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 = 'CF66D' 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 = 'CF66D' 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 03FDEA00387Plate · tornNR 279 FORWARD PIT, BETWEEN FS 920-960 RIGHT CEILING PANEL 2 EA ATTACHED PRESSURE RELIEF DOOR SCREEN PLATES ARE TORN, BENT, ABRADED AND ALSO LAMP CUT-OUT SCRAP PLATE. CLOSING ACTION. 04/05/03. ON BLENDED DAMAGE AREA ON PANELS IAW SRM 53-02-01. NEG MATERIAL LOSDR 02FDEA00976Engine · failedIN CRUISE, FL 330, NR 1 ENGINE FAILED. OIL PRESSURE 0, OIL QUANTITY AND TEMPERATURE NORMAL. FUEL PRESSURE NORMAL. HYDRAULIC QUANTITY, PRESSURE AND TEMPERATURE NORMAL. ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 ENGINE. CLOSED COWLING IAW SMPSDR 02FDEA00812Engine · failedSETTING STANDARD POWER ON EWR 4L, WIND 3309, AIRCRAFT BEGAN TO ROLL, AND IMMEDIATELY AND EXPLOSION OCCURRED, PULLING THE AIRCRAFT HARD LEFT. AIRCRAFT EXITED THE RUNWAY WITH TORCHING FROM LEFT ENGINE REPORTED BY TRAILING AIRCRAFT. NR 1 ENGINE SHUTDOWN ACCOMPLSDR 02FDEA00803Pivot · contaminatedDURING NORMAL GEAR EXTENSION, NOSE GEAR DID NOT COME DOWN, HAD NO GREEN LIGHT, HAD RED DOORS AND UNSAFE LIGHT. MAINS CAME DOWN NORMALLY. FOLLOWED RED TABS TO MANUALLY EXTEND NOSE, CAME DOWN OK. FOUND WATER COMING FROM NOSE LANDING GEAR PIVOT KNUCKLE. REMOVSDR 02FDEA00794Module · malfunctionedON TAKEOFF, LDG GEAR WOULD NOT RETRACT ON NR 2 SYSTEM. SWITCHED TO NR 1 SYSTEM AND GEAR WOULD STILL NOT RETRACT. REMOVED LANDING GEAR CONTROL HANDLE 2GA IAW TSM, CONTINUITY CHECKS GOOD BUT MODULE HAS A VERY SUSPICIOUS RATTLE. REMOVED AND REPLACED 2GA MODULESDR 02FDEA00605Engine · failedNR 3 ENGINE FAILED APPROX 45 MIN INTO FLIGHT AT FL310 FELT VIBRATION, HEARD NOISE AND MONITORED ALL ENGINE GAUGES WINDING DOWN. NO FIRE LIGHT, FOLLOWED RED TABS AND SHUTDOWN AND FIRED ONE FIRE BOTTLE. COULD NOT DUMP FUEL ( BELOW DUMPABLE LIMIT) SO LANDED OVSDR 02FDEA00597Landing Gear · failedIN LANDING PATTERN AT TPA AT GEAR EXTENSION HEARD LOUD BANG AND A/C SHUTTERED SERIOUSLY. NR 3 HYDRAULIC DEC TO ZERO. LEFT MLG READ UNSAFE LIGHTS ILLUMINATED ON BOTH FRONT AND ENGINEER'S PANEL. ACCOMPLISHED APPROPRIATE RED TAB PROCEDURES. LANDED AND EVACUATESDR 01FDEA01028Warning Light · illuminatedALL IND NORMAL EXCEPT OIL STRAINER CLOG LIGHT CAME ON. SHUTDOWN ENG LIGHT STAYED ON.SDR 01FDEA00891Mec · failedON DESCENT NR 2 ENG PWR LEVER FAILED TO CONTROL ENG PWR. SHUTDOWN ENG. REMOVED AND REPLACED NR 2 MAIN ENG CONTROL, FUEL PUMP, FUEL FILTER PER MM.SDR 01FDEA00849Engine · malfunctionedNR 1 ENGINE FAILED AFT THROTTLES REDUCTION. SHUT DOWN. REMOVED AND REPLACED CIT SENSOR AND PERF BORESCOPE PER STALL REQ. RAN ENG OK FOR SERVICE.SDR 01FDEA00841Engine · damagedPER ATC'S NOTIFICATION NR 1 ENGINE LOSING PARTS AND LOSS OF NR 1 EGT.SDR 01FDEA00795Engine · shutdownINFLT SHUTDOWN OF NR 2 ENG IN DESCENT THROTTLES RETARDED.SDR 01FDEA00176Engine · fireNR 2 ENGINE FIRE ON T/O. FIRED FIRE BOTTLES.SDR 01FDEA00185Engine · fireNR 2 ENGINE FIRE AFTER LANDING.SDR 01FDEA00078Engine · overheatedON T/O NR 3 ENGINE N1 ONLY REACHED 90.5 PERCENT WITH FULL THROTTLE. NR 3 EGT READ 80 - 100 DEG HOTTER THAN 1 & 2.SDR 00FDEA00746Fuel Control · sluggishUPON ROTATION NR 2 FUEL FLOW AROUND 5000. 1 & 3 10000 F/F N1 33 PERCENT, N2 97 PERCENT EGT 700. AC WOULD NOT CLIMB, VERY SLUGGISH.SDR 2000UALA00574Battery · failedSLIDE PRESSURE DOOR 4R NO TEST. *S/D* THE REASON FOR SLIDE PRESSURE FAILURE AT DOOR 4 WAS INDICATION AND NOT SLIDE PRESSURE. THIS CONDITION WAS CORRECTED BY REPLACING THE TEST INDICATOR BATTERY PACK.SDR AALA20001555Engine · failedHNL - FLT 0162 - AFTER TAKEOFF DURING CLIMB-OUT PASSING 17,000 FEET, A LOUD BANG WAS HEARD WITH VIBRATION BEING NOTED AS WELL AS SMOKE AND FUMES IN CABIN. NR 1 ENGINE FAILED. ACCOMPLISHED FIRE/SEVERE DAMAGE CHECKLIST, DUMPED FUEL, AIR INTERRUPTED, AND LANDEDSDR 00FDEA00548Limit Switch · inoperativeAFT T/O REVERSER UNLOCK LIGHT CAME ON NR 3 ENG NO ASSOCIATED PROBLEMS. NR 3 THRUST REVERSER INOP. *S/D* REMOVED AND REPLACED NR 3 LT AND RT DRIVE CABLES, REMOVED AND REPLACED SWITCH RIGGED IAW MM DC10-10 78-32-17-2, PDU IAW DC10-10 MM 78-31-01-2.SDR 00FDEA00538Engine · flamed outDURING T/O, NR 1 ENG N1 BEGAN TO DECAY. RETURN TO MEM. THROTTLES RETARDED, ENGINE FLAMED OUT. REMOVED AND REPLACED BOTH GASKETS BETWEEN THE P&D VALVE AND MEC PER DC10-10 MM 73-13-05-2 AND ENG PWR INSUR. CK PER JRH 6-31 AND ENG CK GOOD.SDR 00FDEA00535Engine · vibrationNR 1 ENGINE VIBRATES AT 85 PERCENT N1 AND INCREASES AS PWR IS INCREASED TO T/O. VIB CAN BE DUP ON GROUND. VIB IS FELT IN NR 1 START LEVER AND COCKPIT FLOOR. NO VIB IS FELT IN ANY OTHER THROTTLE. *S/D* REMOVED AND REPLACED, SEE WORK CARD 71T0701-1.SDR 00FDEA00536Gearbox · crackedNR 1 ENGINE HAS 6 INCH CRACK ALONG AFT FACE OF MAIN GEARBOX JUST ABOVE THE LUGS THAT MOUNT THE FORE-AFT ANTI-ROTATION SUPPORT AT 6 O''CLOCK POS. *S/D* REMOVED AND REPLACED PER WORK CARD 71T0701-1.SDR 00FDEA00534Engine · malfunctionedCLIMBING OUT OF 10,000 FT NR 3 ENGINE ROLLED BACK TO IDLE WITH A COMPLETE LOSS OF THROTTLE CONT: REPEAT WRITE-UP. AFT ROLL BACK ENG STAB. *S/D* REMOVED AND REPLACED NR 3 ENGINE PER W/C 71T0101-3.SDR 2000UALA00463Csd · failedON TAKEOFF (90 KTS) NR 2 GEN LIGHTS FLASHED AND AC BUS TRIPPED OFF. *S/D* REPLACED NR 2 CSD. OPS AND LEAK CHECKED OK. SHOP FINDINGS - NO DESCREPANCY FOUND; REPLACED HYDRAULIC LOG ASSEMBLY, SEALS AND FILTER ELEMENT, PER UAL SPECIFICATIONS.SDR 00FDEA00515Line · failedON DEPARTURE ON T/O PWR, NR 1 ENGINE ROLLED BACK TO 5000 FUEL FLOW WITH CORRESPONDING PWR IND. *S/D* REMOVED AND REPLACED CDP LINE FROM FIRE SHIELD TO 13 STAGE CANNED FROM AC 058 NR 1 ENG IN HRGR, REF MM 71-00-00. RAN ENG AND DATA CHECK GOOD PER JRH.SDR 2000UALA00433Battery Pack · failedMID FWD EMERGENCY LIGHT BATTERY PACK FAILED PWR SUPPLY TEST. REPLACED POWER SUPPLY AND BATTERY PACK. CHECKS OK.SDR 2000UALA00496Skin · damagedFUSELAGE SKIN AND FRAME DAMAGE DUE TO JETWAY IMPACT WHEN AIRCRAFT ARRIVED AT GATE . IMPACT FORWARD OF 2L DOOR JUST ABOVE FLOORLINE. SKIN DENTED AND TORN OPEN FROM BS 735 TO 760 BETWEEN L27 AND L26. THE FRAME SHEAR TIE IS DAMAGED AT BS 735. FUSELAGE SKIN RESDR 00FDEA00413Engine · failed00-169 AT 11000 FT PWR REDUCTION. FELT LIKE COMPRESSOR STALL. ON APPROACH SEVERE VIBRATION AND NR 2 ENGINE FAILED. BORESCOPED ENGINE, FOUND TIP CLANG DUE TO STALL. REMOVED ENGINE. DID PYLON INSPECTION DUE TO ENGINE FAILURE.SDR 2000UALA00246Cartridge · blownNR 2 ENG FIRE AGENT 2 LOW LIGHT ON WITHOUT CREW ACTION. *S/D* NR 2 ENGINE FIRE BOTTLE AND CARTRIDGES (P/N: 876296 -2) REPLACED ON 5/5. UPON FURTHER INVESTIGATION, DISCOVERED CARTRIDGE FIRED WITHOUT DISCHARGING FIRE BOTTLE. SUSPECT WHEN NR 2 ENGINE MAINTENASDR 2000UALA00161Duct · failedRETURNED TO ORD UNDER AMBER ALERT AND CANCELLED DUE TO NR 2 ENGINE FIRE WARNING. *S/D* AT THE TERMINAL ORD FOUND 13TH STAGE COOLING DUCT ON THE LEFT SIDE OF ENGINE AT THE 9 O''CLOCK POSITION FAILED. ADJACENT REVERSER BLANKET SECONDARY DAMAGE ON LEFT SIDE OFSDR 2000UALA00141Fire Loop · damagedNR 3 ENG FIRE DET B-LOOP LIGHT ON. INTERMITTENT FIRE WARN B-LOOP JUST PRIOR LANDING. OPERATIONS WAS NOTIFIED BY FLIGHT CREW THAT ENGINE WAS SHUT DOWN AND EMERGENCY DECLARED. LANDING WAS UNEVENTFUL. *S/D* NR 3 ENGINE ''A'' LOOP WAS PREVIOUSLY DEFERRED FOR SDR 2000UALA00139Valve · failedFUMES IN COCKPIT AND CABIN USING NR 2 PACK THRU 1-2 PNEU ISOL VALVE. *S/D* NR 2 BLEED WAS DEFERRED INOP DUE TO A PRESSURE INDICATION PROBLEM. THE NR 2 PACK WAS RUN OFF THE NR 1 BLEED VIA THE 1-2 ISOLATION VALVE. THERE IS NO HISTORY OF A FLUID LEAK FROM THESDR 2000UALA00090Line · separatedDECLARED EMERGENCY DUE TO NR 2 ENG SHUT DOWN BECAUSE OF LOW OIL PRESS/QTY. FLT APPROXIMATELY 90 MINUTES FROM HNL. AMBER ALERT DECLARED. *S/D* AT TERMINAL HNLMM FOUND TRANSFER GEARBOX OIL SUPPLY TUBE/FITTING PULLED FROM CASE. ENGINE CHANGE IS REQUIRED DUE SDR 2000UALA00038Blade · damagedNR 1 ENGINE HAD A LOUD NOISE AT T/O. ABOUT 90 PERCENT POWER SUSPECT COMPRESSOR STALL. TOWER REMARKED ON LARGE FLAME EXITING ENGINE. FOUND METAL PIECES IN TAILPIPE AFTER RETURN TO GATE (LARGER THAN FLAKES, SMALLER THAN BB''S). *S/D* INITIAL ON-WING BORESCOSDR 99UAL900674Skin · damagedDURING MAINTENANCE, THE FWD RT SIDE OF THE PRESSURE BULKHEAD AND FUSELAGE SKIN AT STA 275 WAS DAMAGED DUE TO AN IMPACT WITH AN A320 WHICH WAS BEING TOWED INTO THE HANGAR. *S/D* DAMAGED AREA WAS REPAIRED PER APPLICABLE SRM.SDR 99UAL900648Odor · detectedOIL SMELL IN CABIN, DEBRIEF CREW ON ARRIVAL. HAD UNCOMFORTABLE SMELL THROUGHOUT AIRCRAFT FOR 15-20 AFTER T/O, LIKE A BURNED OIL SMELL POSSIBLY IN NR 2 PNEU SYSTEM. ALL TEMPS, NORMAL. NO SMELL ON APU.SDR 99UAL900600Seal · crackedFLIGHT ATTENDANTS REPORT ODOR OF BURNT RUBBER IN CABIN AFTER T/O WHEN PACKS TURNED ON. ALSO, NOSE GEAR RUMBLING AFTER RETRACTIONS. *S/D* REPLACED DAMAGED SEAL ON NR 3 PACK HEAT EXCHANGER, IN AIR CONDITIONING COMPARTMENT. THERE HAS BEEN NO REOCCURANCE SINCESDR 99UAL900478Indicator · malfunctioned3L DOOR SLIDE LIGHT WILL NOT TEST. *S/D* REPLACED SLIDE REMOTE PRESSURE INDICATOR.SDR 99UAL900433Gear Box · failedOGG-LAX, NR 1 ENGINE FLAMED OUT FOR NO APPARENT REASON. NO VIBRATION, NO ABNORMAL INDICATIONS PRIOR, 32000 FEET, MACH .850, 370000# +/-. AFTER FLAMEOUT, N1: 27.7, N2: 00.1 OIL PRESSURE. DIVERTED TO HNL. *S/D* AT ENGINE SHOP INDUCTION THE GEARBOX WAS PASDR 99UAL900366Bolt · brokenHEARD LOUD BANG WHEN GEAR EXTENDED. BELIEVE IT TO BE NOSE GEAR DOOR AS WE HAD 3 GEAR GREEN LIGHTS. NLG RETRACT ACTUATOR MOUNT BOLT FAILED AND MIGRATED OUT OF THE LOWER CLEVIS ALLOWING GEAR TO FREE FALL UNRESTRICTED BY THE ACTUATOR. NLG RT FWD DOOR DRIVE LINSDR 99UAL900324Compressor · failedON TAKEOFF ROLL APPROX 90 KNOTS, NR 2 ENG FAIL LT ON, DECREASING N1 AND RISING EGT, TO 960 DEGREES C. ABORTED TAKEOFF AND SHUTDOWN ENGINE, TAKEOFF WEIGHT 352.8 NR (NOTED ENGINE STALLED). INCOMING SHOP BORESCOPE FOUND A STAGE 9 HPC BLADE FAILED AT MIDSPAN. SDR 99UAL900304Seal · poppedAIRCRAFT HAD ABNORMAL INFLIGHT NOISE-VIBRATION. SEE AIRCRAFT LOG FOR DETAILS. AIR NOISE ON RIGHT SIDE OF CABIN BETWEEN 28 & 35. *S/D* AREA CHECKED AND FOUND 12 INCHES OF SEAL POPPED ON THE CENTER CARGO COMPARTMENT PIT DOOR. SEAL REINSTALLED AND DOOR OPERASDR 99UAL900263Connector · bentEVAC SIGNAL SOUNDS WHEN DOOR 4L IS ARMED. *S/D* THE CAUSE OF THE EVAC SIGNAL SOUNDING WAS GIRT BAR ARM SWITCH CONNECTOR BENT PINS AND SWITCH (S1-702) AT DOOR 4 LT CLOSED WHEN SHOULD BE NORMALLY OPENED. SWITCH WAS FOUND NORMAL. REPLACED THE FOLLOWING PARTSSDR 99UAL900251Switch · out of adjustDOOR 4L SETS OFF EVAC ALARM WHEN DOOR IS ARMED. *S/D* THE CAUSE FOR THE EVAC ALARM SOUND WAS THAT WHEN THE DOOR WAS ARMED THE EVAC ALARM SWITCH WAS OUT OF ADJUSTMENT. REPLACED AND ADJUSTED EVAC ALARM SWITCH (P/N: BAN70241). EVAC ALARM WAS OP CHECKED AND FOSDR 99UAL900243Battery · dischargedFOUR RIGHT EVACUATION SLIDE-RAFT REMOTE PRESSURE PRESS-TO-TEST INDICATING SYSTEM INOP. LIGHT LENS DAMAGED. *S/D* SYSTEM INOP DUE TO DEAD BATTERIES. BATTERIES REPLACED AND SYSTEMS OPERATIONS CHECK - OK.SDR 99UAL900180Air Dist · odorSTRONG SMELL REPORTED IN REAR CABIN FOR THE FIRST 10 MINUTES FOLLOWING TAKEOFF. DEBRIEF CABIN CREW FOR ADDITIONAL DETAILS. FLIGHT ATTENDANT REPORTED APPROXIMATELY 6-8 ATTENDANTS AND PASSENGER BECAME ILL DURING FLIGHT WITH HEADACHES AND FEELING NAUSEA. *S/D*SDR 99FDEA00096Engine · malfunctionedVIBRATION NOTED INCREASED WITH POWER CHG ON ENG NR 2. POWER REDUCED TO IDLE AND AC RETURN TO MEM. SWAPPED AC PACKS WITH NO CHG IN VIBRATION ALL ENG AND HYD IND NORM. *S/D* REMOVED AND REPLACED NR 2 ENG IAW W/C 71T1101 & 71T1701. NR 2 ENG GROUND CKS NORMALSDR 99UAL900164Manifold · crackedNR 3 HYD SYSTEM TRANSFER VALVE MANIFOLD CRACKED AT FILTER BOWL BOSS LOCATED IN RIGHT WHEEL WELL. *S/D* LARGE FATIGUE CRACK FOUND IN THE PRESSURE FILTER THREADED BOSS DIRECTLY BEHIND THE FLIGHT CONTROL BYPASS VALVE. MANIFOLD ASSEMBLY WAS REPLACED.SDR 99FDEA00059Engine · failed99-0047 - NR 3 ENGINE SUFFERED CATASTROPHIC FAILURE JUST AFTER ROTATION NR 3 EGT 999 DEG FOR 35 SEC. REMOVED AND REPLACED NR 3 ENG IAW FEC DC-10 PWRPLT WORK CARD 71T01101 UP TO ITEM 24. COMPLIED WITH (SEE AML 01224000).SDR 99UAL900086Turbine · failedLOG READS, JUST AFTER TAKEOFF, NR 2 ENGINE FAILED. A LOUD BANG WAS HEARD AND EGT PEGGED. SHUT DOWN AND LANDED. *S/D* ENGINE WAS REPLACED. GE PRELIMINARY BORESCOPE SHOWS THAT THE ENGINE SUFFERED AN HPT STAGE 2 BLADE FAILURE. THE SUSPECT BLADES AS WELL AS SE
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