Pratt & Whitney PW4060
Service difficulty reports · 7,186
Newest first. General aviation reporting is voluntary.
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 2005UALA01238Angle · crackedNR 1 PYLON MID SPAR AT STA 233.120 RT SIDE, ANGLE IS CRACKED AT THE 2ND FROM INBOARD ATTACH FASTENER. NR 1 PYLON MID SPAR P/N 311T3157-1 AT STA 233.120 RT SIDE, ANGLE IS CRACKED AT THE 2ND FROM INBOARD ATTACH FASTENER, VERIFIED WITH HFEC. THIS IS THE CLOSE-OSDR 2005UALA01246Battery · inoperativeEEL OVERHEAD LIGHTS AT SEATS 8B, 6B, 5B, 1B AND FWD OF 1B PLUS FWD LAV EEL LIGHT BAR INOP. *S/D* RESEATED BATTERY ON THE POWER SUPPLY.SDR 2005UALA01245Wire · burnedEMPENNAGE INSIDE AT BS 1809 RT SIDE BELOW CENTER HORIZONTAL STAB FEEDER WIRE BUNDLES, INSULATION NOT SECURE, LOOSE ON APU FEEDER SPLICES AND FEEDER WIRES FOUND BURNT. *S/D* THE FEEDER WIRE, SPLICE AND CONNECTOR WERE REPLACED.SDR 2005UALA01216Pump · overheatedCANCELLED DUE TO INBOUND HYDRAULIC PUMP OVERHEAT AND LOSS OF HYDRAULIC SYSTEM PRESSURE. MAINTENANCE REPLACED RIGHT ENGINE HYDRAULIC DRIVEN PUMP AND CASE DRAIN AND PRESSURE FILTERS. PERFORMED ENGINE RUN AND REQUIRED OP CK. ALL OK.SDR 2006UALA01177Latch · wornR/W, O/W SLIDE COMPARTMENT, NR 4 AND 3 LATCHES ARE WORN. REMOVE AND REPLACE LATCHES IAW B767 MM25-65-98.SDR 2005UALA01161Frame · corrodedAFT CARGO COMPARTMENT, LOWER LOBE DRAIN HOLE IN FRAME AT BS 1562, BL 0, IS CORRODED.SDR 2005UALA01162Shear Tie · corrodedCORROSION ON AFT SIDE OF FRAME BS 1562 FROM BL 0 TO RBL 10 ON SHEAR TIE.SDR 2005UALA01156Attach Angle · crackedFWD CARGO DOOR SILL ATTACHING ANGLE HAS A CRACK AT BS 610.SDR 2005UALA01157Intercostal · corrodedCORROSION ON UPPER SURFACE OF INTERCOSTAL AT STA 852 AND LBL 54.SDR 2005UALA01158Seat Track · crackedCABIN SEAT TRACK AT GALLEY 4A FWD ATTACH POINT IS CRACKED, OUTBOARD SEAT TRACK.SDR 2005UALA01138Flap System · malfunctionedLANDED ORD UNDER AMBER ALERT DUE TO TRAILING EDGE FLAP INDICATION PROBLEM.SDR 2005UALA01126Windshield · crackedCAPTAINS WINDSHIELD CRACKED. FLIGHT DIVERTED TO LHR.SDR 2005UALA01133Battery · dischargedDOOR 1LH AND 1RH EMERGENCY EXIT LIGHTS INOP REPLACED POWER SUPPLY. REPLACED POWER SUPPLY.SDR 2005UALA01134Frame · damagedFOUND SMALL AREA OF ELECTRICAL ARCH DAMAGE TO VERTICAL FRAME RT FLANGE APPROX 1.5 INCHES ABOVE BASE.SDR 2005UALA01118Cable · inoperativeRT SIDE A-ZONE EEL INOPERATIVE. REPAIRED DAMAGED EEL FEEDER CABLE.SDR 2005UALA01119Cable · inoperativeLT FWD LAV EEL LIGHT BAR INOPERATIVE. FOUND LIGHT CABLE BROKEN AND REPAIRED.SDR 2005UALA01087Sill · corrodedFWD PIT LWR DOOR SILL AT APPROX RBL 40 IS CORRODED. STRAP WAS REPLACED.SDR DL76L050590Engine · leakingLEFT ENGINE LOSING OIL AT THE RATE OF 1 - 2 QTS/HOUR. CURRENTLY AT 4 QTS GOT DOWN TO 0 - 1 QTS AND ELECTED TO DIVERT TO LGW. REPLACED ENGINE.SDR 2005UALA01036Door · separatedDIVERTED TO YQX DUE TO AIRFRAME VIBRATION. RAM AIR INLET DOOR ASSY WAS FOUND WITH FORWARD INLET DOOR ASSY P/N 213T3010-1 MISSING. AFT HINGE ASSY P/N 213T3108-4 ATTACHING THE FORWARD AND AFT INLET DOOR ASSY WAS ALSO MISSING. FORWARD HINGE ASSY P/N 213T3109-4SDR 2005UALA01039Warning System · activatedABORTED TAKE OFF DUE TO FLAP CONFIGURATION MESSAGE.SDR DL76L050556Bleed Valve · malfunctionedRIGHT ENG BLEED VALVE WILL NOT OPEN. HPSOV DEACT IN CLOSED POSITION. REACTIVATED VALVE BACK TO NORMAL. ENG GRD RUN OK. A/C OK FOR SERVICE.SDR DL76L050540Engine · malfunctionedAT T/O CREW REPORTED LEFT DUCT PSI FLUX ALONG WITH L-2 DOOR AREA HAVING VIBRATION AND VIBRATION WAS FELT IN CONTROL COLUMN ROLL MODE. RETURNED TO JFK FOR REPAIRS. INSPECTED LEFT ENGINE FOR BIRD STRIKE. BOROSCOPED AND VIBE SURVEYED. REPLACED PRSOV FOR HISTOSDR WRLA2005141Interrogator · inoperativeTPE/ANC AT FIVE HOURS EN ROUTE A SMELL AND VISUAL OBSERVATION OF LITE SMOKE IN COCKPIT. AT SAME TIME DME 2 C/B POPPED, SMOKE AND SMELL DISSIPATED AFTER 20 MIN. INSPECTED NR 2 DME INTERROGATOR AND FOUND UNIT TO BE AT FAULT, NO EVIDENCE OF ANY ELECTRICAL WIRINSDR DL76L050498Valve · malfunctionedRTB - LEFT ENGINE BLEED LIGHT WITH PRV STATUS MSG . REPLACED VALVE.SDR 2006UALA01173Housing · crackedLT O/W SLIDE COMPARTMENT DISCONNECT HOUSING IS CRACKED. REPLACE HOUSING IAW 767 25-65-98.SDR DL76L050489Controller · malfunctionedAPU FAILED WITH FAULT LIGHT ILLUMINATED. FOUND ECU WITH ECU FAULT LIGHT ILLUMINATED. REPLACED ECU, CHECKS GOOD.SDR 2005UALA00792Light · inoperativeLEFT SIDE FIRST CLASS EEL STRIPS INOP.SDR 2005UALA00651Power Supply · dischargedEMERGENCY LIGHTS L900, L908 AND L976 ON WITH SW IN ARMED POSITION. BATTERY PACK NOT HOLDING CHARGE. REPLACED OK.SDR 2005UALA00647Engine · overheatedRETURNED TO THE FIELD DUE TO HIGH OIL TEMPERATURE ON NR 2 ENGINE. REPLACED FUEL/OIL COOLER BYPASS VALVE SOLENOID. TESTED OK AFTER REPLACEMENT.SDR DL76L050353Engine · odorON CLIMBOUT CABIN CREW REPORTED SMOKE DETECTORS SOUNDING. PERFORMED TASK 21-00-21-102-030 NOTHING ABNORMAL FOUND. INSPECT APU BLEED VALVE APU BLEED DUCT RT LT FLOW CONTROL VALVES INSPECTED CABIN INTERIOR NO ODOR. RAN BOTH ENGINES AT HIGH POWER SETTING 1.3 SDR 2005UALA00612Engine · surgesRETURNED TO IAD DUE TO NR 1 ENGINE COMPRESSOR STALL. SURGE ON POWER REDUCTION AT 5500 MSL. EPR = 1.128. TWO ADDITIONAL SURGES AT EPR < 1.128. NOT GROUP-3 SURGE. TEST-21 NOT REQUIRED. IAD HPC BSI: OK. IAD REPLACED: 2.9 BLEED SOLENOID & RELAY, HP BLEED CONSDR 2005UALA00624Lamp · inoperativeEEL LIGHT ADJACENT DR 2R INOPERATIVE. EEL LAMP WAS DAMAGED. REPLACED EEL LAMP, OK.SDR 2005UALA00625Lamp · inoperativeEEL LIGHT RIGHT OF MID GALLEY INOPERATIVE. EEL LAMP WAS DAMAGED. REPLACED EEL LAMP, OK.SDR DL76L050346Cooler · malfunctionedHISTORY OF LEFT ENG HOC USED 10 PTS ON LAST FLIGHT FROM GRU IN 9.2 HRS. PREV REPLACED DEOILER SEAL AND FUEL OIL COOLER. ATL MTC UNABLE TO FIND LEAK. REPLACED THE LEFT ENGINE.SDR 2005UALA00600Skin · corrodedBS 955 CENTER WING BOX UPPER SKIN AT RBL 3 AT AFT SPAR CORRODED, SKIN SPLICE FITTING AND AFT SPAR. CORROSION CAUSED BY MOISTURE IN THE AREA. BLENDED WING SKIN, FABRICATED REPAIR SHIM BETWEEN SKIN AND FITTING, BLENDED SPAR CHORD, AND FABRICATED MODIFIED FITTSDR 2005UALA00601Hinge Fitting · damagedLT INBD FLAP CENTER HINGE FITTING LINE INBD SIDE DAMAGED. LEFT INBOARD FLAP CENTER HINGE FITTING FOUND DAMAGED ON INBOARD SIDE. REPAIRED PER SRM 57-53-02.SDR 2005UALA00593Skin · dentedDENT IN BULK CARGO DOOR, .5 INCHES BELOW EXISTING EXTERNAL REPAIR DOUBLER. INTERIM REPAIR PER EVA MOC1-8779A. ACCOMPLISH A DETAILED, EXTERNAL VISUAL INSPECTION EVERY 'A' CHECK UNTIL NEXT 'C10' CHECK. INTERIM REPAIR PER EVA MOC1-8779A. ACCOMPLISH A DETAILESDR 2005UALA00582Apu · shutdownDIVERTED DUE TO AUXILIARY POWER UNIT AUTO-SHUTDOWN WITH LEFT GENERATOR DEFERRED INOPERATIVE. UPON LANDING APU FOUND 4.0 QUARTS LOW. MM ADDED OIL. ENGINEERING MONITORING OIL CONSUMPTION. TO DATE CONSUMPTION IS .014 QT/HOUR. LIMIT IS .20 QT/HR. SAMC REQUESTEDSDR 2006UALA01172Latch · wornLT O/W SLIDE DOOR LATCH FAILS EDGE MARGIN CHECK (NR 3 LATCH). REPLACE LATCH IAW 767, MM 25-65-98.SDR 2005UALA00552Bearing · brokenDURING PACKING PROCEDURES, 6 BEARINGS BROKE WHEN TENSION PUT ON BAR. AIRFRAME MANUFACTURER IS AWARE OF THIS ISSUE AND IS EVALUATING CHANGE TO MORE DURABLE BEARING MATERIAL. IN THIS CASE, ALL OF THE BROKEN BEARINGS WERE REPLACED.SDR ANCF200400051Heater · defectiveELECTRICAL SMOKE OF UNKNOW ORIGIN FROM THE CAPTAIN'S SIDE, BETWEEN THE LIGHT CONTROL PANEL AND THE GLARESHIELD PANEL, ACCORDING TO THE ABNORMAL CHECKLIST THE RECIRCULATION FANS AND THE UTILITY BUSES WERE SWITCHED OFF AND THE EQUIPMENT COOLING SELECTOR WAS SELESDR DL76P050307Coupling · crackedFUEL LEAK COMING FROM RT ENGINE AREA. FOUND RT ENGINE FUEL FEED TUBE COUPLING BROKEN. REPLACED SAME.SDR 2005UALA00483Adc · failedFAILURE OF F/O AIR DRIVEN COMPUTER AND ALTIMETER. RT AIR DATA COMPUTER RPL, MR41190, NO DASH, BUT S/N=88041280. A/C HAD PREVIOUS HISTORY ON 18 MAY. NO UNIT HISTORY AVAILABLE IN CIDER FOR THIS S/N, SUSPECT THIS IS 1ST REMOVAL.SDR CA050517001Lock · melted(CAN) FAULT: ELECTRICAL BURNING SMELL NOTED AROUND VCR IN FORWARD GALLEY, LAVATORY AND OVERHEAD AREA. RETURNED. ACTION: BURNED ELEC SMELL LOCATED AS COMING FROM COCKPIT DOOR LOCK SOLENOID. SOLENOID AND HARDWARE REMOVED AND PLACED IN PLASTIC BAG IN OPB. AREA SDR CA050516001Tire · failedFOUND NR 1 MAIN WHEEL RECAP, 3/4 THICK, MISSING. TIRE PRESS STILL 220PSI. NR 1 MAIN WHEEL CHANGED AS PER MM32-45-01.SDR 2006UALA01168Latch · failedLT O/W SLIDE COMPT DOOR DISCONNECT HOUSING HAS FAIL CHECK. REMOVE AND REPLACE REF: UALB767 MM 25-65-98.SDR 2005UALA00392Floorbeam · puncturedE&E COMPARTMENT BS 246 FLOORBEAM WEB PUNCTURED APPROX RBL 45, WL 200. REPAIRED FLOORBEAM WEB.SDR 2005UALA00395Wire · brokenRAM AIR TURBINE FAILURE. DURING ROUTINE MAINTENANCE CHECK, A DISCREPANCY WAS NOTICED ON THE RAT SPEED SENSING. UPON FURTHER TROUBLESHOOTING, A WIRE INSIDE THE RAT SPEED SENSOR WAS FOUND BROKEN. AFTER REPAIR, THE RAT TEST WAS COMPLETED SUCCESSFULLY.SDR 2005UALA00389Bulkhead · damagedNOSE WW BULKHEAD HAS DAMAGE. AUX NOSE JACK ACCIDENTALLY OVERLOADED. BOEING AOG TEAM PERFORMED PERMANENT STRUCTURE REPAIR TO STATION 287 BULKHEAD ASSY AND REPLACED DAMAGED SKIN PANEL.SDR 2006UALA01164Latch · failedLT OFFWING SLIDE LATCH CHECK FAILS TORQUE CHECK. TORQUE TO OPEN 200 IN/LBS, MAX ALLOWED 175.
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