Pratt & Whitney PW4060
Service difficulty reports · 7,181
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 UIEA2021011200038Inlet · damagedNR 1 INLET COWL HAS A SMALL DAMAGE AT 5:00 POS TAIL. ACCOMPLISHED PERMANENT HOT BOND COMPOSITE REPAIR OF NR 1 INLET COWL AT 5 O'CLOCK POSITION, PER AVENIR AVIATION FAA CAS 8AVR479B WO W15287 FEAM RO 5002395 FAA FORM 8130-3 ATTACHED.SDR UIEA2021010600012Blade · damagedITEM NR 7 BORESCOPE INSPECTION NR 2 ENGINE SN: P724690, FOUND HPT NR 2, TWO EA BLADES WITH LEADING EDGE DENT AND CRACKS DAMAGE. REQUIRE ENGINE REPLACEMENT WITHIN 5 CYCLES. TRANSFERRED TO NON-MEL NR 140527.SDR UIEA2020122402612Start Valve · malfunctionedDURING T/C "T2051" FOUND UPON IDLE ENGINE RUN UP (L) START VALVE LIGHT DOES NOT INDICATE. REMOVED AND REPLACED LT ENGINE START VALVE, PER AMM 80-11-02. OPERATIONS CHECK SUCCESSFUL.SDR UIEA2020121502567Warning Message · malfunctionedRIGHT ENGINE ANTI-ICE VALVE INITIALLY STAYED ILLUMINATED WHEN SELECTED ON. AFTER A FEW MINUTES IT WENT OUT AND OPERATED NORMALLY. THIS OCCURRED AFTER ENGINE START. PERFORMED OPERATIONS CHECK OF RIGHT ENGINE ANTI ICE VALVE, IAW 30-21-00. NO DEFECTS NOTED ATSDR ABXA20200803224Pressure Switch · deterioratedRT ENGINE OIL PRESS DISCRETE LIGHT + EICAS MESSAGE WERE ILLUMINATED AFTER ENGINE START. AICRAFT BACK TO BLOCK AND GROUNDED. REMOVED AND REPLACED LOW OIL PRESSURE SWITC,H AS PER B767 AMM 79-33-01. LEAK CHECK + OPERATIONS CHECK GOOD. AIRCRAFT REMAINS ETOPS 18SDR UIEA2020113002489Eec · faultedEEC CATEGORY 2 FAULTS, EEC CHANNEL A AND B T5 CROSS CHECK FAIL ON ENGINE NR 1. T/S FIM 71-01-TASK 858, TIGHTENED ALUMEL; CHROMEL CONNECTION ENGINE 1; EBT SYS, PER AMM 77-21-03/501. OPERATIONS TEST OK.SDR UIEA2020113002491Seal · wornRT WING KRUEGER FLAP OUTBOARD SIDE SEAL IS WORN OUT. PREPARED, CLEANED AND REPAIRED WORN SEAL AT RT WING KRUEGER FLAP AT OUTBOARD SIDE, PER B767-300 AMM 52-09-00-358-056.SDR UIEA2020113002494Seal · deterioratedNR 2 ENGINE DRAIN MAST PROTECTOR SEAL IS DETERIORATED. REPAIRED DETERIORATED FIRE INSULATION AT NR 2 ENGINE DRAIN MAST, IAW B767-3 AMM 78-31-01.SDR UIEA2020113002495Seal · deterioratedNR 2 ENGINE OUTBOARD T/R COWL AIR COOLER DUCT SEALANT REPAIR IS DETERIORATED. REPAIRED DETERIORATED PROTECTOR SEAL (FIRE INSULATION), IAW B767-3 AMM 78-31-01 AT NR 2 ENGINE OUTBOARD T/R COWL AIR COOLER DUCT.SDR UIEA2020112502462Bleed Air Sys · malfunctionedONLY APPROXIMATELY 5 PSI BLEED AIR PRESSURE, UNABLE TO START ENGINES. ITEM TRANSFERRED TO DMI NR 138466, IAW DDG MEL 49-11-01A CAT C DUE 05DEC20. MCC NOTIFIED, PLACARDS INSTALLED. PERFORMED OPERATIONS TEST APU BLEED AIR SYSTEM, PER AMM 49-52-00 NO FAULTS ONSDR UIEA2020112302447Nut · missingNR 1 ENGINE BLEED START VALVE FWD V BAND MISSING FASTENER. REPLACED V BAND CLAMP NUT, IAW AMM 80-11-02. OPERATIONS CHECK GOOD.SDR ABXA20200803219Start Valve · bindingRIGHT ENGINE START VALVE WILL NOT OPEN. AIRCRAFT BTB AND GROUNDED. R & R RT ENGINE START VALVE, IAW B-767 AMM 80-11-02. OPERATIONS GOOD. AIRCRAFT RELEASED.SDR UIEA2020101302232Exciter · inoperativeLEFT ENGINE DID NOT START WITH NR 2 IGNITOR SELECTED. SWITCHED TO BOTH IGNITORS AND START WAS SUCCESSFUL. TRANSFERRED TO DMI 135990, IAW MEL 74-00-01B, CAT "C" DUE DATE 23OCT20, PLACARD INSTALLED. DISPATCH JD 06:40Z. CVG MX, 15OCT. REMOVED & REPLACED NR 2SDR UIEA2020101272184Unknown · leakingDURING WALK AROUND NOTICED OIL POOLING AT THE BOTTOM OF THE LEFT ENGINE COWL. PERFORMED ENGINE VENTS & DRAIN INSPECTION, IAW AMM 71-71-00. LEAK FOUND TO BE WITHIN LIMITS, NO FURTHER DEFECTS NOTED AT THIS TIME.SDR UIEA2020090101914Line · leakingON WALKAROUND FOUND HYD FLUID DRIPPING FROM LEFT ENGINE STRUT DRAIN.(<P><SPAN>FOUND HYD SUPPLY LINE ON STRUT ACCESS LOOSE, SECURE BNOT ON SUPPLY LINE, LEAK CHECK OK AS PER AMM 77-71-00 AT # 1 ENG.</SPAN><BR /></P>)SDR UIEA2020082801888Indicator · inoperativeUPON ENTERING COCKPIT NOTICED "RIGHT FUEL INDICATOR AND FUEL TOTAL INDICATOR" NOT DISPLAYED.(<P>PERFORMED ENG RUN. RESET FUEL SYSTEM PAGE ON FMC PER 71-00-00<BR /></P>)SDR IPXA2020080558669Bulkhead Web · wornNR 1 ENGINE INLET COWL, OTBD SESE LINE BULKHEAD FITTING HOLE IN WEB WAS WORN, AND ENLARGED. REMOVED & REPLACED THE WEB IAW SRM 54-10-00, FIG 201.SDR UIEA2020071001516Transducer · malfunctionedDURING TAKEOFF RIGHT ENGINE DID NOT SPOOL UP. RIGHT THRUST LEVER WAS SUBSTANTIALLY FRAIL TO BE UNRESPONSIVE TO INPUTS. REMOVED AND REPLACED; RH ENG. T/R POSITION FEED BACK TRANSDUCER IAW AMM 78-36-03. RIG CONFIRMED. REQUIRES HIGH POWER RUN TO COMPLETE OPERATIOSDR UIEA2020071001519Combust Chamber · crackedDURING A BOROSCOPE INSPECTION, FOUND THE NR 1 ENGINE WITH A CONTINUOUS AXIAL CRACK ON THE COMBUSTION CHAMBER OUTER LINER, AT THE 3 O`CLOCK POSITION. THE COMBUSTER 13 WAS PERMITTED TO CONTINUE ON A REDUCED TIME INSPECTION INTERVALS OF 125 CYCLES IAW AMM 72-00SDR UIEA2020070701490Plug · undersizeDURING BOROSCOPE INSPECTION, DISCOVERED AP-9 BOROSCOPE PLUG AT THE 3.0 CLOCK POS ON DIFFUSER CASE, SHAFT DIAMETER IS METER IS LESS THAN 0.100 IN NR 2 ENGINE. REMOVED AND REPLACED AP-9 BOROSCOPE PLUG IAW 767 AMM 72-00-00-206-364.SDR UIEA2020060101193Eec · faultedSTATUS MSG RT ENG EEC C1. PERFORMED FIN PROG TASK 71-01. FAULT TREE 803. EICAS MSG CLEARED, NO FAULTS NOTED, UNABLE TO RUN ENGINE TO VERIFY FAULT. TRANSFERRED TO DMI 129093, MEL 73-21-01-04, CAT 'A'. DUE FAULT LEVEL B DUE 21JUNE 20. REMOVED AND REPLACED EESDR UIEA2020051101013Probe · faultyR ENG EEC MODE EICAS(<P>TRANS TO DMI #128110 MEL 73-21-01-02.</P><P>LOG PAGE 1140400 ITEM #7: REMOVED AND REPLACED PT2/PT7 PROBE IAW MM 73-21-03. RAN R ENG SEVERAL TIMES PER MM 71-00-00. NO EICAS STATUS MSG, NO ADVISORY MSG AND NO PIMU MSG. THIS CLEARS MDDR 12SDR UIEA2020051200919Probe · faultyR ENG EEC C1 STATUS MESSAGE UPON LANDING.(<P>TRANSFERRED TO MDDR 127726 PER MEL 73-21-01-04, CAT A, DUE DATE 1000 FH.</P><P>LOG PAGE 1140400 ITEM #7: REMOVED AND REPLACED PT2/PT7 PROBE IAW MM 73-21-03. RAN R ENG / SEVERAL TIMES PER MM 71-00-00. NO EICAS STATUSSDR UIEA2020042700879Filter Housing · leaking#1 ENGINE FUEL PUMP FILTER LEAKING.(<P>REMOVED AND REPLACED #1 ENG FUEL PUMP FILTER HOUSING PACKING AS PER MM CHP 73-11-02. LEAK CHECK OK.</P>)SDR UIEA2020032000502Engine · oil consumptionRIGHT ENG OIL QUANTITY CONTINUALLY DROPS IN OIL QUANTITY DURING FLIGHT, ENGINE QUANTITY AT START INDICATED 23 QTS OIL QUANTITY AT ELAPSE TIME 98:55 IS 4 QTS.(<P>REMOVED AND REPLACED ENGINE 2 I.A.W ATLAS W/C A-71-999-02-01.</P>)SDR 2020F00102Duct · brokenCAPTAIN REPORTED STRANGE NOISE AND HE WAS UNSURE WHERE IT CAME FROM. TORUBLESHOOTING STARTED AND FOUND NOISE FROM THE MAIN WHEEL BAY. DOORS WERE OPENED AND FOUND BLACK MARKINGS AND HISSING NOISE FROM SUPPLY DUCT FROM THE APU TO THE A/C SYSTEM. FOUND BLEED AIR SDR DALA2020022091293Idg · failedSHIP 181 - ATO - AT 15KTS DUE TO #2 ENGINE DID NOT ACCELERATE ABOVE IDLE WHEN THROTTLES ADVANCED. CORRECTIVE ACTION: MAINTENANCE REPORTED NO ENGINE RELATED FAULTS ON EICAS, EEC, PIMU AND WHEN #2 IDG DISCONNECTED ENGINE IMMEDIATELY SPOOLED UP TO NORMAL IDLE SPESDR UIEA2020012750123Exciter · failedNR 2 ENG RISE, NO LIGHT OFF ON FIRST HALF. IGNITION SET TO BOTH AND ENGINE STARTED NORMALLY ON SECOND ATTEMPT. PERFORMED AMM 74-00-00-705-012 AUDIBLE TEST. FAILED ON THE NR 1 POSITION. REMOVED AND REPLACED THE NR 1 IGNITION, NR 2 ENGINE EXCITER BOX IAW SDR UIEA2019123096162Vane · delaminatedLEFT ENGINE 7 O'CLOCK POSITION EXIT VANE WITH DELAMINATION. REMOVED DAMAGE FROM EXIT VANE IAW AMM 72-33-02.SDR UIEA2019121806101Circuit Card · failedL ENG SPEED CARD STATUS MSG.(<P><SPAN>FOUND WATER DAMAGE TO N2 ENG SPEED CARDS (L & R).<BR DATA-MCE-BOGUS="1" /></SPAN></P><P><SPAN>LP 1186382 - M12: REMOVED AND REPLACED RIGHT N2 ENG SPEED CARD </SPAN><SPAN>(OFF PART: P/N </SPAN><SPAN>285T0458-203, S/N 2003)<SDR UIEA2019121326063Blade · nicked#2 ENGINE #14 C1 FAN BLADE HAS A NICK IN THE TIP AREA.(<P>BLENDED NICK IN TIP AREA ON #2 ENG #14 C 1 FAN BLADE IAW AMM 72-31-02-308-003. REMOVED APPROXIMATELY .030", WITHIN LIMITS.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>(NOTE: LP 1075824 - M6: DMI 121960 OPENEDSDR UIEA2019120205969Status Message · false activationCARGO A/C TEMP STATUS MSG PERFORMED FIM 21-60 FAULT TREE 804, NO FAULTS FOUND AT THIS TIME. MESSAGE CLEARED, OPS CHECKS GOODSDR UIEA2019110755854Guide Vane · looseENGINE #1 FAN EXIT GUIDE VANE METAL L/E, 1 EA MISSING AND 1 EA LOOSE AT 4 O'CLOCK POSITION. (<P>ITEM M8: REMOVED #1 ENG FAN EXIT GUIDE VANE AT 4 O'CLOCK POSITION (#14 CCW FROM 6 O'CLOCK) IAW B767 AMM 72-33-02, NO DEFECTS NOTED.</P><P>ITEM M9: REMOVED #1 ENG FASDR UIEA2019102205777Oil System · leakingOIL POOLED IN RIGHT ENGINE COWLING, AROUND N1 BLADES. (<P>CHECKED AND FOUND TO BE OK IAW B767 FIM 71-08 FAULT TREE 813.</P><P><BR /></P><P><BR /></P>)SDR ABXA201910172160Duct · leakingWHILE CLIMBING AFTER TAKEOFF, STATUS MESSAGES "L ENG OH LP 2" AND "L ENG OH LP 2" DISPLAYED AND EICAS MESSAGE "L ENG OH" DISPLAYED. THE CREW SHUT DOWN THE LEFT ENGINE AND RETURNED TO THE AIRPORT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE MESSAGESDR UIEA2019082305270Thermocouple · failedDURING ENGINE CHECK, FOUND PIMU MSG EEC CH-A T 29 RNG FAIL. REMOVED AND REPLACED LEFT 2.9 BLEED VALVE THERMOCOUPLE PROBE IAW AMM 75-32-06, OPS CHECK GOOD.SDR IPXA2019081645692Engine · flamed outENGINE 2 FLAME OUT ON DECENT. EMERGENCY DECLARED. PERFORMED WINDMILLING INSPECTION. PERFORMED EXTERNAL INSPECTION FOLLOWING EXPOSURE TO FIRE EXTINGUISHING AGENT. DID GVI OF ENGINE EXTERNAL COMPONENTS. DID BORESCOPE INSPECTION OF COMBUSTION CHAMBER, HPT BLADSDR UIEA2019081205005Fuel Filter · cloggedAFTER TAKEOFF, R ENG FUEL FILT EICAS AND STATUS MESSAGE. REMOVED AND REPLACED THE FUEL FILTER ELEMENT REF AMM 73-11-03-404-001-H00. NO LEAKS NOTED.SDR UIEA2019072204820Cone · erodedL ENG CONE FOUND WITH EROSION PEELING ALL OVER THE CONE. (<P>REMOVED AND REPLACED CONE SEGMENT PER AMM 72-31-01.</P>)SDR UIEA2019071204744Unknown · malfunctioned"LEFT ENGINE POOR N2 ACCELERATION DURING START W/ APU BLEED. LOW DUCT PRESSURE OBSERVED. INFO ONLY."(<P><SPAN>PERFORMED DRY MOTOR OF ENGINE #1 IAW AMM 71-00-00.</SPAN><SPAN>OPS CHECK NORMAL AT THIS TIME.</SPAN></P><P><SPAN>ENGINE DRY MOTORED BY CREW</SPAN></PSDR UIEA2019061904527Spinner · crackedFOUND THE NR 1 ENGINE FAN BLADE SPINNER CRACKED. R & R THE NR 1 ENG SPINNER DOME IAW AMM 72-31-01.SDR UIEA2019061764501Spinner · crackedFOUND # 1 FAN BLADE SPINER CRACKED (<P>REMOVED AND REPLACED #1 ENGINE SPINER DOME IAW AMM 72-31-01</P>)SDR UIEA2019060314364Eec · malfunctionedLEFT ENGINE EEC MODE DISPLAYED ON EICAS. PERFORMED EEC OPS TEST IAW BOEING AMM 73-21-04. OPS TEST PASS.SDR UIEA2019041763894Vane · damaged(SEVERAL) # 2 ENGINE FAN EXIT CASE VANES HAVE MISSING SEALANT AT INSTALLATION BOLTS .(<P>APPLIED SEALANT AT # 2 ENGINE FAN EXIT CASE VANES BOLTS IAW B767 AMM 72-34-06-404-001-N00.</P>)SDR CALA2019041200566Fairing · missingINTERMEDIATE CASE STRUT FAIRING MISSING FROM LT ENG S/N 724379 AT THE 9 O CLOCK POSITION LOOKING FWD FROM THE AFT OF ENGINE. REF GMM 02-30-95 PDA PROGRAM CAT 2 APPROX SIZE OF PANEL 14" X 6" IAW AMM 72-34-05 MISSING FAIRING IS TO BE REPLACED BEFORE THE 51ST HOUSDR CALA2019041200569Fairing · missingLEFT ENGINE INTERMEDIATE CASE STRUT FAIRING MISSING, 9 O''CLOCK STRUT UPPER SIDE. INTERMEDIATE CASE FAIRING MISSING FROM L/H ENG 9 O CLOCK POSITION NEEDS TO BE REPLACED BEFORE 51 HOURS OF OPERATION. PER TABLE 601 AMM 72-34-05-206-005. NO OTHER DAMAGE OR LOOSE SDR UIEA201904113841Exciter · malfunctionedON ENGINE START #1 ON #1 IGNITER NO LIGHT OFF, SECOND ATTEMPT SUCCESSFUL ON BOTH. (<P>TRANSFERRED #1 IGNITER TO MDDR 109996 AS PER DDG 74-00-01B CAT "C".</P><P>LP 1015599 - M5: REMOVED AND REPLACED L/H ENG NO. 1 IGNITER. NO FIX. REF B767 AMM 74-21-02. REMOVEDSDR UIEA2019040403771Anti-Ice System · malfunctionedENG. ANTI-ICE LIMITATION EXCEDED A/I ON AT 18C.(<P>PERFORMED OPERATIONAL TEST ON ENGINE PROBE HEAT SYSTEM PER AMM 30-34-00, OPS CHECK GOOD. COULD NOT DUPLICATE FAULT, MCC NOTIFIED. ALSO PERFORMED FIM 30-21 FT 805, SYSTEM OK.</P>)SDR UIEA2019040433769Unknown · unknown# 2 ENG FUEL LEAK AFTER SHUTDOWN, FOLLOWED BY A STRONG ODOR INSIDE AFT CABIN (FUEL) ROWS 30-37.(<P>RAN # 2 ENG I.A.W AMM 71-00-00 NO LEAKS NOTED & ODOR NOTED. </P>)SDR CALA2019032900484Unknown · malfunctionedPOSSIBLE COMPRESSOR STALL. VERY LOUD BANG RIGHT SIDE/ WITH FLASH. PERFORMED ENGINE INSPECTION REF FIM 71-05-00-815-803-N00 UP TO AND INCLUDING STEPS 7 SUB TASK AMM 72-00-00/601 PLUGS REMOVAL. COMPLIED WITH BORESCOPE OF NR 2 ENGINE AS REQUIRED BY 767-3 FIM 71-0
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