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 2004UALA00500Scanner · inoperativeFLIGHT DIVERTED DUE TO LOSS OF WEATHER RADAR. THE WEATHER RADAR SCANNER UNIT WAS DEFECTIVE . SCANNER WAS REPLACED.SDR 2004UALA00483Fitting · crackedRT WING INBOARD FLAP, MIDDLE T/E HINGE FITTING IS CRACKED AT SPAR. INSTALLED ANGLE REPAIR.SDR 2004UALA00484Fitting · crackedLEFT INBOARD T/E MAIN FLAP MIDDLE AFT FLAP HINGE FITTING CRACKED ON INBOARD SIDE NEAR FLAP AFT SPAR. INSTALLED ANGLE REPAIR.SDR 2004UALA00485Stiffener · crackedSTA 246 FLOORBEAM RBL 46 FWD SIDE STIFFENER CRACKED (BUCKLED). MAJOR REPAIR ACCOMPLISHED. REPLACED STIFFENER.SDR 2004UALA00501Bulb · incorrectE&E SMOKE DETECTOR FAILS TEST. REPLACED E&E SMOKE DETECTOR. INCORRECT BULB INSTALLED. FOUND BULB ML382 INSTALLED, SHOULD BE CM382AS10.SDR 2004UALA00465Wire · damagedRIGHT SIDE AISLE NEXT TO MID GALLEY 1 EEL LIGHT STRIP SECTION OUT. *S/D* REPLACED CABLE AND SPLICED IN A NEW SECTION.SDR 2004UALA00412Window · vibratesRETURNED TO FIELD WITH A COCKPIT WINDOW VIBRATION. THE VIBRATION WAS CAUSED BY A LOOSE TAPE THAT WAS APPLIED ON WINDOW 3L TO PROTECT UNCURED (SOFT) SEALANT. THE SEALANT WAS APPLIED WHEN THE EXISTING NR 3L WINDOW WAS REPLACED,SDR 2004UALA00437Display · malfunctionedWX RADAR GREEN BAND RING DISPLAY AT APPROX 6.5 MILE IN FRONT OF ACFT. RADAR DISPLAYS A GREEN ARC THAT SEEMS TO MOVE WITH RADAR TILT.SDR 2004UALA00399Light · inoperativeFWD GALLEY EEL STRIP IS INOPERATIVE. REPAIRED EEL FEEDER. CHECKS GOOD.SDR 2004UALA00400Radar · failedDIVERTED TO MIA DUE TO LOSS OF WEATHER RADAR. FLIGHT CREW REPORTED A GREEN BAND ON THE RADAR DISPLAY APPROX. 6.5 MILES IN FRONT OF AIRCRAFT. MAINTENANCE REPLACED C-BAND WX RADAR CONTROL PANEL. SHOP FOUND CONTROL PANEL TILT CONTROL MISADJUSTED TO 14.5 DEGREESSDR 2004UALA00377Light · inoperativeEEL FLOOR PATH LIGHT STRIP AT MID GALLEY RT INOPERATIVE. REPAIRED DAMAGED SECTION. OPS CHK'D NORMAL.SDR 2004UALA00371Connector · looseLT OVERWING SLIDE SQUIB TEST FAILED. PROBLEM CAUSED BY LOOSE CONNECTORS. PROBLEM CLEARED BY RE-SEATING CONNECTORS ON BACK OF FLIGHT DECK PANEL.SDR DL76L040348Start Valve · malfunctionedLEFT STARTER CUTOUT EICAS MSG AND VALVE LIGHT ILLUMINATED ON TAKEOFF. FOLLOWED QRH. START VALVE REPLACED.SDR 2004UALA00357Engine · vibrationREPORTS OF VIBRATION NR 2 ENGINE. DUE TO REPORTS OF ENGINE VIBRATION THE ENGINE WAS BOROSCOPED, CHIP DETECTORS INSPECTED AND INLET AND EXHAUST CHECKED. NO DEFECTS NOTED. THE ENGINE THEN HAD A TRIM BALANCE AND RETURNED TO SERVICE.SDR 2004UALA00346Hydraulic System · leakingRETURNED TO THE FIELD DUE TO HYDRAULIC FLUID LOSS AND UNSUITABLE WEATHER. ACTUAL FLUID LOSS UNDETERMINED, NO SIGNIFICANT LEAKS FOUND AND NO FURTHER LOSS OF FLUID.SDR DL76L040337Carbon Seal · leakingMID CABIN SMOKE DETECTORS AND AFT CABIN SMOKE DETECTORS CAME ON SHORTLY AFTER T/O, NOTICED MUSTY ODOR AND AGAIN AT TOD IN PASSENGER CABIN. ATL MAINT ALSO FOUND OIL LEAK AT NR 2 ENG INLET. FOUND 100 CCS OIL IN NR 2 ENG INTAKE. SUSPECT FROM FRAME LE OIL CONSUSDR 2004UALA00303Solenoid · failedRIGHT ENGINE COMPRESSOR STALLS. CREW REPORTED SURGE. AIRCRAFT SYSTEM DID NOT CONFIRM THE SURGE EVENT. ALL TROUBLESHOOTING WAS ACCOMPLISHED AND THE 2.9 BLEED SOLENOID WAS REPLACED.SDR 2004UALA00301Connector · looseEICAS MESSAGE, RIGHT ENGINE FUEL FILTER DISPLAYED DURING CLIMBOUT. FUEL FILTER DIFFERENTIAL PRESSURE SWITCH WAS REPLACED. THE SWITCH WAS TESTED IN THE SHOP, AND FOUND TO BE SLIGHTLY OUT OF CALIBRATION, BUT NOT ENOUGH TO CAUSE THE EVENT. AS A RESULT OF SHOP SDR 2004UALA00290Squib · inoperativeLEFT OVERWING ESCAPE SLIDE SQUIB TEST LIGHT DOES NOT WORK WHEN PRESSED TEST NR 1. RESEATED PLUGS ON BACK OF TEST PANEL - -TESTS OK.SDR 2004UALA00281Slide · unserviceableDOOR 1 LEFT SLIDE RAFT PRESSURE AT 2500 PSI. REPLACED 1L DOOR ESCAPE SLIDE.SDR 2004UALA00280Battery Pack · dischargedEMERGENCY EXIT LIGHTS INTERMITTENT ROWS 15-18 LEFT SIDE. REPLACED EEL BATTERY POWER SUPPLY PACK.SDR 2004UALA00263Support · crackedRIGHT INBOARD FLAP, CENTER SUPPORT IS CRACKED ON THE LOWER INBOARD FLANGE AT THE MID FLAP ATTACH POINT. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR TO HINGE FITTING.SDR 2004UALA00264Battery Pack · inoperativeRIGHT EMERGENCY LIGHT PATH INOP FROM 15 THROUGH ROW 18. REPLACED EMERGENCY LIGHT BATTERY PACK, CHECKED OK.SDR 2004UALA00262Fitting · crackedRIGHT INBOARD T/E FLAP, MAIN FLAP INBOARD T/E HINGE FITTING SUPPORT CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCMENT REPAIR ANGLE TO HINGE FITTING.SDR 2004UALA00258Hinge · crackedLEFT WING INBOARD FLAP MAIN TO AFT FLAP HINGE IS CRACKED ON BOTH SIDES. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIRS.SDR 2004UALA00259Stiffener · crackedSTA 246 FLOORBEAM VERTICAL STIFFENER IS CRACKED AT LBL 23. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STIFFENER.SDR 2005UALA00243Compressor · stalledFLIGHT ABORTED TAKEOFF DUE TO A COMPRESSOR STALL IN THE NR 1 ENGINE. ABORTED TAKEOFF AT 100 KIAS DUE TO COMPRESSOR SURGE. ENGINE REPLACED AT EZE. UA TURBINE SHOP FINDINGS: N2 WILL NOT ROTATE. ALSO, BORESCOPE INSPECTION REVEALED HEAVY HPC 5TH STAGE BLADE DSDR 2004UALA00213Warning Light · illuminatedSTABILIZER TRIM ADVISORY ILLUMINATED DURING TAKEOFF ROLL. UNABLE TO DUPLICATE DURING TROUBLE SHOOTING. ACCOMPLISHED ADDITIONAL TROUBLE SHOOTING AS A PRECAUTION. NO FAULTS FOUND. NO ADDITIONAL INCIDENTS NOTED.SDR 2004UALA00152Light · inoperativeEXTERIOR EMERGENCY LIGHT INOP AT LT FUSELAGE AFT OF TRAILING EDGE. RELAMPED, CHECKED OK.SDR 2004UALA00167Wire · damagedWIRE DAMAGE AFT CARGO PIT STA 1230. THERE WAS NO CONCLUSIVE INDICATION OF WHAT INITIATED THE WIRE DAMAGE. THERE WAS NO APPARENT CHAFING. THERE WERE METAL CHIPS NOTED IN THE AREA, BUT NONE FOUND DIRECTLY ON OR BELOW THE WIRE BUNDLE. IT IS UNKNOWN, AS TO WHETHERSDR 2004UALA00133Light · inoperativeEMERGENCY EXIT LIGHT AT NR 2AB ROW INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT, OPS OK.SDR 2004UALA00131Autothrottle Sys · malfunctionedFLIGHT ABORTED TAKEOFF AT 100 KTS DUE TO AUTOTHROTTLE INDICATION. RETURNED TO BLOCKS. THRUST MANAGEMENT COMPUTER WAS REMOVED AS A PRECAUTION. UNIT CHECKED OK IN THE SHOP. MCDP FAULT DATA DID NOT RECORD ANY TMC-RELATED FAULTS DURING THE EVENT. REASON FOR TSDR 2004UALA00118Jackscrew · failedFLIGHT DIVERTED DUE TO LEFT PACK TEMPERATURE CONTROL MESSAGE AND LIGHT. THE LEFT PACK INLET ACTUATOR WAS FOUND MECHANICALLY FROZEN. THE JACK SCREW ASSEMBLY FAILED. THE ACTUATOR WAS REPLACED AND NO FURTHER PROBLEMS WERE REPORTED.SDR 2004UALA00111Light · inoperativeEXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE, 4TH LIGHT AFT OF OVERWING, LT SIDE. RELAMPED. CHECKS GOOD.SDR DL76L040141Engine · stalledNR 2 ENG STALLED ON TAKEOFF ROLL 110 KNOTS, RT ENG SURGE DET ON EICAS ENG EXCT RECORD 660 FOR 12 SEC. REPLACED NR 2 ENG S/N 723843 PER TRANS 1T149.SDR 04FDEA00304Engine · malfunctionedDURING CLIMBOUT IN VMC NR 2 ENG (LOUD NOISE) FROM TAIL AREA. NEXT HIGH EGT (RED) AND VIBRATION. REF QRH SHUT NR 2 ENG DOWN. LANDED RPLL. CREW DEBRIEF AT CLIMBOUT 19,000 FT ENCOUNTERED LOUD NOISE FROM TAIL AREA AND VIBRATION, PERFORMED WALK-AROUND INSPECTIOSDR CA040127011Gear · inoperative(CAN) WHEN GEAR WAS LOWERED, NOSE DID NOT LOCK. CREW WAS ABLE TO EXTEND AND LOCK USING THE ALTERNATE METHOD, CONTINUING THE LANDING WITHOUT FURTHER INCIDENT. ACFT REMOVED FROM SERVICE FOR INVESTIGATION.SDR 2004UALA00049Battery · inoperativeEMERGENCY EXIT PATH LIGHTS ROW 15-17 BLINK ON AND OFF. REPLACED M737 BATTERY ASSEMBLY.SDR 2004UALA00417Warning System · activatedFUEL CONFIGURATION LIGHT ON 1 HOUR INTO FLIGHT. FUEL IMBALANCE.SDR CA040120001Windshield · broken(CAN) WHILE IN FLIGHT, R1 WINDSHIELD OUTER PANE SHATTERED. (FL370) R1 WINDOW REPLACED IAW AMM 56-11-01 REMOVED: UNI 56-10-0174 MPN: 141T4801-50 INSTALLED: UNI 56-10-0174 MPN: 141T4801-50SDR 2004UALA00415Squib · blownRT OVERWING SLIDE DOOR SQUIB BLOWN. SQUIB BLOWN IN CONJUNCTION WITH INADVERTANT SLIDE DEPLOYMENT. SQUIB REPLACED.SDR CA040113004Windshield · failed(CAN) WHILE IN FLT ENROUTE FROM YYZ TO TLV, R1 WINDSHIELD OUTER PANE SHATTERED. FLT CONTINUED WITHOUT FURTHER INCIDENT. MTCE POOLED A WINDOW AND CHANGED.SDR 2004UALA00047Wedge · dentedT/E WEDGE DENTED ON UPPER SURFACE OF NR 4 SLAT. MAJOR REPAIR. REPLACED WITH NEW T/E WEDGE.SDR 2004UALA00419Light · malfunctionedEEL LIGHTS BLINKING FROM ROWS 20 TO 28 CHECKED SYSTEM PER WDM33-51-11 & 33-51-14, SPLICES SM42, SM41,SM5 OVER M1559 OK. SPLICES SM44, SM43 & SM45 OVER M1556 ALSO OK.SDR 2003UALA00978Wire · brokenEMERGENCY LIGHT INOP AT DR1 FWD CROSSAISLE. REPLACED BROKEN FEEDER CABLE. OPS CKD NORMAL.SDR 2003UALA00967Light · inoperativeEXTERIOR EMERGENCY LIGHT INOPERABLE AT DOOR 4L. RELAMPED, OPS CHECKED NORMAL.SDR 2003UALA00948Skin · crackedCRACK ON FWD UPPER PYLON SKIN INSIDE ACCESS PNL 432BR, NR 1 ENG. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00946Skin · dentedTWO EACH SKIN DENTS WITHIN 22 INCHES OF E&E BAY DOOR, ONE BETWEEN STATION 303 & STATION 325 (STR35L). MAJOR REPAIR ACCOMPLISHED. REPAIRED PER SRM 51-00-01.SDR 2003UALA00947Bolt · missingRETURN TO FIELD DUE TO GEAR DISAGREEMENT EICAS MESSAGE. DAMAGE INCURRED FROM HANGING BRAKE ROD AFTER SEPARATION FROM BRAKE. ROD BELIEVED TO HAVE DETACHED FROM TORQUE ARM DUE TO MIGRATION OF BRAKE TORQUE ARM PIN. SAFETY BOLT BELIEVED TO HAVE COME LOOSE OR POSDR 2003UALA00936Wire Harness · damagedEMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT NEAR GALLEY 402. ACCOMPLISHED WIRE BUNDLE REPAIR PER MM 33-51-10-301. DEVICE WORKS FINE.
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