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 DL76L954081Compressor · stalledAT 1,100 FT AFTER T/O, THE LT ENG COMP STALLED AND EGT WENT TO 652 DEGREES. PWR WAS REDUCED TO IDLE AND ENG OPS NOR TO LANDING. REVERSERS NOT USED, OVERWT LANDING ACCOMP VSI 300 FPM SPEED AT 170, LANDING SMOOTH. EVIDENCE OF BIRD STRIKE ON NOSE COWL, PERFORMSDR 95UAL900218Eel · inopEMERGENCY ESCAPE PATH LIGHTING INOP AT GALLEY. REPLACED LIGHT, CHECKS OK.SDR 95UAL900200Seal · stickingFOUND FUEL IN APU OIL SYSTEM AND REPLACED APU PRECAUTIONARY. FUEL CONTROL WAS DISASSEMBLED AND CARBON SEAL ON THE SIDE OF THE FUEL CONTROL SHAFT SEAL WAS FOUND STICKING. SEAL WAS REPLACED.SDR 95UAL900204Fan Blade · bentPOSSIBLE BIRD STRIKE/INGESTION IN LEFT ENGINE, HAD UNUSUAL NOISE AND VIBRATION DURING CLIMB, RETURNED TO LHR. FOUND TWO FAN BLADES WITH BENT LEADING EDGES AT BLADE MID SPAN. REPLACED BENT BLADES AND THEIR MATCHING PAIRS.SDR DL76L953988Eec · malfunctionedRT ENGINE COMPUTED THRUST LIMIT INDICATOR IN EPR GAUGE INDICATES APPROXIMATELY .10 LOW IN CRUISE, LT ENGINE 1.69 RT ENGINE 1.57. REPLACED RT ENG EEC, R/U OK AT HIGH POWER. R/U REP TEST 15 PFHB.SDR 95UAL900183Eel Battery · dischargedEMERGENCY ESCAPE PATH LIGHTING INOP ON THE LEFT SIDE IN FIRST CLASS. REPLACED BATTERY PACK, CHECKS OK.SDR DL76L953925Engine · failedFOUND METAL ON CHIP DETECTORS AND OIL SCREEN. REPLACED ENGINE, ROUTED TO SHOP.SDR DL76L953804Idg · failedDURING CRUISE, HAD RT GENERATOR DRIVE LIGHT. PER POM DISCONNECTED DRIVE, STARTED APU AND AFTER 20 MIN HAD APU LOW OIL STATUS MSG WITH AUTO SHUTDOWN, DIVERTED DUB. REPLACED NR 2 IDG, SERVICED APU WITH OIL AND RETURNED TO SERVICE.SDR 95UAL900132Eel Strip · inopEMERGENCY ESCAPE PATH LIGHTING INOP AT AFT GALLEY BETWEEN DOORS NR 2 LEFT AND NR 2 RIGHT. REPLACE LIGHT STRIP. CHECKS O.K.SDR DL76L953447Compressor · stalledNUMBER 1 ENGINE HAD 2 COMPRESSOR STALLS AT TOP OF CLIMB. LOST LEFT HYDRAULIC SYSTEM FLUID AND OIL QUANTITY WENT TO ZERO. ENGINE WAS SHUTDOWN, AIRCRAFT RETURNED FRA. FOUND TURBINE CASE COOLING TUBING BROKEN, HYDRAULIC PRESSURE LINE LEAKING AT HYDRAULIC PUMP,SDR 95UAL900098Harness · arcedFOUND WIRE BUNDLE ARCING ALONG SIDEWALL FLOOR BETWEEN SEATS 2A AND 3A. FOUND CHAFED WIRES DUE TO CONTACT WITH SIDE WALL GRILL. REPAIRED WIRES. SYSTEM OPS CHECKS OK.SDR DL76L953319Charger · malfunctionedMAIN BATTERY CHARGER EICAS STATUS MESSAGE OCCURED AFTER T/O JFK - DIVERTED TO BOSTON. REPLACED MAIN BATTERY CHARGER AND INSPECTED BATTERY GRD CABLE FOR CORROSION, NONE FOUND. BATTERY CHARGER OPS CKS. NML PER M/M PERFORMED OVERWEIGHT LNDNG INSP AND OVERWATERSDR 95UAL900057Eel Battery Pack · dischargedEMERGENCY LIGHTS RT SIDE NR 5, 6 AND 7 ARE OUT. REPLACED BATTERY PACK, OPS CHECK NORMAL.SDR 95UAL900045Pseu · malfunctionedAIRCRAFT RETURNED TO BLOCKS WITH EICAS AMBER ADVISORY MESSAGE FOR RIGHT OVERWING SLIDE. REPLACED PSEU DUE TO ANNUNCIATOR PANEL LIGHT NOT ACCOMPANYING EICAS ADVISORY MESSAGE. SUSPECT FAULTY DRIVER CARD.SDR 95UAL900036Eel · inoperativeEEL LIGHT IN RIGHT AISLE OF FORWARD GALLEY INOP. REPLACED POWER STRIP CONNECTOR.SDR 95UAL900034Compressor · stalledABORTED TAKEOFF AT 121 KNOTS DUE TO COMPRESSOR STALL. FOUND EXCESSIVE BLADE TIP CLEARANCE IN THE REAR STAGES OF THE HIGH PRESSURE COMPRESSOR. OVERHAULED COMPRESSOR TO THE NEW PRATT BUILD STANDARD.SDR DL76L952950Hpt Blade · missingDURING BORESCOPE INSPECTION, FOUND AN HPT BLADE MISSING. ENGINE WAS REMOVED AND ROUTED TO SHOP.SDR 95UAL900003Chip Detector · fell outRETURNED TO FIELD WITH NR 2 ENGINE SHUTDOWN, DUE TO LOW OIL QUANTITY. FOUND CHIP DETECTOR LYING IN COWL. CHANGED PROCEDURES TO REQUIRE LOCKWIRE OF THESE CHIP DETECTORS.SDR DL76P952466Compressor · stalledON CLIMBOUT AT 500, NR 2 ENGINE HAD COMPRESSOR STALL, AND EGT OVERTEMP TO 735 DEGREES. REDUCED ENGINE POWER AND RETURNED TO JFK. ENGINE WAS REPLACED AND ROUTED TO SHOP. ETOPS UNSCHEDULED ENGINE REMOVAL.SDR DL76L952163Engine · failedAFTER REVIEW OF ENGINE HISTORY, NR 1 ENGINE WAS REMOVED AND ROUTED TO SHOP FOR REPAIRS, DUE TO HIGH EGT AT ISA RESTRICTION.SDR 95UAL767017Bleed Valve · malfunctionedABORTED TAKEOFF DUE TO NR 2 ENGINE BLEED VALVE PROBLEM. REPLACED HI-STAGE VALVE.SDR 95UAL767016Bearing · failedOIL FILTER BY-PASS LIGHT FOR THE NUMBER TWO ENGINE CAME ON, CREW BROUGHT BACK THROTTLE TO IDLE. SHORTLY, THEREAFTER THE NUMBER TWO ENGINE FLAMED-OUT. ANGLE GEARBOX BEARING FAILED.SDR DL76L951637Engine · damageNR 2 ENGINE FAILED BORESCOPE INSPECTION, FOUND FIRST STAGE GUIDE VANE DAMAGE BEYOND LIMITS. REPLACED ENGINE FOR RETURN TO SERVICE.SDR 95UAL767014Pressurization · squeal noiseLOUD SQUEALING NOISE IN COCKPIT CAUSED DIVERSION.SDR 95UAL767012Chip Detector · misinstalledNR 2 ENGINE SHUTDOWN IN FLIGHT FOR LOW OIL PRESSURE (79-89PSI). ENGINE WINDMILLED APPROXIMATELY 20 TO 30 MINUTES WITH POSITIVE PRESSURE. THE NUMBER THREE CHIP DETECTOR WAS FOUND MISINSTALLED. RE-INSTALLED CHIP DETECTOR AND LEAK CHECKED SYSTEM.SDR 95UAL767011Light · damagedEMERGENCY EXIT LIGHTS DAMAGED. REPLACED LIGHT STRIP AT 1E. REPLACED FORWARD GALLEY CROSS AISLE LIGHT STRIP AND FEEDER CABLE.SDR 95UAL767010Metering Unit · malfunctionLEFT ENGINE CAUGHT FIRE DURING START. NO COCKPIT INDICATION OF FIRE. BOTTLES DISCHARGED FIRE EXTINGUISHED. NO PIMU FAULTS. REPLACED FUEL METERING UNIT AS A PRECAUTION.SDR 95UAL767008Circuit Breaker · trippedTHE C327 CIRCUIT BREAKER TRIPPED IN FLIGHT, CAUSING THE LOSS OF THE RIGHT 115 VOLT A/C TRANSFER BUSS.SDR 95UAL767006Compressor Blade · failedSHUTDOWN LEFT ENGINE DUE TO COMPRESSOR STALLS AND LANDED UNDER AMBER ALERT. EIGHTH STAGE BLADE FAILED, DUE TO SEVENTH STAGE INNER SHROUD DOWL PIN LIBERATION.SDR 95UAL767007Valve · malfunctionSTARTER VALVE, AND STARTER SEQUENCE LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT RETURNED TO FIELD. UNABLE TO FIND FAULT WITH VALVE. OVERHAULED IT AS A PRECAUTION AND RETURNED TO STOCK.SDR DL76L950658Transmitter · malfunctionDURING CLIMBOUT, HAD NO OIL PRESSURE INDICATION ON NR 2 ENGINE, SHUT ENGINE DOWN, RETURNED JFK. FOUND FAULTY OIL PRESSURE TRANSMITTER, REPLACED SAME, OPERATION NORMAL. SUPPLEMENT 1: SHOP EVALUATION OF TRANSMITTER DID NOT FIND ANY FAULT. DUE TO LOW OIL PRESSUSDR DL76L950627Engine · high oil consumpAFTER REVIEWING OIL CONSUMPTION HISTORY, IT WAS DETERMINED CONSUMPTION RATE WAS BEYOND LIMITS, ENGINE WAS REMOVED AND ROUTED TO SHOP.SDR 95UAL767003Lamp · malfunctionedLEFT EXTERIOR EMERGENCY LIGHTS WON'T TEST. REPLACED LAMPS.SDR DL76L950220Compressor · stalledDURING TEST FLIGHT FOR ETOPS ENGINE CHANGE ACCEPTANCE, NR 2 ENGINE HAD COMPRESSOR STALLS ON TAKEOFF. RETURNED CPH. ENGINE WAS REMOVED AND ROUTED TO SHOP.SDR DL76L950219Engine · failedON PUSHBACK, DURING ENGINE START DID NOT HAVE N2 ROTATION. RETURNED TO BLOCK. STARTER AND TRANSMISSION TOWER SHAFT WAS REMOVED DURING TROUBLESHOOTING. DETERMINATION WAS MADE TO REPLACE ENGINE FOR RETURN TO SERVICE AND CONTINUE TROUBLESHOOTING STARTER AND TRSDR DL76L950083Engine · failedDURING CLIMB-OUT AT FL 120, HAD VIOLENT VIBRATION ON RIGHT ENGINE. EGT SHOT UP TO 756 DEGREES. SHUT DOWN NR 2, RETURNED TO AMS. ENGINE WAS REPLACED AND ROUTED TO SHOP.SHUTDOWN
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