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 engine_model_key = 'GE90115B' 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 engine_model_key = 'GE90115B' 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 Q2SA20190110400Battery Pack · dischargedAIRCRAFT GROUNDED. LT DR1 BATTERY PACK CAPACITY CHECK FOUND EMERGENCY LIGHTS AND SIGNS STAY ON LESS THAN 15 MINUTES. LT DR1 BATTERY PACK REPLACED AND TEST OK AS PER AMM 33-51-06.SDR Q2SA20190110401Battery Pack · dischargedAIRCRAFT GROUNDED. RT DR1 BATTERY PACK CAPACITY CHECK FOUND EMERGENCY LIGHTS AND SIGNS STAY ON LESS THAN 15 MINUTES. RT DR1 BATTERY PACK REPLACED AND TEST OK AS PER AMM 33-51-06.SDR Q2SA20190104397Skin · crackedAIRCRAFT GROUNDED. LT NR 7 SLAT INBD L/E SKIN CRACKED AT ISS 196. SKIN REPAIRED.SDR Q2SA20190104398Skin · crackedAIRCRAFT GROUNDED. RT NR 8 SLAT SKIN CRACKED AT ISS 186. SLAT SKIN REPAIRED.SDR Q2SA20190104399Skin · crackedAIRCRAFT GROUNDED. RT NR 8 SLAT ISS 196 SKIN CRACKED. SKIN REPAIRED.SDR Q2SA2018103028395Light · inoperativeAIRCRAFT GROUNDED. RT SLIDE - OVERWING EMERGENCY LIGHT INOP DURING TEST. RT EXIT SLIDE LIGHT RELAMPED IAW AMM 33-51-04-960-801. TEST SATIS.SDR QEMY2018101600001Diffuser · damagedCOMBUSTOR DIFFUSER ASSEMBLY HAS MULTIPLE INDICATIONS NOTED IN FPI PROCESS UP TO 0.450" IN LENGTH. PART IS AN LLP AND REMOVED FROM SERVICE EARLY. PART TO BE REMOVED FROM SERVICE AS ITS AFFECTED BY SB72-0784.SDR AALA2018082219024Carbon Seal · leakingOIL QUANTITY ON THE NR 2 ENGINE HAD DROPPED FROM 11 QUARTS TO 5 QUARTS. FLIGHT HAD REMAINED OVERNIGHT DUE TO HIGH OIL CONSUMPTION THE PREVIOUS DAY. AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. LT ENGINE OIL DECREASED FROM 16 QUARTS TO 11 QUASDR Q2SA20180307391Fault Light · illuminatedMAIN GEAR STEERING FAULT. AIRCRAFT GROUNDED. OPENSDR Q2SA20180114387Wire · damagedNO SIDEWALL LIGHTS ON LEFT AND RIGHT SIDE OF MAIN CARGO DECK DO NOT ILLUMINATE. AIRCRAFT GROUNDED. SIGN OF BURN WITH CONNECTED WIRES DISCOLORED AND BURNED AS WELL ON RELAY K24051. RELAY K24051, TERMINAL MODULES TB400(5) &(6), AND ASSOCIATED WIRING REPLACEDSDR Q2SA20171219386Light · inoperativeAIRCRAFT GROUNDED. FOUND DURING WALK AROUND EMERGENCY LIGHT ON L1 DOOR INOP. MX REPLACED EMERGENCY BULB. SYSTEM OPS CHECKED GOOD.SDR Q2SA20170513382Turbine Blades · separatedLEFT ENGINE INDICATED A VIBRATION OF 5.2 AFTER TAKE OFF AIRFRAME VIBRATION WAS FELT UNTIL POWER PULLED BACK. VIBRATION REMAINED AT 4.6 UNTIL ENGINE SHUT DOWN. AIRCRAFT DIVERTED. AIRCRAFT GROUNDED. ENGINE REMOVED AND REPLACED. LEAK CHECKED SATISFACTORY. OPERASDR 2016F00089Turbine Case · damagedMISSING TRIPOD CLAMPS AND NUTS ON TCF MODULE. TCF MODULE, TURBINE CENTER. PN: 2497M12G05, SN: FCP5C9TL. THIS TCF MODULE, PN 2497M12G05, SN FCP5C9TL HAS BEEN REMOVED FROM ENGINE. THIS TCF MODULE WAS SENT TO AF SUBCONTRACTOR FOR REPAIR. DURING TCF INCOMING SDR 2016FA0000288Clamp · missingTHIS TCF MODULE, HAS BEEN REMOVED FROM ENGINE INCOMING VISUAL INSPECTION, 72-54-00, OBSERVED 24 TRIPOD CLAMPS AND NUTS WERE MISSING ON THE 1ST FORWARD ROW, ON OUTER SIDE. DUE TO THE TCF WORKSCOPE APPLIED DURING THE QUICK TURN SHOP VISIT, THIS TCF AREA WAS NOTSDR CA160303003Relay · failed(CAN) SMOKE DETECTED IN CABIN. FLIGHT DIVERTED. DUMPED FUEL TO BE LIGHTER FOR LANDING. PAN PAN WAS DECLARED. RESOLUTION BITE TEST CARRIED OUT OF IFE SYS, SPM FAILED ON TEST. SPM REPLACED. INSPECTION C/O OF ALL SEATS AND ABOVE CEILING AND ABOVE GALLEY WITH PWRSDR CA160223006Unknown · unknown(CAN) AFTER COMPLETING DE-ICING THE ACFT, TAXIED TO RUNWAY FOR DEPARTURE. DURING THE BEFORE T/O CHECK RUDDER TRAVEL CHECK NORMAL, HOWEVER AILERON IMMOVABLE AND ELEVATORS ONLY MOVABLE VERY SLIGHTLY. ACFT TAXIED BACK TO GATE WHERE MAINTENANCE MET FLIGHT AND WERSDR CA150930004Brake · overheated(CAN) AFTER LANDING ANOTHER ACFT ADVISED OF SMOKE COMING FROM THE LT MAIN GEAR AFTER THEY EXITED THE RUNWAY. CREW NOTICED A SMALL FLAME AND SMOKE COMING FROM THE LT MAIN GEAR VIA THE ONBOARD CAMERA. MAYDAY WAS DECLARED AND FIRE TRUCKS ATTENDED THE SCENE. BRAKSDR CA150929002Hydraulic System · low(CAN) CENTER HYDRAULIC QUANTITY LOW EICAS. CTR SYS HYD SERVICED IAW AMM 12-12-01 PB301. DELTA P INDICATOR ON CENTER SYS FILTER CHECK SERVICEABLE.SDR Z3KY20150630001Compressor Blade · damagedDURING POSTTEST BORESCOPE INSPECTION DAMAGE WAS IDENTIFIED ON THE HPC STAGE 6 BLADES. THIS DAMAGE WAS NOT EVIDENT AT INCOMING INSPECTION. INVESTIGATION WITH THE OEM ENGINEER ON SITE, IDENTIFIED THAT A SINGLE HPC STAGE 6 VANE SEGMENT HONEYCOMB SEGMENT HAD SEPSDR CA150316001Fan · failed(CAN) SMOKE ODOR NOTICEABLE ON CAPTAINS SIDE OF COCKPIT, NONE IN PASSENGER CABIN. PHONE PATCH WITH MOC, TURNED OFF WEATHER RADAR, ODOR DISSIPATED. PROCEEDED AS NORMAL. RESOLUTION RT EQUIPMENT COOLING SUPPLY FAN REPACED IAW AMM 21-27-03, PB 401.SDR CA150310013Indication Sys · malfunctioned(CAN) APPROX 5 HOURS AFTER T OFF FLIGHT CREW RECEIVED A STATUS MSG ENG EEC C1, FUEL IMBALANCE EICAS MSG, CAME UP & THERE WAS A 1900KG IMBALANCE IN FUEL BETWEEN THE RT & LT TANK. ENG PARAMETERS ALL NORMAL IAW FLIGHT CREW. FUEL DRIP CHECK CARRIED OUT ON LT TANSDR CA150115001Valve · failed(CAN) CREW HAD ISSUES WITH TRIM AIR VALVE. AFTER RESET ATTEMPTS (AS PER MOC), NO IMPROVEMENT IN CABIN/FLIGHT DECK TEMPERATURE HAD OCCURRED. FLIGHT ELECTED TO RETURN. FLT DECK ZONE TRIM AIR VALVE REPLACED IAW AMM 21-61-02-401 OPS CHECK OK.SDR CA141103016Anti-Ice Valve · failed(CAN) ENROUTE, THE RIGHT ENGINE ANTI-ICE VALVE FAIL IN THE CLOSED POSITION. WITH FORECAST AND ACTUAL ICING CONDITIONS PRESENT AT ARRIVAL, AIRCRAFT DIVERTED. EAI VALVE REPLACED IAW AMM 30-21-02-401 EAI VALVE CONTROLLER REPLACED IAW AMM 30-21-03 PB 201 ENGINESDR Z3KY20141031001Seal · failedHIGH PRESSURE TURBINE ROTOR FORWARD SEAL RADIAL CRACK, LENGTH=160MM, WIDTH=1MM, DEPTH=35MM. DEFECT IDENTIFIED DURING ENGINE DISASSEMBLY AND IMMEDIATELY REPORTED TO THE ENGINE OEM. OEM HAS PREVIOUSLY INITIATED FAA NOTIFICATION AND DEFECT INVESTIGATION IS ON-GSDR CA141022002Tee Fitting · cracked(CAN) INCIDENT DETAILS: AFTER DEPARTURE, FLIGHT ENCOUNTERED A HYDRAULIC PROBLEM AND ELECTED TO DIVERT TO FRA WHERE AN OVERWEIGHT LANDING WAS CARRIED OUT. MTC CONTROL, FLEET MANAGER AND DUTY PILOT WERE ADVISED. RESOLUTION FOUND CRACK ON TEE FITTING OF FLAPERONSDR AALA20141021002Coupling · leakingLEFT ENG FUEL LEAK FROM MAIN FUEL SUPPLY HOSE DISCONNECT COUPLING. REPLACED LT ENG MAIN FUEL SUPPLY HOSE ASSEMBLY.SDR CA140926013Fmc · failed(CAN) INCIDENT DETAILS:PAN PAN DECLARED AT 40W DUE TO LOSS OF 2 FMCS. AUTOPILOT SERVICEABLE.REBOOTED SYSTEM,NOW OK,CANX PAN PAN WITH ATC.CARRYING ON RESOLUTION ON THE MAT FOUND MSG 31-83172 NOT ACTIVE. GRND TEST THROUGH MAT TEST PASS. NO FAULT HISTORY.SDR CA140912004Hydraulic Line · cracked(CAN) "HYD QTY LO C" E1CAS DURING CRUISE. QTY FELL FROM .40 TO .36 BY APPROACH. AFTER GEAR EXTENSION QTY FELL TO 0.28. LHR A/C MTCE.FOUND HYD.FLUID LEAKING FROM CRACK IN CENTRE RUDDER PCU RETURN LINE,LOCATED IN FWD.VERTICAL STAB,AREA IMMEDIATE ACTIONS TAKEN: SDR CA140818008Tee Fitting · broken(CAN) APPROXIMATELY 5 HOURS INTO THE FLIGHT THE CREW REPORTED A RIGHT HYDRAULIC LOW QUANTITY INDICATION. FOUND THE RT HYD SYS TEE BROKEN. REPLACED THE TEE AND RT EDP.SDR Q2SA20140810210Apu · smokeDURING START UP OF APU, SMOKE ENTERED COCKPIT. APU OIL QTY DROPPED FROM 7.0 TO 1.2 WITHIN 10 MINUTES.SDR Q2SA20140721208Skin · damagedDURING WALK AROUND, MAINTENANCE FOUND NR 5 SLAT NOSE SKIN DAMAGE. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-01/105. REPAIRED IAW SRM 57-43-01/201. REPAIR 1. OK FOR SERVICE.SDR CA140602034Brake · overheated(CAN) ONCE ACFT ARRIVED AT GATE, FLIGHT CREW ADVISED OF HOT BRAKES AND 4 BLOWN TIRES. BLOWN TIRES, HAPPENED ON THE GATE NOT ON LANDING OR TAXI. ALL PASSENGERS, AND FLIGHT CREW WERE ON-BOARD, AND CRF WAS NOT REQUIRED. FOUND FUSE PLUG MELT ON WHEELS NR 1, 5, SDR CA140522018Line · failed(CAN) DURING WALK AROUND FOUND HYD FLUID LEAKING FROM AFT BELLY DRAIN NEAR POTABLE WATER SERV PANEL. UPON FUTHER INSPECTION BULK CARGO, RT SIDE BEHIND WATER TANKS, FOUND HYD SYS RETURN LINE LEAKING. PN 272W4690-56. BS 2150 PIN HOLE IN RADIUS NEAR UNION RESOSDR CA140508006Lens · melted(CAN) LIGHTNING STRIKE ON CLIMBOUT AT APPROXIMATELY FL160 IN CLOUD AND LIGHT RAIN. MOST LIKELY THE NOSE AREA. MOC FOUND LT REAR WHITE NAV LIGHT- LENS COVER GLASS MELTED. REPLACED LT REAR WHITE NAV LIGHT LENS ASSY IAW AMM 33-43-02-960-802. SYSTEM CHECKED SSDR CA140508001Control Unit · failed(CAN) EICAS ANTI-SKID MESSAGE, POSSIBLE HYDRAULIC LEAK TO 1 BOGEY. LANDING 15L WILL STAY ON RUNWAY FOR INSPECTION. FAULTED BRAKE SYS CONT UNIT. REPLACED IAW AMM 32-42-01, PB401 MAT TEST PASSED.SDR CA140407004Controller · failed(CAN) AFTER DEPARTURE, FROM PEAK FLIGHT HAD A LT ENGINE ANTI-ICE VALVE FAILURE ON ECAM. RE-SET INFLIGHT UNSUCCESSFUL. QRH PRECLUDED OPERATION INTO ICING CONDITIONS. EXPERIENCING ICING CONDITIONS AT ARRIVAL TIME. DECIDED TO DIVERT. LT ENGINE ANTI-ICE CONTROLSDR CA131015002Unknown · odor(CAN) ACFT WAS ON THE GATE WITH THE ENGINE SHUTDOWN, SWITCHING TO EXTERNAL POWER WHEN THE EXTERNAL PLUG FELL OUT. THERE WAS AN ABRUPT POWER CHANGE, AND AN ELECTRICAL BURNING ODOR WAS NOTICED IN THE GALLEY AND CABIN. THE CREW BUNK SMOKE DETECTOR ALSO WENT OFFSDR CA131007021Fan · failed(CAN) APPROXIMATELY 7 HRS IN TO FLIGHT, AN ELECTRICAL BURNING ODOR, OR AN ODOR OF MELTING PLASTIC WAS DETECTED IN THE MID GALLEY. ODOR RAPIDLY DISSIPATED. OCCURED CONCURRENTLY WITH STATUS MESSAGE RECIRCULATION FAN. REPLACED FWD UPPER RECIRCULATION FAN IAW SDR CA131009009Unknown · odor(CAN) APPROXIMATELY 30 MINUTES BEFORE ARRIVAL THE CREW REPORTED THERE WAS AN ELECTRICAL ODOR IN THE CABIN FOR BRIEF DURATION. ON ARRIVAL THE CREW REPORTED NO FURTHER OCCURRENCE AFTER THE INITIAL REPORT OF THE ELECTRICAL ODOR IN THE CABIN. THEY DID REQUEST A PSDR CA130906004Engine · leaking(CAN) WHILE ENROUTE, AN OIL LEAK DEVELOPED FROM THE LT ENGINE. THE CREW OBSERVED THE EICAS QUANTITY DECREASE BY 16 LITRES DURING CRUISE. RESULTING IN ENGINE CHANGE.SDR Q2SA20130723204Tire · delaminatedLEFT GEAR, INBD MIDDLE TIRE DELAMINATED ON LANDING. R & R LT GEAR INBD MIDDLE TIRE ASSY IAW AMM 32-45-01.SDR CA130604005Circuit Board · shorted(CAN) SHORTLY AFTER PUSHBACK, SMOKE STARTED COMING INTO THE CABIN THROUGH THE VENTS. CREW RETURNED TO GATE FOR DEPLANING OF PASSENGERS AND MAINTENANCE INVESTIGATION. FOUND QSEB 11K AT AFT RT J CLOSET INTERNAL CIRCUIT BOARD SHORTED DUE TO EVIDENCE OF DRIPPINGSDR Q2SA20130505202Power Supply · failedEMERGENCY LIGHTS FOUND AT RIGHT DOOR EXTERIOR EMERGENCY LIGHT INOP. TROUBLESHOT TO RIGHT DOOR EMERGENCY POWER SUPPLY. REMOVED AND REPLACED POWER SUPPLY. OPS CHECK OK IAW A/M/M 33-51-06.SDR CA130313004Circuit Breaker · overheated(CAN) AFTER PUSHBACK AND PRIOR TO ENGINE START, A FAILURE OF THE CAPTAIN`S PFD, MFD, FMC, AUDIO PANEL, UPPER EICAS AND VHF-L WAS EXPERIENCED. THE ACFT RETURNED TO GATE AND THE FLIGHT WAS CANCELLED. MAINTENANCE INVESTIGATION FOUND EVIDENCE OF HEAT DAMAGE AND SDR CA130128016Outflow Valve · failed(CAN) THE FLIGHT CREW WAS UNABLE TO PRESSURIZE THE ACFT DURING DEPARTURE. IN CONJUNCTION WITH MAINTENENCE, FLIGHT DISPATCH & FLIGHT OPERATIONS, THE ACFT WAS DIVERTED BACK. THE FLIGHT MAINTAINED 9000FT ALTITUDE, WHILE "DUMPING" APPROXIMATELY 70,000 KG OF FUELSDR CA121217005Pump · failed(CAN) FUEL EMERGENCY DECLARED ON APPROACH. CENTER TANK FUEL SYS WOULD NOT SCAVENGE WITH 900 KGS, FUEL TRAPPED IN CENTER TANK. MINIMUM FUEL WAS 7.1 INCLUDING CENTER TANK TRAPPED FUEL, LANDED WITH 6.9 FOB. ASR TO FOLLOW IAW L4880810 CENTER TANK SCAVENGE BURNEDSDR CA121123004Regulator · corroded(CAN) ENGINEERING REQUEST A REGULATOR REPLACEMENT ON PASSENGER O2 BOTTLE NR 10. ON INSPECTION FOUND CORROSION ON THE REGULATOR AND SURROUNDING O2 BOTTLE AND SYSTEM COMPONENTS. THE CORROSION IS DUE TO LEAKING LAV WASTE LINE SITUATED ABOVE AFFECTED AREAS. DRIPSDR CA120626012Turbine · damaged(CAN) IAW CAMPAIGN 7-0018 CARRY OUT BORESCOPE INSPECTION OF THE HPT STAGE 2 NOZZLE AND HPT STAGE 1 STATOR SHROUD. IAW AMM 72-00-00-290-805, ITEM 7, N 4. HOLE FOUND IN FLOWPATH SURFACE GREATER THAN 31.61 MM AT TIME STOP 2.44 MINUTES OF THE VIDEO. L4601970 RASDR CA120529002Blades · damaged(CAN) REPORTED BY GROUND PERSONNEL SOMETHING HAS FALLEN OFF AN ACFT, HAS SHUTDOWN AN ENGINE AND IS IN THE PROCESS OF DUMPING FUEL AND RETURNING. AT 1000` AGL, RAPID EGT RISE RT ENGINE RAPID POWER LOSS. ENGINE SHUTDOWN. STAGE 6 TURBINE BLADES DAMAGED, AND TSDR CA120525009Electrical Box · odor(CAN) CREW REPORTED A VERY STRONG ACRID ODOR AROUND SEAT 11A. QRH WAS CARRIED OUT AND A PHONE PATCH WITH MAINTENANCE CONTROL WAS ESTABLISHED. POWER WAS DISCONNECTED FROM THE AREA AND THE ODOR DISSIPATED. THE CREW INCREASED SPEED AND ELECTED TO DECLARE A PAN
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