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 ALG2003F00037Fuel Cap · bentDURING PREFLIGHT, PILOT DISCOVERED WATER IN THE FUEL SAMPLE, THE MECHANIC DEFUELED THE AIRCRAFT AND REMOVED AND REPLACED THE AIRFRAME FUEL FILTER, FUEL NOZZLE, FUEL CAP, FUEL LINES WERE FLUSHED WITH FRESH FUEL, THE MECHANIC DETERMINED THE OLD FUEL CAP WAS SLIGSDR USAASA02091Drain Valve · leakingPHL - FLT 596 - EN ROUTE SJU-PHL, A FUEL ODOR WAS REPORTED AT THE EMERGENCY EXIT ROW DURING THE FLIGHT. ADDITIONALLY, THE RIGHT HAND INNER FUEL TANK QUANTITY DECREASED ABOVE NORMAL UNITS. ALL TANK PUMPS WERE TURNED OFF AT GRAVITY FEED ALTITUDE. FLIGHT LANDESDR CA021031004Fuel Tank · cracked(CAN) ALUMINUM SPAR WINGS.- CRACK LOCATION ON WELD OF PREVIOUS REPAIR.SDR QXEA0201830Bracket · misinstalledPDX- BRACKET NUMBER IS INSTALLED IN THE REVERSE POSITION. REPARIED IAW HORIZON AIR EO R-28-82 "A".SDR 2002FA0001228Fuel Cell · contaminatedPILOT REPORTS FILLING MAIN TANK THINKING IT IS FULL. AFTER A TIME GAUGES INDICATE LESS THAN FULL. INSPECTION OF INSIDE TANK THROUGH FILLER HOLE REVEALED DATA PLATE FROM FUEL PROBE COVERING THE FLANGE ASSY WHICH ALLOWS FUEL TO CROSSFEED TO OTHER TANK. REMOVESDR NSVA200200001Check Valve · failedBOS- AFTER TAXIING TO GATE THE LT ENGINE WOULD NOT SHUT DOWN. FIRE T-HANDLE WAS PULLED, NO EFFECT. THE ENGINE CONTINUED TO RUN. MAINTENANCE VERIFIED THE FIREWALL SHUTOFF VALVE WAS CLOSED. THE MANUAL SHUTOFF VALVE WAS CLOSED AS WELL WITH NO ENGINE SHUT DOWNSDR ALG2003F00010Fuel Cell · leakingDURING RUN-UP, GROUND SUPPORT DETECTED THE ODOR OF FUEL FROM THE REAR PASSENGER COMPARTMENT. THE MECHANIC REMOVED AND REPLACED RIGHT FORWARD FUEL CELL AND AIRCRAFT WAS RETURNED TO SERVICE.SDR P5CA0200703Fuel Cell · leakingDURING EXTENDED GROUND TIME, NOTICED FUEL SEEP/STAIN RT WING GEAR DOOR FWD EDGE. SEEP SEALED PER FSM 4-05-1 NR 3 MAIN KICK FITTING AREA. STAIN WIPED CLEAN. OK FOR SERVICE.SDR RY3A02007Float Valve · leakingDURING APPROACH, CONTROL TOWER ADVISED THAT A VAPOR TRAIL WAS OBSERVED FROM LT WING. AIRBORNE TECH CONFIRMED FUEL COMING FROM UNDER LT WING. FLT WAS DEVIATED TO AND LANDING MADE, WITH FIRE EQUIPMENT STANDING BY. FUEL FROM LT WING AND LEAK STOPPED. NORMAL LSDR CA021007005Fuel Tank · cracked(CAN) CRACK IN LT INBOARD FUEL TANK UPPER SURFACE AT OUTBOARD END OF CENTER PREFORMED STIFFENER. - IN ALUMINUM SPAR WINGS.SDR 2002FA0001105Fuel Cap · blockedAIRCRAFT WAS AT A CRUISE ALTITUDE OF 1800 FT WHEN ENGINE QUIT RUNNING. MADE AN EMERGENCY LANDING IN A HAY FIELD. FUEL SELECTOR WAS SELECTED ON RT TANK. POST INSPECTION FOUND ORIGINAL TYPE FUEL CAP VENTING WAS BLOCKED (RT TANK). INSPECTION OF FUEL AND OIL SCRESDR 01645Tank · overservicedOn departure aircraft was notified by the Tower that aircraft was streaming fuel out of left wing tip area, Fuel stream was verified and called for immediate return to YIP. Declared an emergency. Landed normal not high energy stop or overweight. Maitenance detSDR GJR2002F00000Fuel Tank · crackedCRACK WAS FOUND ALONG THE LOWER SEAM ON THE INBOARD SIDE. APPLICATION 180HP FLOAT PLANE. INSUFFICIENT AMOUNT OF MATERIAL ALONG WELDED SEAMS.SDR 2002FA0000998Spacer · burnedLT ENGINE AUX FUEL TANK ASSY HAS INCURRED HEAT RELATED DAMAGE ON THE ENGINE FIREWALL SIDE. THE FIRE SPACER SCREEN AND THE RETARDANT COATING ON THE TANK ASSY HAS SINGED AND MELTED ALONG THE FIREWALL SIDE AND UNDERSIDE OF ASSY. IN SOME AREAS THE COATING HAS RESDR AUS20020945Strap · broken(AUS) LH FUEL TANK REAR STRAP ASSEMBLY LOOSE. RH FUEL TANK REAR STRAP ASSEMBLY BROKEN NEAR THE SCREW END. FOUND DURING INSPECTION IAW CESSNA CONTINUED AIRWORTHINESS PROGRAM 28-30-01.SDR CA020830023Structure · cracked(CAN) FUEL FITTING BOSS FOUND CRACKED AROUND WELD APPROXIMATELY 1 INCH IN LENGTH. THE CRACK IS IN THE LOWER AFT RT THREADED NIPPLE.SDR 2002UALA01303Disk · rupturedFLIGHT DIVERTED UNDER AMBER ALERT DUE TO FUEL IMBALANCE. FOUND BURST DISC BETWEEN LEFT INNER AND CENTER FUEL TANKS BROKEN. REPLACED DISC.SDR TIM2002F00013Flange · crackedLEFT CENTER SECTION FUEL CELL CRACKED AT SUPPLY LINE FLANGE.SDR UPS02M39218Doubler · corrodedINSPECTION TYPE:C, UPPER AUX TANK UPPER EXTERNAL SKIN HAS SLIGHT SURFACE CORROSION AT STA 1375 X=-47 TO X=-90. UPPER AUX TANK UPPER EXTERNAL SKIN CORROSION REMOVED BY HAND, CLEAN AND TREATED IAW SRM 51-21-01 VOL II REV 31. CORROSION FOUND WITHIN LIMIT EXCEPTSDR 2002UALA01263Disk · burstRETURN TO FIELD WITH A FUEL IMBALANCE PROBLEM. OVER PRESSURE BURST DISC BETWEEN THE LEFT INNER WING FUEL TANK AND THE CENTER FUEL TANK RUPTURED. FUEL TRANSFERRED FROM THE LEFT WING TO THE CENTER CAUSING AN IMBALANCE BETWEEN THE INNER WING TANKS.SDR YENA200218Seal · crackedFLT 106, IAD TO LGB, A/C DEVELOPED FUEL MIGRATION FROM LEFT MAIN TO CTR TANK. LEVELED OFF AT FL280, DID AN EMERGENCY LANDING AT PITTSBURG. A/C TOUCHDOWN V/S WAS LESS THAN 100 FPM. FOUND OVERPRESSURE PROTECTOR 96QM SEAL CRACKED ON VALVE. REPLACED OVERPRESSUSDR GJR2002F00001Fuel Tank · crackedCRACK WAS FOUND ALONG THE LOWER SEAM ON THE OUTBOARD SIDE.SDR CA030106018Strap · broken(CAN) FUEL LEAK. RT WING. UPON REMOVAL OF THE FUEL TANK WING PANEL, DISCOVERED THE AFT FUEL TANK STRAP TO BE BROKEN. DUE TO THE BROKEN STRAP THE SCREEN ASSEMBLY HAD CHAFED THROUGH THE TOP OF THE FUEL TANK CAUSING A FUEL LEAK. FUEL TANK REPAIRED AT AN APPROVESDR 02FDEA00517Shroud · crackedCENTER CARGO COMPARTMENT, FUEL DRAIN SHROUD ASSEMBLY CRACKED AT BS 1801. PERFORMED STOP DRILL ON CRACK PER SRM.SDR AUS20020825Drain Valve · corroded(AUS) LH FUEL DRAIN VALVE CORRODED DUE TO WATER CONTAMINATION.SDR AUS20020824Drain Valve · corroded(AUS) RH FUEL SYSTEM DRAIN VALVE CORRODED DUE TO WATER CONTAMINATION. PERSONNEL/MAINTENANCE ERROR.SDR GUUA07270212Rivet · leakingFUEL LEAKING FROM RIVET TOP OF LEFT WINGINSTALLED CLICK PATCHSDR VNAA0207012Panel · malfunctionedFLIGHT 9405 RETURNED TO THE FIELD AFTER THE AIRCRAFT BEHIND THEM REPORTED SOMETHING FELL OFF THE AIRCRAFT. THE CREW ALSO RECEIVED A FEEDER TANK LOW CAS MESSAGE. MAINTENANCE INSPECTED AND FOUND THAT A SMALL BIRD HAD STRUCK THE VERTICAL STABILIZER. MAINTENANCSDR AUS20020648Fuel Tank · collapsed(AUS) RH AUXILIARY FUEL CELL COLLAPSED. VELCRO ATTACHMENT PADS HADBECOME UNGLUED AND SEPARATED FROM THE TOP SURFACE OF THE FUEL CELL. INSPECTION FOUND THAT THE RH FUEL VENT HEATING ELEMENT HADFAILED, ALLOWING THE VENT TO BECOME BLOCKED WITH ICE CAUSING THEFUELSDR HEEA080201Seal · crackedFUEL CAP SEAL CRACKED.SDR ASAA0240060Skin · gougedJNU - DURING CHECK, FOUND GAUGE IN CENTER FUEL TANK SKIN ABOVE RIGHT PACK TURBO FAN VALVE. REPAIRED IAW EA. (M)SDR 2002FA0000794Tank · leakingWING TANKS INSTALLED IN THIS AIRCRAFT DURING 200-2001 WING RECOVER. TANKS REMOVED FOR REPAIR AFTER COMPLAINT ABOUT LEAKAGE. RIGHT TANK HAD LEAKED AT WELD SEAM AND WAS PREVIOUSLY REPAIRED BY OWNER. LEFT TANK HAD A LEAK AT THE ROOT OF TANK IN THE WELD BEAD WHESDR HEEA079709Fuel Cell · leakingFUEL CELL LEAKING.SDR HEEA079649Cap · brokenFUEL CAP SCREW BROKE OFF (HARD TO OPEN) SCRAPPED.SDR HEEA079648Cap · brokenFUEL CAP RIVETS BROKEN. SCRAPPED.SDR HEEA079493Fuel Cap · damagedLEVER ON FUEL CAP WILL NOT STAY LOCK DOWN WHEN SECURED. SCRAPPED.SDR 2002F00800Relief Valve · damagedJFK - FLT 580 - DURING CLIMB, AN IN FLIGHT FUEL TRANSFER WAS EXPERIENCED FROM RIGHT TANK TO THE CENTER TANK. AIRCRAFT RETURNED TO JFK STATION FOR MAINTENANCE. AT JFK STATION, TECHNICIANS PERFORMED INSPECTION AND FOUND THE OVERPRESSURE PROTECTOR 96 QM DAMAGEDSDR VNAA0205015Panel · faultyDURING TAKEOFF, THE CREW RECEIVED A FUEL QUANTITY FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE REFUELING PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELESDR QXEA0200829Fuel Cap · openBOI - AIRCRAFT RETURNED TO FIELD WHEN THE RIGHT WING FUEL CAP OPENED IN FLIGHT. MAINTENANCE INSPECTED AND REINSTALLED FUEL CAP. AIRCRAFT RETURNED TO SERVICE.SDR HEEA079275Fuel Cap · leakingFUEL CELL CAP LEAKS WHEN FUEL TANK IS FULL. SCRAPPED.SDR HEEA078909Fuel Cap · missingFUEL CELL CAP MISSING.SDR OG5R092NFuel Tank · crackedDURING ANNUAL INSPECTION A FUEL LEAK WAS NOTED ON THE BOTTOM OF THE LEFT WING BENEATH THE FUEL TANK. UPON MORE DETAILED INSPECTION THE INTERNAL BAFFLING OF THE FUEL TANK WAS FOUND TO BE SEPERATED AND THE TANK TO BE LEAKING FROM ONE OF THE BAFFLE ATTACH WELDS. SDR HEEA078801Cap · damagedTABS AROUND OUTER EDGE OF FUEL CAP MISSING.SDR 2002F00493Valve · damagedFLT GU970 - SJO-GUA - DURING CRUISE, AN IN FILGHT FUEL TRANSFER WAS EXPERIENCED FROM RIGHT TANK TO THE LEFT, AND CENTER TANK. AIRCRAFT DIVERTED ITS FLIGHT TO EL SALVADOR STATION FOR MAINTENANCE. AFTER LANDING, TECHNICIANS PERFORMED INSPECTION TO THE LEFT WINSDR SIMA200213001Odor · detectedMIA - FLT 9534 - A/C SMELLS LIKE FUEL BOTH ON GROUND AND IN THE AIR. INSPECTED INSIDE CABIN FOR FUEL LEAK, OUTSIDE FOR FUEL LEAKS. AIRED OUT CABIN AND CROSS FEED FUEL AND RAN ENGINES. NO SMELL OF FUEL FOUND INCABIN. (M)SDR CA020515014Rivet · sheared(CAN) UPON INVESTIGATION OF A FUEL LEAK LT AUXILIARY FUEL TANK, "PRC" REMOVED AND FOUND 6 RIVET HEADS ATTACHED TO THE "PRC", AT LT KEEL RIB INSTALLATION BL.91.75. SHANK'S REMOVED AND NEW RIVETS INSTALLED.SDR WC72002F00000Valve · stuckDURING A PREFLIGHT INSPECTION, WHILE DRAINING THE FUEL SUMP ON THE RIGHT WITN, THE DARIN VALVE BECAME STUCK IN THE OPEN POSITION. THE TOPPED OF WING WAS PROFUSELY DRAINING ON THE HANGER FLOOR. AFTER THE AIRCRAFT WAS DEFUELED AND THE DRAIN VALVE REMOVED. IT SDR BAQA094304Manifold · unserviceableWARRANTY. ENG S/N 30178. MANIFOLD DUE TIME CHANGE. ABOVE INFORMATION REFLECTS TIMES AT 03/06/2002. BELINDA WILL CREDIT OUTSTANDING ACCOUNT. REPLACED WITH SERVICABLE UNIT. 04/30/2004SDR YENA200208Relief Valve · faultyFLIGHT 91, JFK TO OAK, AIR TURNBACK TO JFK DUE CENTER TANK MODE SEL FAULT. THE ONLY TANK THAT BURNED FUEL WERE THE LEFT WING TANK. NO FUEL BURNED FROM CENTER OR RIGHT WING TANK. FOUND LT TANK TRANSFERRING FUEL TO CENTER TANK. REMOVED AND REPLACED LT CENTERSDR CA020322009Vent Line · obstructed(CAN) DURING SCHEDULED 100 HOUR ANNUAL & 12 MONTH INSPECTION. PROCEEDED TO CHECK OP OF LOW FUEL WARNING SYS. REMOVED FUEL LINE GOING TO AIRFRAME FUEL FILTER AND ATTACHED LONG FUEL LINE SO WE COULD DRAIN FUEL CELL VIA A/C FUEL BOOST PUMPS. WE PUT A/C POWER ON A
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