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 DL76L081450Shutoff Valve · faultedLEFT ENG ANTI-ICE AFTER TAXI. FOUND HPSOV AT FAULT. FWD TO MEL.SDR DL757081457Channel · corrodedCORROSION SUPPORT CHANNEL FWD OF AFT DUMP VALVE IS CORRODED BS 1685, RBL 14-24. REMOVED AND REPLACED SUPPORT CHANNEL DUE TO OUT OF LIMITS CORROSION.SDR DL757081458Channel · corrodedSUPPORT CHANNEL INBD OF AFT DUMP VALVE CORRODED ALL THE WAY THROUGH BS 1690 RBL 10. REMOVED AND REPLACED CHANNEL DUE TO OUT OF LIMITS CORROSION.SDR DL757081459Channel · corrodedSUPPORT CHANNEL AFT OF AFT DUMP VALVE IS CORRODED BS 1690 RBL 24. REMOVED AND REPLACED SUPPORT CHANNEL DUE TO OUT OF LIMITS CORROSION.SDR 2008UALA06281Generator · malfunctionedLOST RT GENERATOR AND APU. FLIGHT DIVERTED. NR 2 ENGINE GENERATOR REPLACED. (OFF: P/N 745329C, S/N G0796)
SDR 2008UALA06298Wire · exposedWIRES EXPOSED ON EMERGENCY FLOOR LIGHTS.
SDR UALA2008111306298Wire · exposedWIRES EXPOSED ON EMERGENCY FLOOR LIGHTS. REPLACED EEL LIGHT STRIP AND COVER.SDR UALA2008111306281Generator · failedLOST RT GENERATOR AND APU. FLIGHT DIVERTED. NR 2 ENGINE GENERATOR REPLACED. APU REPLACED (P/N 3800298-1-7). AFTER APU REPLACEMENT FAULT LIGHT AND MSG FUEL SEL VLV. REPLACED FUEL CONTROL UNIT (P/N 3882500-17), NO HELP. REPLACED APU CONTROLLER (P/N 2117342SDR DL757081439Battery Pack · inoperativeFOUND SEVERAL EMERGENCY LIGHTS INOP IN PASSENGER COMPARTMENT. REMOVED AND REPLACED L-2 DOOR EMERGENCY LIGHTS BATTERY PACK, AND RELAMPED SEVERAL EMERGENCY LIGHTS PER AMM 33-51-07-902-001 AND PERFORMED SATISFACTORY OPS CHECK PER AMM 33-51-00-715-075.SDR DL764081444Flap System · malfunctionedRTB DUE TO T/E FLAP DISAGREE MSG ON TAXI. FLAP SELECTED 15 W/ONLY SLAT MOVEMENT. T/S PER FIM. RAN FLAP/SLATS. NO FAULTS. OK FOR SERVICE.SDR DL757081453Splice · corrodedCORROSION FWD CARGO BAY FLOOR PANEL SPLICE AT BS 748, RBL 13-20. REMOVED AND REPLACED SPLICE DUE TO CORROSION OUT OF LIMITS IAW SRM 51-40-02.SDR 2008UALA06270Blade · damagedNUMEROUS FAN BLADES HAVE SMALL NICKS & DENTS ON BOTH NR 1 & NR 2 ENGINES.SDR UALA2008112006595Switch · malfunctionedAFTER RT OVERWING SLIDE DEPLOYMENT, FOUND FWD RT OVERWING EXIT DOOR AUTO ARM AND AUTO FIRE SWITCHES NOT IN THE FULLY DOWN POSITION.SDR UALA2008111306270Fan Blade · dentedNUMEROUS FAN BLADES HAVE SMALL NICKS & DENTS ON BOTH NR 1 & NR 2 ENGINES. ALL DAMAGED FAN BLADES BLENDED ON BOTH NR 1 & NR 2 ENGINES.SDR DL76P081438Line · leakingAIRCRAFT ATB FOR NR 2 ENG LOSS OF OIL QTY AND OIL PRESSURE. CREW SHUT DOWN ENGINE PRIOR TO LANDING. T/S IN PROGRESS AIR/OIL COOLER OIL RETURN LINE FOUND CRACKED. REPLACED NR 2 ENGINE.SDR DL76P081462Engine · failedOIL LOSS IN FLIGHT AND IFSD. REPLACED RT ENG PER TRANSMITTAL 1T149AD9.SDR DL76L081430Engine · malfunctionedAFTER LEVEL OFF AT FL 364 THE LEFT ENGINE SPOOLED BACK ON ITS OWN FOLLOWED BY NUMEROUS EEC AND ENGINE OUT MESSAGES. T/S PER FIM INSPECTION FUEL SAMPLES PLUS NR 1 ENG FUEL FILTER FOR CONTAMINATION. FILTER PLUS FUEL SAMPLE FOUND CLEAN C/W ENG FU SUCTION FEED OSDR 2008UALA06273Attach Fitting · crackedLT WING OUTBOARD FLAP, OUTBOARD, AUX TRACK ATTACH FITTING TO RS, IS CRACKED. REPLACED FITTING.SDR 2008UALA06258Slide · blownRT OFF-WING SLIDE DEPLOYED DURING RE-ACTIVATION PROCEDURE. FOUND RIGHT OFF WING SLIDE SPOILER OVERRIDE ACTUATOR BLOWN. REPLACED INFLATION CYLINDER.SDR UALA2008111306273Fitting · crackedLT WING OUTBOARD FLAP, OUTBOARD, AUX TRACK ATTACH FITTING TO RS, IS CRACKED. REPLACED FITTING.SDR UALA2008111306257Control Unit · faultyRUDDER AND AILERON TRIM EXCESSIVE WITH AILERON DEFLECTED. SUSPECT LEFT INBD AILERON STUCK IN UP POSITION, AS IND ON EICAS FLT CONT, IS DEFLECTED APPX HALF UP AND NOT RESPONDING TO INPUT. RUDDER AND AIL TRIM IS EXCESSIVE. AILERON FOR 6 HRS WAS ABOUT HALF DEFSDR HALA2008102300814Starter · malfunctionedETOPS SIGNIFICANT SYSTEM - RETURNED TO GATE. RIGHT ENGINE STARTER FAILED TO ACCELERATE PAST N2 10 PERCENT. MAINT REQUESTED TO EXAMINE PROBLEM. REMOVED AND REPLACED STARTER ASSY PER AMM 80-11-01. OPS CHECK OK.SDR HALA2008102300823Starter · malfunctionedETOPS SIGNIFICANT SYSTEM - RETURNED TO GATE. RIGHT ENGINE STARTER FAILED TO ACCELERATE PAST N2 10 PERCENT. MAINT REQUESTED TO EXAMINE PROBLEM. REMOVED AND REPLACED STATER ASSY PER AMM 80-11-01. OPS CHECK OK.SDR HALA2008102300825O-Ring · deterioratedETOPS SIGNIFICANT SYSTEM - NR 1 ENGINE OIL CONSUMPTION RATE HIGH. T/S PER FIM 71-05-00 & 71-08-00-101 FOUND OIL TANK SERVICE CAP O-RING DETERIORATED REPLACED O-RING AND GRD ENGINE RUN LEAK CHECK GOOD.SDR 2008UALA06259Power Supply · dischargedDURING TAXI IN, F/A REPORTED ESCAPE PATH LIGHTING CYCLING OFF AND ON. REPLACED M1557 BATTERY PWR SUPPLY. GOOD OP CHECK.SDR 2008UALA06212Anti-Ice System · malfunctionedCREW REPORT: WING ANTI ICE DISAGREEMENT L-R.
SDR UALA2008111306212Relay · faultyCREW REPORT: WING ANTI ICE DISAGREEMENT L-R. ACP T-S REF MM30-11-00 PG1 04 FIG 103 AND WD 30-11-11, REPLACED RELAYS K414, K520, K1156 AND K1155. REPLACED TEST SWITCH ON P61 PANEL. ALL TESTS AND OPS CHECKS SATISFACTORY.SDR DL76L081625Engine · failedNR 2 ENGINE FAILED 25 CYCLE RE-INSPECT OF GEARBOX FOR BLAST CONTAMINANT. REPLACED NR 2 ENGINE.SDR DL76L081394Nozzle · failedNR 1 ENG FAILED INSPECTION OF MAIN GEARBOX OIL NOZZLES PER EA-51470869-12. C/W EA 51-470869-12 FOUND CONTAMINATES IN BOTH NOZZLES. REQUIRES ENG CHG. REPLACED NR 1 ENG PER R/C TRANSMITTAL 23-.SDR 2008UALA06223Rib · crackedLT WING O/B LEADING EDGE CAVITY, LWR RIB FWD END CRACKED AT OFSS 688. MAJOR REPAIR ACCOMPLISHED. REMOVED RIB, INSTALLED NEW RIB AND LOWER STRUT.SDR 2008UALA06224Rib · crackedLT WING O/B LEADING EDGE CAVITY LWR RIB FWD END CRACKED AT OFSS 547. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED DOUBLER TRIMMED DAMAGE AND INSTALLED DOUBLER.SDR 2008UALA06226Slide · faultyLT OVERWING SLIDE IS FAULTY.SDR UALA2008111306226Slide · no testDURING LT OVERWING SLIDE DEPLOYMENT TEST, AFT HATCH STEP FAILED TO DROP DOWN, CABLE KINKED, STEP WILL NOT DROP FREELY. REPLACED AFT SUPPORT CABLE. OPS CHECKS GOOD. SLIDE FAULTY. AFTER CHECKING THE SLIDE SYS OUT, VERIFIED THE BOTTLE PRESSURE AND WHITE DISKSDR 2008UALA06192Engine · stalledTWO ENGINES STALLED AT FL380.SDR 2008UALA06193Wire Harness · corrodedAPU POWER CABLE (W236-006-1-0) HAS A CORRODED SPLICE CAUSING OVERHEAT AT BS 1783-1800 IN EMPENNAGE COMPARTMENT BELOW HORIZ STAB RIGHT SIDE. REMOVED AND REPLACED HARNESS ASSY. INSTALLED ASSOCIATED SPLICES FOR HARNESS. OPS CHECK OF APU GENERATOR GOOD.SDR 2008UALA06194Relay · damagedRELAYS K417 AND K383 IN P-19 PANEL SHOW SIGNS OF OVERHEATING. REMOVED AND REPLACED RELAYS. PERFORMED A GOOD OPS CHECK OF THE NS-FSB SIGNS AND OPS CHECK OF L-1 DOOR.SDR 2008UALA06196Flange · brokenNR 1 ENG ANGLE GEAR BOX AFT END HAS LOOSE BOLTS AT 12:00 AND FLANGE EAR IS BROKEN AT 1:00.SDR DL757081455Pan · crackedAFT LAV PAN CRACKED AROUND RIGHT DUMP VALVE T HANDLE CUTOUT. REPAIRED PER ER/A 465404-14 REV ORG.SDR UALA2008111306194Relay · damagedRELAYS K417 AND K383 IN P-19 PANEL SHOW SIGNS OF OVERHEATING. REMOVED AND REPLACED RELAYS. PERFORMED A GOOD OPS CHECK OF THE NS-FSB SIGNS AND OPS CHECK OF L-1 DOOR.SDR UALA2008111306192Engine · stalledTWO ENGINES STALLED AT FL380. DFDR INVESTIGATION REVEALED THAT ONLY THE NUMBER 2 ENGINE STALLED. AIRPLANE ENCOUNTERED AN ATMOSPHERIC WAVE AT .80 MACH CAUSING AUDIBLE COMPRESSOR STALLS AND A FLUCTUATION IN THE MACH METER FROM .75 TO .84 RETURNING TO .80. CRESDR UALA2008111306196Gearbox · damagedNR 1 ENG ANGLE GEAR BOX (AGB) AFT END HAS LOOSE BOLTS AT 12:00 AND FLANGE EAR IS BROKEN AT 1:00. REPLACED NR 1 ENGINE. ENGINE WAS SUBSEQUENTLY FIELD REPAIRED. THE ANGLE GEARBOX (AGB), HORIZONTAL DRIVESHAFT, AND CP07 FUEL TUBE WERE REPLACED.SDR 2008UALA06186Spring · weakL1 DOOR GAS SPRING WEAK. REMOVED AND REPLACED GAS SPRING. OPS CHECK GOOD.SDR 2008UALA06187Terminal · overheatedP19 PANEL, T180 AND T184 TERMINAL LUGS SHOW SIGNS OF OVERHEATING. REMOVED AND REPLACED TERMINAL LUGS. OPS CHECK GOOD OF FWD INDIRECT CEILING LIGHTS AND SIDEWALL LIGHT.SDR DL757081432Floor Support · corrodedCORROSION IN AND AROUND FASTENER AND HOLES AT BS 791-818 RBL 7 FLOOR STRINGER. FLOOR STRINGER REMOVED AND REPLACED DUE TO CORROSION OUT OF LIMITS IAW SRM 51-40-02.SDR DL757081443Stringer · corrodedCORROSION IN AND AROUND FASTENERS AND HOLES AT BS 814-BS 840 RBL 16 FLOOR STRINGER. REMOVED AND REPLACED DUE TO CORROSION OUT OF LIMITS IAW SRM 51-40-02.SDR DL757081452Floorbeam · corrodedCORROSION IN AND AROUND FASTENER HOLE AT BS 739, RBL 9 FLOORBEAM, OUT OF LIMITS. REPAIRED PER DELTA ER/A 465406-14 REV ORIG.SDR DL76L081373Start Valve · failedLEFT ENGINE START VALVE FAILED TO OPEN. CONFIRMED START VLV INOP. PERF MANUAL START FWD TO MCO AND PLC PER MEL 80-00-02.SDR 2008UALA06164Heater · odorELECTRICAL ODOR IN FLIGHT DECK. FLIGHT DIVERTED. IDENTIFIED CAUSE TO THE FO'S NR 1 WINDOW HEAT LOWER AFT CONNECTION AND ASSOCIATED WIRES AND CONTACTS. TURNING OFF WINDOW HEAT INDUCED CESSATION OF ODOR. AREA COOLED TO NORMAL TEMPERATURE. REPLACED FIRST OFFISDR 2008UALA06172Lamp · inoperativeEXTERIOR EMERGENCY LIGHT AT DOOR 2L INOP. RELAMPED EMERGENCY LIGHT. OPS CHECK PASSED.SDR 2008UALA06132Warning System · activatedAFTER T/O, AIR-GND DISAGREE STATUS MSG. RTFL.
Back to Pratt & Whitney PW4060