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 2004UALA00943Floorbeam · crackedFLIGHT DECK FLOORBEAM AT STA 246 FORWARD FACE STIFFENER CRACKED LOWER CORNER AT LBL 25. BOEING SERVICE BULLETIN RECOMMENDED ROUTINE INSPECTION IN PLACE TO MONITOR THIS CRACKING OF STA 246 FLOORBEAM. CRACKING OCCURS DUE TO HIGHER THAN INITIALLY ANTICIPATED LOSDR 2004UALA00939Hydraulic System · leakingFLIGHT DIVERTED DUE TO RIGHT HYDRAULIC SYSTEM QUANTITY LOSS. REPLACED RIGHT SYSTEM EDP. NO FURTHER REPORTS NEXT 20 AC CYCLES.SDR 2004UALA00960Light · inoperativeEEL LIGHTS INOP BY ROWS 15AB THRU 19AB. REPLACED POWER STRIP.SDR 2004UALA00924Floorbeam · crackedFLOORBEAM STA 246 STIFFENER AT APPROX RBL 20 IS CRACKED. CRACK CAUSED BY CYCLIC DEFLECTION FATIGUE. FABRICATED & INSTALLED NEW STIFFENER.SDR 2004UALA00925Hinge Fitting · crackedLT WING IB FLAP OB HINGE FITTING CRACKED AFT VANE. SUPPLEMENTAL DATA UPDATE REPAIRED FITTING WITH ANGLE AND FILLER REPAIR.SDR 2004UALA00921Floorbeam · crackedFLOORBEAM STA 246 STIFFENER AT RBL 15 IS CRACKED. CRACKS CAUSED BY CYCLIC DEFLECTION FATIGUE. FABRICATED AND INSTALLED NEW BRACKET.SDR 2004UALA00926Idg · vibrationDIVERTED WHEN LEFT ENGINE INDICATED IDLE FUEL FLOW AND IDLE THRUST. SHOP FOUND LOG PISTON FAILURE ON REMOVED LT IDG. CORRESPONDENCE BETWEEN COMPONENTS ENGINEERING, POWER PLANT ENGINEERING, SUNDSTRAND, AND PWA, INDICATES THERE IS A POTENTIAL ANOMALY FOR A WORSDR 2004UALA00894Check Valve · failedNR 2 ENGINE COMPRESSOR STALL. REPLACED ENGINE DUE TO UNABLE TO ROTATE. UPON SHOP TEARDOWN OF ENGINE, ROOT CAUSE OF THE SURGE WAS DETERMINED TO BE CATASTROPHIC FAILURE OF THE PNEUMATIC 8TH STAGE CHECK VALVE.SDR DL76L040940Engine · shutdownAT TOD - A/T ON LEFT ENGINE SHUTDOWN, RESTARTED AFTER 5 MINUTES. UNDER INVESTIGATION.SDR 2004UALA00911Hinge · crackedRIGHT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP HINGE WITH REPAIR ANGLES AND FILLER.SDR 2004UALA00912Seat Track · crackedMAIN CABIN SEAT TRACK LBL 88 AT BS 747.5 TO 808 BROKEN, CRACKED AND CORRODED. DAMAGED SEAT TRACK REPLACED.SDR 2004UALA00913Spar · crackedNR 2 NACELLE UPPER SPAR WEB IS CRACKED SEVERAL PLACES AS SEEN THROUGH ACCESS 446BL. REPAIRED UPPER SPAR WEB WITH DOUBLER AND FILLER JUST FWD OF PYLON AFT BLKHD PER SRM 54-53-01, FIG 208. PER SB 767-54-0092 R1 PROBABLE CAUSE OF CRACKING IS FLEXING OF PYLON MISDR 2004UALA00914Hinge · crackedLEFT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE WITH REPAIR ANGLES.SDR 2004UALA00909Arm · crackedLT IB AFT FLAP, IB HINGE ARM CRACKED BOTH SIDES AT ATTACH POINT TO MAIN FLAP. REPAIRED & INSTALLED FITTING.SDR 2004UALA00908Seat Track · crackedMID CABIN SEAT TRACK AT STA 725 AND STA 759, APPROX LBL 90, AFT END CRACKED. *S/D* DAMAGED SEAT TRACKS WERE REPLACED.SDR 2004UALA00910Support Fitting · crackedRIGHT WING INBOARD MAIN FLAP REAR SIDE LINKAGE SUPPORT FITTING CRACKED, INBOARD AND OUTBOARD SIDES. MAJOR REPAIR ACCOMPLISHED. REPAIRED & INSTALLED SUPPORT FITTING.SDR DL76L040861Combust Chamber · crackedENGINE FAILED BORO OP 5067 COMBUSTION CHAMBER LINER CRACKED. REPLACED ENGINE.SDR 2004UALA00841Control Unit · malfunctionedELECTRICAL UTILITY BUSS PROBLEM. LT AND RT UTILITY BUSS TRIPPED ABOUT 20 MINUTES OUT. UNABLE TO RESET AND THE AIRCRAFT RETURNED TO IAD. RELAYS K148 (SYS 1 AIR/GND) AND K10109 (UTIL/GALLEY PWR FLT RESET) WERE REPLACED AS A PRECAUTION. M116 BUSS POWER CONTROSDR DL76L040850Valve · malfunctionedABORTED T/O PRIOR TO 80 KTS EICAS CAUTION LT ENGINE PRV W/AURAL CHIME. STATUS MSG L IDG VALVE. REMOVED AND REPLACED LT ENGINE PRV VALVE AND CONTROLLER. AIR SUPPLY BITE FAULTS PRV PRC AND FAS LAST 2 LEGS. FAULTS CLEARED ERASED. RAN ENGINE TO BLEED SHIFT ANSDR 2004UALA00915Seat Track · crackedCABIN SEAT TRACK STA 755, AND RBL 85 CRACKED. DAMAGED SEAT TRACK REPLACED.SDR 2004UALA00808Outflow Valve · failedFLIGHT RETURNED TO FIELD WITH CABIN PRESSURE FAULTS. THE EQUIPMENT COOLING OVERBOARD EXHAUST VALVE FAILED. THE VALVE WAS NOT DEACTIVATED PER THE MEL CAUSING A LOSS OF CABIN PRESSURIZATION ON THE SUBSEQUENT FLIGHT. THE VALVE WAS RE-DEFERRED PER THE MEL AND REPLSDR 2004UALA00809Floorbeam · corrodedCABIN FLOORBEAM UPPER SURFACE CORRODED, STA 808-813, RBL 57. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SPLICE.SDR 2004UALA00810Hinge · crackedRT INBD AFT FLAP EXTERNAL HINGE IS CRACKED AT THE MID FLAP AFT SPAR. REPAIRED FITTING WITH ANGLE REPAIR.SDR 2004UALA00824Battery Pack · dischargedCABIN DOORS 2R AND 2L EXTERIOR EMERGENCY LIGHTS INOP. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACED BATTERY PACK M734 IN RT AFT CABIN.SDR 2004UALA00825Battery Pack · dischargedDOOR 2R UPPER INTERIOR EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACED BATTERY PACK AT AFT RT ATTENDANTS SEAT.SDR 2004UALA00826Battery Pack · dischargedDOOR 2L UPPER INTERIOR EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACED BATTERY PACK M739.SDR 2004UALA00827Battery Pack · dischargedCENTER LT OVERWING EMERGENCY LIGHT HAS ONE INOP LAMP. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED BATTERY PACK M738 AND RELAMPED LT CENTER OVERWING LIGHT ASSEMBLY.SDR 2004UALA00828Hinge · brokenLT WING, REAR SPAR, OUTBOARD FLAP OUTBOARD HINGE FITTING BROKEN IN HALF. FLAP TRANSMISSION OVER TORQUE LIMIT INDICATOR ALSO POPPED. SUPPLEMENTAL DATA UPDATE, REAR SPAR RIB POST PART NR 113T1369-1 REPLACED. FLAP TRANSMISSION OVERTORQUE LIMIT INDICATOR RESET.SDR 2006UALA01153Latch · wornLT O/W COMPT DOOR LATCH NR 3 PINHOLE EDGE MARGIN WORN BEYOND LIMITS, LATCH REPLACED.SDR 2006UALA01154Latch · failedRIGHT OVERWING DOOR LATCH INTEGRATOR FAILS TORQUE CHECK. REMOVE AND REPLACE LATCHES IAW 767 MM 25-65-98SDR DL76L040811Compressor · stalledDURING ENGINE RUN-UP NR 1 ENGINE STALLED. REPLACED NR 1 ENGINE.SDR DL76L040779Engine · failedIN CLIMB OUT OF VCE. L SCV TEMP 1 AND L SCV TEMP 2 EICAS STATUS MSG DISPLAYED. LATER OIL QTY DROPPED TO 7 THEN 0 FLT DIVERTED TO LGW. LANDED SAFELY OVERWEIGHT/C ADDED 14 QTS OF OIL NO EXTERNAL LEAKS ENGINE CHANGED ETOPS CATEGORY (B): DIVERSION OR TURNBACK.SDR DL76L040781Bearing · leakingNR 2 ENGINE REPLACED DUE OIL LEAK FROM NR 3 BEARING BREATHER.SDR DL76L040800Engine · failedA/C DIVERTED INTO LGW WITH LOW OIL QTY AND STATUS L SAV TEMP 1 AND L SAV 2 ON LWR EICAS. ON ARR OIL UPLIFT REQUIRED 14 QTS. REPLACED ENGINE.SDR 2004UALA00767Pump · leakingLOST RIGHT HYDRAULIC SYSTEM EN ROUTE, CONTINUING TO DESTINATION. LOSS OF PRESSURE DUE TO FAILED NR 2 ENGINE DRIVEN PUMP. PUMP HAS INDICATION OF OVERHEAT CONDITION. NO ADDITIONAL DETAILS FROM OSV REPORTED.SDR 2004UALA00701Control Panel · failedFLIGHT DIVERTED DUE TO WX RADAR FAILURE. CREW REPORTED WX RADAR INOP. DOES NOT PAINT AND GREEN ARC ON DISPLAY. ALSO, NO GROUND RETURNS. ( THE GREEN ARC IS A FLAT PLATE ANTENNA ANOMALY THAT DOES NOT AFFECT WX RADAR PERFORMANCE.) MAINTENANCE REPLACED THE WX RSDR DL76L040703Proximity Switch · malfunctionedAMBER REV ANNUNCIATION OCCURRED ON TAKE/OFF, UPON PUSHING LEVER UP TOWARD TAKEOFF POWER. ANNUNCIATION OCCURRED LESS THAN 40 KNOTS. REPLACED PROX SWITCH.SDR DL76L040684Engine · leakingSMOKE OIL ODOR IN CABIN FOUND OIL LEAK AT THE CARBON SEAL ON THE NR 1 BEARING, REPLACED SEAL.SDR 2004UALA00632Blades · damagedCOMPRESSOR STALL AT ROTATION ON RIGHT ENGINE. RETURN TO FIELD. BOROSCOPE OF ENGINE FOUND COMPRESSOR BLADE DAMAGE AND ENGINE WAS REMOVED FROM THE AIRCRAFT. FINDINGS AT SHOP VISIT FOUND C-5 BLADE WITH A PIECE MISSING FROM THE T/E TIP (APPROX. 0.750 X 0.750 ISDR 2004UALA00621Warning Light · illuminatedRETURN TO FIELD DUE TO RUDDER TRIM PROBLEM. REPLACED RUDDER TRIM ACTUATOR.SDR 2004UALA00618Stiffener · crackedCRACK IN U-STIFFENER BS 246, APPROX RBL 75, FWD SIDE OF FLOORBEAM. FABRICATED & INSTALLED STIFFENER.SDR 2004UALA00610Bearing · burnedELECTRICAL BURNING ODOR IN COCKPIT, FIRST AND BUSINESS. BURNING SMELL WAS CAUSED BY FAILED ROTOR SPIN BEARING IN COCKPIT STANDBY ATTITUDE INDICATOR (SAI). SHOP CONFIRMED SAI HAD OVERHEATED ROTOR BEARING. STATIC INVERTER (ON E1-4 SHELF) ALSO WAS FAILED. UNCSDR 2004UALA00597Hinge · crackedRIGHT INBOARD FLAP-CENTER EXTERNAL HINGE FITTING IS CRACKED ON INBOARD AND OUTBOARD FLANGES AT THE TOP. REPAIRED HINGE WITH REPAIR ANGLES AND FILLERS.SDR DL76L040572Blade · damagedDURING REPLACEMENT OF NR 1 BEARING CARBON SEAL, FOUND DAMAGE TO 5TH STAGE HPC BLADES. FAILED BOROSCOPE INSPECTION. REPLACED ENGINE.SDR 2004UALA00545Control Unit · overheatedLOMBAR CONTROL SEAT 9A IS HOT AND MELTING. REPLACED SWITCH. THE BURNED BACK CYCLER SWITCH WAS AN OLDER, ORIGINAL UNIT. THE ORIGINAL BACK CYCLER SWITCH WAS UPGRADED IN 2001 DUE TO RELIABILITY PROBLEMS. AN IMPROVED, REPLACEMENT SWITCH WAS DEVELOPED AND INTRODUCSDR CA040603006Brake · disintegrated(CAN) NR 5 AFT BRAKE DISINTEGRATED ON T/O. NR 5 BRAKE ASSY REPLACED IAW J/C 6-232A, NR 5 WHEEL ASSY REPLACED IAW J/C 6-232B.SDR DL76L040494Flange · crackedNR 1 ENGINE FLANGE CRACK FOUND DURING ROUTINE BORESCOPE. REPLACING ENGINE.SDR DL76L040499Engine · malfunctionedHARD TO START AND OIL IN THE TAIL PIPE. CHANGED ENGINE.SDR 2004UALA00524Generator · inoperativeRETURN TO FIELD DUE TO L-GENERATOR INOP. TEARDOWN REVEALED THAT THE DIFFERENTIAL AND CLUSTER GEARS WERE SEVERELY DAMAGED BEYOND REPAIR. IT APPEARS THAT SOME KIND OF CONTAMINATION WAS INTRODUCED WHICH EITHER INTERRUPTED/DILUTED THE OIL SUPPLY TO ONE OF THE SDR 2004UALA00509Warning Light · illuminatedRETURNED TO BLOCKS TWICE DUE TO FLAP INDICATIONS.
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