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 UIEA2016113000945Tank · abnormalHIGH RESISTANCE BETWEEN RT MAIN TANK OVER-WING FILL PORT TO STRUCTURE. RT OVER-WING FILL PORT REMOVED AND ALL MATING SURFACES CLEANED. FILL PORT REINSTALLED IAW AMM 28-11-04-404-019 REV 119. ELECTRICAL BONDING RESISTANCE MEASURED FOUND WITHIN LIMITS..SDR UIEA2016113000944Tank · abnormalHIGH RESISTANCE BETWEEN LT MAIN TANK OVER-WING FILL PORT TO STRUCTURE. LT OVER-WING FILL PORT REMOVED & ALL MATING SURFACES CLEANED. FILL PORT REINSTALLED IAW AMM 28-11-04-404-019 REV 119. ELECTRICAL BONDING RESISTANCE MEASURED FOUND WITHIN LIMITS.SDR ASAA2016112018769O-Ring · failedTBV TARGETED REPLACEMENT. DURING LEAK CHECK FOUND PHP CAP ON FUEL PUMP LEAKING. ACFT GROUNDED. REPLACED THE O-RING ON PHP PLUG, TORQUED PER CMM 73-11-15 ITEM 4. L. ACCOMPLISHED LEAK CHECK, NO LEAKS NOTED.SDR ASMF201612011Shutoff Valve · malfunctionedDURING FUELING, A FUEL SPILLAGE IN THE LEFT TANK WAS DETECTED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. THE PLATFORM WAS CLEANED BY FIREMEN AND MAINTENANCE PERSONNEL CLOSED THE VALVE MANUALLY AND THE REFUELING SHUTOFF VALVE WAS DEFERRED BY MEL 28-10-2 CAT C. AT SDR DALA2016111808938Stiffener · crackedRT VERTICAL STIFFENER ON FWD FACE OF CENTER FUEL TANK IS CRACKED. VERIFIED WITH HFEC, MARKED. REMOVED CRACKED RT VERTICAL STIFFENER AND REPLACED WITH SERVICEABLE STIFFENER IAW SRM 51-41-05. LEAK CHECK WILL BE COMPLETED ON 72816-0100-0123.SDR 2016FA0000534Cap · separatedFUEL CAP SEPARATED FROM LEFT TIP TANK.SDR 2017FA0000418Fuel Cell · deterioratedDURING PREFLIGHT, SMALL PARTICLES WERE FOUND WHILE CHECKING THE FUEL SUMPS. ON FURTHER INVESTIGATION, IT WAS DETERMINED THAT THE EC776 SLOSHING COMPOUND INSTALLED BY THE FACTORY WAS SEPARATING FROM THE TANK. WE WERE ABLE TO REMOVE SOME PIECES THE SIZE OF ASDR DXTA2016101206319Vent · leakingAT FL280, LT WING TANK OVER FULL EICAS MESSAGE CAME ON. VISUALLY INSPECTED AND FOUND THE LEFT WING VENTING FUEL. UNABLE TO BALANCE WITH CROSSFEED . DIVERTED. ON DESCENT AT APPX 11000 FT. WING STOPPED VENTING FUEL. GAINED ACCESS TO LEFT OVER FULL SWITCH AND VESDR IPXA2016102209705Fuel Tank · corrodedINSPECTION TYPE: 3C, CENTER FUEL TANK CORRODED. REPAIRED IAW EA 011-5730-01-A6525 REV. IR AND EO MD11-5730-62225-A.SDR IPXA2016102209702Fuel Tank · corrodedINSPECTION TYPE: 3C, CENTER WING TANK CORRODED. REPAIRED IAW EA 011-5730-01-A6525 REV. IR AND EO MD11-5730-62225-A.SDR ASOA20161001056Flapper Valve · leakingTHE CREW REPORTED FUEL STREAMING FROM THE LEFT WING INFLIGHT. MAINTENANCE INSPECTED AND FOUND RIGHT WING FLAPPER VALVE DAMAGED. REPLACED THE FLAPPER VALVE AND OPERATIONAL CHECKS WERE GOOD.SDR SWAA2016100408422Vent · faultyAFTER TAKE-OFF, TOWER NOTIFIED FLIGHT CREW OF POSSIBLE SMOKE TRAILING FROM LEFT WING. NO ABNORMAL INDICATIONS NOTED. ALL FLIGHT CONTROLS NORMAL. RETURNED TO DEPARTURE SUSPECTED FUEL LEAK, NO LOSS OF FUEL NOTED FROM LEFT TANK. FIRST OFFICER NOTED FUEL ON UNDSDR AALA20160915009Seal · damagedABOUT 10-15 MINS IN FLIGHT, PASSENGER ALERTED CREW ABOUT A LEAK FROM THE LT OVERWING FUEL CAP. F/O DID VISUAL INSPECTION AND FOUND A STEADY STREAM OF FUEL LEAKING FROM LT WING CAP. AN EMERGENCY WAS DECLARED AND ACFT LANDED WITHOUT FURTHER INCIDENT. ON GROUNSDR CALA2016090895724Door · damagedFUEL PANEL DOOR SUSTAINED DAMAGE DUE TO CONTACT WITH LE SLAT ON RETRACTION. REPLACED FUEL PANEL DOOR IAW MM 57-41-37.SDR 2016FA0000399Fuel Cell · leakingNEW FUEL CELL INSTALLED, FOUND TO LEAK AT OTBD SEAM. FUEL CELL WAS REPLACED WITH REPAIRED FUEL CELL.SDR RU3A20160822011Float Valve · leakingCREW REPORTED FUEL ODOR/FUMES. FOUND LEAK COMING FROM FUEL WING FLOAT VALVE ASSEMBLY. IAW COMMUNIQUE 2012-04, REPLACEMENT KIT 101-9081-5, INSTALLED ON ACFT.SDR AALA20160812001Fuel Cap · leakingAIRCRAFT WAS GROUNDED. AIR INTERRUPT, EMERGENCY NOT DECLARED. LANDING UNEVENTFUL. DURING CRUISE A PASSENGER OBSERVED FUEL LEAKING FROM THE LT OVERWING FUEL CAP. MAINTENANCE R & R LEFT OVERWING FUEL CAP IAW AMM 28-11-04. LEAK CHECK NORMAL.SDR IPXA2016083107680Fuel Cell · corrodedINSPECTION TYPE: 3C, CENTER WING TANK UPPER AFT SKIN CORRODED AT XCW 114 ALONG STRINGER 3. REPAIRED IAW EA 011-5730-01-A6395 REV. IR AND EO MD11-5730-61653-A.SDR CALA2016071400425Cap · failedON ARRIVAL, CAPTAIN HAD SOME PHOTOS FROM FLIGHT WHICH CLEARLY SHOWED FUEL LEAKING FROM OVERWING REFUEL CAP. CAP REPLACED AND REFUEL CAP HOUSING INSPECTED WITH NO FAULTS EVIDENT, CAP REPLACED IAW MM28-11-04 AND TRANSFERRED 40,000LBS OF FUEL TO RIGHT WING FOR LSDR UIEA2016071000573Sealant · damagedFUEL LEAK ABOVE LT PACK HEAT EXCHANGER, CTR TANK AREA. CENTER TANK ENTRY PERFORMED IAW 28-11-00, REV 118, FOUND LEAK BETWEEN 2ND SPAM BEAM. SEALANT REPAIRED IAW AMM 28-11-00-308-013, REV 118, ACCESS DOORS 531BB 136KZ, CLOSED FOD CKD PERFORMED IAW AMM 28-11-0SDR IPXA2016071505878Fuel Tank · corrodedINSPECTION TYPE: 3C, MAIN CABIN UNDER FLOOR CENTER TANK UPPER SKIN HAS CORROSION AT XCW=-50 AT STR. 15.REPAIRED CORRODED CTR. WING SKIN AT STA. XCW=-50 IAW EA 011-5730-01-A6345 REV. I/R AND EO MD11-5730-61283-A. MAJOR REPAIR.SDR K11A2016062616001Fuel Tank · corrodedCORROSION ON THE FORWARD SIDE OF THE FUEL TANK AT STA 598, RBL 34.SDR 2016FA0000294Fuel Cap · pluggedPILOT EXPERIENCES A LOSS OF 500 RPM'S ON THE TAKEOFF ROLL, HE ABORTS THE TAKEOFF. HE HAS THE CARBURETORS O/H AND INSTALLED BY THE O/H SHOP. 1ST FLIGHT AFTER O/H WAS FINE, 2ND FLIGHT AFTER FUELING THE AIRPLANE, HE HAS 500 RPM DROP ON TAKEOFF ROLL, HE ABORTS TSDR XHCR2016FA0000362Fuel Cell · leakingFUEL CELL: PN 206-064-633-101, SN 85633 MANUFACTURED IN 06/20/04 WAS FOUND TO BE IN AN UNAIRWORTHY CONDITION DURING A ROUTINE 24 MONTH INSPECTION. IT IS THE METHOD OF FAILURE AND THE TRENDING OF FAILURES OF CELLS MADE BY THIS COMPANY THAT HAS SPURRED THIS REPSDR XHCR2016FA0000360Fuel Cell · leakingFUEL CELL, PN 407-362-633-101, SN 00777 MANUFACTURED IN 06/23/2006 WAS FOUND TO BE IN AN UNAIRWORTHY CONDITION DURING A ROUTINE 24 MONTH INSPECTION. IT IS THE METHOD OF FAILURE AND THE TT OF THE PART THAT HAS SPURRED THIS REPORT. THE FUEL CELL MATERIAL WAS FSDR 2016FA0000333Fuel Sys · malfunctionedDURING FLIGHT, PILOT REPORTED LOW LEVEL FUEL LIGHT CAME ON AND TURNED ON FUEL BOOST PUMP, LOW LEVEL FUEL LIGHT EXTINGUISHED. FLIGHT CONTINUED AND THEN LOW LEVEL FUEL LIGHT CAME BACK ON AND PILOT NOTICED FUEL FLOW METER NEEDLE STARTED TO FLUCTUATED AND THEN ENSDR DXTA2016060506250Float Valve · defectiveWING TANK O'FULL R CAS MSG CLIMBING THROUGH 37000' 270 KIAS WITH 30LBS FUEL IN CENTER TANK & APPROX 3100 LBS IN EACH WING TANK. VISUALLY OBSERVED FUEL VENTING. LOST 200 LBS IN 2 MINUTES. DE-FUELED ACFT, DOWN TO BE ABLE TO REMOVE OTBD WING ACCESS PANEL. REMSDR JIKA2016052301Fuel Cell · leakingEN-ROUTE THE PILOT REPORTED A STRONG FUEL ODOR FROM THE CABIN AREA. DEPRESSURIZED THE CABIN, USED OXYGEN & OPENED THE FRESH AIR VENTS, LANDED WITHOUT INCIDENT. INSPECTED THE ACFT, THE INSPECTION INCLUDED REMOVING THE CABIN FLOORBOARDS & INSPECTING FOR ANY SISDR CALA2016050495333Skin · corrodedCORROSION ON UPPER SURFACE OF CTR TANK, STATION 955.1, RLB 86. REPAIRED UPPER SURFACE OF CTR TANK, BS 955.1, RBL 86 IAW ECRA 5710-02530.SDR FDEA201605011438Skin · corrodedTOP SURFACE OF CTR WING TANK AT STATION 1224, LBL 90 - 105 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-01 VOL II FOUND TO BE OUT OF LIMITS IAW SRM 57-20-00 FIG 8A VOL I. INSPECTED AREA IAW NTSPM 06-10-01 & 06-00-03. NO DISCREPANCIES NOTED. COMPLIED WITHSDR DALA2016040402524Line · looseSTRONG JET FUEL ODOR IN AIRPLANE AFTER STARTING APU GROUND PERSONNEL POINTED OUT FUEL FROM LT SIDE OF ACFT. FOUND RT WHEEL WELL UPPER AFT FUEL LINE IN SHROUD UNSAFTIED AND LOOSE. RESECURED LINE IAW AMM 28-20. REINST SHROUD IAW AMM 28-20.SDR DALA2016040402511Line · looseSTRONG JET FUEL ODOR IN AIRPLANE AFTER STARTING APU GROUND PERSONEL POINTED OUT FUEL FROM LT SIDE OF ACFT. FOUND RT WHEEL WELL UPPER AFT FUEL LINE IN SHROUD UNSAFTIED AND LOOSE. RESECURED LINE IAW AMM 28-20. REINST SHROUD IAW AMM 28-20.SDR EVCA201603151Fuel Cell · leakingUPON PRE-FLIGHT PILOT FOUND FUEL POOLING UNDER ACFT. UPON INSPECTION FOUND THAT FUEL WAS SEEPING THROUGH THE RT FWD FUEL CELL, PN 206-063-632-102. FUEL PERMEATING THROUGH RUBBER CELL MEMBRANE.SDR DALA2016031501940Fuel Tank · corrodedLEFT CTR WING TANK UPPER SURFACE, BS 706 SKIN EXFOLIATED. REPAIRED IAW PRI 543588-14, REV 3 AND ER/A 543588, REV A.SDR JR2R03102016374Fuel Tank · crackedAFT AUX FUEL TANK CRACKED AT UPPER SKIN STIFFENER, NR 1 STRINGER, AFT END. REPAIR WAS ACCOMPLISHED IAW SRM 53-05 FIGURE 46 UNDER WO 1012616-1600 0091 & WO 00283925 M301 NR 374.SDR ASOA2016030914625Structure · corrodedFUEL TANK PANEL LAND 540BB ENTIRE SURROUND HAS CORROSION, PITTING. BLENDED AND REMOVE PITTING DAMAGES IAW SRM 51-12-00-00. COMPLIED WITH EC/TC EO 600-57-81 CW IAW REO 60R-57-21-030, REV L.SDR CA160308002Drain · damaged(CAN) THE AIRCRAFT WAS ON A 72 MONTH CHECK WHICH REQUIRED INSPECTION OF THE WING BOX UPPER SURFACE. THE AME DISCOVERED THAT THE DRAIN LINE FOR THE L/H AND R/H WING UPPER FUEL (GRAVITY FEED) CAVITY SCUPPER WAS COMPLETELY ROTTED AWAY. THE AIRCRAFT HAS 646.2 TSN.SDR DALA2016030901772Fuel Cell · damagedCENTER WING BOX FUEL TANK UPPER SKIN BS 708, RBL 50: 2 FASTENERS HOLES ELONGATED. REPAIRED CENTER WING BOX FUEL TANK UPPER SKIN AT BS 708, RBL 50, 2 FASTENER HOLES IAW PRI 540750-14, REV 0, PRI 540753-14, REV 0- REV 2 AND ER/A 540753-14, REV ORIGINAL ASSOCIATESDR J7SA20160306001Fuel Cap · defectiveDIVERTED DUE TO FUEL LEAKING FROM OVER THE WING FUELING CAP. R & R WING GRAVITY FUEL FILLER CAP. LEAK CHECKED GOOD.SDR ASAA2016030215736Fuel Cell · corrodedAFTER REMOVAL OF RT DRAG LINK ASSY. FOUND CENTER FUEL TANK SKIN CORRODED. ACFT GROUNDED. BLENDED CORRODED RT CENTER FUEL TANK SKIN, OUT OF LIMITS, IAW SRM 5710-01-1A-2, ACCOMPLISHED EA 700-57EA-16677, W-1.500, O-.304, R-.268, L-1.600, D-0.036.SDR JRAA20160229001Check Valve · leakingRIGHT FUEL TANK DUMPING FUEL INTO CTR TANK IN FLIGHT. TURNED ON CTR TANK RT BOOST PUMP & TURNED OFF RT TANK FUEL PUMPS. LANDED WITH 5400 LBS LT TANK, 4000 LBS RT TANK & 2000 LBS IN CTR TANK. FLIGHT BEGAN WITH 16000 LBS FUEL ON BOARD & CTR TANK ALMOST EMPTY.SDR DALA2016022201276Fuel Tank · corrodedLEFT WHEEL WELL TO RT WHEEL WELL FUEL TANK SKIN PLANK PANEL T/E CORRODED AT SEVERAL LOCATIONS. CLEAN/ EVAL, TREAT & PAINT REF OR NRC 62937-0100-0065. BLENDED OUT CORROSION ON RT WHEEL WELL FUEL TANK SKIN PLANK PANEL. MEASURED THICKNESS LOSS OF .015 TAG 3310SDR ASOA20160211007HFlapper Valve · leakingATC ADVISED THE CREW THAT FUEL WAS LEAKING OUT OF THE WING DURING CLIMBOUT. THE ACFT RETURNED, WHERE OT LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE RT WING OTBD FLAPPER, CHECK, VALVE, LEAK CHECKED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURNSDR CA160208006Light · failed(CAN) THE FUEL SHUT-OFF TANK 1 LIGHT ON THE REFUEL/DEFUEL PANEL WAS NOTED AS WEAK AND INTERMITTENT, AND A WISP OF SMOKE WAS OBSERVED. THE REFUEL/DEFUEL PANEL WAS REPLACED AND SATISFACTORY CHECKS CARRIED OUT.SDR KO0R201601260041Skin · corrodedEVIDENCE OF CORROSION ON THE CTR WING TANK UPPER SURFACE AT STATION 1229, RBL 84.SDR KO0R201601260040Skin · corrodedEVIDENCE OF CORROSION ON THE CTR WING TANK UPPER SURFACE AT STATION 1229, RBL 78.SDR EVGR201601280001Fuel Tank · leakingDURING A 100 HR. INSPECTION THE LT FUEL TANK WAS REMOVED TO ACCESS A SEEPING HYDRAULIC FITTING. WHEN THE TANK ASSY WAS REMOVED, FUEL STAINS WERE SEEN ON THE LOWER FRONT EDGE OF THE TANK ASSY. THE END SECTION OF THE FUEL TANK WAS REMOVED, MORE FUEL STAIN WAS SDR SWAA2016012748433Cap · leakingFUEL LEAKED ON TOP OF LT WING. R & R LT CAP IAW MM.SDR AALA20160201001Skin · corrodedAIRCRAFT WAS IN BASE MX. CORROSION ON UPPER SURFACE OF CTR FUEL TANK, UPPER SKIN AT FS 955 & BL 0. REPAIRED SKIN IAW SRM 51-10-02 & EA 257525 DATED 01 29 2016.SDR DALA2016012100481Fuel Tank · corrodedTHE UPPER LT EXTERNAL SURFACE OF THE CENTER WING FUEL TANK HAS AREAS OF CORROSION FROM BS 696 TO 737, LBL 30 TO FUSELAGE SKIN. AREAS MARKED. REF 63165-0100-0187. BLENDED AND REMOVED CORROSION ON UPPER SKIN IAW SRM 57-10-01. MATERIAL REMOVED .010 IN SKIN IS WI
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