaking(AUS) LT WING FUEL TANK LEAKING INTO DRY BAY AT WBL 616.75 LOWER AFT CORNER.SDR ALG2004F00018Fuel Cap · missingAFTER APPROX 5 MINUTES OF FLIGHT AFTER TAKE OFF FROM EC-160, PILOT NOTICED A STRONG ODOR OF FUEL AND GAUGE WAS FUNCTIONING PROPERLY. RETURNED TO EC-106, SHUT DOWNED AND INSPECTION OF AIRCRAFT SHOWED MISING FUEL CAP. FUEL CAP HAD BEEN REPLACED AFTER REFUELINGSDR RAIA00403017Valve · leakingSTL FUEL LEAK/VENTING. TOWER REPORTED LARGE AMOUNT OF WHITE SMOKE COMING FROM AIRCRAFT. MAINTENANCE REMOVED AND REPLACED BOTH LT AND RT WING FUEL VENT VALVES.SDR MAFPAPUADrain · failedWHILE INSTALLING THE WING FUEL TANK SUMP DRAIN AT THE MFG RECOMMENDED TORQUE VALUE OF 90 IN-LBS, THE DRAIN ITSELF FAILED, SEPARATING AT THE DRILLED HOLES JUST ABOVE THE FITTING HEAD.SDR RAIA00403018Valve · leaking5642 - STL - TOWER REPORTED FUEL LEAKING FROM AIRCRAFT. MAINTENANCE REMOVED AND REPLACED DE-FUEL SHUTOFF VALVE.SDR AUS20040232Check Valve · damaged(AUS) WING REFUELING MANIFOLD CHECK VALVE DAMAGED. CHECK VALVE HAD DAMAGE ON THE VALVE BODY, SPRING AND FLAPPERS. WEAR ALSO FOUND ON THE FLAPPER ATTACHMENT LUGS AND THE LUGS ON THE VALVE BODY WHICH HOLDS THE FLAPPER PIN. THE FLAPPER SEPARATED FROM THE VALVE ASDR LER2004F00000Tube · fracturedFUEL LINE FRACTURED CAUSING FUEL STARVATION AND ENGINE FAILURE.SDR 2004FA0000249Hose · misroutedLANDING GEAR (IN-TRANSIT) LIGHT CAME ON INTERMITTENTLY. DURING TROUBLESHOOTING, FOUND FUEL FEED LINE FROM ELECTRIC PUMP TO ENGINE DRIVEN PUMP MISROUTED. HOSE WAS BEING JAMMED BETWEEN NLG TIRE AND ENGINE MOUNT WHEN GEAR IS RETRACTED. THIS CAUSED NLG TO INCOMSDR AUS20040156Fuel Tank · contaminated(AUS) RT ENGINE MISFIRING IN FLIGHT. INVESTIGATION FOUND CONTAMINATION IN THE LT FUEL TANK. A HAIR LIKE FIBER WAS FOUND IN THE FUEL FILTERS AND INJECTOR NOZZLES.SDR NACA20040012Check Valve · stuckHEAVEY FUEL VAPOR IN CABIN DURING CLIMBOUT. REPAIRED AFT ONE WAY CHECK VALVE ON RT SIDE OF BULK FUEL VENT SYSTEM.SDR RAIA00402019Valve · leakingIAD - FUEL LEAKING FROM RIGHT WING VENT DURING CLIMB. MAINTENANCE VERIFIED RIGHT WING VENT VALVE CLOSED.SDR BAQA091139Drain Valve · leakingWARRANTY. UNIT LEAKING. REPLACED WITH SERVICABLE UNIT. 02/12/2004SDR QXEA200400153Fuel Tank · leakingFOUND FUEL LEAKING FROM OB SIDE OF NR 2 COWLING. MAINTENANCE INSPECTED AND FOUND THE LEAK TO BE COMING FROM THE BOTTOM OF THE WING BOX, AFT OF STATION YW 171.2. MAINTENANCE LOCATED THE SPECIFIC AREA OF THE LEAK AND APPLIED SEALANT TO THE SAME. THE FUEL TANKSDR 2004FA0000242Fuel Tank · leakingWITH FULL FUEL TANKS AND THE AIRCRAFT ON THE GROUND AN AMOUNT OF FUEL (.5 GALLON +) WILL DRAIN FROM THE VENT OF THE LT FUEL TANK AFTER A FORWARD OR AFT MOVEMENT OF THE AIRCRAFT. (GL13200305339)SDR 2004FA0000164Fuel Cap · misinstalledFUEL TANK CAPS ARE VERY DIFFICULT TO SECURE PROPERLY. IT IS EASY TO PUT THE CAP ON PARTIALLY. THE FACTORY RECOMMENDS THE CAP GASKETS BE LUBED WITH SILICONE SPRAY. WE ARE ALSO PUTTING ALIGNMENT MARKS ON THE CAP AND WING FOR POSITIVE ENGAGEMENT INDICATION.SDR CA040206002Sight Glass · cracked(CAN) SIGHT GLASS ON FORWARD SIDE OF RANGE EXTENDER WAS FOUND TO BE THE CAUSE OF A SLOW FUEL LEAK. WHEN THE AIRCRAFT WAS FULL OF FUEL AND KEPT IN THE HANGAR OVER NIGHT A SMALL POOL OF FUEL WAS NOTICED ON THE FLOOR. A CRACK RUNNING ACROSS FROM TWO SCREWS WAS SDR QXEA200400038O-Ring · leakingPDX - FUEL WAS FOUND LEAKING FROM THE NR 2 ENGINE NACELLE. MAINTENANCE INSPECTED THE AREA AND RESEATED THE FUELING ADAPTER POPPET VALVE O-RING. NO OTHER DEFECTS WERE NOTED AND NO PARTS WERE REPLACED. OPERATIONAL CHECKS WERE PERFORMED AND WERE GOOD. THE AIRSDR 2004FA0000172Fuel Cap · loosePILOT ENCOUNTERED LOSS OF POWER ON LT ENGINE AND MADE AN UNSCHEDULED LANDING. WATER WAS FOUND IN LT TANK AND LT FUEL LINES. WATER WAS SUMPED OUT, ENG TEST RUN, AC RETURNED TO HOMEBASE. LT SIDE CAP WAS FOUND TO BE LOUSY FIT, PROBABLY ALLOWED WATER TO ENTERSDR 2004FA0000139Cap · loosePILOT ENCOUNTERED LOSS OF POWER ON LT ENGINE AND MADE PRECAUTIONARY (UNSCHEDULED) LANDING. WATER WAS FOUND IN LT TANK AND LT FUEL LINES. WATER WAS SUMPED OUT, ENGINE TEST RUN, AND AIRCRAFT RETURNED TO HOMEBASE. AT HOMEBASE LT SIDE FUEL CAP WAS FOUND TO BE A SDR UG8AGM0414Fuel Tank · leakingWING TANK (0) FILL ON AND VENTING FUEL FOR 3 MIN. 3400 LBS. FUEL. CREW REMINDED OF SL750-28-02 LETTER IN ALL AIRCRAFT LOG BOOKS REGARDING THIS CONDITION AND WHAT STEPS ARE NEEDED TO CORRECT THIS CONDITION. NO ACTION TAKEN. CONDITION IS NORMAL REGARDING THE SDR GTIA031068Bladder · leakingDTW - FUEL LEAKING FROM FUSELAGE AFT OF WHEEL WELL. REMOVED AND REPLACED AFT AUX BLADDER. LEAK CHECK GOOD. INSPECTED INSTALLATION OF AFT AUX TANK BLADDER AND FUEL DRAIN SHROUDS. NO LEAKS NOTED. (M)SDR GTIA031047Bladder · leakingFLT 982 - DEN - UPON ARRIVAL, FOUND FUEL LEAK AFT OF MAIN WHEEL. REMOVED AND REPLACED AFT AUX BLADDER. LEAK CHECK GOOD. INSPECTED INSTALLATION OF AFT AUX TANK BLADDER AND FUEL DRAIN SHROUDS. NO LEAKS NOTED. (M)SDR 03FDEA02206Skin · corrodedCORROSION WHILE WORKING FLOOR CLOSE FOUND CORROSION ON CENTER TANK SKIN BS 825 LBL 10.SDR DEBA4324V1Fuel Cap · out of adjustFUEL VENTED FROM LT IB FUEL CAP ON TAKEOFF. AIRCRAFT RETURNED TO BASE AND UPON INSPECTION FOUND THE CAP WAS LOOSE WHEN LATCHED. THE COTTER PIN WAS MISSING AND IT AND THE ADJUSTMENT NUT HAD LOOSENED. ADJUSTED CAP AND REPLACED COTTER PIN.SDR 03FDEA02157Fuel Tank · corrodedFOUND CORROSION ON UPPER SURFACE OF WING CENTER TANK BS 825 RBL 12. REMOVED CORROSION ON UPPER SURFACE OF WING CENTER TANK AT BS 825, RBL 12 PER SRM 51-10-06. FOUND DAMAGE AREA TO BE OUT OF LIMITS PER SRM 53-10-1, FIG 1. REMOVED DAMAGE AND REPAIRED PER SSDR RO32004F00000Fuel Cell · chafedDURING 48 MO. G INSPECTION, REQUIREMENTS TO REMOVE THE DORSAL FUEL TANK REVEALED SEVERE CHAFING ON THE AFT LOWER TANK SKIN. CHAFING WAS FOUND TO BE CAUSED BY A SEAL RETAINER FLANGE MOUNTED TO THE VERTICAL STABILIZER. AFTER REPAIRS WERE ACCOMPLISHED TO THE TASDR CA031209003Bladder · leaking(CAN) WHEN FUEL TANK FILLED TO MAXIMUM CAPACITY A DRIP WOULD SHOW ON THE BELLY OF THE AIRCRAFT NEAR THE FUEL CAVITY DRAIN HOLE.SDR 2003FA0001299Bladder · failedDISCOVERED FUEL LEAKING, LOWER WING LT ENGINE NACELLE. REMOVED FUEL BLADDER AND FOUND THE LOWER IB NIPPLE CRACKED AND ALLOWING FUEL TO LEAK. FUEL CELL HAD BEEN REPAIRED A YEAR EARLIER. DATE OF MFG AUGUST 1978. INSTALLED NEW BLADDER, IT WAS FELT THAT THIS BSDR C2XA03BT111Switch · out of positionCREW REPORTED, FUEL NR 1 LOW LEVEL MESSAGE CAME ON INFLIGHT ON ARRIVAL INTO EWR. NR 1 FUEL QTY INDICATOR SHOWS ZERO FUEL. DECLARED EMERGENCY AND LANDED UNEVENTFULLY IN EWR. MAINTENANCE FOUND REFUELING SWITCH TO BE IN THE OPEN POSITION ON THE REFUELING PANELSDR 2003FA0001204Pad · deterioratedREPORTED (AFT FUEL LOW) LIGHT ILLUMINATING WITH 300-400 LBS REMAINING ON GAUGE. (SHOULD BE 110 LBS). TROUBLESHOOTING REVEALED FLAPPER PAD (SEAL) WAS DETERIORATED TO THE CONSISTENCY OF A (GUMMY BEAR). AS FUEL IS MOVED INTO THE NR 5 (ENG FEED) TANK, BY MOTIVESDR QXEA200301437O-Ring · leakingPDX- ON FLIGHT 2048 FUEL DRIP FROM SPR DOOR. RESEATED ADAPTER HOUSING O-RING UNDER FUEL CAP. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR QXEA200301415O-Ring · out of positionPDX- ON FLIGHT 2044 FUEL LEAK AT SPR. RESET AND SEATED BLUE O-RING ON FUELING ADAPTER POPPET VALVE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR DXTA200300156Float · stuckAFTER TAKEOFF, AMBER CAS MESSAGE WING O FULL RT ILLUMINATED. FUEL CAN BE VISUALLY SEEN DUMPING OUT OF RIGHT WING FROM VICINITY OF SURGE TANK VENT. FUEL IMBALANCE BECAME EVIDENT AT A RATE OF APPROX 100 LBS PER MIN. PRESSURIZED RIGHT WING, FOUND NO LEAKS IN DSDR 2003FA0001209Skin · corrodedLOWER TANK SKINS CORRODED THROUGH IN STRAINER ASSEMBLY SUMP. CORROSION NOTED IN OTHER AREAS OF TANK LOWER SURFACE CONSISTENT WITH STANDING BEADS OF WATER. CORROSION NOTED AROUND FUEL DRAIN VALVE PAD. STRAINER ASSEMBLY SUMP IS LOW POINT IN THE TANK AND HAS N
Back to JASC 2810