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 IPXA11564127Clamp · corrodedINSPECTION TYPE:C1, FUEL PANEL 631AB, 631BB, 631CB, 641BB, 641CB, 641DB, 641JB, 641KB, 641LB CLAMP RINGS ARE CORRODED. REPLACE CLAMP RING 641KB IAW AMM.SDR IPXA11564126Clamp · corrodedINSPECTION TYPE:C1, FUEL PANEL 631AB, 631BB, 631CB, 641BB, 641CB, 641DB, 641JB, 641KB, 641LB CLAMP RINGS ARE CORRODED. REPLACE CLAMP RING 641JB IAW AMM.SDR IPXA11564125Clamp · corrodedINSPECTION TYPE:C1, FUEL PANEL 631AB, 631BB, 631CB, 641BB, 641CB, 641DB, 641JB, 641KB, 641LB CLAMP RINGS ARE CORRODED. REPLACE CLAMP RING 641DB IAW AMM.SDR IPXA11564124Clamp · corrodedINSPECTION TYPE:C1, FUEL PANEL 631AB, 631BB, 631CB, 641BB, 641CB, 641DB, 641JB, 641KB, 641LB CLAMP RINGS ARE CORRODED. REPLACE CLAMP RING 641CB IAW AMM.SDR IPXA11564121Clamp · corrodedINSPECTION TYPE:C1, FUEL PANEL 631AB, 631BB, 631CB, 641BB, 641CB, 641DB, 641JB, 641KB, 641LB CLAMP RINGS ARE CORRODED. REPLACE CLAMP RING 631CB IAW AMM.SDR IPXA11564120Clamp · corrodedINSPECTION TYPE:C1, FUEL PANEL 631AB, 631BB, 631CB, 641BB, 641CB, 641DB, 641JB, 641KB, 641LB CLAMP RINGS ARE CORRODED. REPLACE CLAMP RING 631BB IAW AMM.SDR IPXA11564118Clamp · corrodedINSPECTION TYPE:C1, FUEL PANEL 631AB, 631BB, 631CB, 641BB, 641CB, 641DB, 641JB, 641KB, 641LB CLAMP RINGS ARE CORRODED. REPLACE CLAMP RING 631AB IAW AMM.SDR IPXA11564117Clamp · corrodedINSPECTION TYPE:C1, FUEL PANEL 531AB, 531CB, 541AB, 541BB,541CB,541EB CLAMP RINGS ARE CORRODED. REPLACE CLAMP RING 541EB IAW AMM.SDR IPXA11564116Clamp · corrodedINSPECTION TYPE:C1, FUEL PANEL 531AB, 531CB, 541AB, 541BB, 541CB, 541EB CLAMP RINGS ARE CORRODED. REPLACE CLAMP RING 541CB IAW AMM.SDR IPXA11564115Clamp · corrodedINSPECTION TYPE:C1, FUEL PANEL 531AB, 531CB, 541AB, 541BB, 541CB, 541EB, CLAMP RINGS ARE CORRODED. REPLACE CLAMP RING 541BB IAW AMM.SDR IPXA11564113Clamp · corrodedINSPECTION TYPE:C1, FUEL PANEL 531AB,531CB,541AB,541BB,541CB,541EB CLAMP RINGS ARE CORRODED. REPLACE CLAMP RING 541AB IAW AMM.SDR IPXA11564112Clamp · corrodedINSPECTION TYPE:C1, FUEL PANEL 531AB,B531CB,541B,541BB,541CB,541EB CLAMP RINGS ARE CORRODED. REPLACE CLAMP RING 531CB IAW A.SDR IPXA11564111Clamp · corrodedINSPECTION TYPE:C1, FUEL PANEL 521AB, 521CB, 541AB, 541BB, 541CB, 541EB CLAMP RINGS ARE CORRODED. R & R CLAMP RING 531AB IAW AMM.SDR IPXA11564103Panel · corrodedINSPECTION TYPE:C1, FUEL CELL PANEL 642CB CORRODED. REPLACE IAW SRM.SDR 2011FA0000012Fuel Tank · crackedLT AUX FUEL TANK LEAKS AT MULTIPLE SPOT WELDS. THIS IS THE FOURTH CRACKED AND LEAKING AUX TANK (LT OR RT) WE HAVE CHANGED IN OUR FLEET.SDR SIMA201100301Receptacle · leakingON FLIGHT 2750 THE CREW REPORTED THAT AFTER THE ENGINE START/SHUT DOWN OF APU, FUEL ODOR WAS DETECTED IN THE COCKPIT. THE ODOR THEN DISAPATED. EN ROUTE A HINT OF FUEL ODOR RETURNED. THE FLIGHT ATTENDANT REPORTED NO ODOR IN CABIN. THE AIRCRAFT WAS REMOVED FSDR CA101220011Fuel Cell · leaking(CAN) . ACFT PARKED STATIC INSIDE HANGER. FUEL LEAKS THROUGH FUEL CELL MATERIAL. REPLACED.SDR CA110103007Fitting · disconnectedWHILE INSPECTING TANK FOR A SUSPECTED LEAK, IT WAS NOTED THAT THE FUEL FILLER FITTING ON THE INBOARD FILLER HAD BECOME DETACHED FROM THE TANK. A WHITE FLAKEY RESIDUE WAS OBSERVED INSIDE THE TANK AND IS SUSPECTED OF BEING THE GLUE USED TO BOND THE METAL FITTINGSDR DXTA2010121904368Fuel Cell · leakingDURING CLIMB, FUEL OBSERVED LEAKING FROM UNDER LT WING. FUEL WAS TRANSFERRING FROM FUSELAGE TANKS AND WING FUEL GAUGES, INDICATED FULL LEVELS. DURING DESCENT, FUEL LEAKAGE APPEARED TO STOP, APPROX 15 MINUTES AFTER INITIAL DISCOVERY OF LEAK. INSTALLED NEW PILSDR FDEA201012104632Fuel Cell · corrodedCTR FUEL TANK UPPER SURFACE HAS CORROSION UNDER STUB BEAM ATTACHMENTS AT STA940, RBL64. ACCOMPLISHED WING-CTR-UPPER SKIN PLANK CORROSION REPAIR, WS 18, RBL 65, IAW EA F-5710-146245, STEPS 1-10. REF FAA FORM 8100-9, DATED 03/11/2011. CAT. "A" MAJOR REPAIR.SDR CA101217001Fuel Tank · cracked(CAN) ANTI CHAFE RUBBER STRIPS UNBONDED FROM STRAPS LOOSENING TENSION ON TANK. TANK MOVEMENT IN WING CAVITY CAUSED A FATIGUE CRACK WHERE FILLER NECK WAS WELDED TO TANK SINCE FILLER IS SCREWED TO STRUCTURAL PANEL (UPPER WING SKIN). FUEL LEAK WHEN TANK WAS FILLESDR NX4R00003Fuel Tank · crackedDURING AN ANNUAL INSP, THE TECH NOTICED A WET FUEL STAIN UNDER THE LT AUX FUEL TANK. WHEN THE TANK WAS REMOVED, THE TANK WAS FOUND TO BE CRACKED AROUND SEVERAL OF THE AFT SPOT WELD LOCATION ON THE LOWER AFT SURFACE OF THE TANK.SDR C2XA10TY186Tank · gougedBOTTOM CENTER OF VENTRAL TANK IS GOUGED FROM FAIRING. REPAIRED GOUGE AND REWORKED FAIRING IAW EC2810-01053.SDR NX4R00006Fuel Cell · crackedDURING AN ANNUAL INSP, THE TECH NOTICED A WET FUEL STAIN UNDER THE RT AUX FUEL TANK. WHEN THE TANK WAS REMOVED, THE TANK WAS FOUND TO BE CRACKED AROUND SEVERAL OF THE AFT SPOT WELD LOCATION ON THE LOWER AFT SURFACE OF THE TANK.SDR CHQA201000213Unknown · leakingDURING CLIMB A PASSENGER REPORTED SEEING FLUID LEAKING FROM THE LEFT WING AND RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE PERFORMED A VISUAL INSPECTION WITH NO DEFECTS NOTED, INSPECTED ALL FUEL PANELS FOR LEAKS WITH NONE NOTED, AND PERFORMED LEAK CHECK OFSDR CA101122028Baffle · detachedBAFFLE DIVIDING FORWARD AND AFT SECTIONS OF FUEL CELL, FOUND DETACHED. FUEL IS ABLE TO MOVE AROUND POTENTIALLY CAUSING C OF G ISSUES. IN LOW FUEL SITUATIONS, SLOSHING FUEL MAY CAUSE SUPPLY TO THE PUMPS TO DIMINISH, POTENTIALLY CAUSING ENGINE FUEL STARVATION. SDR NX4R20101118001Tank · cracked(N3XR) DURING AN ANNUAL INSP, THE TECH NOTICED A WET FUEL STAIN UNDER THE LT AUX FUEL TANK. WHEN THE TANK WAS REMOVED, THE TANK WAS FOUND TO BE CRACKED AROUND SEVERAL OF THE AFT SPOT WELD LOCATION ON THE LOWER AFT SURFACE OF THE TANK.SDR IXXA10SMN112SWeb · crackedDURING ROUTINE C-CHECK INSP FOUND NR 3 MAIN TANK WEB CRACKED AT STATON XRS 168.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED STRAP, SHIMS, SPLICES, FILLER, ANGLE, TEE, AND FISDR DXTA2010111104304Fuel Sys · unknownDURING CLIMBOUT TROUGH 9500 FT, NOTICED STEADY STREAM OF FUEL LEAK FROM UNDER THE LT WING. ABOUT 2 MIN LATER THE LEAK STOPPED. CONNECTED FUEL HOSE AND TRANSFERED FUEL TO FUSELAGE TANKS. FILLED LT WING. LET PUMP RUN TO CHECK FOR FUEL BYPASS INTO SURGE TANK. SDR DXTA2010111004303Fuel Cell · overservicedDURING CLIMBOUT THROUGH 8000 FT, NOTICED A STEADY STREAM OF FUEL COMING FROM UNDER THE LT WING. DURING RETURN TO AIRPORT, NOTICED THE STREAM STOPPED AS ACFT LEVELED OFF AT 5000 FT. FOUND FUEL CELL OVERSERVICED.SDR SIMA201031203Valve · leakingON FLIGHT 2813 THE CREW REPORTED VIA LOG PAGE THAT AFTER TAKEOFF ANOTHER AIRCRAFT REPORTED A WHITE TRAIL COMING FROM THE RIGHT SIDE OF THE AIRCRAFT. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED SAFELY WITHOUT INCIDENT. SDR NX4R00005Fuel Tank · crackedDURING AN ANNUAL INSP, THE TECH NOTICED A WET FUEL STAIN UNDER THE RT AUX FUEL TANK. WHEN THE TANK WAS REMOVED, THE TANK WAS FOUND TO BE CRACKED AROUND SEVERAL OF THE AFT SPOT WELD LOCATION ON THE LOWER AFT SURFACE OF THE TANK.SDR CA101115019Bushing · corroded(CAN) FUEL SUMP DRAIN BUSHING CORRODED AT FUEL DRAIN COCK. FUEL SUMP ASSEMBLY REPLACED WITH NEW UNIT.SDR CA101104013Bushing · corroded(CAN) REAR FUEL CELL SUMP PANEL HAS A CORRODED SUMP DRAIN PLUG BUSHING. PANEL REPLACED WITH NEW UNIT.SDR ASAA1058462Packing · leakingRT AND LT MAIN FUEL TANK SUMP DRAIN VALVES LEAKING. REPLACED PRIMARY DRAIN SEAL O-RING ON RT AND LT MAIN FUEL TANK SUMP DRAIN VALVES REF MM 28 11 61 600 80. OP AND LEAK CHEAK GOOD.SDR CA101103005Screw · failed(CAN) FUEL CAP RETAINING SCREW LOOSENED AND CAP SEPARATED PERMITTING INTERNAL PARTS OF THE FUEL CAP TO FALL INTO THE FUEL TANK. THE FUEL CAP AND SCREW WAS FOUND ON THE RUNWAY. THE AIRCRAFT WAS CONDUCTING NIGHT CIRCUITS AT THE TIME OF THE OCCURRENCE.SDR AALA20101027MIA01Screw · looseMIA - FUEL REPORTED COMING FROM LEFT WING AFTER TAKEOFF. EMERGENCY DECLARED RETURNED MIA LANDED WITHOUT INCIDENT. TRANSFERRED FUEL OUT OF AND INTO LEFT AND RIGHT MAIN TANKS TO VERIFY PROPER VALVE OPERATION. ALL OK. FOUND EVIDENCE OF FUEL SEEPAGE AROUND LEFSDR CA101027001Fuel Tank · cracked(CAN) DURING INSPECTION AUXILIARY FUEL TANK LT FOUND LEAKING. TANK FOUND CRACKED AT WELDS FWD OF REAR MOUNTING STRAP, LOWER SIDE TANK.SDR QMLA2010102410069Fillercap · missingWHILE IN FORWARD FLIGHT, CREW DETECTED STRONG ODOR OF FUEL. AFTER AN UNSCHEDULED LANDING AND VISUAL INSPECTION OF ACFT FOUND THAT THE FUEL FILLER CAP WAS MISSING NEW FUEL CAP INSTALLED ACFT RETURN TO SERVICE.SDR UALA2010101903865Drain Valve · leakingRIGHT TANK FUEL SUMP HAS FUEL SEEP AT OUTER CIRCUMFERENCE. REPLACED RT TANK SUMP DRAIN VALVE. OPS NORMAL.SDR CA101116008Valve · torn(CAN) THE C156003-0101 FUEL CAP HAS A RED/ORANGE ONE WAY VENT GASKET LOCATED ON THE BOTTOM OF THE FUEL CAP. THE PART NUMBER FOR THIS VENT GASKET IS NO LONGER AVAILABLE FROM CESSNA. INVESTIGATION REVEALED THAT THE VENT GASKET WAS COMPROMISED ON BOTH INBOARD ASDR NX4R00004Fuel Tank · crackedDURING THE PREFLIGHT INSP, THE PILOT NOTICED A WET FUEL STAIN UNDER THE RT AUX FUEL TANK. WHEN THE TANK WAS REMOVED, TANK WAS FOUND TO BE CRACKED AROUND SEVERAL OF THE AFT SPOT WELD LOCATION ON THE LOWER AFT SURFACE OF THE TANK.SDR NX4R0004AAFuel Tank · crackedDURING A PREFLIGHT INSP, A WET FUEL STAIN WAS OBSERVED BELOW THE RT AUX FUEL TANK. THE FUEL TANK WAS FOUND TO BE CRACKED ALONG THE ROW OF SPOT WELDS. THE FUEL TANK WAS REPLACED WITH PN-D60-2814-12-00.SDR NX4R20101004001Tank · crackedDURING AN ANNUAL INSP, THE TECH NOTICED A WET FUEL STAIN UNDER THE LT AUX FUEL TANK. WHEN THE TANK WAS REMOVED, THE TANK WAS FOUND TO BE CRACKED AROUND SEVERAL OF THE AFT SPOT WELD LOCATION ON THE LOWER AFT SURFACE OF THE TANK.SDR UALA2010100403660Fuel Tank · leakingRAMP REPORTED FUEL COMING OUT OF FWD SMALL HOLE ON APU DRAIN MASK. WHILE IN STAB COMPARTMENT, OBSERVED RUNNING FUEL LEAK (ALMOST A STEADY STREAM) FROM THE AFT LT CORNER OF CTR SECTION OF STABILIZER TANK. FUEL IS EXITING ACFT FROM FUSELAGE DRAINS AND DRAIN HOSDR FDEA201010023863Panel · corrodedRIGHT WING FUEL TANK PANEL 641DB CORROSION FOUND IN THE EXTERNAL SKIN AREA THROUGHOUT. RH WING TANK PANEL 641 DB REMOVED AND REPLACED IAW AMM 28-11-01-4 REV. 98. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 2010FA0001117Fuel Cell · corroded(MTND) CORROSION IN RT FEEDER TANK BY ENGINE JET PUMP MOUNT AREA, FOUND ON INSP CARD ZL-621-01-1 FOR ZONE INSPECTION. THE CORROSION WAS LOCATED UNDER THE JET PUMP BETWEEN RIBS 4 RT AND 5 RT AND BETWEEN STIFFENERS 8 AND 9. POSSIBLE CAUSE WOULD BE WATER CONTAMSDR 2010FA0001116Fuel Cell · corroded( MTVD) CORROSION IN LT FEEDER TANK BY ENGINE JET PUMP MOUNT AREA, FOUND ON INSP CARD ZL-521-02-1 FOR ZONE INSPECTION. THE CORROSION WAS LOCATED UNDER THE JET PUMP BETWEEN RIBS 4LT AND 5LT AND BETWEEN STIFFENERS 8 AND 9. POSSIBLE CAUSE WOULD BE WATER CONTAMISDR SIMA201026704Unknown · contaminatedFOR FLIGHT 4458 WHILE AT THE GATE WITH PASSENGERS BOARDED THERE WAS A NOTICEABLE FUEL ODOR APPARENT TO PASSENGERS AND FLIGHT CREW WITH ENGINES AND APU NOT RUNNING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AND FOUND RESIDUAL FUEL UNDER FLOOR BOARDS BESDR UALA2010092103501Cap · leakingLT OVER WING FUEL LEAK, FLIGHT DIVERTED. REPLACED LT OVERWING FUEL CAP.
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