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 FDEA201110014235Panel · corrodedCABIN - COROSION ON CTR WING AUX TANK TOP PANEL SURFACE AT STA 1219 TO STA 1239, X = -8 TO X = -27.5. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.041INCH; MATERIAL REMAINED = 0.131 INCH - FOUNDSDR FDEA201110014234Panel · corrodedCOROSION ON CENTER WING AUX TANK TOP PANEL SURFACE AT STA 1219 TO STA 1239, X = -27.5 TO X = -47.5. CORROSION REMOVED AS PER MD-11 SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.041INCH; MATERIAL REMAINED = 0.131 INCH - SDR FDEA201110014233Panel · corrodedCABIN - COROSION ON CTR WING AUX TANK TOP PANEL SURFACE AT STA 1219 TO STA 1239, X = -47.5 TO X = -75. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.030 INCH; MATERIAL REMAINED = 0.142 INCH - FOUSDR FDEA201110014232Fuel Cell · corrodedCOROSION ON CTR WING AUX TANK TOP PANEL SURFACE AT BS 1219-1239, X = -75 TO X = -107. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.048 INCH; MATERIAL REMAINED = 0.124 INCH - FOUND EXCEEDED LIMIT SDR FDEA201110014231Fuel Cell · corrodedCOROSION ON CTR WING AUX TANK TOP PANEL SURFACE AT BS 1199-1219, X = -75 TO X = -107. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.028 INCH; MATERIAL REMAINED = 0.144 INCH - FOUND EXCEEDED LIMITSDR FDEA201110014230Fuel Cell · corrodedCORROSION ON CENTER WING AUX TANK TOP PANEL SURFACE AT BS 1199-1219, X = -75 TO X = -107. CORROSION REMOVED AS PER MD-11 SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.247 INCH; MATERIAL REMOVED = 0.014 INCH; MATERIAL REMAINED = 0.233 INCH - FOUND SDR DALA1156805532Flange · leakingDURING APPROACH PASSING 1200 FEET A STRONG SMELL OF JET FUEL BECAME APPARENT. LASTED STRONG ENOUGH THRU TOUCHDOWN AND DISSIPATED BY TAXI SPEED. FLIGHT CREW FILLED OUT AIRCRAFT FUME QUESTIONNAIRE. ONCE ON GROUND MAINTENANCE FOUND FUEL LEAK IN THE LEFT ECS BASDR GLBA20110930FLine · leakingPILOT REPORTED THAT FUEL WAS DRIPPING FROM HYD LINES IN LT WHEEL WELL. MX CLEANED AND INSPECTED THE AREA, NO LEAK FOUND.SDR GLBA20110922FLine · leakingPILOT REPORTED THAT FUEL WAS LEAKING FROM THE RT WING OR WHEEL WELL. MX TIGHTENED THE LINE ON THE RT FUEL VENT IAW BMM 28-20-01, LEAK CHECKED GOOD.SDR UALA2011091905023Fuel Cap · missingLEFT AND RIGHT FUEL RECEPTACLE CAP(S) INOPERATIVE OR MISSING. DEFERRED PER MEL. -INF- :FUELING CAPS (PCN 192-2130). REPLACED MISSING FUEL CAPS.SDR DXTA2011091904731Float Valve · stickingIN LEVEL CRUISE FLIGHT AT FL310, AMBER CAS "WING TANK OVER FILL R", CAME ON AND FUEL WAS VENTING OUT OF THE RT WING. THE CAS MESSAGE WENT OUT, FUEL STOPPED VENTING. THIS ISSUE REPEATED IT SELF TWICE DURING THIS FLIGHT. FOUND FUEL PANEL WITH RELIEF VALVE ISDR UALA2011090904878Drain Valve · leakingBAD SMELL FROM PACKS DURING DESCENT FROM 5000FT DOWN TO TOUCHDOWN. ACCOMPLISHED ENG RUN, LET PACKS RUN, UNABLE TO DUPLICATE ON GROUND. PROBLEM RECURRED TWO SEGMENTS LATER. FOUND FUEL LEAKING AT THE FUEL DRAIN VALVE CENTER TANK RT SIDE PNL 196BB AREA, RESET SDR UALA2011090704854Unknown · malfunctionedTANK TO ENG 1000LBS IMBALANCE NUMBER 3 GREATER THAN 2 TANK. PERFORMED MANIFOLD PRESS CK WITH ALL PUMPS ON. FUEL LEAKS INTO TNKS NR 2 AND 3 AT THE RATE OF 500LB TO 600LB EVERY 30 MIN. PRESSURE CKD USING FUEL TANKER. NO FUEL TRANSFER OBSERVED. PERFORMED FUSDR CA110907006Fuel Cell · leaking(CAN) FUEL WAS OBSERVED LEAKING FROM THE RT WING ON LANDING. THE INBD AFT FUEL CELL WAS R & R. THIS CORRECTED THE FUEL LEAK. ON INSPECTION OF THE REMOVED FUEL CELL, IT WAS NOTED THAT THE SMALL INTERCONNECT NIPPLE HAD COME LOOSE FROM THE INSIDE OF THE CELL. SDR UALA2011090704833Valve · leakingLEFT WING SUMP VALVE LEAKING APPROX 90 DROPS PER MINUTE. REPLACED SUMP DRAIN CHECK VALVE O-RING, NO HELP. FUEL COMING FROM AROUND HOUSING. LEFT WING FUEL TRANSFERED OUT AND WING SUMPED AS PREP WORK FOR DEN EFS. REPLACED SUMP VALVE AND RESEALED SUMP VALVE CSDR C2XA11IA199Flapper Valve · leakingMEM - FLIGHT 2233, THE CREW REPORTED A FUEL LEAK FROM THE RIGHT WING ON TAKEOFF. THE AIRCRAFT RETURNED TO MEM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAPPER VALE AT RIB 19, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 2011FA0000573Fuel Cell · leakingFOUND INBOARD LEADING EDGE FUEL CELL IN RT WING LEAKING AT RUBBER NIPPLE REINFORCEMENT FLANGE. THIS PMA FUEL CELL WAS INSTALLED 3 MONTHS AGO.SDR C2XA11IA198Flapper Valve · leakingIAH - FLIGHT 2816, THE CREW REPORTED FUEL LEAKING FROM THE LEFT WING ON TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLAPPER VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR HNAA11091100274AFuel Cap · unsecureAFTER LIFTOFF, CREW NOTICED WING FUEL CAP LIFTING UP. RETURN TO FIELD. INSPECTED LT WING FUEL CAP AND UPPER WING SURFACE. NO DEFECTS NOTED. R & R FUEL CAP AS PRECAUTION. CLEANED UP EXCESSIVE FUEL. OK FOR SERVICE.SDR FDEA201109013613Fuel Cell · crackedLT FUEL TANK STRUCTURE STRINGER END NR 10 SUSPECTED CRACKED. REPAIRED IAW SRM 57-00-03, REV 47, REPAIR 5 FIG 202 AND EA 1-5710-154208. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.SDR CA110823002Cap · missing(CAN) ACFT WAS LOSING FUEL FROM RT WING TANK. DECLARED EMERGENCY AND LANDED OVERWEIGHT. SINK RATE WAS APROX 200 FT IAW SECOND AND LANDED WITHOUT INCIDENT. ON WALKAROUND FOUND RT WING FUEL CAP MISSING. (SEE ALSO FAA SDR 2011100100589/SIMA201123505)SDR SIMA201123505Fuel Cap · missingON FLIGHT 3898 THE CREW REPORTED THAT JUST AFTER ROTATION THEY WERE INFORMED OF FUEL COMING FROM THE RIGHT WING. SHORTLY THEREAFTER RECEIVED A FUEL IMBALANCE MESSAGE AND SAW THE RIGHT FUEL QUANTITY DECREASING. THE CREW DECLARED AN EMERGENCY AND LANDED AT IADSDR CA110824006Fuel Tank · contaminated(CAN) WHILE LEVELING OFF AT 9000 FT, AFTER FLIGHT IDLE DECENT, NT 2 ENGINE POWER ADVANCED TO 30 PERCENT TORQUE, CREW RECEIVED A FUEL PRESS CAUTION LIGHT TEMPORARY, MOMENTARY TORQUE SURGE AND RETURNED TO NORMAL, HAPPENED AGAIN WHEN LEVELING OFF AT 6000 FT ON SASDR C2XA11CL191Flapper Valve · tornCLE FLT 3095 THE CREW REPORTED ON DEPARTURE FROM CLE THE TOWER INFORMED THEM OF A FLUID LOSS COMING FROM THE RIGHT WING. THE AIRCRAFT RETUNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE RIGHT WING OUTBOARD FLAPPER VALVE SEAL TORN.SDR QMLA2011081511085Fuel Cap · leakingUPON DEPARTURE AND CLIMBOUT, THE PILOT AND CREW SMELLED A RAW FUEL ODOR THROUGHOUT THE ACFT. THE PILOT IMMEDIATELY ABORTED THE MISSION AND RETURNED TO THE BASE. THE MECHANIC ARRIVED AND PERFORMED BOTH VISUAL AND OPS CHECKS OF THE FUELS SYS. IT WAS REVEALED SDR UALA2011080103973Drain · leakingLEFT WING MAIN TANK SUMP DRAIN LEAKING FUEL. MEASURED FUEL LEAK TO BE 42 INCHES LONG FROM SUMP DRAIN AFTER 15 MINUTE EVALUATION. ACCOMPLISHED REPAIR. SEALED AND REPLACED SUMP DRAIN. LEAK CHECK GOOD.SDR C2XA11IA171Flapper Valve · leakingMKE - FLIGHT 2350, THE CREW REPORTED FLUID LEAKING FROM THE TOP OF THE RIGHT AILERON RIGHT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO MKE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT WING OUTBOARD FLAPPER VALVE, AND THE AIRCRAFT SDR UALA2011072703873Valve · leakingRT WING WATER VENT IS LEAKING FUEL. REPLACED OUTER VALVE, CHECKED OKSDR UALA2011072503807Drain Valve · leakingLEFT OUTER FUEL H20 DRAIN DRIPPING. REPLACED LEFT WING OUTER FUEL DRAIN VALVE 21QM IAW AMM.SDR UALA2011072103700Fuel Cell · leakingFUEL LEAKING THRU RT OTBD FLAP INBD TRACK SUPPORT FITTING. FOUND THE SOURCE OF LEAK INTERNALLY & EXTERNALLY. REMOVED OLD SEALANT FROM FASTENERS. REMOVED NUT. REPLACED WET WITH NEW WASHER. RESEALED ALL AREAS WITH A1-2 A ND B1-2 AT 0415 HRS. FOUND A SECONDSDR UALA2011071903664Structure · leakingUNWANTED FUEL XFER INTO CENTER TANK. TROUBLESHOT PER TSM. CONTINUED SUMPING & PREP FOR CTR TNK ENTRY - NEED TO CHECK AIR INLET VLV & FLOAT VENT VLV. LT WING FUEL LEAKING OUT OF DRY BAY DRAIN HOLES. LT WING HAD MAX LEVEL FUEL FOR TROUBLESHOOTING PURPOSE. LSDR UALA2011071203495Access Panel · leakingCONTINUOUS FUEL SEEP FROM LT DRAIN INBD OF NR 1 ENGINE. FUEL IS POOLING IN THE LT DRY BAY. CONTINUOUS FUEL SEEP FROM LT DRAIN INBOARD OF NR 1 ENGINE. FOUND FUEL LEAKING FROM UPPER FWD INBD ANGLE OF DRY BAY. REPAIRED SEALANT. LEAK CHECKED LEFT WING DRY BAY ANSDR SIMA201119305Flapper Valve · faultyON FLIGHT 2737 THE CREW REPORTED THAT DURING THE CLIMB THE FLIGHT ATTENDANT NOTICED THE RIGHT WING WAS STREAMING. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT HAD AN OVERWEIGHT LANDING BUT UNDER 300 FEET MINIMUM DESCENT RATE. THE AIRCRAFT LANDED WITHOUT SDR UALA2011070503329Valve · malfunctionedON TAXI OUT AT SFO FUEL WAS COMING OUT THE RT SIDE VENT. WILL NEED TO CHECK FUEL FILL VALVES PER MM. IF GOOD WILL NEED TO CHECK FUEL VENT VALVES. ALL TANK FUEL VALVES OPERATE NORMAL AND ARE CLOSING. FILLED WING TANKS TO FULL TAXIED AIRCRAFT 15 MINUTES NO FSDR C2XA11RI121Valve · damagedFLIGHT 5836 - RIC - FLIGHT CREW REPORTED FUEL LEAKING OUT OF LEFT WING. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. RIC MX REMOVED AND REPLACED LEFT WING FLAP VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR QMLA2011070211074Unknown · leakingPILOT REPORTED FUEL ODOR IN CABIN/COCKPIT DURING FLIGHT. INSPECTED THE ENGINE, TRANSMISSION AREA, FUEL SYSTEM INCLUDING TANK AREA, UNDERSIDE OF ACFT, BAGGAGE AREA'S, AND COCKPIT/CABIN AREA FOR SIGNS OF FUEL AND/OR FUEL ODOR, LOOSE LINES, OR DAMAGE. NONE FOUNSDR FDEA201107012532Seal · crackedMETALLIC VAPOR SEAL CRACKED ON LT SIDE AT FR 42-43, R & R METALLIC VAPOR SEAL ON LT SIDE FR 42-43.SDR 2011FA0000423Fuel Tank · corrodedCORROSION FOUND ADJACENT TO THE FUEL SUMP DRAIN IN THE WELD HEAT AFFECTED ZONE. CORROSION PIT CAUSED LEAK. NO FIRE DANGER. METAL FUEL TANKS IAW STC SA82CH.SDR FDEA201106262428Fuel Tank · corrodedCORROSION ON CTR O/W FUEL TANK UPPER SURFACE AT STA1251 X=-107. ON CTR O/W FUEL TANK UPPER SURFACE AT STA 1251 X= -107, CORRODED AREA REPAIRED IAW EA1-5710-143599. TITLE: WINGS -CTR WING UPPER SKIN SURFACE CORROSION - REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMSDR CA110627019Valve · bentDURING POST-FLIGHT INSPECTION, ANTI-SIPHON VALVE IN RT OTBD WING FUEL FILLER WAS FOUND FORCED OUT AT FLAPPER SEAL AREA AND CRACKED UP TO ATTACH FLANGE. VALVE WAS REPLACED WITH NEW PART, SAME PN. DAMAGE WAS CAUSED BY FUELLER`S FORCING FUEL NOZZLE IN FILLER ANSDR CA110623007Fuel Tank · contaminatedWATER FOUND IN FUEL CONSISTENTLY, IN BOTH LT AND RT SEAL AND WING TIP TANKS POSSIBLE SOURCE OF WATER CONTAMINATION BEING INVESTIGATED ARE FOR VENTS AND CAPS.SDR FDEA201106172316Structure · corrodedMAIN DECK CORROSION ON CTR O/W FUEL TANK UPPER SURFACE AT STA 1249 X=107. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201106172315Structure · corrodedMAIN DECK CORROSION ON THE CTR O/W FUEL TANK UPPER SURFACE AT STA 1236 X=107. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201106172314Structure · corrodedMAIN DECK CORROSION ON CTR O/W FUEL TANK UPPER SURFACE AT STA 1242 X=107. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201106172313Structure · corrodedCORROSION ON CTR O/W FUEL TANK UPPER SURFACE AT STA 1244 X=-107. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201106172312Structure · corrodedMAIN DECK CORROSION ON CTR O/W FUEL CELL UPPER SURFACE AT STA 1229 X8 TO 27.5. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201106172311Structure · corrodedMAIN DECK CORROSION ON CTR O/W FUEL TANK UPPER SURFACE AT STA 1229, 47.5. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201106172310Structure · corrodedMAIN DECK CORROSION ON CTR O/W FUEL TANK UPPER SURFACE AT STA 1229 X=8 TO -8. REPAIRED AS PER EA 1-5710-143599. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR DALA1139919881Fuel Line · disconnectedAIRCRAFT RETURNED TO ATL DUE TO UNCOMMANDED FUEL VENTING FROM LEFT WING TIP IN FLIGHT. FUEL VENTING STOPPED ONLY AFTER CENTER TANK WENT DRY. MAINTENANCE FOUND FUEL LINE AFT OF RIGHT AFT FUEL BOOST PUMP FITTING DISCONNECTED. RE-INSTALLED LINE AND SECURED FITSDR C2XA11IA106Flapper Valve · leakingOMA - THE CREW REPORTED A FUEL LEAK FROM THE LEFT WING DURING CLIMB. THE AIRCRAFT RETURNED TO OMA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAPPER CHECK VALVE AT RIB 19 ON THE LEFT WING, AND THE AIRCRAFT WAS APPROVED FOR RETURN
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