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 UIEA2019031803582Unknown · leakingLEFT ENGINE HAS NOTABLE OIL LEAK. (<DIV>CLEANED EVIDENCE OF OIL LEAK. INSPECTED FOR LEAKS, NONE NOTED AT THIS TIME ON LEFT ENGINE IAW AMM 79-00-00. OK FOR SERVICE.</DIV>)SDR CA190304001Bleed Valve · failed(CAN) CREW REPORTED THAT THEY MAY HAVE BLOWN A TIRE ON TAKE OFF. HEARD AND FELT SOMETHING ABNORMAL AND THE CREW NOTICED FLAMES/SPARKS COMING OUT OF ONE ENGINE. SUSPECTED THAT TIRE DEBRIS MAY HAVE BEEN INGESTED BY THE ENGINE.TOWER WAS CONSULTED TO SEE IF ANY TISDR UIEA2019020603137Unknown · leaking#2 ENGINE HAS SIGNS OF OIL LEAK IN AREA OF THE LOWER HALF O/B SIDE OF IDG.(<P>CLEANED AREA IAW B767 AMM 20-10-22,LEAK CHECK ACCOMLPISHED ON TASK CARD A-24-017-01-02.</P>)SDR UIEA2019020603136Blade · damaged#1 ENGINE 1ST STAGE FAN ROTOR LAS 1EA BLADE WITH A NICJ=K IN THE LE APPROX 12" FROM TIP.(<P>BLENDED AND PERFORMED DPI IAW B767 AMM 72-31-02 AND B767 SOPM 20-2-02,PERFORMED TEST #8 IAW B767 AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</P>)SDR UIEA2019020603135Cable · worn#2 ENGINE EXCITER TO IGNITER PLUG CABLE "B" IGNITER END IS WORN AND "C" CLIP IS FALLING OFF.(<P>REMOVED AND REPLACED #2 ENGINE IGNITER TO EXCITER CABLES CHANNELS "A" + "B" IAW AMM 74-21-01,PERFORMED ENGINE IGNITION AUDIBLE TEST IAW B767 AMM 74-00-00,NO DEFECTSSDR UIEA2019020603134Blade · nicked#1 ENGINE 1ST STAGE FAN ROTOR HAS !EA BLADE WITH A NICK IN THE LE APPROX. 7" FROM TIP.(<P>BLENDED AND PERFORMED DPI OF DAMAGED AREA IAW B767 AMM 72-31-02 AND B767 SOPM 20-20-02,PERFORMED TEST #8 IAW B767 AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</P>)SDR UIEA2019020603133Blade · nicked#2 ENGINE #4 BLADE HAS NICK.(<P>BLENDED AND PERFORMED DPI OF DAMAGED AREA IAW B767 AMM 72-31-02 AND B767 SOPM 20-20-02,PERFORMED TEST #8 IAW B767 AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</P>)SDR UIEA2019020603132Blade · nicked#2 ENGINE #13 BLADE HAS NICK.(<P>BLENDED AND PERFORMED DPI OF DAMAGED AREA IAW B767 AMM,72-31-02 AND B767 SOPM 20-20-02,PERFORMED TEST #8 IAW AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</P>)SDR UIEA2019020603130Blade · nicked#1 ENGINE 1ST STAGE FAN ROTOR HAS 1EA BLADE WITH A NICK IN THE LE APROX 5" FROM THE ROOT SECTION.(<P>BLENDED AND PERFORMED DPI OF DAMAGED AREA IAW B767 AMM 72-31-02 AND B767 SOPM 20-02-02,PERFORMED TEST #8 IAW B767 AMM 71-00-00,NO DEFECTS NOTED AT THIS TIME.</SDR UIEA2019020603128Unknown · leaking#2 ENGINE HAS OIL PUDDLING AFT OF FAN BLADES.(<P>CLEANED #2 ENGINE OIL PUDDLE AFT OF FAN BLADES,FOUND TO BE WITHIN LIMITS IAW B767 FIM 71-08 FAULT TREE 813,NO DEFECTS NOTED.</P>)SDR HALA2018120430621Oil System · lowETOPS SIGNIFICANT SYSTEM - LEFT ENGINE OIL QUANTITY 18 ETS. // PILOT PERFORMED ENG 1 IDLE RUN FOR 5 MIN ADDED 2 PINTS OF OIL. OK FOR SVCSDR UIEA2018113002740Anti-Ice Valve · malfunctionedSTATUS MSG L ENG TAI VALVE (<P>REMOVED AND REPLACED L ENG TAI VALVE I.A.W AMM 30-21-03 SYS OPS AND LK CHECK NORMAL </P>)SDR UIEA2018110102478Relay · malfunctionedLEFT NACELLE VENT VALVE EICAS MESSAGE WILL NOT ERASE. TROUBLESHOT AND FOUND THE VENT SHUTOFF VALVE IN THE OPEN POSITION. R & R THE RELAY K676 AT P36 IAW FIM 7523, WDM 75-23-11, AND SWPM 28-81-22. MESSAGE NO LONGER APPEARED.SDR DALA2018070304409Ring · brokenENGINE SURGE SUSPECTED ON DESCENT THROUGH FL340-280 INDICATED BY UNUSUAL NOISE AND VIBRATION. FOUND 2.5 BLEED VALVE RING BROKEN. REPLACED NR 2 ENGINE. SYSTEM OPERATION IS NORMAL.SDR CALA2018062101470Engine · damagedLEFT ENGINE OVERHEAT AND VIBRATION. 711 DEGREE. SHUTDOWN AND LANDED IMMEDIATELY. THE NR 1 ENGINE WAS REPLACED IAW TASKCARD 63-7100-1-9800.SDR CALA2018062201516Engine · damagedLEFT ENGINE OVERHEATED AND VIBRATION. 711 DEGREE. SHUTDOWN AND LANDED IMMEDIATELY. NR 1 ENGINE WAS REPLACED IAW TC 63-7100-1-9800.SDR HALA2018061100291Fmu · malfunctionedAIR TURNBACK, LT FMC FAILED. RAN QRH, FMC 2, LT FMC REMAINED INOPERATIVE. REMOVED AND REPLACED THE LEFT FMC IAW AMM 34-61-01-424-005. PERFORMED A CROSS LOAD IAW AMM 34-61-00-422-009-005. NO FAULT NOTED, OPS CHECKED GOOD ON GROUND, OK TO CONTINUE.SDR CALA2018060601414Check Valve · failedDURING DECENT, THE CREW REPORTED A RUMBLE FROM THE RT ENGINE, FOLLOWED BY AN EGT OF 666 DEGREES. THE ENGINE WAS SHUTDOWN, RAN QRH AND THE ENGINE WAS RESTARTED BUT UNABLE TO ADVANCE THROTTLE, ENGINE CONTINUED TO RUN AT IDLE. REMOVED IP CHECK VALVE IAW AMSDR UIEA2018052900994Warning Light · false activationDURING LEFT ENGINE START, LT DEMAND PUMP EICAS AND PRESSURE LIGHT ILLUMINATED, DUCT PRESSURE DROPPED TO 7 PSI. PERFORMED A NORMAL ENGINE OPERATION IAW AMM 71-00-00-712-021-N00. ENGINE STARTED NORMAL.SDR UIEA2018051600906Switch · failedRIGHT ENGINE VALVE LIGHT INOPERATIVE. REMOVED AND REPLACED THE SWITCH RT ENG VALVE IAW SWPM 20-84-18, AND WDM 33-16-18. OPS CHECKED GOOD.SDR HALA2018042400184Warning Message · false activationDIVERTED DUE TO A RT OIL FILTER EICAS MESSAGE INTERMITTENTLY DISPLAYED WITH ASSOCIATED R OIL FILTER STATUS MESSAGE CONTINUOUS. PERFORMED A RT ENGINE MAIN OIL FILTER INSPECTION IAW AMM 79-21-05-216-001-N00. NO DEBRIS DETECTED. INSTALLED A NEW FILTER ELEMENT IASDR HALA0218040900147Warning Message · false activationDURING DESCENT, STATUS MESSAGE FOR THE LT ENGINE EEC NR 1 DISPLAYED. NO STATUS FOUND ON GROUND. AIRCRAFT OK FOR SERVICE.SDR HALA2018032900130Oil System · lowDURING CLIMB, LEFT GENERATOR DRIVE EICAS MESSAGE, COMPLETED QRH AND GOING TO DISCONNECT DRIVE, THE MESSAGE AND LIGHT EXTINGUISHED. GENERATOR VOLTS AND FREQUENCIES NORMAL. DURING CLIMB IDG TEMP OUT 80/80, RISE 20/10, DURING CRUISE, IDG TEMP OUT 83/90, RISE SDR HALA2018031300092Bleed Valve · fluctuatesRIGHT HIGH PRESSURE BLEED VALVE FLUCTUATING FROM 20-40 PSI DURING DESCENT WITH THRUST NEAR IDLE. PERFORMED AIR SUPPLY DISTRIBUTION TEST IAW AMM 36-11-00-715-149. AIR SUPPLY BITE TEST GOOD NO FAULTS NOTED, OK FOR SERVICE.SDR DALA2018020300702Unknown · malfunctionedSTARTING LEFT (1) ENG PUSH CREW OBSERVED SPARKS ABORTED ENG START TOWER OBSERVED SMOKE ENG STARTED NORMAL UNTIL GET STAGNATED THEN TUG CREW REPORTED OBSERVATIONS. DRY RUN ENG FOUND LEFT STARTER FAULTY AND REPLACED.SDR DALA2018011500286Blade · crackedWHILE PERFORMING BOROSCOPE INSPECTION OF THE SECOND STAGE NR 1 ENG HPT BLADES, FOUND LEADING EDGE DENTED IN AREA B WITH AXIAL CRACK APPROX .223 INCH IN LENGTH ON CONCAVE SIDE & INTERSECTING RADIAL CRACKS ON CONVEX SIDE .564 INCH. REPLACED THE NUMBER 1 ENGINESDR CA180102001Outflow Valve · malfunctioned(CAN) FLIGHT WAS IN CRUISE AT FL350 JUST WEST OF YHZ WHEN THEY HAD AN EICAS MESSAGE (CABIN AUTO INOP). CREW REVERTED TO MANUAL CONTROL OF CABIN. AFTER CONSULTING WITH MOC AND DISPATCH, IT WAS DECIDED TO DIVERT TO YYZ. AFTER TURNING BACK FOR YYZ THE CABIN STSDR HALA2017110600266Eec · malfunctionedAFTER 3 MINUTES AT CRUISE, 11,000' MSL. RT ENGINE HAD APPROX 5 SURGES WITH ASSOCIATED HPSOV CYCLING, WHEN ADDITIONAL THRUST APPLIED, DUE TO LOSS OF AIRSPEED. RT ENGINE UNABLE TO ACHIEVE MORE THAN 2,600 LBS FUEL FLOW, NO EPR/N1/N2 RESPONSE. AFTER APPROX 30 SESDR CALA2017092903344O-Ring · damagedNR 2 ENGINE LOST OIL QTY & OIL PRESSURE IN FLIGHT. OIL QUANTITY WENT TO ZERO. INSPECTED ALL CHIP DETECTORS, NO DEBRIS. REPLACED THE O-RINGS FOUND AFT CHIP DETECTOR O-RING CUT. REMOVED & INSPECTED MAIN OIL FILTER, NO DEBRIS. INSTALLED NEW FILTER IAW AMM 7SDR HALA2017081500221Warning Light · false activationON STARTING THE NR 2 ENGINE, FUEL SPAR VALVE LIGHT STAYED ON DURING START. START WENT TO 50% N2, THEN STARTED TO SPOOL DOWN, FUEL CONTROL SWITCH TO CUT OUT AT ABOUT 43% N2. PERFORMED AN OPS CHECK OF THE NR 2 ENGINE IAW AMM 71-00-00. OPS CHECKED GOOD. OK FSDR CALA2017072102284Engine · surgesRT ENGINE SHUT DOWN IN FLIGHT DUE TO ENGINE VALVE EICAS AND ENGINE SURGE. CREW REPORTS ENGINE WINDMILLED FOR APPROX 7-10 MINUTES WITH POS ITIVE OIL PRESSURE. REPLACED THE NR 2 ENGINE IAW AMM 71-00-02.SDR HALA2017070300173Fmu · faultyIN CRUISE FLT AT FL370 WHEN THROTTLE IS RETARDED TO APPROX 1.13 EPR ON THE RT ENGINE, THE ENGINE SURGES. NOTED + - 3 EPR, + - .5 N1, ALSO RT PAC DUCT PRESSURE CYCLES FROM LOW TO HIGH FLOW 42 - 25 PSI. IN SUMMARY RT ENG SURGES AT LOW POWER SETTING. REMOVED RT FSDR HALA2017062200162Bleed Air Sys · inoperativeNR 2 ENGINE BLEED AIR INOPERATIVE. REMOVED AND REPLACED PRSOV IAW AMM 36-11-09. REMOVED AND REPLACED FAN AIR VALVE IAW AMM 36-11-16. OPS CHECKED GOOD. OK FOR SERVICE.SDR DALA2017012600722Line · damagedDURING TAXI OUT , THE RIGHT ENGINE SHUTDOWN BY ITSELF AFTER BEING STABILIZED AT IDLE. ANOTHER AIRCRAFT REPORTED SMALL TAIL PIPE FIRE AFTER THE ENGINE HAD SHUT DOWN. REPLACED THE RIGHT FCU, INSPECTED INLET AND EXHAUST. SYSTEM OPERATION IS NORMAL. AS FOLLOW SDR DALR2016120500001Mount · wornDURING ROUTINE MAINTENANCE AND INSPECTION, THE GUIDE AND SHEAR PIN HOLES OF THE SUBJECT AFT ENGINE MOUNT WERE FOUND TO BE ELONGATED BEYOND SERVICEABLE LIMITS IAW CMM 221-0260-501. REPAIRED IAW ERA.SDR HALA201606210241Oil Filter · leakingON TAXI OUT, RT OIL FILTER EICAS CAME ON. REPLACED RT MAIN OIL FILTER AND INSPECTED PRESSURE DIFFERENTIAL SWITCH IAW AMM 79-21-05, OPERATED ENGINE FOR 3 MIN, NO LEAKS NOTED. OK TO CONTINUE.SDR HALA2016042700143Fan · contaminatedFOUND OIL IN NR 2 ENGINE AFT OF FAN AT 6 OCLOCK. CLEANED OIL RESIDUE FROM ENGINE. RAN NR 2 ENGINE AT IDLE. LEAK CHECKS OK. OK FOR CONTINUED SERVICE.SDR HALA2016032000089Warning Light · false activationSTATUS LT ENGINE ELECTRONIC ENGINE CONTROL C1. PERFORM LT ELECTRONIC ENGINE CONTROL MAINT TEST ON GROUND, NO FAULTS NOTED MSG CLEARED.SDR CALA2016031495214Battery Pack · dischargedEPL AT SEATS 19 - 22 RT INOPERATIVE. R & R BATTERY PACK & POWER SUPPLY UNIT, POSITION M1209 IAW AMM 33-51-07. PERFORMED EMER LIGHTS TEST, EPL SEATS 19 - 22 RT IAW AMM 33-51-07, FOUND NORMAL.
SDR CALA2016031495218Floorbeam · corrodedMAIN DECK, STATION 302, RBL 13 - 16, FLOORBEAM FOUND CORROSION. CORROSION FLOORBEAM REPAIR IAW SRM 53-00-51 FIG 201 REPAIR 1.SDR CALA2016030895209Floorbeam · corrodedMAIN DECK CABIN STATION 287, LBL 11 FLOORBEAM FOUND CORROSION. CORROSION FLOORBEAM REPAIRED AT BS 287, LBL 32 TO RBL 90 IAW SRM 53-00-51 REPAIR 1 FIG 201.SDR CALA2016030395204Structure · crackedLEFT STATION 1809 HORIZONTAL INNER CHORD, ONE EACH FAST FOUND CRACKED, AT 8 O CLOCK POSITION, RUNNING TO EDGE. AREA REPAIRED IAW EA 5312-0 1059 REV B OP 9 STEP 1 & SRM 53-80-08 REP 10 FIG 201.SDR HALA2016030200065Eec · malfunctionedETOPS SIGNIFICANT SYS, LT ENGINE ELECTRONIC ENGINE CONTROL MODE, COME ON ICAS SCREEN. RAN CHECKLIST IN FLIGHT. ON ARRIVAL, NO, LT ENGINE, ELECTRONIC ENGINE CONTROL MODE, EICAS MESSAGE DISPLAYED. RESET LT AND RT EEC SWITCH TO, NORM AND RESET ELECTRONIC ENGINSDR HALA2016030200066Eec · malfunctionedSTATUS MSG LT ENGINE, ELECTRONIC ENGINE CONTROL C1 ILLUMINATED ON DECENT. T/S IAW FIM 73-21 FAULT TREE 828. PIMU REPORTED TCC TRACK FAIL CH A AND CH B. AFTER RESET FOR PIMU IAW FIM 71-01-803, NO MORE MESSAGES PRESENT. NO PREVIOUS HISTORY, OK FOR SERVICE.SDR CALA2016030895206Structure · crackedLEFT STATION 1809 HORIZONTAL INNER CHORD, ONE EACH FOUND CRACK AT 8 O CLOCK POSITION RUNNING TO EDGE. AREA REPAIRED IAW EA 5312-0 1059 REV B OP9 STEP 1 & SRM 53-80-08 REP 10 FIG 201 DET II.SDR CALA2016030395205Slide · departedIMMEDIATELY AFTER TAKEOFF CREW REPORTED RT WING SLIDE DEPLOYED & DEPARTED AIRPLANE. DECLARED EMER & RETURNED. INSTALLED RT OVERWING SLIDE IAW AMM ECRA 5300-02305A CREATED FOR INSPECTION & ATTACHED TO TOCS LOG FOR DAMAGE EVALUATION.SDR CALA2016030895208Door · openLEFT OFF WING SLIDE COMPARTMENT DOORS CAME OPEN DURING RE-ACTIVATION PROCEDURE. INSTALL LT OVERWING SLIDE IAW AMM & SLIDE COMPARTMENT DOORS.SDR CALA2016022900134Actuator · unserviceableCREW REPORTS SURGE ON RT ENG, FLAGGING SDR DUE TO RETURN TO FIELD. SVA FAILED IN CLOSED POSITION. R & R NR 2 ENG VARIABLE STATOR VANE ACTUATOR. BORESCOPE COMPLETED WITH NO DAMAGE FOUND.SDR CALA2016030395202Battery Pack · dischargedSUPPORT TASK, EMER LIGHTS ASSOCIATED WITH BATTERY PACK M99082 ARE INOPERATIVE. R & R EMERGENCY BATTERY PACK M99082. TESTED NORMAL IAW AMM 33-51-07.SDR CALA2016022995190Floorbeam · crackedMAIN DECK STATION 303, LBL45 FLOORBEAM PANEL FLANGE FOUND CRACK. MAIN DECK CABIN STATION 303, LBL 45. FLOORBEAM UPPER CHORD CRACKED AREA, REPAIRED IAW SRM 53-00-51 REPAIR 2 FIG 201 DETAIL I.
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