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 UPS00434032Pipe · corrodedINSPECTION TYPE:C, LT WING SURGE TANK DRAIN PIPE FLANGES FOUND CORRODED AT WS 889.5 AND WS 982 TWO PIPES IN TOTAL. TWO SURGE TANK DRAIN PIPES REPLACED IAW MM 28-21-19.SDR 20000912SH005Fuel Cap · leakingDURING DAILY INSPECTION, FOUND FUEL CAP LEAKING, CRACKED AT LOCKING MECHANISM. (X)SDR 20000920SH001Vent Line · bentINITIAL FLIGHT INFORMATION REVEALED RIGHT FUEL TANK WOULD RUN DRY LONG BEFORE LEFT. AFTER MANY LEAK TESTS, THE FUEL VENTS WERE SET TO FACTORY SPECS. NEXT FLIGHT INDICATED THE REVERSE OF TANKS. THE FOLLOWING FLIGHTS AND ADJUSTMENTS OF FUEL VENTS LEFT AND RIGSDR 20000809SH003Fuel Cap · tornTHESE GASKETS APPEAR NOT TO BE COMPATIBLE WITH 100LL FUEL. ALSO COMPOSITION IS WEAK MATERIAL. SOFT AND BREAKS EASY. SUBMITTER STATED OTHERS ON FLEET HAVE SAME PROBLEM. (X)SDR 20000809SH006Fuel Cap · swollenTHESE GASKETS APPEAR NOT TO BE COMPATIBLE WITH 100LL FUEL. THE MATERIAL USED CONTINUED TO SWELL AND RIP AFTER ONLY A SHORT PERIOD OF TIME. (X)SDR SIMA1942Fuel Cell · leakingGRR - FLT 3532 - AFTER TAKEOFF TOWER NOTED A VAPOR TRAIL COMING FROM AIRCRAFT, F/O''S THOUGHT SOMETHING WAS COMING FROM RT WING AREA. DECLARED AN EMERGENCY AND RETURNED TO FIELD. AIRCRAFT EXPERIENCED AN OVERWEIGHT LANDING. PERFORMED OPERATIONAL CHECK AND INSDR 20000809SH008Gasket · tornAFTER SHORT PERIOD OF USE, GASKET HAD DETERIORATED AND TORN. SUBMITTER STATED HAVING SEEN NUMEROUS CASES OF THIS IN FLEET OF ARCHER III''S. (X)SDR 20000809SH005Gasket · tornGASKET TEARS AFTER A SHORT USAGE. TIME, APPROXIMATELY 2 WEEKS USAGE. (X)SDR 20000809SH009Gasket · tornAFTER SHORT PERIOD OF USE, GASKET HAD DETERIORATED AND TORN. SUBMITTER STATED HAVING SEEN NUMEROUS CASES OF THIS IN FLEET OF ARCHER III''S. (X)SDR CA000719007Valve · stuck(CAN) ON TAKEOFF OUT OF WINNIPEG, CREW NOTED THAT FUEL WAS VENTING OUT OF LT WING. CREW ELECTED TO RETURN YWG, & LANDED WITH NO FURTHER EVENTS. MAINT INVEST. REVEALED NR 1 TANK OVERFLO W VALVE WAS STUCK IN OPEN POS, CONFIRMED BY GREN IND ON A/C REFUELING PANELSDR 2000UALA00362Fuel Cell · overservicedABORTED TAKEOFF AT 120 KNOTS DUE TO AIRCRAFT VENTING FUEL FROM NR 1 TANK. *S/D* MAINTENANCE SUSPECTED TOO MUCH FUEL WAS PUT IN NR 1 TANK. DRIPPED TANK AND TRANSFERRED EXCESS FUEL.SDR CA000712013Retainer · separated(CAN) WHEN THE AIRCRAFT WAS BEING REFUELED, THE GAS ATTENDANT HAD ROTATED THE GAS CAP TO REMOVE THE CAP. THIS ACTION IN TURN ROTATED THE RETAINER (P/N 531-035), CAUSING IT TO BECOME UNLOCKED FROM THE FILLER NECK. THE CAP WAS THEN PUT BACK ON AND LOCKED DOWN GSDR UPS00232915Web · crackedINSPECTION TYPE:C, WHILE WORKING CUSTOMER CARD 134185, FOUND CRACK IN VERTICAL WEB IN CENTER FUEL CELL BS 825, LBL 27, WL 193 FWD SIDE OF WEB. REMOVED VERTICAL WEB FROM LBL 25 FOR ACCESS, REMOVED DAMAGED AREA 3 X 3, FABRICATED REPAIR DOUBLER FOR WEB. INSTALLSDR 20000731SH010Gasket · tornTHE FUEL CAP GASKET DETERIORATES AND TEARS AFTER PUTTING THE FUEL CAP ON AND OFF A FEW TIMES. APPROXIMATELY 10 TIMES OF TAKING THE FUEL CAP ON AND OFF. (X)SDR RRXA001001Seam · crackedFUEL LEAK I/B NR 1 PYLON, WING LEADING EDGE CRACK 22.25 INCHES I/B NR 1 PYLON FWD TANK SEAM APPROX 4.5 INCH LONG.SDR 20001102SH039Vent Line · chafedLEFT WING FUEL VENT LINE CHAFED AT WS 601.5 AND WS 656.5. (X)SDR 20000809SH010Gasket · tornGASKET TEARS AND BREAKS APART AFTER A FEW TIMES OPENING THE GAS CAP. (X)SDR 20000620SH026Fuel Line · shearedPILOTS REPORTED RT REMOTE FUELING SHUTOFF AND FLOAT PRE-CHECK INOPERABLE. INVESTIGATION REVEALED THE PRESSURE LINE FROM THE HIGH-LEVEL PILOT VALVES TO THE TANK PRESSURE SENSING VALVE INSIDE THE WING AT RBL 90.00 SHEARED OFF AT THE FORWARD ATTACH FITTING. (X)SDR CA000925002Fuel Tank · leaking(CAN) FUEL LEAK.NOTE: TANK P/N 500.6154.000.001 S/N 9106808 WAS REPLACED (CHAFED), ALSO BECAUSE IT IS INTER-CONNECTED TO TANK P/N 500.6153.0000.001.SDR DHL2000706001Fluid · leakingAFTER T/O, TOWER AND ANOTHER A/C REPORTED A SIGNIFICANT AMOUNT OF FLUID LEAKING FROM LFT WING. FUEL WAS DUMPED DOWN TO LANDING WT AND RETURNED TO SERVICE. INSPECTED FUEL LINES AND TANK PANELS, NO LEAKS NOTED. INSPECTED FUEL TANK VENT SYS PER M/M 28-13-00. SDR CA000614046Fuel Tank · cracked(CAN) FUEL TANK CRACKED ALONG SIDE WHERE WELDED. AUTOMATIC FUEL CATCH SHIELD DID NOT WORK AND GAS DRIPPED INTO CABIN NOT OVERBOARD AS SUPPOSED TO.SDR AU000426Fuel Tank · fod(AUS) RIGHT WING FUEL TANK FOD. ON REMOVAL OF THE RIGHT WING FUEL TANK ACCESS PANEL, A PIECE OF RAG MEASURING APPROXIMATELY 300 MM BY 300 MM (11.8 INCHES BY 11.8 INCHES) WAS FOUND IN THE BOTTOM OF THE TANK COVERING ONE FUEL TANK FLOW VALVE AND THE MAIN FUEL SSDR AU000406Lead · arced(AUS) RT FUEL TANK BONDING LEADS (3OFF) EXHIBITED SIGNS OF ARCING.FOUND DURING SPECIAL INSPECTION IAW SB 8.28.31.SDR AALA20000787Seal · defectiveMCO - FLT 1125 - AFTER TAKEOFF FROM MCO, FLIGHT CREW NOTED FUEL LEAK FROM RIGHT WING 10 FEET FROM WING ROOT. RETURNED AND LANDED MCO WITHOUT INCIDENT. TIGHTENED SCREW ON BOOST PUMP. SYSTEM GROUND CHECK NORMAL OPERATION. REPEATED ON TRIP 0712 SAME DAY PIREPSDR AT0000235Fuel Cap · missingON TAKEOFF, PASSENGER REPORTED FUEL COMING FROM RIGHT WING. FOUND FUEL CAP MISSING FROM RIGHT WING. REPLACED CAP.SDR 20000503SH013Fuel Tank · crackedNR 3 MAIN TANK CRACKED MID-SPAR WEB APPROXIMATE WING STA 569 AFT SIDE OF UPPER CHORD. REPAIRED PER ECRA 479-57-134-2. (X)SDR RRXA002197Plate · damagedDURING A MAINTENANCE VISIT FOUND AN ELONGATED SCREW HOLE ON THE NR 4 MAIN FUEL TANK LAND PANEL 505D, DAMAGE HAS EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 00SDR 20000601SH018Fuel Cell · puncturedRIGHT NACELLE FUEL CELL FOUND LEAKING FUEL. INSPECTION REVEALED A PUNCTURE IN THE SIDE OF THE CELL CAUSED BY A TANK HANGER THAT HAD BECOME DISLODGED FROM ITS ORIGINAL LOCATION. THE HANGER PROTRUDING CLIP HAD REPOSITIONED TOWARD THE TANK LINER CAUSING THE TANSDR IXXA0000015Fuel Tank · contaminatedEN ROUTE FROM MHZ TO WRI, DURING CRUISE THE NUMBER TWO AND THREE ENGINE FLAMED OUT. THE FLIGHT CREW FOLLOWED COMPANY EMERGENCY PROCUDERS, DECLAIRED EMERGENCY AND RETURNED TO MHZ FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE WITH NO EXTERNAL DISSDR AU000345Fuel Tank · leaking(AUS) FUEL TANKS LEAKING. FOUND FOLLOWING COMPLIANCE WITH AD/GEN/80.SDR AU000343Fuel Tank · leaking(AUS) FUEL TANKS LEAKING. FOUND FOLLOWING COMPLIANCE WITH AD/GEN/81 .LEAKS WERE NOT PRESENT PRIOR TO INTRODUCTION OF WATER OR IPA.SDR AU000342Fuel Tank · leaking(AUS) FUEL TANK LEAKING. INSPECTION FOUND FAULTY SEALANT. FOUND FOLLOWING COMPLIANCE WITH AD/GEN/80.SDR 20000510SH006Line · defectiveDURING A 100-HOUR INSPECTION, THE FUEL LINE BETWEEN THE RIGHT HEADER TANK AND THE FUEL SELECTOR WAS FOUND LEAKING AT THE FITTING. UPON REMOVAL, DETERMINED THE FLARE WAS DEFECTIVE. (X)SDR CA001013004Support Bracket · cracked(CAN) AFTER THE FUEL CELL WAS REMOVED FOR INSPECTION, CRACKS WERE DETECTED IN THE AREA OF THE UPPER TWO BOLT HOLES FOR THE FUEL CELL SUPPORT SADDLES. CRACKED WERE REPAIRED AS PER MRR 53-10-21-777.SDR CA000329019Fuel Cap · misinstalled(CAN) SHORTLY AFTER TAKEOFF, THE CREW NOTICED FUEL LEAKING FROM THE LEFT NACELLE FUEL CAP AREA. MAINTENANCE INSPECTED CAP AND FOUND NO FAULT. SUSPECT CAP WAS NOT PROPERLY INSTALLED.SDR RRXA001930Structure · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN AT THE RIGHT LWR SURFACE I/B AUX TANK AT STA XFS 88 TO 132, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IASDR 20000802SH009Tank · leakingDURING 100-HOUR INSPECTION, DISCOVERED THE RT AUXILIARY FUEL TANK LEAKING FROM A JOINT WELD LOCATED ON THE TOP LEFT SIDE, AND LEAKING FROM THE AFT SIDE OF THE TANK WHERE THERE WAS EVIDENCE OF THE ELECTRODE TOUCHING THE TANK DURING ITS PRODUCTION, AND BURNING ASDR AU000284Fuel Cell · deteriorated(AUS) RIGHT FORWARD AND AFT AND LEFT FORWARD FUEL CELLS HOLED DUE TO CELL DETERIORATION. FUEL LEAKING FROM CELLS.SDR AU000283Fuel Cell · deteriorated(AUS) RIGHT FORWARD AND AFT AND LEFT FORWARD FUEL CELLS HOLED DUE TO CELL D TERIORATION. FUEL LEAKING FROM CELLS.SDR AU000282Fuel Cell · deteriorated(AUS) RIGHT FORWARD AND AFT AND LEFT FORWARD FUEL CELLS HOLED DUE TO CELL DETERIORATION. FUEL LEAKING FROM CELLS.SDR AU000218Fuel Cell · deteriorated(AUS) RIGHT FORWARD AND AFT AND LEFT FORWARD INBOARD FUEL CELLS DETERIORATED AND LEAKING.SDR AU000217Fuel Cell · deteriorated(AUS) RIGHT FORWARD AND AFT AND LT FORWARD INBOARD FUEL CELLS DETERIORATED AND LEAKING.SDR AU000216Fuel Cell · deteriorated(AUS) RIGHT FORWARD AND AFT AND LEFT FORWARD INBOARD FUEL CELLS DETERIORATED AND LEAKING.SDR DL76L000523Coupling · failedON TAXI REPORTED MASSIVE FUEL LEAK RT WING. MTC TRACED LEAK TO BROKEN COUPLING IPC REF 28-22-07-07 SHEET 2 ITEM 345 (P/N 343T0010-44). REPLACED FUEL FEED LINE AND ASSOCIATED COUPLING AND O-RINGS. LEAK CHECKED FUEL LINES, NO LEAK DETECTED. SDR DL76L000534Coupling · brokenFUEL LEAK, PUSHED WITH 137,000 FUEL. ON TAXI OUT, GROUND CONTROL REPORTED WHITE SMOKE FROM RIGHT ENGINE. FUEL DROPPEDTO 127000. FUEL USED STILL SHOWED .3 LEFT AND RIGHT. FUEL LOAD AT SHUTDOWN: L/40.8 C/50.7 R/36.2 TOTAL/127.7. INITALL LOAD: L/40.8 C/55.8 RSDR AU000015Fuel Cell · contaminated(AUS) FUEL SYSTEM CONTAMINATED WITH ETHYLENE DIAMINE. MOBIL BRAND FUEL WAS USED OUTSIDE OF PUBLISHED DATES. CARBURETTOR ALSO CONTAMINATED.SDR MALA000168Fuel Cap · separatedRT UPPER WING SURFACE FUEL CAP CAME OFF INFLIGHT, A/C DIVERTED TO RST AND LANDED WITHOUT INCIDENT. MX FOUND CAP IN AN UNLOCKED POSITION, TAB WAS UP AND ROTATED COUNTER CLOCKWISE IN THE OPEN POSITION. MX INSPECTED FUEL CAP, WING SURFACE. NO DEFECTS NOTED. RESDR 20000524SH015Strap · brokenIT WAS NECESSARY TO PULL THE RT WING FUEL TANK TO CONFIRM FUEL LEAK LOCATION. THE AFT OUTBOARD STRAP ASSY WAS FOUND BROKEN ACROSS THE SCREW HOLE. FURTHER EXAM OF STRAP REVEALED THE GRAIN OF THE ALUMINUM WAS PARALLEL TO THE BREAK AS WELL AS THE BEND. IT IS BSDR 2000ZZZX584Cell · crackedFUEL CELLS CRACKING INTERNALLY IF TANKS ARE NOT TOPPED OFF. HAVE RECEIVED 28 OF SUCH CELLS SINCE 11-30-99. CELLS ARE OF FAA APPROVED MATERIAL, ETC. SUBMITTER CONCERNED ABOUT THEIR RELIABILITY IN THE FUTURE IN THAT THERE ARE A LOT OF THESE CELLS OUT THERE. SDR 20000501SH001Shutoff Valve · failedTRANSFER SHUTOFF VALVE IS BYPASSING FUEL THROUGH ELECTRICAL CONDUIT. TOP OF SOV BYPASSES FUEL THROUGH ''POTTING'' AND IS FOUND DOWNSTREAM OF ELECTRICAL CONDUIT WITNESS HOLES. SUBMITTER STATED THIS IS THE THIRD LEFT FUEL TRANSFER SOV TO BE REPLACED. FIRST, N
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