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 ASMF200609011Fuel Tank · leakingAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HMO DUE TO A FUEL LEAK IN THE RT WING PANEL. CAPTAIN REPORTED A LOSS OF 500 FUEL POUNDS IN 20 MINUTES. DURING MAINTENANCE CHECK, THE FUEL TANK INDICATIONS WERE RT TANK 5700 POUNDS AND LT TANK 6250 POUNDS. THE MEASURSDR HALA0600727Fuel · migratedETOPS SIGNIFICANT SYSTEM, FUEL MIGRATES TO CENTER TANK: STARTED FLT WITH ZERO IN CENTER TANK INDICATION 1200 LBS IN WORK.SDR C2XA06TY057Fuel Tank · corrodedCORROSION ON FWD SKIN OF VENTRAL TANK UNDERNEATH FLAME ARRESTER ATTACH BRACKET. CUT OUT AFFECTED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER. ALODINED AND PRIMED IAW EC 2810-01027.SDR HAALA0600705Tank · leakingBTB - ETOPS SIGNIFICANT SYSTEM - MAIN TANK FUEL TRANSFERRED FUEL INTO CENTER TANK, 1220# IN 1 HOUR. FUEL SEEMED TO COME FROM BOTH TANKS BUT SLIGHTLY MORE FROM LEFT TANK. FOUND FUEL TRANSFER IN UPPER RIB WHICH SEPARATES LEFT AND CENTER TANK. REPAIRED LEAK PESDR HALA0600705Tank · leakingBTB - ETOPS SIGNIFICANT SYSTEM - MAIN TANK FUEL TRANSFERRED FUEL INTO CENTER TANK. 1220# IN 1 HOUR. FUEL SEEM TO COME FROM BOTH TANKS BUT SLIGHTLY MORE FROM LEFT TANK. FOUND FUEL TRANSFER IN UPPER RIB WHICH SEPARATES LEFT AND CENTER TANK. REPAIRED LEAK PER ASDR CA060913004Fuel Cell · leaking(CAN) A/C DEVELOPED A FUEL LEAK. LEAK WAS MEASURED AND FOUND TO BE THE DRIP TYPE AND COMING FROM THE WING TIP AREA.UPON INSPECTION IT WAS DETERMINED THAT THE FUEL LEAK WAS COMING FROM THE RT FUEL CELLS. DUE TO PREVIOUS REPLACEMENT OF CELLS NR 3 THROUGH NR 8 ITSDR CIEA200600006Fuel Cap · leakingAFTER TAKEOFF, THE PILOT NOTICED FUEL EXITING THE AIRCRAFT FROM THE RT WING FUEL CAP AREA. THE PILOT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RT FUEL CAP LANYARD TO BE PINCHED BETWEEN THE FUEL CAP AND THE FUEL INSDR C2XA06TY055Skin · corrodedTYS - DURING A CURRENT 2C INSPECTION CORROSION WAS FOUND ON THE FORWARD SKIN OF THE VENTRAL TANK UNDERNEATH A SUPPORT BRACKET FOR AN ARRESTOR LINE. MAINTENANCE CUT OUT THE DAMAGED AREA, FABBED A DOUBLER AND FILLER, ALODINE AND PRIME, INSTALL DOUBLER, FILLER ASDR UPS06147816Fuel Tank · leakingFUEL MIGRATION IN FLIGHT. EMERGENCY DECLARED. UPON LANDING, CAPT NOTIFIED DISPATCHER HAD OBSERVED AN ABNORMAL DECREASE IN THE FUEL QUANTITY OF HIS LEFT OUTER TANK. R&R LT. O/B REFUEL/DEFUEL VALVE IAW 28-25-12-04 OPS & LK CHECK GOOD. AFTER REPEATED ATTEMPTS WSDR DXTA200601572Computer · faultyDURING CRUISE AT FL230 IN SMOOTH FLYING CONDITION THE LEFT WING VENTED FUEL. T/S YAW DAMPENING SYSTEM AND FOUND YSAC B FAILING. REMOVED AND REPLACED YSAC WITH A REPAIRED UNIT. OPERATIONAL CHECKS SATISFACTORY IAW CE 750 MM 27-24-01.SDR QXEA200602175Coupling · leakingONT - ON POST FLIGHT INSPECTION NOTED FUEL LEAK FROM THE BELLY OF THE AIRCRAFT AT A RATE OF 3 DRIPS PER SECOND. THE FUELER, UNAWARE OF THE PROBLEM, BEGAN REFUEL OF THE AIRCRAFT RESULTING IN ABOUT 5 GALLONS OF FUEL LEAKING FROM THE AIRCRAFT BEFORE SHUTDOWN. MSDR 2006FA0000816O-Ring · splitTHE RT FUEL TANK CAP O-RING SPLIT AND FUEL SIPHONED OUT OF THE RT TANK DURING FLIGHT.SDR ASAA0680876Skin · corrodedAUX FUEL TANK ACCESS PANEL MOUNTING FLANGE CORRODED. REPLACED DOUBLER PER DWG 5936434 AND SRM 51 30 5.SDR CA060821003Fuel Cell · leaking(CAN) UPON INSPECTION IT WAS DETERMINED THAT THE FUEL LEAK WAS COMING FROM THE RT FUEL CELLS. ALL 8 FUEL CELLS WERE REMOVED AND INSPECTED AND FUEL CELLS NRS 3 AND 4 AND 6 AND 8 WERE LEAKING P/N AND S/N AND POSITION OF LEAKING CELLS. 215-64002-4 S/N 74730 NR 3SDR C2XA06TY051Tank · corrodedTYS DURING A 2C INSPECTION CORROSION WAS FOUND BENEATH A FUEL LINE SUPPORT BRACKET ON THE VENTRAL TANK. MAINTENANCE CUT OUT THE CORRODED AREA, FAB A DOUBLER IAW EC2810-01017, SRM 57-10-03, APPLIED FUEL TANK SEALANT AND FUEL VAPOR COATING IAW EMB XR SRM 51-40SDR C2XA06TY050Fuel Cell · leakingTYS FLIGHT 2205 MADE A UNSCHEDULED LANDING DUE TO SOME FUEL LEAKING FRON THE LEFT WING. MAINTENANCE REMOVED SEALANT FROM THE EFFECTED AREA AND RESEALED IAW EMB 145XR 51-20-01. LEAK CHECKS WERE GOOD AND A/C WAS RELEASED BACK INTO SERVICE.SDR DXTA200601536Check Valve · stuckDURING FLIGHT AT 27,000 FT WITH FUEL X FEED SELECTED FROM RIGHT TO LEFT (2710 RIGHT TANK AND 2720 LEFT TANK ) WING TANK O FULL LCAS MESSAGE CAME ON . SHUT FUEL X FEED OFF AND PERFORMED CHECKLIST. FUEL WAS VENTING FROM LEFT OVERFULL TANK. STARTED DOWN AND CASSDR DXTA20060136Check Valve · stuckDURING FLIGHT AT 27,000 FT WITH FUEL X FEED SELECTED FROM RT TO LT (2710 RT TANK AND 2720 LT TANK ) WING TANK O FULL LCAS MESSAGE CAME ON . SHUT FUEL X FEED OFF AND PREFORMED CHECKLIST. FUEL WAS VENTING FROM LT OVERFULL TANK. STARTED DOWN AND CAS MESSAGE EXTINSDR 2006FA0000782Fitting · undertorquedAS REPORTED FROM THE PILOT, THE MAINTENANCE VENDOR FOUND NUMEROUS FUEL FITTINGS WHICH CONNECT THE FUEL LINES TO THE HEADER TANKS TO BE SEEPING FUEL. APPROXIMATE TIME OF SERVICE 532 HOURS. PIPE THREADED FITTINGS HAD NO THREAD LUBE/SEALANT. THE VENDOR NOTED THATSDR CHQA200600092Fluid · leakingCREW REPORTED FUEL LEAKING FROM OVER LT FLAP AREA DURING DESCENT. MAINTENANCE PERFORMED GVI OF LT WING AND FLAP AREA AND NO LEAKS NOTED. AIRCRAFT LT STATION WITH 8800 POUNDS OF FUEL LOAD, AIRCRAFT HAS HAD 3 OVERFILLS IN 2 DAYS, EVIDENCE OF RESIDUAL FUEL FROMSDR CA060911002Fuel Filter · contaminated(CAN) DURING A ROUTINE 100 HOUR INSPECTION, A LARGE AMOUNT OF PARTICLES WERE FOUND IN THE MAIN FUEL FILTERS AND THE FUEL PUMP INLET FILTERS. THE PARTICLES WERE SENT TO A LAB AND IT WAS DETERMINED THAT IT WAS ORGANIC MATERIAL SIMILAR TO THE EXPLOSION SUPPRESSANSDR 06FDEA2582Fuel Tank · crackedCRACK FOUND ON RIGHT WING TANK AT END OF STR -10, XORS 760, APPROX 9 INCHES LONG DURING HFEC INSPECTION.SDR 06FDEA2578Tank · corrodedM/D CARGO UPPER CTR TANK UNDER FLOOR AREA STA 1225 FOUND SURFACE CORRODED. REPAIR CARRIED OUT AT MM/D CARGO UPPER CTR TANK UNDER FLOOR AREA AS PER FEDEX EA 1-5710-102122. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR CA060713004Fuel Cell · leaking(CAN) AC 2032 DEVELOPED A FUEL LEAK IN THE LT WING ON JULY 10/2006. ALL LT FUEL CELLS WERE REMOVED AND TESTED. CELLS NR 8 PT NR 215-64075, NR 6 PT NR 215-64002-2, NR 4 PT NR 215-64002-4, NR 3 PT NR 215-64006-6 WERE FOUND TO BE LEAKING UPON TESTING. LEAKING CESDR 06FDEA2502Fuel Tank · crackedCRACK FOUND DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 9. REPAIR CARRIED OUT PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR PCSA7090601Fuel Tank · leakingDURING THE MAINTENANCE WALK AROUND INSPECTION, A FUEL LEAK WAS DISCOVERED AT THE REAR SPAR OF THE NR 2 FUEL TANK (WING BOX CENTER SECTION). FURTHER INSPECTION REVELED CORROSION BEYOND LIMITS IN THE NR 2 FUEL TANK AT THE REAR SPAR. REPAIR WEB DOUBLER AND STIFSDR AMW78306Fuel Cap · missingLT FUEL CAP CAME LOOSE ON CLIMB OUT AND WEDGED IN BETWEEN WING AND AILERON. EXTRA TRIM WAS REQUIRED FOR CLIMB, BUT AILERONS REMAINED FULLY CONTROLLABLE IN FLIGHT. THE CREW RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE WAS CALLED AND PERFORMED AILESDR SIMA200618604Control Unit · malfunctionedLBB - FLT 3661 - SMOKE COMING FROM REFUEL/DEFUEL PANEL WHEN POWERED ON BY FUELER. REMOVED AND REPLACED REFUEL/DEFUEL CONTROL UNIT IAW CRJ AMM 28-25-18 AND OPS CHECKED IAW CRJ AMM 28-25-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR A6WA200640268Cap · leakingFOUND FUEL LEAKING FROM CENTER WING CAP COVER. REMOVED AND REPLACED CAMLOCK FASTENER. (M)SDR UIEA200600168Skin · bulgedCENTER TANK TOP SKIN AT STA 1238 LBL 38.8 - 48.0 AREA FOUND SIGN OF SKIN BULGING. AFTER CLEAN- UP BLENDED AREA IS BETWEEN LBL 57 & LBL 65 AT STA 1241.TO CARRIED OUT OPEN HOLE HFEC PER BOEING MSG 1-200482565-1. CORROSION REMOVAL CARRIED OUT IAW SRM 51-10-01. SSDR KBM2006F00217Sump · sticksFUEL SUMP, UNIT STICKS OPEN, REMOVED AND REPLACED. (K)SDR CA060622002Drain · broken(CAN) AFTER FUELING THE AIRCRAFT THE FIRST OFFICER HEARD A SPLASH AND FOUND FUEL LEAKING FROM UNDER THE LEFT WING. THE T PORTION OF THE FUEL DRAIN HAD FALLEN OUT AND THERE WAS NO WAY TO SHUT THE QUICK DRAIN VALVE OFF. THE TOP PART OF THE VALVE AND ORING WERESDR AALA20060378Seal · leakingPHX - INFLIGHT, FUEL LEAK COMING FROM RIGHT WING FUEL BOOST PANEL. LANDED PHX WITHOUT INCIDENT. REPLACED DOME NUTS FOR TANK PLATE. RESEALED RUBSTRIP AND PANEL. REINSTALLED TANK PLATE AND SECONDARY OVER WITH NEW GASKET AND SEALED FASTENERS. SYSTEM GROUND SDR 0609200602Valve · leakingON GROUND, FUEL SPILL THRU RT WING, AFTER REFUELING AIRCRAFT. FOLLOW PROCEDURES IN FUELING MANUAL FOR FUEL SPILLAGE. DURING INSPECTION, FOUND BOTH THE NR 2 AND NR 3 DRAIN VALVE LEAKING. REPLACED BOTH VALVES, CLEAN FUEL TANKS, INSPECTED, AND CLOSED TANK PLATSDR 2006FA0000591Sleeve · brokenCREW REPORTED STRONG ODOR OF FUEL IN CABIN.MX INSPECTED FOUND FUEL LEAKING ONTO CARPET ON THE FWD LEFT SIDE OF CABIN. TRACED LEAK TO THE VENT LINE HEADER TANK ATTACH FITTING. FITTING FOUND TO BE TIGHT BUT LINE CRACKED AT COMPRESSION SLEEVE CONNECTOR. LINE AND SDR 2006FA0000590Vent Line · crackedCREW REPORTED STRONG SMELL OF FUEL IN CABIN. MX INSPECTED FOUND FUEL LEAKING ONTO CARPET ON THE FWD LT SIDE OF CABIN. TRACED LEAK TO THE VENT LINE HEADER TANK ATTACH FITTING. FITTING FOUND TO BE TIGHT BUT LINE CRACKED AT COMPRESSION SLEEVE CONNECTOR. LINE ANSDR C2XA06TY034Tank · gougedTYS DURING A 2C INSPECTION THE VENTRAL TANK WAS FOUND GOUGED ON THE FORWARD LOWER SIDE. MAINTENANCE BLENDED THE AREA SMOOTH, ALODINED AND REFINISH IAW EMB IC2006/4527. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF THE 2C INSPECTION.SDR HALA0600440Fuel Cap · corrodedSEVERE CORROSION I/B LEFT WING FUEL CAP (OVERWING) 1" X 5/8".036 DEPTH. REMOVED CORROSION I/B LEFT WING FUEL CAP .036 DEPTH. OK AS IS PER HALM105 FILE, OK FOR SERVICE.SDR DXTA200601423Fuel Sys · leakingAT FL 330, WING OVER FULL LT CAS MSG ILLUMINATED. SHORTLY AFTER FUEL BEGAN STREAMING FROM WING. CONDUCTED A RT 360 DEGREE TURN AND VENTING STOPPED. 5 MINS LATER FUEL BEGAN TO VENT AGAIN AND THEN STOPPED. THIS OCCURRED A TOTAL OF 3 TIMES WITH A LOSS OF 400 LBS SDR QXEA200601373Valve · leakingPDX FLIGHT NR 2268 NR 2 NACELLE FLUID LEAK. MAINTENANCE RESEATED SPR ADAPTER POPPET VALVE. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR HALA0600415Flange · corrodedACCESS CUTOUT FLANGE 641 MB HAS FRETTING DAMAGE. REMOVED FRETTING DAMAGE FUEL CELL CUT-OUT FLANGE 641 MB ORIGINAL THICKNESS MATERIAL .202". REMOVED LESS THAN .002 MATERIAL IN 1/2" BY 25" AREA. AREA WORKED REMAIN WITHIN LIMITS IAW 767 SRM 57-20-00/201 SHEET SDR HALA0600416Flange · corrodedACCESS CUTOUT FLANGE 632BB HAS FRETTING DAMAGE. REMOVED FRETTING DAMAGE FUEL CELL CUT-OUT FLANGE 632BB. ORIGINAL THICKNESS MATERIAL .203". REMOVED LESS THAN .001" MATERIAL IN 1/2" BY 20" AREA. AREA WORKED REMAINED WITHIN LIMITES. REMAINING MATERIAL THICKNSDR HALA0600420Flange · corrodedACCESS CUT-OUT FLANGE 641GB HAS FRETTING DAMAGE. REMOVED FRETTING DAMAGE FUEL CELL CUT-OUT FLANGE 641GB. ORIGINAL THICKNESS MATERIAL .202. REMOVED LESS THAN .002 MATERIAL IN 1/2" X 18" AREA. AREA WORKED REMAIN WITHIN LIMITS, IAW 767 SRM 57-20-01/201 SHEET 3SDR HALA0600419Flange · corrodedACCESS CUT-OUT FLANGE 641LB HAS FRETTING DAMAGE. REMOVED FRETTING DAMAGE FUEL CELL CUT-OUT FLANGE 641LB. ORIGINAL THICKNESS MATERIAL .204". REMOVED LESS THAN .005" MATERIAL IN 1/2" BY 20" AREA. AREA WORKED REMAINED WITHIN LIMITS IAW 767 SPM 57-20-01/201 ANSDR HALA0600418Flange · corrodedACCESS CUTOUT FLANGE 641BB HAS FRETTING DAMAGE. REMOVED FRETTING DAMAGE FUEL CELL CUT-OUT FLANGE 641BB. ORIGNINAL THICKNESS MATERIAL .203. REMOVED LESS THAN .002 MATERIAL IN 1/2 BY 20" AREA. AREA WORKED REMAIN IN LIMITS. REMAINING MATERIAL THICKNESS .201"SDR DXTA200601394Valve · deterioratedRT WING VENTED FUEL IN FLIGHT. RT WING OVERFILL EICAS MESSAGE RAN PROCEDURES 4 TIMES WITH AIRCRAFT YAWING BEFORE IT STOPPED. REMOVED PANELS ON OB RT WING AND IB RT SURGE TANK. INSPECTED SURGE TANK DRAIN FLOAT, APPEARED GOOD. INSPECTED CHECK VALVE ON DRAIN FSDR CA060515003Vent Line · corroded(CAN) REFUELLING WAS C/O, MASTER REFUEL PANEL CHECK C/O TO CHECK VALVE FOR OPERATION, WHAT WAS NOTICED, FUEL CAME OUT OUT OF THE LT NACA SCOOP APPROXIMATE 2 GALLON, THEN STOP. MAINT WAS ADVISED,THIS WAS ONLY HAPPENING WHEN A/C WAS PARK OVERNIGHT. SO MAINT CREWSDR CA060515002Vent Line · corroded(CAN) MASTER REFUEL PANEL CHECK TO CHECK VALVE FOR OP, FUEL CAME OUT OF LT NACA SCOOP APPROX 2 GALLON, THEN STOP. MAINT WAS ADVISE THIS WAS ONLY HAPPEN WHEN AC WAS PARKED OVERNIGHT. FIGURED THERE WAS A BAD O-RING IN VENT SYS. FUEL WAS DRAINED, FUEL PANELS REMOSDR 710850206Fuel Cap · not seatedFUEL CAP NOT PROPERLY SEATED, CAUSING FUEL LEAK AROUND CAP AND FUEL ODORS IN COCKPIT AND CABIN RESULTING IN UNSCHEDULED LANDING. MECHANIC ADJUSTED CAP AND THE PROBLEM WAS CORRECTED.SDR SWAA061458Relief Valve · malfunctionedDIVERSION, ON DEPARTURE FROM SAT, FUEL SPRAY REPORTED OUT OF RT WING, IMBALANCE OF 600 POUNDS. RESET RT WING PRESSURE RELIEF VALVE PER MM.
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