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 CA120529004Reinforcement · detached(CAN) THE STAINLESS STEEL REINFORCEMENT ROD SHOULD BE RETAINED WITHIN 2 CARBON FIBER TUBES. DURING INSPECTION THE STAINLESS STEEL REINFORCEMENT ROD WAS FOUND LOOSE IN THE FUEL CELL.SDR QMLA2012041212058O-Ring · failedCREW REPORTED SENSING A STRONG ODOR OF FUEL IN CABIN ON THE RETURN LEG TO THE BASE FOLLOWING A REFUELING STOP. ON LANDING AT BASE THE ODOR HAD DISSIPATED. INSPECTED BEHIND THE INTERIOR WALLS IN THE AREA OF THE FUEL VENT TANK AND SHUT OFF VALVES FOR THE FUELSDR 2012F00086Line · damagedFRETTING DAMAGE ON PUMP FITTINGS WHERE WIGGINS CLAMP W991-18DE CLAMPS ONTO. FRETTED THROUGH LINE 100 PERCENT.SDR FDEA201204051259Fuel Cell · leakingLEFT WING INNER TANK LOWER SURFACE 1 EA BOLT FUEL SEEPING NEAR REAR SPAR RIB 8 POSITION. USED OPTIONAL INSP METHOD WITH HIGH LEVEL FUEL SENSING. TORQUED NUT WITH APPLICABLE VALUE CLEAN UP THE FASTENERS AND RESEALANT ON THE NUT IAW SRM 51-49-00. APPLIED NEW SDR FDEA201204051258Fuel Cell · leakingRIGHT OUTER TANK REAR SPAR, FUEL SEEPING AT NR 6 SPOILER BLOCK VALVE SUPPORT FITTING LWR RT FITTING FASTENERS. USED OPTIONAL INSPECTION METHOD WITH HIGH LEVEL FUEL SENSING. TORQUED NUT WITH APPLICABLE VALUE CLEAN UP THE FASTENERS AND SEALANT ON THE NUT IAW SRSDR UALA2012040202040Valve · stuckFUEL LEAKING FROM RT WING SURGE TANK VENT. SUSPECT UNWANTED FUEL TRANSFER FROM NR 2 MAIN TO NR 3 MAIN. AIRCRAFT WAS FUEL TO NR 2 MAIN LEVEL OF 84800 LBS AND NR 3 MAIN TO A LEVEL OF 84700 LBS WITHIN OVER AN HOUR, THE LEVEL IN NR 2 MAIN HAD DECREASED TO 81900SDR P5CA2012040100023Relief Valve · faultyNRT TOWER OBSERVED FLUID STREAMING FROM UNDER THE RIGHT WING. NO NOTICEABLE REDUCTION IN FUEL, HYDRAULIC OR OIL QUANTITIES. (DURING MAINTENANCE WALK AROUND THE RIGHT INBOARD FUEL PRESSURE RELIEF VALVE WAS FOUND TO BE OPEN SLIGHTLY. REMOVED AND REPLACED THESDR UALA2012033001989Valve · malfunctionedDURING REFUELING, FOUND CENTRE TANK LT REFUEL VALVE DID NOT OPEN. DEPOWERED AND REPOWERED. CENTER TANK LT REFUEL VALVE NOW OPERATING NORMALLY.SDR AALA20120325007Fuel Cap · leakingORD - INFLIGHT DFW-FRA. CREW REPORTED FUEL LEAKING NEAR THE LEFT OVERWING REFUEL CAP AREA. EMERGENCY DECLARED FLIGHT DIVERTED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT OVERWING REFUELING CAP. SYSTEM GROUND CHECK NORMAL OPERSDR UALA2012032201819Drain Valve · leakingFOUND LEFT HST SUMP DRAIN SOLENOID LEAKING EXTERNALLY. RE-ACTIVATED HST ISO VALVES DV439 AND DV440 AS REQUIRED. ON ARRIVAL CHECK FOUND FUEL SEEPAGE FROM RT HORIZONTAL STABILIZER DRAIN HOLE NEAR STA 285. MUST EMPTY TANK AND CONFIRM NO LEAKS BEFORE DEPT. HST SDR L7OA201203270127Valve · malfunctionedON CLIMBOUT FROM SJU, IT WAS NOTICED THAT FUEL WAS COMING FROM THE LEFT WING VENT AREA. THE AIRCRAFT RETURNED TO SJU WITHOUT INCIDENT.SDR UALA2012031901783Seal · leakingRUNNING FUEL LEAK FROM LEFT WING MAIN TANK LOWER SURFACE IMPACT RESISTANT DOOR WHERE STICK NR 3 IS LOCATED. LEAK FAILS 15 MINUTE TEST PER AMM. REPLACED SEAL.SDR UALA2012031601729Cap · damagedREFUEL COUPLING CAP DAMAGED. REMOVED DAMAGED CAP. COMPLIED WITH CDL. REPLACED CAP.SDR UALA2012022801203Fitting · leakingFUEL LEAKING FROM LOWER RIGHT AFT SPAR TO FUSELAGE ATTACH FITTING (CENTER TANK). RESEALED FITTING RESEALED LEAKS IN CTR TANK, (SEE SEQ 8012030, 8012031, 8012032, 8012034-6).SDR UALA2012022801202Structure · leakingFUEL LEAKING FROM CENTER TANK SEAM ABOVE THE LEFT AC PACK REHEATER (AREA WASHED AWAY). RESEALED SEAM.SDR UALA2012022801201Structure · leakingFUEL LEAKING FROM LEFT LOWER AFT SPAR TO FUSELAGE ATTACH FITTING (CENTER TANK). RESEALED FITTING & RESEALED SEAM IN CTR TANK.SDR CA120223007Plug · leaking(CAN) FUEL FOUND LEAKING ON HANGER FLOOR. FOUND TO BE PLUG ON FUEL TANK, THIS ITEM IS MADE OUT OF RUBBER. RUBBER WAS CRACKED AROUND INTERAL CIRCUMFERENCE. REPLACED PART, NO FURTHER PROBLEM.SDR FDEA201202220646Fuel Tank · leakingSTRONG ODOR OF FUEL IN CABIN. SUSPECT CENTER TANK LEAK. TROUBLESHOOT AND REPAIRED INBD CENTER TANK FUEL LEAK ALL WORK ACCOMPLISHED.SDR ASOA201218004Tank · chafedACFT IS IN FOR A 3C INSPECTION, WHEN INSPECTION FOUND THE VENTRAL TANK BOTTOM CENTER CHAFED. MX PERFORMED A DOUBLER REPAIR ON THE VENTRAL TANK. FABRICATED AND INSTALL THE DOUBLER AFTER ALLODINED, PRIMED, PAINTED, SEAL AND REMOVED FAIRING 197 BB TO PREVENT FUSDR 2012FA0000189Fuel Tank · leakingTHIS ACFT HAS BEEN REPEATEDLY REPAIRED TO CORRECT FUEL LEAKS. EVERY DRAIN HOLE HAS BEEN COVERED UP ALLOWING WATER AND FUEL TO BE TRAPPED IN THE OTBD BAYS. ALSO THE DRAIN VALVE RECEPTACLE DRAIN HOLES WERE COVERED WITH SEALANT CAUSING WATER TO COLLECT UP TO .5SDR N81R20120215001Fuel Cell · contaminatedWHILE PERFORMING AN INSPECTION TASK ON THE ABOVE ACFT, TASK ITEM NR 2810001 WING TANK- REMOVAL FUEL TANK ACCESS PANELS AND PERFORM VISUAL INSP (REFER TO 5-10-00, PAGE 201). DURING THE VISUAL INSP A ROLL OF ADHESIVE TAPE WAS FOUND IN THE LT WING AFT FUEL BAY ASDR RU3A20120201001Fuel Cap · unsecureAFTER REACHING FL200, FUEL STREAMING FROM LEFT OUTBOARD FUEL CAP WAS OBSERVED BY CREW. EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS MADE.SDR UALA2012020300679Seal · leakingFOUND FUEL SEEPAGE UNDER LT WING NR 6 DRIPSTICK PANEL. NO REPAIR PROCEDURE IS NECESSARY, EXAMINE THE FUEL LEAK FREQ TO MAKE SURE IT DOES NOT GET LARGER PER MM. REPLACED SEAL ON NR 6 FUEL STICK PANEL. LT MAIN FUEL TANK. LEAK CHECKS GOOD.SDR FDEA201202020434Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND CORRODED AT AREA UNDER BS 940 RT STUB BEAM. REPAIRED IAW EA F-5710-157294.SDR FDEA201201240322Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND CORRODED AT AREA UNDER BS 980. LT STUB BEAM CENTER TANK UPPER SKIN REPAIRED IAW EA F-5710-157292 & F-5710-157283.SDR FDEA201201240321Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND CORRODED AT AREA UNDER BS 1000 LT STUB BEAM. CENTER TANK UPPER SKIN REPAIRED IAW EA F-5710-157286 & F-5710-157286.SDR FDEA201201240320Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND LIGHT SURFACE CORROSION AT AREA UNDER BS.960. RT STUB BEAM CENTER TANK UPPER SKIN REPAIRED IAW EA F-5710-157284.SDR FDEA201201230314Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND LIGHT CORROSION AT AREA UNDER BS.1020 RT STUB BEAM CORROSION. REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT. CARRIED OUT IAW SRM 57-10-01 FOUND WITHIN LIMITS.SDR FDEA201201230313Panel · corrodedCENTER TANK UPPER SKIN FOUND LIGHT SURFACE CORROSION AT AREA UNDER BS.920 LT STUB BEAM CORROSION. REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT CARRIED OUT IAW SRM 57-10-01 FOUND WITHIN LIMITS.SDR FDEA201201230312Panel · corrodedCENTER TANK UPPER SKIN FOUND LIGHT SURFACE CORROSION AT AREA UNDER BS 920 RT STUB BEAM CORROSION REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT CARRIED OUT IAW SRM 57-10-01. FOUND WITHIN LIMITS.SDR FDEA201201230311Panel · corrodedCENTER TANK UPPER SKIN FOUND LIGHT SURFACE CORROSION AT AREA UNDER BS.940 RT STUB BEAM CORROSION REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT. CARRIED OUT IAW SRM 57-10-01 FOUND WITHIN LIMITS.SDR FDEA201201230310Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND CORRODED AT AREA UNDER BS.940 LT STUB BEAM CORROSION. REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT CARRIED OUT IAW SRM 57-10-01, FOUND WITHIN LIMITS.SDR BSYA2012005Fuel Sys · contaminatedON TAKEOFF OUT OF RST, RIGHT ENGINE QUIT, ABORTED TAKEOFF AND RETURNED TO SIGNATURE RAMP. MAINTENANCE DRAINED WATER FROM FUEL SUMPS, RUN UP ENGINES, OPS CHECK NORMAL, NO DEFECTS NOTED.SDR UALA2012010400077Fuel Tank · leakingFOUND FUEL LEAKING FROM BOTTOM OF RIGHT WING NR 3 MAIN TANK AFT MID SPARE SEAM, 6 INCHES OTBD OF WING ROOT. ACCOMPLISHED PERMANENT REPAIR REF SERVICE TIP MM 57-52-96.SDR WRLA20120102533Fuel Cell · corrodedFOUND CORROSION ON CENTER WING TANK UPPER SURFACE AT XCW = 96.5 S-15-S-18. REPAIRED IAW EI W2012A57B-051. REV:00, REV:01 & REV:02SDR WRLA20120101530Fuel Cell · corrodedDURING 2C CHECK, MECHANICS FOUND CORROSION ON CENTER WING TANK UPPER SKIN SURFACE AT XCW = 99.0 S-15. REPAIR ACCOMPLISHED AS PER EGAT EI NO: W2012A57B-027 REV:00, REV:01 & REV:01.SDR ASOA20111231002Flapper Valve · leakingRT WING LEAKING FUEL DURING CLIMB. CREW DECLARED AN EMERGENCY, RETUNED AND LANDED WITHOUT INCIDENT. MX INSPECTED AND CLEANED THE FLAPPER VALVE ON THE RT WING. OPS CHECKS WERE GOOD. THE ACFT WAS RELEASED FOR SERVICE.SDR UALA2011123007167Packing · leakingLEFT WING FILL VALVE LEAKING 6 DROPS PER MINUTE AT THE MOUNT OF THE VALVE. REPLACED PACKING'S, OP'S AND LEAK CHECKED NORMAL, NO DEFECTS NOTED, PER AMM.SDR USAA2011122300021Fuel Tank · leakingFLT 803. EN-ROUTE, CREW EXPERIENCED A RAW FUEL ODOR AFTER ENGINE START. REPAIRED FUEL LEAKS IN CENTER TANK NEAR KEEL BEAM, BY RIGHT HAND PACK BAY.SDR ASOA20111218016Valve · leakingDURING FLIGHT IT WAS NOTED THAT FUEL WAS VENTING FROM THE RT WING. THE CREW ELECTED TO DIVERT, WHERE THE ACFT LANDED WITHOUT INCIDENT. MX REPLACED THE RT WING TANK VENT VALVE, OPERATIONALLY CHECKED THE SYS AND CLEARED THE DISCREPANCY.SDR UALA2011121906971Door · openAT DEPARTURE CENTER FUEL PUMPS REMAINED ON WHEN THEY SHOULD HAVE SHUTOFF. FOUND FUELING DOOR AJAR SECURED FUELING DOOR, OPS CKS OKAY.SDR FDEA201112155281Fuel Cell · contaminatedIN CRUISE, BOTH CTR TANK PUMPS FAULTED FOLLOWED BY LT OUTER TANK QTY WINDING DOWN TO ZERO. SUMPED ALL TANKS AND FOUND SOME WATER IN LT OUTER TANK ONLY. ENTIRE TIME TRANSFERING FUEL OUT OF LT OUTER TANK AND QTY INDICATION WER STABLE. SUMPED LT OUTER TANK AGAISDR FDEA201112155280Fuel Cell · leakingRT WING BOTTOM SKIN HAD FUEL SEEPAGE AT SLAT TRACK NR9 CANISTER DRAIN PORT FASTENER. REMOVED AND CLEANED THE DAMAGED SEALANT AREA. RE-APPLIED NEW SEALANT FOR REPAIRING IAW EO 6-5710-7-3304 PT3 AND EA 6-5710-149029 (FOR REPAIR OF FUEL TANK SEALING). THE REPAIR SDR FDEA201112155276Fuel Cell · leakingRT WING FRONT SPAR HAD FUEL SEEPAGE AT RIB 18. REMOVED AND CLEANED THE DAMAGED SEALANT AREA. RE-APPLIED NEW SEALANT FOR REPAIRING IAW EO 6-5710-7-3304, PT3 AND EA 6-5710-149029. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201112155274Canister · leakingRT WING SLAT JACKSCREW NR 3 CANISTER DRAIN PORT HAD FUEL SEEPAGE IAW EA 6-5710-149029. REMOVED FUEL PANEL 540BB, 540CB IAW AMM 28-11-22. RE-SEALED SCREWJACK CANISTER IAW EO 6-5710-7-3304C PT1. RE-INSTALLED FUEL PNL 540BB, 540CB IAW AMM 28-11-22. LEAK CHSDR ASOA20111213018Valve · faultyTHE CREW REPORTED FUEL LEAKING FROM WING AFTER TAKE OFF. THE ACFT RETURNED TO AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE FLAP VALVE ON THE NR2 RT FUEL TANK. PERFORMED LEAK CHECK. NO LEAKS FOUND.SDR 2011FA0000788Diaphragm · deterioratedENGINE LOST POWER IN FLIGHT, MADE A PRECAUTIONARY LANDING AND COULD NOT BE RESTARTED. PROBLEM WAS AN EXTREMELY HARDENED DIAPHRAGM IN THE ENGINE'S FLOW DIVIDER. THE DIAPHRAGM WAS SO INFLEXIBLE THAT THE FLOW DIVIDER CLOSED AND COULD NOT BE OPENED NO MATTER HOWSDR USAA2011121200012Fuel Tank · leakingCLT - FLT 876 CLT TO AUA. F/A REAR OF A/C DETECTED STRANGE ODOR THAT DID NOT DISSIPATE. MOSTLY IN REAR OF A/C. MAINTENANCE DETERMINED SOURCE OF ODOR TO BE FUEL LEAK AT LT WING DRY BAY. ACCOMPLISHED REPAIR OF LEAK. MAINTENANCE ALSO REPLACED THE LEFT ENGISDR UALA2011120806755Structure · leakingLT WING INBD DRY BAY HAS FUEL LEAK. DUE TO SEVERAL REPORTS OF LEFT WING INBOARD DRY BAY STAIN WITH LEFT TANK FUELED, ACCOMPLISH LEAK CHECK PER MM AND EVALUATE PER FIGURE 602. AFTER COMPLETING THE EVALUATION ACCOMPLISH WING DRY BAY ACCESS DOOR INSPECTION AND SDR USAA2011120700023Tank · leakingPHX FLT 702 EN ROUTE PHX TO PHL. STRONG KEROSENE ODOR OBSERVED IN COCKPIT AND CABIN AFTER ENGINE START. BOTH PACKS ON. BOTH BLEEDS ON. ISOLATION VALVE CLOSED. MX CLEANED AND RESEALED THE LT WING STRINGER TIE FITTING AT THE BULKHEAD SEPARATING THE LEFT A
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