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 UALA2013052003450Cap · missingRIGHT FUEL RECEPTACLE CAP MISSING. NO LEAKAGE FROM RECEPTACLE AFTER FUELING COMPLETED. INSTALLED FUEL CAP, OK TO CONTINUE.SDR CWQA20130517Flapper Valve · detachedTOWER INFORMED CREW THAT THEY WERE LOSING FUEL AFTER TAKEOFF. CREW CONFIRMED FUEL COMING OUT OF THE RT WING VENT. FUEL STOPPED FLOWING FROM VENT AFTER FIVE MINUTES. ACFT PERFORMED UNSCHEDULED LANDING SAFELY. MX EVALUATION REVEALED A DETACHED FLAPPER VALVE,SDR UALA2013051503375Fuel Cell · leakingFUEL LEAK IN RT DRY BAY LOCATED AT THE AFT UPPER OTBD CORNER. LOCATED FUEL LEAK SOURCE FROM INSIDE TANK. SEALED AREA INSIDE TANK AND IN DRY BAY. APPLIED (A 1-2) SEALANT AT 2300, 12 HR CURE TIME.SDR UALA2013051303321Unknown · unknownLEFT TANK FUEL SLOWLY SEEPS BACK TO CENTER TANK. ACCOMPLISHED TEST OF FUEL SYS IAW AMM. RAN PUMPS FOR 1 HOUR. NO FUEL TRANSFER NOTED.SDR ASMF20130531009Gasket · leakingDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED ON LT PANEL 533BB. MX PERSONNEL REPLACED THE PANEL AND CORRESPONDING GASKET IAW AMM 28-11-11- 020-005, TESTED CORRECT.SDR CA130516003Valve · dislodged(CAN) FUEL SPILL FROM ACFT WING SUMP VALVE JAMMED IN OPEN POSITION DURING FUELLING. APPROXIMATELY 1 LITER OF FUEL COVERING AREA 2 X 2.5 SQUARE METERS. SPILL CONTAINED AND ABSORBAL USED FOR CLEAN UP. FOUND DRAIN VALVE REQUIRED RESEATING, RESEATED DRAIN SUMP VASDR 9JLA2013061104429Fuel Cell · leakingTHE FLIGHT CREW REPORTED THAT PRIOR TO DEPARTURE THEY NOTED FUEL LEAKING FROM AROUND THE RT WING ROOT AREA. TROUBLESHOOTING IDENTIFIED THE FUEL LEAK WAS COMING FROM THE RT FUEL VENT TUBE ELBOW ATTACHMENT ON THE FUSLAGE FUEL CELL. THE FUEL CELL WAS REMOVE FOR SDR A8OA2013050800005Fuel Cell · leakingDURING CLIMB NOTICED FUEL LEAKING FROM TOP OF LT WING. LEAK STOPPED AT 21,000 POUNDS INDICATED. AS A PRECAUTION THE CREW RETURNED TO DEPARTURE AND LANDED SAFELY. FOUND SCREWS LOOSE ON PANELS 21-FT UPR-25 AND 21-FT UPR-26 TIGHTENED SCREWS AND CHECKED FOR FUESDR DXTA2013050805379Unknown · unknownAFTER LANDING, CREW NOTICED STRONG FUEL ODOR. NOTICED FUEL DRIPPING NEAR PRESSURE REFUEL DOOR AND FROM SKIN SEAM FORWARD OF DOOR. SHINED LIGHT INTO DOOR RECESS AND ENTIRE AREA IS WET. CLEANED OFF RESIDUAL FUEL FROM SINGLE POINT CONNECTION. WIPED DOWN KEEL SDR ASOA20130427064Flapper Valve · leakingTHE CREW REPORTED FUEL LEAKING FROM THE RT WING. THE AIRCRAFT RETURNED TO SAV WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE FLAPPER VALVE AT RIB 19 OF THE RT WING, LEAK CHECKED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130426032Flapper Valve · leakingTHE CREW REPORTED A FUEL LEAK FROM RT WING AFTER TAKEOFF. FUEL QTY DROPPED 300LBS AND THEN FUEL LEAK STOPPED. MX INSPECTED AN REPLACED THE RT WING FLAP VALVE. OPS CHECKS WERE GOOD.SDR DALA1308816802Fuel Cell · corrodedMAIN CABIN CTR TANK UPPER SURFACE HAS CORROSION BS 1038, LBL 67. REPAIRED IAW ERA 511589-14, REV ORIGINAL.SDR FDEA201304110766Warning Light · false activationAFTER TAKEOFF, RECEIVED A LVL 1 FUEL CONTAMINATED ALERT. DURING RETURN TO LANDING ALERT WENT AWAY. INTERROGATED ALL THREE AIU'S. NO FAULTS FOUND. R & R NR 1, 2, AND 3 ENG FUEL FILTERS IAW MM 73-11-02. NO CONTAMINANTS FOUND. RAN NR 1, 2, AND 3 ENGINES SDR GTIA20130407635Fuel Tank · fodFOUND 6" DIAMETER, APPROX 2 FT LENGTH OF PVC CONDUIT WEDGED IN RT WING FUEL TANK AFT SURGE DOOR. REMOVED PVC PIPE AND INSPECTED IAW MM.SDR GTIA20130407634Fuel Tank · fodFOUND 6 INCH DIAMETER, APPROXIMATELY 2 FEET IN LENGTH OF PVC CONDUIT WEDGED IN LT WING FUEL TANK AFT SURGE DOOR. REMOVED PVC PIPE AND INSPECTED IAW MM.SDR UALA2013040302175Valve · leakingCREW REPORTS RIGHT WATER SUMP DRAIN HAS FUEL DRIP. SAMC TEXT: OPERATE SUMP DRAIN. REPLACED SUMP OUTER VALVE PER AMM. NO LEAKS.SDR 2013FA0000261Fuel Cap · failedPILOT MADE A PERCAUTIONARY LANDING DUE TO A ROUGH RUNNING ENGINE. PILOT CHECKED FUEL AND HEARD A "WOOSHING" SOUND WHEN OPENING THE RT TANK FUEL CAP. PILOT THOUGHT HE CORRECTED A VENTING PROBLEM, TOOKOFF, ACFT LOST POWER ON CLIMB OUT. INVESTIGATION REVEALED SDR UIEA2013040200170Sump · leakingLT MAIN TANK FWD FUEL SUMP LEAKING. RESEATED LT MAIN SUMP IAW MM 12-11-03 NO LEAK NOTED.SDR ASOA20130329046HFlapper Valve · leakingTHE CREW REPORTED FUEL LEAKING FROM THE LT WING. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, R & R THE FLAPPER VALVES ON RIB 19, LEAK CHECKED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASAA2013032794277Fuel Cell · icedAFTER FUELING, FUEL GAUGES READ L 8.46, CTR 22.2, R 8.51 AT PRIOR TO PUSH CHECK RT FUEL GAUGE DROPPED BETWEEN 400-500 LBS OF FUEL. ACCOMPLISHED E/A 800-28, EA-10038 FUEL QTY INDICATION SYS AFFECTED BY ICE FORMATION PROCEDURE. SUMPED CTR FUEL TANK AND WING MSDR DXTA2013032805341Fuel Sys · ventingACFT HAD JUST LEVELED OFF AT FL250, AMBER CAS MESSAGE, WING TANK OVER FULL RT, ILLUMINATED. FUEL OBSERVED VENTING OUT OF RT WING TIP. CTR WING TRANSFER SWITCHES WERE IN NORM, RT WING FUEL TANK HAD 3300 LB OF FUEL, & APPROX 300 LB OF FUEL IN CENTER TANK. CASDR 2013FA0000219Line · leakingPILOT REPORTED FUEL ODOR IN CABIN. DURING THE ANNUAL INSPECTION, HEAVY FUEL STAINING WAS NOTED IN THE SPAR BOX AND IT WAS DETERMINED THAT THE RIGID FUEL CROSS FEED LINES THAT RUN THROUGH THE FUSELAGE, INSIDE OF THE MAIN SPAR BOX, HAD CORRODED INTERNALLY RESULSDR CA130311020Fuel Cell · leaking(CAN) A FUEL LEAK FROM THE RT WING RESULTED IN A 10 FT X 20 FT PUDDLE OF FUEL ON THE GROUND. THE LEAK DID NOT ENTER ANY CATCH BASIN AND WAS CONTAINED. EMERGENCY SERVICES RESPONDED TO THE ACFT.SDR ASAA2013030994109Fuel Cell · contaminatedLT AND RT FUEL TANK GAUGES FLUCTUATE /- 700 POUNDS DURING FUELING, CLIMB AND CRUISE. ACFT GROUNDED. FQIS BITE IAW FIM 28-41, TASK 801 SHOWS FAULT CODES 28-41108 COMPENSATOR DATA BAD AND 28-41208 COMPENSATOR DATA BAD FOR NR 1 AND NR 2 TANKS RESPECTIVELY AND DSDR UALA2013031101437Valve · faultyDURING REFUELING BOTH WING TANKS INBD VALVES AND CENTER TANK LEFT VALVE WOULDN'T OPEN. DEFERRED CENTER LEFT REFUEL VALVE. APPLIED STICKER. REFER LOG 3 AND LOG 4 FOR LEFT WING INBD VLV AND RIGHT WING INBD VLV RESPECTIVELY.SDR ASAA2013030694114Fuel Cell · contaminatedON DESCENT AT 6000 FT, THE IMBALANCE LIGHT ILLUMINATED. FUEL STATE WAS 7.62 LT MAIN, 5.56 CTR, 8.62 RT MAIN. CROSSFEED TO BALANCE WORKED. NO LOW PRESSURE BOOST PUMP LIGHTS ILLUMINATED. REMOVED ICE AND RESIDUAL WATER FROM NR 2 FUEL TANK. R & R NR 2 F/Q SDR UALA2013030401266Fuel Tank · damagedDURING HMV2, MISDRILLED HOLE FOUND ON THE CENTER TANK UPPER SKIN AT Y153 STRINGER 2. REPAIRED PER ECRA 5710-02271 AND REO L01389.SDR FDEA201302260474Fuel Cell · corrodedFUEL CELL BS1016, RBL53, WL196, CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 57-10-01, FIG 201, PAGE 102, NOTE A-1. MAJOR REPAIR.SDR ASAA2013022694000Fuel Cell · contaminatedAT THE GATE IN OAK BOTH FUEL TANKS NR 1 & NR 2 READ 8.54 (FULL). DURING CLIMB NR 2 TANK INDICATED 8.18 (DROP OF APPROX 400 LBS) WHILE STILL BURNING FROM CENTER TANK. IMMEDIATELY UPON LEVEL OFF AT CRUISE ALT NR 2 TANK QTY STEADILY INCREASED TO 8.66. NR 1 FUELSDR R61A201302240268Solenoid · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT REFUEL CONTROL SOLENOID CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT REFUEL CONTROL SOLENOID IAW EMB 170 AMM 28-23-05. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR R61A201302240267Solenoid · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT WING REFUEL CONTROL SOLENOID CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT REFUEL CONTROL SOLENOID IAW EMB AMM 28-23-05. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR R61A201302240266Pressure Switch · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT WING REFUEL PRESSURE SWITCH CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT WING REFUEL PRESSURE SWITCH IAW EMB 170 SWPM 20-50-10. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR R61A201302240265Pressure Switch · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE REFUELING PRESSURE SWITCH CORRODED. MAINTENANCE REMOVED AND REPLACED THE REFUELING PRESSURE SWITCH IAW EMB 170 SWPM 20-50-10. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR UALA2013022401083Fuel Tank · corrodedCORROSION ON CENTER TANK UPPER SURFACE BS 980 UNDER LEFT STUB BEAM. REMOVED CORROSION, FLAP PEENED REWORK AREA, REFINISHED AREA IAW ECRA 5730-02747.SDR YENA20130222047Float Valve · failedFLT 253, DECLARED EMERGENCY AND RETURNED TO DEPARTURE DUE TO FUEL IMBALANCE MESSAGE. LEFT WING ABOUT 900 LBS MORE THAN RIGHT, FOLLOWED QRH. TOTAL FUEL IN FMS WAS LARGER THAN FUEL ON EICAS. 2000 LBS DIFFERENCE. FOLLOWED QRH, FUEL WAS OBSERVED COMING OUT SDR SWAA2013022513087Fluid · leakingAIR TURNBACK/DECLARED EMERGENCY -- TOWER NOTED SIGNIFICANT FLUID COMING FROM LEFT WING ON TAKEOFF AND ADVISED CREW AIRBORNE. COCKPIT VERIFIED LEAK, DECLARED EMERGENCY, AND RETURNED TO AND. DEFERRED PER MEL. ON 2-26-13, FLOAT SWITCH OPERATED NORMAL.SDR UALA2013022201064Fuel · leakingFOUND CONTINUOUS FUEL LEAK AT RIGHT TANK, INBOARD OF ENGINE PYLON. SUSPECTED LEAK IN FUEL VENT CAVITY LINES.SDR ASAA2013022093948Fuel Cell · contaminatedWHILE BURNING CENTER TANK FUEL, THE LT FUEL QUANTITY DROPPED TO 8.6K FOR APPROX 20 MINUTES AT CRUISE, THEN RETURNED TO 8.94K. THE RT FUEL QUANTITY REMAIN AT 8.94 DURING THIS TIME. REMOVED ICE AND RESIDUAL WATER FROM LT FUEL TANK. NR 1 FUEL QTY OPS NORMAL RESDR ASOA20130217021Flapper Valve · leakingTHE CREW REPORTED THAT AFTER TAKE OFF THE F/A CALLED WITH A VISUAL VENTING FROM THE RT WING. THE CREW RAN THE QRH AND RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE RT FUEL TANK FLAPPER VALVE AT RIB 19, LEAK CHECKED WITH NO DEFECTS NOTESDR CA130212025Fuel Cell · leaking(CAN) FUEL CELL FOUND WEEPING FROM MULTIPLE LOCATIONS IN THE MIDDLE OF THE SIDES. ACFT FUEL RT FUEL CELL HAD A SLOW LEAK SO THE CELL WAS REMOVED AND INSPECTED. USING AIR THERE WAS NO APPARENT LEAK, BUT WHEN FILLED WITH WATER, THE SIDES OF THE CELL ARE FOUND TSDR IXXA20120212003SValve · damagedON POST FLIGHT INSPECTION, FOUND HOLE IN LOWER LT WING SURFACE (LT CENTER FUEL TANK). UPON INSP, INSIDE LT CENTER FUEL TANK, DAMAGE WAS FOUND TO THE FUEL TANK VENT VALVE AND ON THE L5 STRINGER. TEMPORARY REPAIR ACCOMPLISHED TO LOWER LT WING SURFACE IAW DWG 57-SDR DT1R20130212001Baffle · unlacedDURING PRE-FLIGHT CHECK, FUEL CELL INTERNAL BAFFLE STRING WAS FOUND UNLACED AND SHREDDED. NEW LACE CORD WAS INSTALLED FOLLOWING THE MALFUNCTION.SDR EOPA20130123407O-Ring · leakingFUEL VAPORS WERE NOTICED IN CABIN. AFT CELL FUEL PROBE O-RING WAS TORN.SDR ASAA2013011193662Fuel Cell · contaminatedNR 2 FUEL QTY INDICATION VARIED 400 LBS. SUMPED NR 2 MAIN TANK IAW MM 12-11-00, FOUND & REMOVED WATER FROM TANK. PERFORMED FQIS OPS CHECK IAW MM 28-41-00. NO FAULTS FOUND. GROUND VERIFICATION SUCCESSFUL. PERFORMED FUEL COMPARISON CHECK IAW MM 28-41-00 & FSDR 2013FA0000050Bladder · mismanufacturedBRAND NEW TANK, INSTALLED AND WAS LEAKING IMMEDIATELY DURING FIRST FUEL UP. AFTER HOURS OF TROUBLESHOOTING SOURCE OF LEAK IT WAS DETERMINED THAT THE NEW TANK WAS IN FACT, UNAIRWORTHY AND GLUE WAS MISSING FROMT HE OTBD "NIPPLE" AREA WHERE ANOTHER FUEL TANK INSDR ASAA2013010493616Fuel Cell · contaminatedNR 1 AND 2 FUEL TANK GUAGES ERRATIC. FLUCUATIONS UP TO 800 LBS IN NR 2 TANK AND UP TO 400 LBS IN NR 1 TANK, WHILE BURNING FROM CENTER TANK. FLUCTUATIONS CEASED ONCE LEVEL. CRUISE ALTITUDE OF FL340 AFTER APPROX 30 MIN. REMAINDER OF FLIGHT FUEL BURN PLUS TOTASDR DXTA2012123105219Line · disconnectedAPPROX TWO HOURS AFTER FUELING AND 1.5 HOURS OF CLOSED CABIN, FUEL ODOR WAS NOTICED ENTERING CABIN. INSPECTING LUGGAGE COMPARTMENT REVEALED EVEN STRONGER ODOR, ESPECIALLY COMING OUT OF INSPECTION PANELS. GAINED ACCESS TO AFT FUSELAGE FUEL TANK. INSPECTED AFTSDR BTEA20121220001Fuel Tank · leakingLEFT FUEL TANK WAS SEEPING FUEL, IT WAS NOTICED WHILE SETTING IN THE HANGAR. DEFUELED AIRCRAFT, RESEALED FASTENER AT AFT SEAM OF TANK, STA 215.SDR QXEA2012131301694Panel · leakingFUEL COMING FROM THE CENTER POINT REFUELING AREA OF THE FUELING PANEL.SDR SWAA2012121410673Skin · crackedMAIN CABIN CENTER TANK UPPER SKIN LBL 6.14" STA 544 4TH FASTENER HOLE FROM FWD HAS A CRACK INDICATION PER HFEC PART 6 51-00-00 FIG 16. REPAIRED SKIN PER EA.
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