Pratt & Whitney PW4060
Service difficulty reports · 7,186
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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 = 'PW4060' 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 = 'PW4060' 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 2003UALA00951Line · failedC-HYDRAULIC SYSTEM QTY SLOWLY DECREASING. LEFT MAIN GEAR HYDRAULIC LINE FOUND LEAKING AT UPPER TRUNNION LOCATION. RESERVICED CENTER SYSTEM TO NORMAL. RYNGLOK REPAIR ACCOMPLISHED ON BRAKE HYDRAULIC LINE/TUBE. SPECIFIC HYDRAULIC LINE AND CAUSE OF LEAK NOT IDESDR 2003UALA00916Battery Pack · malfunctionedLT SIDE OF CABIN EEL LIGHT FLOOR PATH LIGHTING IS INOP INCLUDING OVERWING EXIT MARKERS STARTING AT COACH SEATS. REPLACED BATTERY PACK. TESTS OK.SDR 2003UALA00894Seat Track · corrodedSEAT TRACK BETWEEN STA 764-784, LBL 62 IS CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF SEAT TRACK AND FABRICATED SPLICE REPAIR PER BAC DWG 145T2222-4 AND SRM 51-40-2.SDR 2003UALA00895Hinge · crackedRIGHT WING INBOARD FLAP, AFT FLAP HINGE MID ATTACH FITTING, OUTBD AND INBD SIDES CRACKED AT LOWER ENDS. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP HINGE PER SRM 57-53-02, FIG 201 AND REINSTALLED FITTING PER MM 27-51-06.SDR 2003UALA00896Skin · crackedNR 2 PYLON OUTBOARD SIDE, FWD TORQUE BOX, NACELLE STA 240 AND WL 150, EXTERIOR SKIN IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED SIDE SKIN WITH DOUBLER-TRIPLER PER SRM 54-53-01.SDR 2003UALA00897Stiffener · crackedFLOORBEAM STATION 246 STIFFENER IS CRACKED AT LBL 26, FWD SIDE. MAJOR REPAIR ACCOMPLISHED. REPLACED STIFFENER PER SRM 51-40-2 AND BAC DWG 141T5814.SDR 2003UALA00888Attach Fitting · crackedLT WING, INBOARD FLAP, AFT FLAP MID ATTACH FITTING IS CRACKED ON OUTBOARD AND INBOARD SIDES, T/E FLAP HINGE FITTING. MAJOR REPAIR ACCOMPLISHED. REPAIRED FITTING PER SRM 57-53-02, FIG 201.SDR 2003UALA00882Skin · dentedBULK CARGO DOOR LOWER AFT SKIN IS DENTED AND GOUGED BS 1450. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00859Wire · wornEMERGENCY EXIT LIGHTS - FLOOR STRIPS ON. ALSO FLASHING ON AND OFF. FOUND SEVERAL LOCATIONS WHERE STRIP WAS TORN AND PINS PUSHED IN. REPAIRED WITH SPLICE TOOL. OPS CK NORMAL.SDR 2003UALA00840Hinge Fitting · crackedRIGHT WING INBOARD FLAP AT CENTER HINGE FITTING IS CRACKED BROKEN. MAJOR REPAIR ACCOMPLISHED. REPAIRED FITTING PER SRM 51-40-2 AND 57-53-02, FIG 201.SDR 2003UALA00827Screw · looseNR 2 ENGINE FLAMEOUT. FLAME OUT WAS CAUSED BY FUEL LEAK AT THE AIR/OIL COOLER MUSCLE LINE. THE FUEL MUSCLE LINE WAS REPLACED AND THE ENGINE WAS REMOVED WITH IN 25 CYCLES DUE TO A SURGE ABOVE 1.25 EPR CAUSED BY THE FLAME OUT. THE MUSCLE LINE FAILED DUE TO VIBRSDR 2003UALA00831Compressor · leakingNR 1 ENGINE SURGE ON TAKEOFF. ENGINE SELF RECOVERED AND CONTINUED NORMAL OPERATION. ENGINE EXPERIENCED GROUP 3 SURGE ON TAKE OFF. CAUSE OF THE SURGE IS OPEN CLEARANCES IN THE REAR OF THE HPC. FINAL FIX FOR SURGE ISSUES IS THE OVERHAUL OF THE ENGINE TO A RINGSDR 2003UALA00807Radar · inoperativeRETURNED TO FIELD DUE TO INOP WEATHER RADAR. THE WX RADAR R-T. SHOP FINDINGS FOR THE REMOVED WX RADAR R-T WERE LOW POWER OUT. THIS CONDITION WAS CORRECTED IN THE SHOP BY REALIGNING THE FREQUENCY MULTIPLIER OF THE UNIT.SDR 2003UALA00799O-Ring · missingDIVERTED DUE TO OIL LOSS IN NR 1 ENGINE. NR 3 CHIP DETECTOR FALLING OUT OF THE DETECTOR HOUSING AND A MISSING O-RING ON THE CHECK VALVE IN THE HOUSING CAUSED THE LOSS OF OIL. THERE WAS NO WEAR ON THE HOUSING TO CAUSE THE DETECTOR TO BECOME FREE. A COA WILL RSDR CA031020004Priority Valve · malfunctioned(CAN) BEFORE LANDING (GEAR DISAGREE) MSG CAME ON AND NOSE GEAR WOULD NOT EXTEND. ALTEXTENSION USED AND GEAR DOWN AND LOCKED. REPLACED NOSE GEAR PRIORITY VALVE AND GEAR SWING CARRIED OUT AND ALL NORMAL.SDR DL76L030932Engine · bird ingestionAT FL 2000 F/A REPORTED STRONG ODOR THROUGH OUT CABIN, LIKE ELECTRICAL BURNING ODOR. CABIN LIGHTS, GALLEY COMPONENTS AND IFE WERE ALL OFF AT THE TIME OF THE ODOR. NO C/BS TRIPPED. WITH ENGS RUNNING AND PACKS ON, POWERED UP GALLEY COMPONENTS, CABIN LIGHTING SDR DL76P030906Compressor · stalledON T/O NR 1 ENG COMPRESSOR STALLED AT 500 FT AGL, COMPLETED CHECKLIST PER QRH RETURNED FOR LANDING RSW. MAX EGT 850C FOR APPROX 1 MIN 30 SECS. ENG SHUTDOWN BY CREW. REPLACED NR 1 ENG PER TRANS 1T148.SDR 2003UALA00728Compressor · stalledCANCELLED DUE TO NR 2 ENGINE COMPRESSOR STALL AT FL210. ENGINE SURGED ABOVE 1.25 EPR AND WAS REMOVED. SURGE CHECKS SHOWED NO IRREGULARITIES AND ENGINE PASSED TEST-21. PILOT REPORT STATED THAT AIRCRAFT HAD WAKE TURBULENCE DURING CLIMB.SDR CA031002004Pump · failed(CAN) A/C WAS ENROUTE FROM YYZ TO FCO AND WHILE OVER YQB HAD A NR 1 ENG LOW OIL PRESSURE WARNING. CREW SHUTDOWN NR 1 ENG AND DIVERTED TO YUL. APPEARS TO BE MAIN OIL PUMP FAILURE. METAL HAS BEEN FOUND IN GEARBOX. ENGINE CHANGE UNDERWAY.SDR 2003UALA00724Skin · dentedSKIN DENTED AT STATION 1241 STRINGER 39L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER.SDR CA031003002Bushing · loose(CAN) ROLLING AILERON BEYOND 3 UNITS ON CONTROL COLUMN BINDING FELT. WHEEL VERY SLOW TO RETURN TO NORMAL. NOT AS STIFF WITH INPUT TO THE LEFT. WHEEL WOULD NOT RETURN TO NEUTRAL ON ITS OWN. FOUND INBOARD DROOP QUADRANT SIEZED. (CROSS SHAFT) ON INSPECTION OFSDR 2003UALA00688Engine · surgesNR 2 ENGINE, SURGE. ENGINE SURGE IN FLIGHT AT TOP OF DECENT. EPR BELOW 1.25. ENGINE REMOVED TO PERFORM SURGE CHECKS AND TEST-21. PERFORMED EXTERNAL CHECKS AND FOUND NO DISCREPANCIES.SDR 2003UALA00668Engine · surgesENGINE 2 SURGE DETECTED. ENGINE SURGE IN FLIGHT AT TOP OF DECENT. EPR BELOW 1.25. SURGE CHECKS ACCOMPLISHED SHOWED NO IRREGULARITIES. NO CAUSE FOUND.SDR 2003UALA00650Switch · failedFWD EQUIP OVERHEAT MSG DISPLAYED. THE CABIN PRESSSURIZATION CONTROL MODULE M17, ROTARY SWITCH FAILED. THE SWITCH WAS REPLACED.SDR DL76L030746Carbon Seal · leakingON TAKEOFF ACRID ODOR IN CABIN. SMOKE DETECTORS WENT OFF. FOUND OIL IN INLET OF NR 2 ENGINE. CARBON SEAL REPLACEMENT IN PROGRESS.SDR DL76L030737Fuel Control · surges3 HRS INTO FLT LEFT ENG STARTED SURGING LEFT EPR CYCLES. BETWEEN 1. 20 - 1.23 N1 CYCLES WITH THROTTLES RETARDED 80.5 TO 81.8 ALL OTHER ENG PARMETERS CYCLING IN SIMILAR RANGE FLT LEVEL 320 TRYED ALT EEC BUT NO HELP HAD NO EFFECT FUEL FUEL FLOW 4520-4650 STABSDR 2003UALA00610Compressor · stalledABORTED TAKEOFF DUE TO NR 1 ENGINE COMPRESSOR STALL. AIRCRAFT SURGED ON TAKE OFF AT EPR ABOVE 1.25. SURGE CHECKS FOUND NO DISCREPANCY. EVENT CLASSIFIED AS A GROUP 3 SURGE DUE TO TIP CLEARANCES IN THE HPC.SDR HALA0300647Pseu · inoperativeTRAILING EDGE FLAP LIGHT ON. FLAPS SELECTED TO 5 DEGREES, FLAPS ONLY EXTENDED TO 1 DEGREE. PSEU CODE 27-81041. REPLACED NR 1 OUTBOARD RDVT IAW MM 27-31-11 OPS CHECK FLAP/SLAT OK.SDR 2003UALA00575Seat Track · corrodedMAIN CABIN BETWEEN BS 785.9 AND BS 814, LBL 55, SEAT TRACK CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SPLICE SECTION.SDR 2003UALA00582Battery · damagedMAIN BATTERY CHARGER STATUS MESSAGE. MAIN BATTERY REPLACED. SHOP REPORTS THE BATTERY WAS COMPLETELY DISCHARGED. BATTERY WAS PROCESSED THROUGH THE OVERHAUL CYCLE AND PASSED ITS ACCEPTANCE TEST.SDR DL76P030673Eec · defectiveON DESCENT INTO FLL RT ENGINE SURGED. EGT WENT INTO YELLOW. BOROSCOPE PER FIM 71005-00 ALL OK. EEC AND PT2 PROBE REPLCD C/W ALL INSP PER FIM 71-05-00. ENGINE RUN PER PFHB 6-7-4-14 AND T/O PWR CHECK ALL OK.SDR DL76L030659Engine · surgesNBR 1 ENGINE SURGED DURING CLIMB AT FL230. FLAMES REPORTED BY PAXS AND F/A. ENGINE RECOVERED AND NORMAL INDICATIONS. ENGINE CHANGE IN PROGRESS. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.SDR 2003UALA00562Seat Track · corrodedSEAT TRACK CORRODED LBL 12 FROM BS 859-999. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS.SDR 2003UALA00563Floorbeam · corrodedCABIN AT BS 852, RBL 56, TRANSBEAM UPPER CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE, ANGLE AND FILLER REPAIR.SDR 2003UALA00564Fitting · crackedLEFT INBOARD FLAP, INBOARD FITTING FOR AFT FLAP ATTACH POINT CRACKED ON INBOARD SIDE OF FITTING. MAJOR REPAIR ACCOMPLISHED. REPAIRED FITTING.SDR 2003UALA00565Frame · puncturedAFT PIT FRAME HAS 3 INCH PUNCTURE STA 1351, STR 24R TO 25R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER REPAIR.SDR 2003UALA00566Floor Support · corrodedCORROSION OUT OF LIMITS ON FLOOR SUPPORT ANGLE AT STA 368. OTBD BY LWR AFT R-2 DOOR ON STRUCTURE. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION.SDR 2003UALA00567Seat Track · corrodedMAIN CABIN SEATTRACK AT STA 654+14 RBL 89 IS CORRODED OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION WITH SPLICE DOUBLERS.SDR 2003UALA00568Seat Track · corrodedMAIN CABIN AT STA 1197+80 LBL 89 SEAT TRACK HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPLACEMENT TRACK AND SPLICES.SDR 2003UALA00569Seat Track · corrodedMAIN CABIN BETWEEN STA 774 AND 785 AND LBL 55, SEAT TRACK HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SECTION WITH SPLICE DOUBLERS.SDR 2003UALA00558Seat Track · gougedCABIN STA 776-796, LBL 56, SHORT SEAT TRACK IS GOUGED AT CROWN. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SEAT TRACK.SDR 2003UALA00559Floorbeam · gougedMAIN CABIN FLOORBEAM TOP CAP GOUGED AT BS 340, RBL 28 TO RBL 30. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP WITH SPLICE SECTION, ANGLES AND FILLERS.SDR DL76L030657Engine · making metalL OIL FILTER CAUTION AND STATUS MESSAGE CAME ON IN FLIGHT WHILE CRUISING AT FL350. REPLACED NR 1 ENGINE. FOUND MCD COVERED WITH BEARING METAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPSSDR 2003UALA00544Floorbeam · corrodedCABIN FLOOR AT BS 852, RBL 56, TRANSBEAM UPPER CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS.SDR 2003UALA00545Seat Track · corrodedFASTENER HOLES CORRODED AT SEAT TRACK FLANGE BS 830-862, RBL 34 COMMON TO FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS.SDR 2003UALA00546Floorbeam · corrodedFLOOR BEAM TOP CAP CORRODED AT BS 266 RBL 76. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS.SDR 2003UALA00547Floorbeam · corrodedCABIN FLOORBEAM BS 286, RBL 88 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION, ANGLES AND FILLERS.SDR 2003UALA00554Wedge · delaminatedTRAILING EDGE WEDGE SKIN DELAMINATED, SLAT NR 6 MAJOR REPAIR ACCOMPLISHED. REPLACED T/E WEDGE.SDR DL76L030621Engine · bird strikeBIRDSTRIKE RT ENGINE. HIGH VIBES DURING CLIMB UP TO 3.8 N1.DUMPED 33K POUNDS FUEL. OVERWEIGHT LANDING AT SINK RATE OF 100FPM. ENGINE SHUT DOWN AFTER LANDING. BLADE DAMAGE FOUND ON THREE BLADES. LPC AND HPC BOROSCOPE PERFORMED IAW M/M. NO DEFECTS NOTED. FULSDR 2003UALA00535Floorbeam · corrodedFLOORBEAM CORRODED AT STATION 830-873, LBL 12. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE SECTION WITH ANGLES AND FILLERS.
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