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 NACA2024012100001Blade · nicked#2 ENGINE BLADES # 4, 9, 17, 23, 25, 27, 30 31, FOUND WITH NICKS IN VARIOUS LOCATIONS. ALL NICKS BLENDED IAW AMM 72-31-02 AND FOUND WITHIN LIMITS. PERFORMED NDT HFEC AND FPI INSPECTION PER AMM 72-31-02 AND 70-11-06 NO DEFECTS NOTED.SDR NACA2024012100002Spinner · crackedRIGHT ENGINE SPINNER FOUND WITH CRACKS AROUND MOUNTING BOLT HOLES. REMOVED AND REPLACED RIGHT ENG CONE SEGMENT INLET IAW AMM 72-31-04SDR NACA2024011300001Engine · vibrationLEFT ENGINE N1 VIBRATION AVERAGED 3.2 TO 3.5 ON CLIMBOUT AND CRUISE, NO AIRFRAME VIBRATIONS. LUBED MID-SPAN SHROUD PER AMM 72-31-02, CHECKED ALL BLADES, NO DAMAGE NOTED.SDR CALA2023121803659Engine · fireL ENG TAIL PIPE FIRE ON FUEL INTRO NO FIRE INDICATIONS BUT LARGE FIRE REPORTEDSDR NACA2023110400002Unknown · unknownON CLIMBOUT LEFT ENGINE VIB INDICATION .5 TO 5.0 VERY QUICKLY, NO VIBRATION FELT AND IN CRUISE VIBE STAYS AT .4 NO CHANGE. TS PER FIM 77-31-00 FT 803 AND BITE DID NOT SHOW ANY FAULTS, PERFORMED FIM FT 808 AND FOUND LOOSE CABLES, RESECURED CABLES PER FIM 77-31 SDR CALA2023102503171Engine · faultedVIBRATION & STEADY HUM SOUND IN ACFT SINCE REACHING CRUISE ALT. ENTIRE FLT. LOUD HUMMING NOISE NOTABLE INCREASE IN EGT, FUEL FLOW. FLUCTUATING N2 AND VIB INDS. NOISE CHANGED WITH THROTTLE. ON ARRIVAL FOUND RT ENG INTAKE BLOW OUT PANEL UNLATCHED. WITH A SSOSDR NACA2023100300004Engine · failed#1 ENGINE LEAKING FROM SPINNER FAN/SECTION UPON SHUTDOWN. REMOVED AND REPLACED #1 ENGINE IAW MM 71-00-02 ENG RUN IN IDLE OPS CHECK NORMAL IAW AMM 71-00-00SDR NACA2023100300005Unknown · unknownL ENG EEC STATUS AFTER FCF. PERFORMED TROUBLESHOOTING IAW FIM 73-21 FT 828 AND FAULT MSG 350-17. REMOVED AND REPLACED LEFT ENGINE FUEL METERING UNIT IAW B767 AMM 73-21-01 POWER OPS AND LEAK CHECK GOOD.SDR NACA2023100300006Unknown · unknownL ENGINE CONTROL STATUS MESSAGE AFTER FCF. PERFORMED TROUBLESHOOTING IAW FIM 73-21 FT 828 AND FAULT MSG 350-17. REMOVED AND REPLACED LEFT ENGINE FUEL METERING UNIT IAW B767 AMM 73-21-01 POWER OPS AND LEAK CHECK GOOD.SDR DALA2023100308145Unknown · unknownSHIP 0175 -ATO- DUE TO RT GEN OFF INDICATION. CORRECTIVE ACTION: REPLACED IDG PER AMM 24-11. (4613393)SDR NACA2023092200002Unknown · unknownL ENGINE CONTROL EICAS MESSAGE. PERFORMED FIM 73-21 FAULT TREE 825 AND 71-01 TASK 807 AND 826. NO DISCREPANCIES NOTED, OPS CHECK NORMAL.SDR CALA2023090502716Engine · damagedUPON REACHING TO EPR LOUD BANG WITH SWERVE RIGHT . REJECTED T/O . NO FIRE. R REV ISLN VAL EICAS ENG2 SN. 724371 (TSI= 16306) SURGED AT T/OFF POWER, CHEK INLET, LOST N1, OIL PRESSURE IN RED 60 TO 70PSI PER FLIGHT CREW EXHAUST, TAIL PIPE FOR METAL, CHECK ALL CHISDR 2023FA0000003Exhaust Duct · dentedDURING MAINTENENCE INSPECTION FOUND ON ENGINE #2 (PW4060-3) EXHAUST MULTIPLE DENTS, SCATCHES, WELDING REPAIRS AND 2EA DOUBLER REPAIRS BETWEEN NAC STA 228.15 AND NAC STA 283.38 IN ALL CIRCUMFERENCE.SDR CALA2022122303478Blades · damagedNR 2 ENG HAD SEVERAL COMPRESSOR STALLS DURING CLIMB. EGT EXCEEDANCE OBSERVED. HAD THE THROTTLE BACK AT IDLE AND ENGINE STABILIZED. RETURNED TO HKG. IAW FIM 71-05 FAULT TREE 803, FOR T/SHOOTING. CHECKED INLET, EXHAUST. CHECKED MCDS, EPCS PERFORMANCE & EGT EXSDR DALA2022120207710Compressor · stalledRETURNED TO ATL DUE TO RIGHT ENGINE COMPRESSOR STALL DURING CLIMB. T/S RIGHT ENGINE STALL IAW FIM, FAILED VSV SYNCHRONIZING RING INSPECTION. REPLACED NR 2 ENGINE.SDR CALA2022070801675Egt Indication · warning messageRT ENG HIGH EGT ON TAKE OFF. MAX EGT 737 SECONDS DURATION. DUE TO PREVIOUS HISTORY OF EGT FAULTS A POSITIVE FIX IS UNLOCKED FOR UPDATE. REQUIRED. PER CREW WHEN THROTTLES WERE PULLED BACK RIGHT ENGINE EGT DEBRIEF CREW, CAPTAIN STATED THAT ONCE THROTTLES BACK TSDR UIEA2022052300527Switch · fault messageFAILURE L & R PRV OPEN & CLOSE SWITCHES DISAGREE ( POST RUN-UP MESSAGE. PERFORMED AIR SUPPLY CONTROL SYSTEM - BITE TEST IAW AMM 36-23-00. NO FAULTS NOTED, SYSTEM OK AT THIS TIMESDR UIEA2022052300519Plug · wornENG # 2 BOTH IGNITERS PLUGS WORN OUT . REMOVED & REPLACED # 2 ENG. IGNITER PLUGS IAW B767-300 AMM 74-21-02. COMPLIED WITH IGNITION SYSTEM AUDIBLE TEST NO DISCREPANCIES NOTED IAW B767-300 AMM 74-00-00-705-012-N00.SDR UIEA2022052300518Plug · noneENG. # 1 BOTH IGNITER PLUG WERE INSPECTED AND REQUIRE REPLACEMENT . REMOVED & REPLACED BOTH # 1 ENG. LOWER & UPPER IGNITE PLUGS IAW B767-300 AMM 74-21-02, PENDING OPS CHK . PERFORMED ENGINE IGNITION SYSTEM AUDIBLE TEST IAW B767-300 AMM 74-00-00-705-01SDR UIEA2022052300510Spinner · noneREMOVE #1 INLET CONE ( SPINNER ) FOR INTERNAL SURFACE INSPECTION PER W/C A-72-402-00-01 REMOVED FRONT SEGMENT OF THE INLET CONE PER B767-300 AMM 72-31-01.OK TO REINSTALL. REINSTALLED # 1 ENG. FRONT SEGMENT OF THE INLET CONE PER B767-300 AMM 72-31-01.SDR CALA2022051601236None · noneTHIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER CALA2022051601236 SUBMITTED ON 05/16/22.CREW REPORTS LOUD BANG ON CLIMB AND #2 ENGINE SHUT ITSELF DOWN, ENGINES NUMBER WAS REMOVED AND REPLACEDSDR CALA2022040400860None · detachedPDA 1 REF LOG PAGE 8273207 #2 ENG REPEATED SURGE & STALL IN FLIGHT & LOG PAGE 8273259 FOUND SUSPECTED TURBINE BLADE EMBEDDED IN RH STABILIZER LEADING EDGE PDA LOG ITEM RAISED. LP OPEN FURTHER DETAILS AWAITED.SDR CALA2022022400494Engine · failed2 LOUD BANGS FOLLOWED BY RIGHT ENG POWER LOSS - PWR CAME BACK W/IN 10 SECS AT 10000 FEET. R ENG SURGE DET MESSAGE SEE PICTURES FOR INFO. RT ENG PIMU BITE REVEALED NO RELATED OR ASSOCIATED MESSAGES AS T CONTINUING WITH FIM-71-05/803 BLOCK 2 THRU BLOCK 6, VISSDR CALA2022013100280Skin · missingPDA 1 ENGINE 2 NOSE COWL HAS A 19"X12" (228 SQUARE INCHES) PIECE OF THE EXTERNAL HONEYCOMB SKIN MISSING AT APPROXIMATELY THE 2 O''CLOCK POSITION. A/C ARRIVED IN IAH FROM ORD, FLIGHT 2675 IN THIS CONDITION. PERFORMED A VISUAL CHECK AND COULD NOT LOCATE MISSING SDR UIEA2021102202271None · nonePOSSIBLE FOD INGESTION NBR 2 ENGINE.(<P>PERFORMED A VISUAL INSPECTION OF THE INLET APU IAW AMM 72-00-00-211-239-N00. NO EVIDENCE OF ANY INGESTION OF FOD.</P>)SDR UIEA2021100302165None · noneL ENG SPEED CARD STATUS MSG(<P>ACCOMPLISHED SYSTEM CHECK FOR FIM 73-22 FT 871. FOUND OK.</P>)SDR UIEA2021080961736Warning Message · false activationIDLE DISAGREE EICAS MESSAGE ON DESCENT(<P>CHECKED BOTH PIMUS FOR FAULTS ..NO FAULTS STORED ..ALL OK PER FIM 73-21 FAULT TREE 824 ALL TEST OK</P>)SDR CALA2021071401098Turbine · failedMETAL DEBRIS FOUND IN #2 ENGINE EXHAUST. REPLACED #2 ENGINE PER TASK CARD 63-7100-1-9800. OPS AND LEAK CHECKED GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1451053 SN OFF 4665 ENGINE, (PW4060 OFF 76-7200-9-0001 4665 ON 76-7200-9-0001 4674 ACP''D RII INSP SDR CALA2021071201070Engine · stalledRIGHT ENGINE COMP STALL. QUICKLY FOLLOWED BY OVER TEMP OF 712 EG T. ENG SHUTDOWN. ENG FAIL T/O. FURTHER DETAILS AWAITED.SDR UIEA2021070801485Blade · erodedON BORESCOPE INSPECTION FOUND HPT 1 BLADES WITH L/E AND CONCAVES SIDE EROSION ON SEVERAL BLADES ENGINE #1 S/N P729132(<P>BLADES CAN CONTINUE IN SERVICE AT REDUCED INTERVAL INSEPCTIONS OF 125 CYCLES REF B767 AMM 72-00-00/601. TRANS TO ATLAS MCI # A-005 FOR REISDR UIEA2021070101456Starter · failedR ENG EICAS R ENG STARTER ENGINE FAILED TO START.(<P>REMOVED AND REPLACED #2 ENGINE STARTER IAW AMM 80-11-01. OPS CHECK GOOD AT THIS TIME. </P>)SDR UIEA2021070101455Engine · not reported#1 ENG REQ REPLACEMENT. R & R NR 1 ENGINE IAW J/C A71-999-02-01</P>)SDR CALA2021062500961Eec · defectiveRIGHT EPR GAUGE FAILED ON POWER UP FOR T/O R ENG EEC MODE EICAS DISPLAYED TROUBLESHOT #2 ENGINE EPR INDICATION PER FIM 77-11 FAULT TREE 803 AND PERFORMED BITE OF PIMU PER FIM 71-01 FAULT TREE 803. ON LEG #0, HAD EEC UNIT FAIL, FAULT CAT 2, AND P5 LINE FAULT, ASDR UIEA2021061101332Heat Shield · missing# 1 ENGINE LOWER IGNITION LEAD HEAT SHIELDS MISSING.(<P>INSTALLED HEAT SHIELDS ON #1 ENG LWR INGNITION LEAK PER AMM 74-21-01.</P>)SDR UIEA2021061101331Screw · loose#2 ENG TURBINE COOLING, SUPPLY DUCT WITH SCREW LOOSE LOCATE AT 3 O'CLOCK POSITION.(<P>TIGHTENED LOOSE SCREW ON #2 ENG TURBINE COOLING SYPPLY DUCT PER AMM 70-50-00.</P>)SDR UIEA2021061101316Skin · dented# 2 ENG. INLET COWL HAS A DENT AT LOWER NOSE LIP AREA(<P>FOUND DENT WITH IN LIMITS 1.5 MINOR AXY BY .050 DEPTH EQUAL 30 PWER B767-300 SRM 54-13-01-1A-1. PERFORMED NKT, HFEC INSPECTION OF THE DENT AREA. NO CHECK INDICATION NOTED REF NDTM PART 6 51-00-01.<SDR UIEA2021043001029Warning Message · false indication"OVERSPEED" EICAS WARNING FLASHED ON #2 ENG START. C/W FIM 71-08 FAULT TREE 801, A/C OK FOR RETURN TO SERVICE.SDR UIEA2021040200814Engine · contaminatedDURING W/A FOUND ENG OIL IN THE INLET OF ENG #1(<P>NO OIL SERVICE REQUIRED. PERFORMED SYSTEM CLEANING. #1 ENG RUN UP BY FLIGHT CREW ASSISTANT FOR 5 MIN PER AMM 79-00-00. NO EVIDENCE OF LEAK DETECTED AFTER SHUTDOWN. ALL PARAMETERS NORMAL. AC OK FOR SERVICE. OILSDR UIEA2021031600599Unknown · leakingON PREFLIGHT WALK AROUND DISCOVERED FLUID AT BOTTOM OF L ENG COWL FWD OF FAN.(<P>CLEANED FLUID FROM NBR 1 INLET. PERFORMED INSPECTION OF INTERNAL POWERPLANT IAW 71-05-03. NO LEAKS FOUND. NO FURTHER DEFECTS NOTED AT THIS TIME.</P>)SDR UIEA2021031200526Cable · damagedLEFT ENGINE #2 IGNITION INOP ( IGNITION SYSTEMS, EXCEPT ER OPERATIONS (NOTIFY DISPATCH) (R60) )(<P>PARTS NOT TO BE RECEIVED IN TIME. ITEM TRANSFERED TO DMI# 143687 PER MEL 24-00-01B. CAT E. DUE DATE 21MAR21. P/N REQ: 10-609660-7. MCC NOTIFIED. NO MTX ACTION RESDR UIEA2021030800489Blade · nickedFOUND LH ENGINE NBR 8 FAN BLADE LEADING EDGE NICKED.(<P>BLENDED LH ENG NBR 8 FAN BLADE IAW AMM 72-31-02. NO FURTHER DEFECTS NOTED. BLADE W/ IN LIMITS AND NON-MEL ADDED FOR TRACKING PURPOSES ONLY. NON-MEL # 143392.</P>)SDR UIEA2021030500477Panel · missingON POST FLIGHT WALK AROUND FOUND #1 ENGINE INBOARD TR STRUT AT 3 O'CLOCK POSITION LOOKING FWD, PANEL MISSING (INTERMEDIATE CASE)(<P>TRANSFERRED TO NON-MEL 143363 LOWER INTERMEDIATE FAIRING INBOARD SIDE # 1 ENGINE 3 O'CLOCK POSITION FWD FROM AFT OF ENGINE MISSISDR UIEA2021030300472Blade · nickedLEFT ENG BLADE 32 HAS SMALL NICK ABOUT .125" LENGTH AND .031" DEPTH. DAMAGE DEPTH AND LENGTH FOUND TO BE WITHIN REPAIRABLE LIMITS FOR "AREA. A" OF BLADE BLENDED TO SMOOTH EDGE PER AMM 72-31-02, NO FURTHER DEFECTS NOTEDSDR UIEA2021030300470Blade · nickedLEFT ENG BLADE 31 HAS SMALL NICK ABOUT .080". DAMAGE FOUND TO BE WITHIN REPAIRABLE LIMITS FOR 'AREA; A" OF BLADE, BLENDED TO SMOOTH EDGE PER AMM 72-31-02, NO FURTHER DEFECTS NOTED.SDR UIEA2021022200399Valve · faultedLH ENG EEC INOP / ( EEC NORM MODE (PW4000/RB211) (NOTIFY DISPATCH) )(<P>PERF PIMU MX RECALL IAW FIM 71-01 FT. 804 - FAULTED "TCC TR-CK" T/S PER FIM 71-01 TASK 829 PERF TCC ACTUATION CHK IAW FIM 71-08 FT. 807 THROUGH BLOCK 22. SUSPECT TCC CONTROL CABLE / ACTUATSDR ABXA202126008Oil System · leakingLEFTENGINE OIL LEAK, CREW NOTICED OIL QUANTITY DECREASE BACK TO BLOCK, AIRCRAFT GROUNDED BY MAINTENANCE. OIL LEAK WAS FOUND TO BE RESULT OF OIL CAP NOT BEING INSTALLED CORRECTLY. OIL CAP SECURED AND ENGINE RAN TO VERIFY NO LEAKAGE. NO LEAKAGE, AIRCRAFT RELEASESDR UIEA2021011900087Warning Message · false activationEICAS AND STATUS MESSAGE: "RT ENGINE CONTROL" AFTER LANDING, REF B767 FIM 73-21-00-815-825-N00. FIM STATES ACCOMPLISH PIMU BIT. ACCOMPLISHED BIT, PER B767 FIM 71-01 FAULT TREE 803, BIT TEST OK, NO CURRENT FAULTS. OK TO CONTINUE.SDR UIEA2021011900076Fuel Control · malfunctionedITEM NR 1 RIGHT ENGINE FUEL CONTROL EICAS MESSAGE ON LANDING. ACCOMPLISHED PIMU BIT, REF B767 FIM 71-01 FAULT TREE 803, NO FAULTS FOUND. PLACED EEC NORM MODE (BOTH ENGINES) ON DEFERRAL, PER MEL 73-21-01-02 DMI 141111, DUE DATE 29JAN21 CAT C, MCC AND DISPATCHSDR UIEA2021011400057Warning Message · false activationRT ENGINE CONTROL EICAS MESSAGE UPON LANDING. PERFORMED PIMU BITE TEST, IAW FIM 73-21 FT 826. SYSTEM TEST OK.SDR UIEA2021011300045Fuel Control · unknownSTARTING LEFT ENGINE T/O SPEEDS DROP OUT WHEN LEFT FUEL CONTROL GOES FROM OFF TO RUN. ON CDU "SPEEDS DROP OUT". PERFORMED ENGINE RUN, IAW AMM 71-00-00. NO DEFECTS.
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