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 = 'CF680A' 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 = 'CF680A' 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 IXXA10WSAP017SPanel · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON NR 2 PYLON PANEL 447CR. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEANED, TREATED, PRIMED AND PAINTED AREA IAW SRM 51-10-02 REV 101, SRM 54-51-70 FIGURE 101 REV 101, AND SRM 51-20-01 REV 101.SDR IXXA10WSAP019SChannel · crackedDURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON V-FAIRING 447DB FWD EDGE INBD ATTACH SUPPORT CHANNEL CRACKED. REMOVED FASTENER’S AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED CHANNEL. INSTALLED NEW FASTENER’S AND CHANNEL IAW SRM 51-40-02 REV101 AND SRM 54-40-05SDR IXXA10WSAP021SFrame · crackedDURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON V-FAIRING 447DB FWD EDGE INBD ATTACH SUPPORT FRAME CRACKED. REMOVED FASTENER’S AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED FRAME. INSTALLED EXISTING FASTENER’S AND NEW FRAME IAW AMM 20-11-00 REV97, SRM 51-40-02 SDR IXXAWSAP002SAccess Panel · crackedDURING ROUTINE C-CHECK INSP, FOUND RT WING FUEL PUMP ACCESS PANEL NR 631AB CRACKED. REMOVED CRACKED ACCESS PANEL. INSTALLED NEW PANEL IAW MM 20-11-000 REV 97.SDR IXXA10WSAP003SFairing · erodedDURING ROUTINE C-CHECK INSP, FOUND LT WING OTBD T/E FLAP SUPPORT FAIRING FWD FAIRING EXTERIOR SURFACE ERODED. ACCOMPLISHED REPAIR IAW SRM 51-70-06 REV 101 AND MM 51-21-10-REV 97.SDR IXXA10WSAP006SFairing · delaminatedDURING ROUTINE C-CHECK INSP FOUND RT WING OTBD FLAP SUPPORT FAIRING DELAMINATED. ACCOMPLISHED REPAIR IAW SRM 51-70-17 REV 101 AND 51-21-10 REV 97.SDR IXXA10WSAP007SFairing · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON NR 1 PYLON LT AND RT UPPER HINGE FAIRING SUPPORT. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-10-02 REV 101, AND SRM 51-20-01 REV 101.SDR ABXA200911170063Mec · malfunctionedLEFT ENGINE FLAMED OUT AT APPROXIMATELY 1,000 AGL AFTER VNAV SELECTED. RE-LIGHT OF LEFT ENGINE SUCCESSFUL. (WHEN VNAV IS SELECTED THIS CHANGES THE THRUST PROFILE. FLAME OUT OCCURRED AS THROTTLES CAME BACK.) INSPECTED SUMPS AND FOUND NO WATER. FUEL FILTERSSDR AALA20090808JFK01Compressor Blade · damagedJFK - INFLIGHT EWR-LAX. AIRCRAFT HAD BIRD STRIKE TO LEFT ENGINE AND LEFT ENGINE VIBRATIONS ON TAKEOFF. LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED BOROSCOPE INSPECTION AS PER MM 72-00-00-6. NO DISCREPANCIES NOTED. REMOVED ANDSDR CA090630002Line · leaking(CAN) THIS IS THE POTABLE WATER HEATED SUPPLY LINE. LINE WAS LEAKING AND DURING REPLACEMENT MX NOTED SEVERAL HOLES IN LINE SUSPECTED TO HAVE BEEN CAUSED BY ELECTRICAL ARCING OF THE HEAT TAPE.SDR CA090618009Window · broken(CAN) ACFT DEPARTED, ENROUTE, AT 35,000 FT REPORTED LT NR 1 OTBD WINDOW SHATTERED. ACFT DIVERTED FOR REPAIRS. CADOR 2009Q1130 REFERS.SDR ABXA200902030007Engine · malfunctionedRECEIVED "R OIL FILTER", COMPLIED WITH PROCEDURE. AT IDLE THRUST, MESSAGE STILL ILLUMINATED, SHUT DOWN ENGINE. EN ROUTE FROM DFW, FLIGHT 402 AIR DIVERTED TO CVG DUE TO RIGHT OIL FILTER MESSAGE. SECURED ENGINE AND LANDED AT CVG WITH NO FURTHER INCIDENT. NR SDR ABXA200812050267Engine · failedAT APPROXIMATELY 600 FEET ON TAKEOFF, RIGHT ENGINE COMPRESSOR STALLED. EGT EXCEEDANCE OF 1053 DEGREES WAS RECORDED. ENGINE FAILED ON FINAL. REPLACED RIGHT ENGINE IAW JOB CARD 7010.SDR HALA2008111100844Fan Blade · damagedUPON ARRIVAL FOUND NR 1 ENGINE HAD 2 1ST STAGE FAN BLADES WITH DAMAGE OUT OF LIMITS. ALSO 8-9 BLADES NEED TO BE BLENDED. REMOVED & REPLACED NR 1 ENGINE 1ST STAGE FAN BLADES PER AMM 72-31-02, OK FOR SERVICE.SDR ABX2008F00003Spinner · leakingEXHAUST FUMES IN COCKPIT DURING HIGH THRUST SETTINGS. GROUND RAN ENGINES AND FOUND LEFT ENGINE PRODUCING SMOKE EXHAUST FUMES FROM VENTS WITH LEFT BACK ON. FOUND OIL IN NR 1 ENGINE SPINNER. RESEALED NR 1 BEARING MANIFOLD AND FAN ROTOR SPINNER IAW AMM 72-31-00SDR ABXA080198Eec · defectiveCLOSE TO V1 SPEED, LT EEC LIGHT, THEN LT ENG OVERTEMP LIGHT. ENG WENT TO 974, WHEN THRUST LEVEL RETARDED, LIGHT OUT. REMOVED AND REPLACED LT ENG EEC IAW B767 MM 73-21-07-04. EEC TEST GOOD, OPS CHECK GOOD ON GROUND RUN IAW 767 AMM 72-00-00-0. (S)SDR AALA200801585Engine · shutdownJFK INFLIGHT T20/11JUN. AT FLIGHT LEVEL 230 NR ONE ENGINE UNCOMMANDED SHUT DOWN. LANDED JFK WITHOUT INCIDENT. SINGLE ENGINE TIME 20 MINUTES. REPLACED NR ONE ENGINE ON 11JUN AT JFK. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)SDR 08FDEA01955Engine · failedON TAKEOFF ROLL SERIES OF POPS OR BANGS, SPEED LESS THAN 40 KTS, EXPERIENCED LEFT SWERVE, LOW SPEED REJECT. SOUNDED LIKE POSSIBLE COMPRESSOR STALL. GVI OF NR 1 ENG SHOWS VERY SMALL METAL PARTICLES APX 1MM SIZE IN TAILPIPE. ALSO SLIGHT INTERMITTENT SQUEAL WSDR FDEA200805221955Engine · failedON TAKEOFF ROLL SERIES OF POPS OR BANGS, SPEED LESS THAN 40 KTS, EXPERIENCED LT SWERVE, LOW SPEED REJECT. SOUNDED LIKE POSSIBLE COMPRESSOR STALL. GVI OF NR 1 ENG SHOWS VERY SMALL METAL PARTICLES APX 1MM SIZE IN TAILPIPE. ALSO SLIGHT INTERMITTENT SQUEAL W/SDR ABXA080153Control Panel · defectiveAFTER TAKEOFF FROM STA JFK, RIGHT ENGINE OVERHEAT LIGHT AND EICAS MESSAGE. PERFORMED NON NORMAL - SECURED RIGHT ENGINE. LIGHT DID NOT GO OUT AFTER THRUST LEVER RETARDED. AN EMERGENCY WAS DECLARED AND AN AIR TURNBACK TO JFK WAS PERFORMED. TROUBLESHOT PER FISDR ABXA080196Mec · defectiveRT ENG COMPRESSOR STALL ON CLIMBOUT. PERFORMED CALLED FOR ITEMS. ENG RESPONDED OK AT 80-85% N1 BUT STALLED AGAIN AT CLIMB POWER. REMOVED AND REPLACED NR 2 ENG MEC IAW B767 MM 73-21-07-4. TESTED MEC IAW B767 MM 71-00-00. NR 2 ENG COMPRESSOR STALL AT 84%. SDR HALA0800425Circuit Card · faultyETOPS SIGNIFICANT SYSTEM, EICAS STATUS MSG, R ENG OH LPW DISPLAYED. REPLACED RT OVERHEAT DETECTION CARD PER AMM 26-11-02. OPS CK OK.SDR ABXA080193Switch · defectiveRT ENG FUEL FILTER DISPLAYED. REMOVED AND REPLACED RT ENG FUEL FILTER IAW B767 MM 73-11-02/201. REMOVED AND REPLACED RT ENG FUEL FILTER INDICATOR SWITCH IAW MM 73-24-01-4. OPS CHECK AND ENG IDLE RUN IAW 71-00-00-5. LEAK CHECK GOOD. (S)SDR ABXA070427Connector · looseLOST THE LEFT ENGINE AT CRUISE. DID ENGINE SECURE CHECKLIST, NO OTHER ABNORMALITIES. CREW ACCOMPLISHED ENGINE INFLIGHT START. THE ENGINE STARTED FINE, LANDED AT MSP. INSPECTED ENGINE INLET AND EXHAUST, NO DEFECTS. SUMPED MAIN FUEL FILTER, NO DEBRIS NOTED.SDR ABXA070185Engine · defectiveLEFT ENGINE HAD LOUD BANG, LOTS OF YAW AND THE ODOR OF SMOKE. EGT REACHED 1100 AFTER SHUTDOWN, HAPPENED AT 14000FT, AIR TURNBACK TO ILN. REMOVED AND REPLACED NR 1 ENGINE IAW JOB CARD 7010, WORKPACK WO 600274113, L/P 034277-13/1.SDR ABXA070048Control Unit · malfunctionedAS CREW WAS ON FINAL AT ILN, GOING THROUGH 27K, NR 2 ENGINE HAD AN UNCOMMANDED SHUTDOWN. CREW RESTARTED ENGINE WITHOUT ANY FURTHER ISSUES. NO EMERGENCY DECLARED. NO EN ROUTE DELAY. REMOVED AND REPLACED NR 2 ENGINE MAIN ENGINE CONTROL IAW B767 AMM 73-21-01-SDR ABXA060304Fitting · crackedNR 2 ENGINE HAD CRACKED FITTING JUST FORWARD OF INBOARD THRUST REVERSER UPPER ATTACH POINT AREA. REMOVED ALL SEALS AND SEAL RETAINERS. REPAIRED FLANGE PER REA B672-55012. REINSTALLED ALL PARTS REMOVED PER SRM 51-40-2.SDR AALA20060464Engine · failedJFK - ON CLIMBOUT RIGHT HAND ENGINE SHUTDOWN DUE TO OIL QUANTITY LOSS. SLIGHT BANG HEARD AT 27000 FEET. FDR DOWNLOADED. FOUND METAL IN SCREEN. REPLACED NR 2 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AU510001502Strap · crackedREAR SPAR BULKHEAD SIDE FITTING RT FAIL/SAFE STRAP CRACKED. STRAP IS LOCATED AT SECTION 45 STN 955. FOUND DURING INSPECTION IAW AD/B767/201, BOEING ALERT SB 767-53A0100 AND AAES AD ER B76-53-10-39A. FURTHER INVESTIGATION ALSO FOUND CORROSION ON THE RT LONGESDR AU510001598Frame · crackedFUSELAGE-BODY STATION 1809.5 BULKHEAD RT FORWARD OUTER CHORD CRACKED IN LOWER FORWARD HOLE. FOUND DURING INSPECTION IAW AD/B767/146 AMDT2 AND AAES AD ER NO B76-53-36F.SDR ABXA050202Fuel Control · defectiveON TAKEOFF ROLL, RIGHT ENGINE FAILED TO PRODUCE TAKEOFF POWER. WITH LEFT ENGINE ACCELERATING NORMALLY. RIGHT ENGINE STOPPED ACCELERATING AT 58 PERCENT N1. REMOVED AND REPLACED RIGHT ENGINE MAIN ENGINE CONTROL IAW B767 AMM 73-21-01-4. PERFORMED ENGINE RUN, SDR DL76S050419Bolt · looseRT ENG FIRE IND INTERMIT DURING CLM. S/D ENG AND ATB TO ATL.C/A FOUND 4 BOLTS LOOSE ON HPT NOZZLE COOLING DUCTS AT HPC CASE 230 AND 330 POSITION. TIGHTENED SAME. REINSTALLED RMVD LOOPS. CKD SECURITY OF ALL LOOPS. RAN ENG AT 90 PCT FOR 5 MIN AND 103 PCT FRO 5 MSDR DL76S050418Ball Joint · unknownON TAKEOFF GOT VERY RAPID INTERMITTENT R ENG FIRE WARNING. ALSO, GOT INTERMITTENT R ENG FIRE LOOP 1 STATUS MSG. FIRE WARNING GOES AWAY WHEN BELOW ABOUT 85 PERCENT N1. T/S PER FIM. FIRE AND O/H LOOP RESISTANCE VALUES NORM. RAN ENG TO TAKEOFF POWER PER PFHSDR CA050707001Wheel · crackedDURING TRANSIT CHECK ONE OF THE MAIN WHEEL TIRE WAS FOUND WITH LOW PRESSURE. MAIN WHEEL ASSEMBLY WAS REMOVED AND SENT TO THE REPAIR SHOP FOR INVESTIGATION. DURING INSPECTION, THE OUTBOARD WHEEL HALVE WAS FOUND CRACKED APPROX ONE INCH LONG ON LOWER WHEEL WEB SDR AALA20050118Switch · inoperativeLAX - INFLIGHT T0019/15 LEFT ENGINE ROLLED BACK AT 300 FEET. FULL CONTROL MOVED CUTOFF AND RUN. ENGINE NORMAL AT TOUCHDOWN. THROTTLES PARKED UP THROUGH TOUCHDOWN AND ROLLOUT. REVERSED NORMALLY. REPLACED LEFT HAND ENGINE FUEL FILTER AND LEFT AND RIGHT HANDSDR AU510002217Warning Message · activatedSLAT ASYMMETRY WARNING. INVESTIGATION CONTINUING.SDR ABXA040298Structure · vibrationAIRCRAFT HAD AN UNUSUAL VIBRATION. COCKPIT WAS OSCILLATING UP AND DOWN APPROXIMATELY 3 CYCLES IAW SECOND. SLOWED AC TO 280 KIAS, NO CHANGE. AFTER TRANSITION TO MACH NR, OSCILLATION ABATED AS THE IAS DECREASED THROUGH 270 KNOTS. ALL ENGINE INDICATIONS WERE NORMSDR ABXA030345Duct · out of adjustMAINTENANCE COULD NOT OPEN R-2 WINDOW. FOUND WINDOW BINDING ON LOWER AC DUCT. ADJUSTED AND SECURED AC DUCT. WINDOW OPENED NORMALLY.SDR ABXA030342Fan · vibrationRT ENGINE FAN VIBRATION INDICATIONS WERE HIGH. BETWEEN 2.5 AND 3.5, FL 390, M .80. ACCOMPANIED BY AIRFRAME/ENGINE VIBRATION. SETTLED BACK TO 1.5 THEN BACK TO 3.0. THIS CONTINUED FOR APPROXIMATELY 30 MINUTES THEN WENT AWAY. PERFORMED FIM 71-05-00-60, NO DEFECSDR ABXA030341Valve · malfunctionedDURING CLIMBOUT AT 20,000 FEET, RECEIVED FIRE WARNING BELL, EICAS MSG AND FIRE LIGHT IN HANDLE. WHEN POWER REDUCED TO IDLE ALL INDICATION OF FIRE CEASED. OVERWEIGHT LANDING SINK RATE LESS THAN 260 FPM WITH LOW SINK RATE. REPLACED BOTH AFT LOOPS IAW B767 MM.SDR ABXA030328Fire Loop · inoperativeDURING CLIMBOUT, GOT LEFT ENGINE FIRE INDICATIONS. BELL, SHUT OFF SW, T-HANDLE, MASTER WARNING, EICAS MSG. SHUT DOWN AND SECURED ENGINE. CREW PERFORMED AN AIR TURN BACK TO OAK WHERE THE AIRCRAFT LANDED AT APPROXIMATELY 285,000 LBS AS A RESULT OF AN EMERGENCY RSDR ABXA030327Slide · out of positionAFTER CLOSING ENTRY DOOR, ENTRY DOOR ANNUNCIATOR LIGHT ON. WENT TO RESECURE DOOR AND UPON OPENING, EMERGENCY SLIDE BEGAN TO FALL OUT OF DOOR. MAINTENANCE INSPECTED GIRT BAR MECHANISM. NO DEFECTS NOTED AT THIS TIME. REPLACED L1 SLIDE ASSEMBLY IAW B767 MM 25-66-SDR ABX030320Engine · malfunctionedLT ENGINE OIL PRESSURE AND QUANTITY LOSS WITH 5.1 VIBRATION THAT COULD BE FELT THROUGH THE AIRCRAFT AND THE ENGINE SHUT DOWN. REPLACED ENGINE IAW WORK PACK 600178060.SDR ABXA030208Engine · malfunctionedLEVELING AT FL39 M.8-AIRCRAFT EXPERIENCED AN UNUSUAL VIBRATION IN YAW/SHAKING, WITH A SLAPPING NOISE TO THE RIGHT OF THE COCKPIT. ALL NORMAL WHEN THRUST RETARDED FROM CLIMB THRUST, SOUNDED AND LEFT LIKE A DOOR OR PANEL WAS OPEN. REMOVED AND REPLACED THE NR 2SDR AUS20030520Clamp · failed(AUS) APU FUEL CONTROL UNIT LOOSE ON GEARBOX DUE TO BROKEN CLAMP BOLT.SDR ABXA030099Engine · leakingRIGHT ENGINE OIL PRESSURE LIGHT ILLUMINATED EICAS MESSAGE, RIGHT ENGINE OIL PRESSURE WAS ZERO. OIL QUANTITY ZERO. ENGINE SHUT DOWN. N2 RPM WAS NORMAL AFTER SHUT DOWN. REPLACED THE NR 2 OIL SCAVENGE PUMP, NO HELP, OIL CONTINUED TO LEAK. REMOVED AND REPLACED THESDR AALA20021903Engine · leakingSHORLTY AFTER TAKEOFF, AIRCRAFT AIR INTERRUPTED DUE TO SMOKE/VAPOR IN AFT CABIN ON CLIMB-OUT. AIRCRAFT RETURNED TO JFK LANDED WITHOUT INCIDENT. RELACED RIGHT ENGINE DUE TO INTERNAL OIL LEAK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AUS20021427Pump · faulty(AUS) MAIN FUEL TANK BOOST PUMPS (3OFF) DEFECTIVE. FOUND DURING INSPECTION IAW AAES ER B76-28-20-37 AND HAMILTON SUNDSTRAND SB5006003-28-2.SDR AUS20021061Door · separated(AUS) LH MAIN LANDING GEAR TRUNNION DOORS MISSING. DAMAGE CAUSED TO BRAKE AND LANDING GEAR HYDRAULIC LINES. LH HORIZONTAL STABILISERHAD MINOR IMPACT DAMAGE TO THE LEADING EDGE.SDR AUS20020809Module · failed(AUS) RUDDER RATIO MODULE FAILED.
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