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 CALA2017082102808Fuel Cell · corrodedMAIN CABIN CENTER FUEL BOX UPPER SURFACE HAS CORROSION AT BS 980, LBL 60. BLENDED DAMAGED SECTION OF UPPER SKIN PANEL AND REPAIRED MAIN CABIN CENTER FUEL BOX UPPER SURFACE BS 980 LBL 60 IAW UNITED ECRA 5710-02614SDR IPXA2017081820654Web · crackedINSPECTION TYPE: SV, RT WW OVERWING UPPER FUEL TANK AFT WEB IS CRACKED AT BS 1372 AND RBL 80. REPAIRED THE WEB IAW EA 011-5710-01-A6940, REV I/R, AND EO MD11-5710-65307-A. MAJORSDR IPXA2017081820653Web · crackedINSPECTION TYPE: SV, LT WW OVERWING UPPER FUEL TANK AFT WEB IS CRACKED AT BS 1372 AND LBL 80. REPAIRED THE WEB IAW EA 011-5710-01-A6940, REV I/R, AND EO MD11-5710-65307-A. (MAJOR)SDR QMLA2017080317076Panel · delaminatedON REMOVAL OF LOWER FUEL CELL INSPECTION PANELS, DISCOVERED THE LOWER RT FUEL CELL WAS LEAKING FUEL AT THE FWD AND AFT FUEL PROBE PANELS. FUEL PROBE PANELS ARE DELAMINATING FROM THE MAIN FUEL CELL.SDR DALA2017071205367Skin · corrodedCORROSION ON CTR FUEL TANK SKIN STA Y=742 BTW X=-20 TO X=-60 AT RT WHEELWELL SLANT PANEL AREA AMDS 5300-2003. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.SDR DALA2017071205366Skin · corrodedCORROSION ON CENTRAL FUEL TANK SKIN BELOW SLANT PANEL STA Y=742 BTW X=18 TO X=25 LT WHEEL WELL AMDS 0593-2002. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.SDR DALA2017071205365Skin · corrodedCORROSION ON CENTER FUEL TANK UPPER SKIN FROM Y=737 TO Y=756, X=22 TO X=60, ALSO Y=705-710, X=-56 TO X=-60 AT CABIN PAX WING BOX AREA AMDS 5300-2008. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.SDR CALA2017062601979Seal · failedON TAKE OFF ROLL TOWER REPORTED POSSIBLE FUEL LEAK FROM LEFT WING. DISPATCH ADVISED CREW TO RUN QRH PAGE 120.3 WITHIN 5 MINUTES 100LB DIFFERENCE BETWEEN LEFT AND RIGHT WINGS. FOUND SEAL AT THE LT VENT SCOOP ACCESS PANEL 533BB FAILED. REMOVED AND REPLACED THESDR 2017FA0000250Fuel Cap · brokenWING FUEL CAP INTERNAL BLACK PLASTIC RIB BREAKS OFF INSIDE THE LOWER FUEL CAP RETAINER ASSEMBLY.SDR 2017FA0000249Fuel Cap · brokenWING FUEL CAP INTERNAL BLACK PLASTIC RIB BREAKS OFF INSIDE THE LOWER FUEL CAP RETAINER ASSEMBLY.SDR 2017FA0000248Fuel Cap · brokenWING FUEL CAP INTERNAL BLACK PLASTIC RIB BREAKS OFF INSIDE THE LOWER FUEL CAP RETAINER ASSEMBLY.SDR IPXA2017062618633Structure · chafedINSPECTION TYPE: 3C, RT WING FUEL TANK LOWER SKIN UPPER SURFACE IS CHAFED. REPAIRED FUEL TANK IAW EA 011-5730-01-A6850, REV I/R, AND EO MD11-5730-64672-A.SDR IPXA2017062618624Stringer · crackedINSPECTION TYPE: 3C, CENTER FUEL TANK STRINGER 47 IS CRACKED AT RBL 46.5. REPAIRED THE STRINGER IAW SRM 57-10-03, REPAIR 1, FIG 201. MAJORSDR ASOA201705163176Flapper Valve · leakingTHE CREW REPORTED A SUSPECTED FUEL LEAK FROM MID RIGHT WING ON CLIMBOUT. MAINTENANCE FOUND FLAP VALVE AT RIB 19 ON RIGHT WING DAMAGED. THE FLAP VALVE WAS REPLACED IAW 28-11-04. LEAK CHECKED GOOD.SDR SWAA2017051713797Gasket · damagedAIR TURNBACK, ON CLIMB OUT TOWER ADVISED OF FLUID COMING OUT OF LEFT SIDE OF AIRCRAFT. R&R LT WING SURGE TANK ACCESS PANEL 53BB GASKET IAW MM.SDR QMLA2017050817050Fuel Cell · leakingIN FLIGHT CREW REPORTED AN ODOR OF FUEL THROUGHOUT THE CABIN. AIRCRAFT WAS INSPECTED AND FOUND THAT THE LT FORWARD FUEL CELL HAD A SMALL PIN HOLE SIZE LEAK AROUND THE FORWARD FUEL QUANTITY PROBE MOUNT FLANGE RUBBER SEAM. THE RT FORWARD FUEL CELL APPEARS DRY HSDR DALA2017040602823Float Valve · wornRETURNED TO DEPARTURE DUE TO A FUEL STREAM COMING OUT OF THE RIGHT WING VENT. PERFORMED RIGHT WING TANK FLOAT VALVE INSPECTION AND FOUND PLAY. REPLACED FLOAT VALVE. ACFT RETURNED TO SERVICE.SDR 2017FA0000251Fuel Cap · brokenWING FUEL CAP INTERNAL BLACK PLASTIC RIB BREAKS OFF INSIDE THE LOWER FUEL CAP RETAINER ASSEMBLY.SDR JZRR2015011200004Adapter · corrodedWHILE COMPLETING AN ANNUAL INSPECTION, REMOVED FUEL CAPS TO INSPECT THE CAPS, SEALS AND ADAPTERS. FOUND THE LEFT WING MAIN TANK FUEL CAP ADAPTER HEAVILY CORRODED AND PITTED. WITH THE EXTENT OF CORROSION ON THE ADAPTER, THE CAP WOULD NOT SEAL ALLOWING WATER TO SDR DALA2017032402453Fuel Tank · corrodedCORROSION ON CENTER FUEL TANK, BETWEEN BS 898 AND 902, LBL 56. REPAIRED IAW ERA 555641-14AD.SDR DALA2017032402452Fuel Tank · corrodedCORROSION ON CENTER FUEL TANK BS 926, LBL 56. REPAIRED IAW ERA 555641-14AD.SDR HALA201703110060Actuator · faultedDURING CRUISE, AN ECAM MESSAGE. FUEL OUTER TO INNER FAULT. APROX 50 MIN FROM LANDING. FOLLOWED ECAM ACTIONS. T/S IAW TSM 28-26-00-810-806A. REMOVED AND REPLACED LT INNER TANK TRANSFER VALVE IAW AMM 28-31. OPS CHECK ACTUATOR.SDR QXEA2017032100145Channel · corrodedBROKEN ANCHOR NUTS UNDER FUEL PANEL 522BT. REMOVED AND REPLACED GANG CHANNEL PN 85713239-005 AT DISCREPANT LOCATION IAW SRM 51-42-05-02 AND DWG 85713239 REV D.SDR DALA2017030501766Skin · corrodedMLG & W/W, CORROSION ON CENTER TANK UPPER SKIN AFT EDGE BTW STA 755 Z=-9 FROM X=O TO X=-53. AS VIEWED FROM RT FWD BULKHEAD. CORROSION ON UPPER SKIN OF CENTER FUEL TANK WAS REMOVED PER ETI 17-17-032 REV 2 AND ER/A 555628-14 REV ORIGINAL.SDR 2017FA0000384Bladder · leakingFUEL BLADDER LEAKS FROM OVER 15 LEAKS, FUEL BLADDER MATERIAL ACTUALLY POROUS UNDER AIR PRESSURE TEST. FUEL WEEPING FROM ALL 6 SIDES OF THE TANK. FOUND LEAK DURING ANNUAL INSPECTION.SDR DALA2017030501767Skin · corrodedMLG & W/W, CORROSION ON CENTER TANK UPPER SKIN AFT EDGE BTW STA STA 755 Z=-9 FROM X=O TO X=-53. AS VIEW FROM LT FWD BULKHEAD. CORROSION ON UPPER SKIN OF CENTER FUEL TANK WAS REMOVED PER ETI-17-17-032 REV 2 AND ER/A 555628-14 REV ORIGINAL.SDR DALA2017030101639Skin · corrodedTO ACCOMPLISH REMOVAL OF CORROSION ON CENTER TANK UPPER SKIN, CUT/REPAIR WEB/ANGLE AS REQUIRED FROM STA Y=727, 737, AND X=0. AREA WAS REPAIRED ON CENTER TANK UPPER SKIN (WEB/ANGLE) FROM STA Y=726, 755, AND X=0 PER 51-70-11 2R, 51-40-02, AND 51-40-05.SDR DALA2017030101636Skin · corrodedRT MLG WHEEL WELL CORROSION ON CTR FUEL TANK SKIN STA Y=755 AND X=-50 AT SLANT PRESSURE PANEL AREA 5310-2003 (FYT). CORROSION WAS ATTENDED PER ETI-17-17-022 REV 4 AND ER/A 554158-14 REV ORIGINAL.SDR CALA2017022700505Fuel Cell · overservicedFUEL COMING FROM RIGHT WING TIP AND F/A REPORT FUEL ODOR IN GALLEYS. TANK WAS OVERSERVICED AND FUEL CAME FROM SURGE TANK DURING TAXI, REDISTRIBUTED FUEL. NO DEFECTS NOTED TANK WAS OVERSERVICED AND FUEL CAME FROM SURGE TANK DURING TAXI, REDISTRIBUTED FUEL. NO SDR EPUA20170221001Insert · bentDURING FLIGHT, FUEL PRESSURE ON NR 2 ENGINE TO BE UNSTABLE AND LOW. ELECTED TO SHUTDOWN ENGINE AND FEATHER PROP. MADE UNEVENTFUL LANDING. MX INSPECTED THE AIRCRAFT AND DETERMINED RT HAND OUTBOARD FUEL CAP ADAPTER INSERT ASSEMBLY WAS DEFECTIVE AND BENT WHICHSDR ZP7A201702200001Fuel Sys · leakingFUEL LEAK NOTICED FROM RIGHT WING TIP. DECISION WAS MADE TO RETURN TO DEPARTURE.SDR 2017FA0000071Cap · failedDURING THE REMOVAL OF THE LOCKING FUEL CAP FOR SERVICE, LOCK TUMBLER CAME OUT OF CAP. WHILE PULLING CAP OFF, THE ASSEMBLY CAME APART, MANY PARTS DROPPING INTO THE FUEL FILLER NECK AND DOWN INTO THE TANK. FULL DEFUEL AND TANK INSPECTION WAS NEEDED TO FIND AND RSDR DALA2017021701306Fuel Tank · crackedA CRACK WAS FOUND OF 1.450" ON RH CENTER TANK LOWER AFT SKIN BETWEEN STRINGER 17 AND XCW= 15.0. REPAIR IAW ER/A 554113-14AD REV. ORIGINAL.SDR 3HDR2017021500001Tube · leakingFUEL WAS REPORTED DRIPPING FROM THE LOWER CENTER FUSELAGE AREA. FURTHER INVESTIGATION FOUND THE LOWER FUEL ELECTRICAL ISOLATOR TUBE LEAKING BETWEEN THE BONDED AREA OF THE METAL FERRULE AND THE OUTER SURFACE OF THE TUBE. FOLLOWING THE REPLACEMENT OF THE ELECTRSDR IPXA2017020813816Fuel Tank · corrodedINSPECTION TYPE: 3C, CENTER WING TANK UPPER SKIN HAS CORROSION AT RBL 89 TO 101.5 AT STRINGER 15. REPAIRED IAW EA 011 5730-01-A6596 AND EO MD11-5730-63200-A. (MAJOR)SDR DALA2017010600158Fuel Tank · corrodedCABIN AREA CENTER TANK UPPER SURFACE AT BS 955 LBL 70 FOUND CORRODED. REPAIRED IAW ERA 551294.SDR DALA2017011800447Skin · corrodedCORROSION LEVEL: 2 CABIN AREA CENTER TANK UPPER SURFACE AT STA 955 RBL 70 CORRODED AND REPAIRED PER ERA 551298-14.SDR DALA2017011800446Fuel Cell · corrodedBS 955, RBL 88.5 CENTER TANK CORRODED. REPAIRED IAW ERA 551296-14.SDR DALA2017011800445Fuel Cell · corrodedCABIN AREA CENTER TANK UPPER SURFACE AT BS 955, LBL 88 FOUND CORRODED. COMPLIED WITH ERA 551297-14.SDR DALA2017010900161Fuel Tank · corrodedCABN AREA CENTER TANK UPPER SURFACE AT BS 955 RBL 88, FOUND CORRODED. REPAIRED IAW ERA 551296-14.SDR SWAA201701051978Fuel Tank · leakingFOUND FUEL LEAK AT FASTENER IN CENTER WING TANK LOWER SKIN AT BS 612, RBL 1. REPAIRED FUEL TANK IAW SWA EA.SDR SWAA2017010510978Valve · leakingDIVERSION, KEEL BEAM FUEL LEAK ODOR IN CABIN. R&R NR 2 VALVE PER MM.SDR ASAA2016122719172Compensator · no testDURING ACCOMPLISHMENT OF FUEL QUANTITY INDICATION SYSTEM, NR 1 TANK AND COMPENSATOR UNITS TESTING IAW TASK CARD NG-28FCD-18088-1, FOUND COMPENSATORS, F1, F7 AND F8 BAD. ACFT GROUNDED. REPLACED THE PROBES IAW AMM 28-41-21-000/400-801. ALL PROBES CHECKED GOOD.SDR DXTA2016121706344Fuel Tank · contaminatedON FINAL, HAD A LT LOW FUEL PRESSURE CAS MESSAGE, LT ENG BOOST ON CAS MESSAGE & LEFT FUEL BOOST PUMP SWITCH LIGHT ON. THE LEFT ENGINE SHUT DOWN AND DID NOT RELIGHT. ON LANDING, HAD AN AMBER LT ENG CONTROL FAULT' CAS MESSAGE. REMOVED LT AND RT ENGINE FUEL FSDR AALA20161215008Valve · faultyAIRCRAFT NOT GROUNDED. FUEL ODOR IN COCKPIT LASTING THE ENTIRE FLIGHT AND INCREASING IN INTENSITY DURING POWER CHANGES. REMOVED AND REPLACED WATER DRAIN OUTER VALVE FOR LEFT CENTER TANK IAW AMM 28-11-41. OPERATIONAL CHECK GOOD.SDR 2A6R20161213001Fuel Cell · damagedSENT LEFT LOWER FUEL CELL P/N 109-0900-40-201, S/N 99000 OUT FOR CLEANING AND INSPECTION, FUEL CELL WAS RETURNED REPAIRED WITH ONE BLANKING PLATE HOLE MISALIGNED, UNABLE TO USE FUEL CELL, WILL RETURN FOR REPAIR OR REPLACE FUEL CELL WITH SERVICEABLE PART.SDR 2016FA0000626Fuel Tank · leakingFUEL DOES NOT FEED FROM RIGHT WING 17GAL. TANK. 2 FINGER SCREENS IN RT. TANK 1/4 CUP OF DEBRIS REMOVED NEW SCREENS INSTALLED. FUEL GRAVITY FEEDS FROM WINGS TO A HEADER TANK. NO VALVES IN THE TANK LINES. FORCED TO LAND WHEN LEFT WING IS EMPTY AND RIGHT WING FUSDR UIEA2016112200873Screen · damagedFUEL TANK SCREEN IN THE RT WING DAMAGED. REMOVED AND REPLACED SCAVENGE SYSTEM PICK-UP SCREEN. SEALED SCREEN TO LOWER SKIN OF FUEL TANK IAW AMM 28-11-00-300-060 AND CLAMPED SCREEN TO THE SYSTEM LINES IAW 20-10-11-964-001.SDR UIEA2016112200874Screen · damaged1 EA FUEL TANIC SCREEN INT THE LT WING DAMAGED. REMOVED AND REPLACED SCAVENGE SYSTEM PICK-UP SCREENS ON R/H. SEALED SCREEN TO LOWER SKIN OF FUEL TANK IAW AMM 28-11-00-300-060 AND CLAMPED SCREEN TO THE SYSTEM LINES IAW AMM 20-10-11-964-001.SDR UIEA2016112200900Seal · wornCENTER FUEL TANK PANEL HAS ONE WORN SEAL. REMOVED ABD REPLACED THE FUEL TANK PANEL SEAL IAW AMM 28-11-10-908-001 THROUGH STEP 1.
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