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 NACA2025073000001Elec Connector · out of limitsFOUND THE LEFT ENG EEC C2 MAINT MSG. PERFORMED TIS FOUND LT ENG 21B LVDT CONNECTOR 0834OP BETWEEN P2N & PIN 2 RESISTANCE OUT OF LIMITS IAW FIM TASK 8038-71-01, TASK 848, REV 145. REMOVED AND REPLACED LT ENG INBD TR LOCK HYD ACTUATOR & CARRIED OUT INSTALL TESDR NACA2025071800003Wire Harness · wornFOUND THE #2 EGT HARNESS WORN. REPLACED THE #2 EGT HARNESS FOUND SATIS PER AMM 77-21-02. ENGINE INFORMATION NOT AVAILABLE.SDR DALA2025071505335Switch · faultedSHIP 0190 RECEIVED RT OIL PRESSURE LIGHT AND EICAS. R & R SWITCH S1584 RT OIL PRESSURE INSPECT CONNECTOR PLUG AND WIRING IAW B767-300 IPC 79-33-01-07. (1081099).SDR NACA2025070700005Shutoff Valve · no testFOUND RH ENGINE PRSOV HEALTH CHECK FAIL. REMOVED AND REPLACED #2 ENGINE PRSOV AND CARRIED OUT TEST AS PER 767-300 AMM 36-11-09SDR NACA2025070300002Indicator · inoperativeRH ENGINE OIL PRESS IND BLANK. CLEANED AND RESECURED ELECTRICAL CONNECTOR P4208P IAW WPM 36-11-62 OPS CHECK OK.SDR CALA2025063006080Compressor · no discrepancyLOUD BANG AND BRIGHT FLASH ON LEFT SIDE AFTER TAKE OFF POSSIBLE BIRD STRIKE CREW SAID THEY FELT KICKED TO THE LEFT WITH THE LOUD BANG AND THE WHITE FLASH FROM THE LEFT SIDE, ACCMP OVERWEIGHT LANDING INSPECTION AND BIRD STRIKE INSPECTION. REF AMM TASK 05-51-35-SDR CALA2025062505870Idg · faultedRT GEN DRIVE LIGHT ILLUMINATED.FL310 35 MINS INTO FLIGHT.. UPDATE WITH EICAS MESSAGE, R GEN DRIVE HIGH IDG RISE TEMP UPDATE WITH BPCU INFO REMOVED AND REPLACED #2 ENGINE IDG AS PER AMM 24-11-01-404-001-006. OPS CHECK GOOD. FOUND OIL LEAKING FROM IDG SERVICE SDR NACA2025061800001Igniter · no test#2 ENGINE #1 IGNITOR FAILED OPS CHECK. REMOVED AND REPLACED #2 ENGINE #1 IGNITOR PLUG IAW AMM 74-21-02SDR UIEA2025061700785Oil System · leakingOIL QUANTITY ON RIGHT ENGINE DROPPED TO 8 QUARTS.(<P>ALL ITEMS FOR ACTION TAKEN TO CORRECT IAW B767 AMM 79-21 & 79-31. LP 1219035 M9: SERVICED #1 ENG 4 QTS & SERVICED #2 ENG 8 QTS IAW B767 AMM 12-15-03. NO FURTHER DEFECTS NOTED.</P>)SDR NACA2025061500001Meter · within limitsR ENGINE VIBE METER GOES UP AND DOWN FROM 0.0 TO 1.1 PERFORMED AMM 71-00-00 R ENG VIBRATION N1 WITHIN LIMIT. PERFORMED R ENG FAN BLADE PART-SPAN SHROUD LUBE PER TASK CARD 72-433-01-02SDR NACA2025060700001Shutoff Valve · failedLH ENGINE BLEED DOES NOT CLOSE ON ENGINE SHUTDOWN, CAUSES A LOW RUMBLING NOISE WITH AIR HISSING OUT FROM APU BLEED. THIS HAS BEEN AN INTERMITTENT ISSUE. REMOVED AND REPLACED THE LH PRSOV IAW AMM 36-11-09 OPS NORMALSDR NACA2025060600001Oil System · lowTHE OIL QTY ON THE RIGHT ENGINE WAS SHOWING AT 5 IN FLIGHT. LEFT ENGINE WAS 16. SERVICED RH ENGINE TO FULL PER AMM 12-13-01 RH ENGINE OIL CONSUMPTION WITHIN LIMITS. CLEANED RH ENGINE OIL TRANSMITTER PER SWM 20-60-01, NO LEAKS FOUND.SDR CALA2025060405267Idg · faultedAT CRUISE ALT, LEFT GEN DRIVE LIGHT FIRST THEN GEN OFF. 1X GEN OFF RESET FAILED REF FM 2.60.35 ON ARRIVAL LEFT IDG DELTA P POPPED OUT. IDG FILTER REMOVED AND FOUND CONTAMINATION. IDG REMOVAL/ INSTALLATION CARRIED OUT I.A.W AMM 24-11-01-004-002-006/ 24-11-01-40SDR NACA2025052400001None · noneRIGHT ENGINE START AT THE GATE ABORTED DUE TO N2 NOT STABILIZED AT 2 MINUTES. N2 AT ABOUT 48% AT 2:25. FOUND INADEQUATE FROM GROUND AIR CART. REPLACED START CART, SECOND START WAS NORMAL IAW AMM 71-00-00SDR NACA2025052400002Duct · crackedON CLIMBOUT AT 400FT AGL, ENG #2 EGT EXCEEDED LIMITS, TOPPED AT 650 DEGREES F AFTER 3 SECONDS. REDUCED THRUST, EGT STAYED WITHIN LIMITS. ON FURTHER CLIMB, #2 OIL TEMP APPROACHED LIMITS (158 DEGREES F). INSPECTED RH ENGINE AND FOUND INTERMEDIATE BLEED AIR DUCT SDR CALA2025052204903Tube · corrodedDURING ENGINE INSPECTION FOUND R ENG FIRE EXTINGUISHING TUBE BROKEN. IPC REF 26-21-55-02, ITEM 65. RT ENG FIRE EXTINGUISHING TUBE REMOVED AND REPLACED IAW AIPC: 26-21-55-02 AND AMM: 20-10-09.SDR NACA2025051100001Feeder Cable · damagedFOUND TOP EXCITER TO IGNITER CABLE ON #1 ENGINE IGNITER END DAMAGED. REPLACED #1 ENGINE EXCITER TO IGNITER PLUG CABLE IAW AMM 74-21-01 OPS TEST GOOD.SDR NACA2025050900001Engine · vibration#1 ENGINE N1 VIBE STARTED AT 1.8 AT LEVEL OFF AND SLOWLY CREEP UP TO 2.3 MAX OBSERVED IN FLIGHT WAS 2.5. DEFERRED LEFT ENGINE VIBRATION INDICATING SYSTEM PER MEL 77-31-01 CAT C.SDR NACA2025043000001Blade · damagedON PREFLIGHT LEFT ENGINE FAN BLADE DAMAGE #30. REPAIRED BLADE ON LH ENGINE #30 PER AMM 72-31-02SDR NACA2025042800001Accelerometer · failedRIGHT ENGINE VIBRATION INDICATOR INTERMITTENTLY READS BETWEEN 0.3 AND 5.0 DURING CLIMB OUT OF SPJC. REPLACED RH ACCELEROMETER IAW AMM 77-31-01SDR NACA2025042200001Sensor · faultedOIL QUANTITY ON RIGHT SIDE DROPS DURING FLIGHT (8 QUARTS) - PERFORMED T675 TEST ON OIL QTY TRANSMITTER CHECK IAW WDM 79-31-11 NO DISCREPANCIES NOTED. SERVICED OIL TO 21 AS REQUIRED PER SERVICE CHECK TASK CARD B767-2BSDR NACA2025042200002Monitor · malfunctionedRIGHT SIDE VIBRATION MONITOR OSCILLATES BETWEEN 0.5 TO 5.0 DURING CLIMB WITH NO VIBRATION FELT IN AIRCRAFT. ACCOMPLISHED WIRING CHECK FROM R ENG FAN ACCELEROMETER TO H132 D2708B NO WIRING ISSUES. ALSO APPLIED FIM 77-31 FT 807 AVM BITE/ERASE PROCEDURE. NO EICASSDR NACA2025041400001Probe · faultedR ENG EEC STATUS MESSAGE. PERFORMED FIM 71-01 FT 803 PMU BITE PROCEDURE SHOWED 2.9 BLEED VALVE THERMOCOUPLE PROBE CH-B OPENED. REMOVED AND REPLACED CH-B PROBE IAW AMM 75-32-06SDR NACA2025040800002Signal Cond Unit · failedLEFT ENGINE VIBRATIONS SEEM STUCK AT ZERO ALL CHANNELS. DEFERRED L ENG VIBRATION INOP PER MEL 77-31-01. REMOVED AND REPLACED AVM SIGNAL CONDITIONER IAW AMM 77-31-03.SDR NACA2025040500001Unknown · unknownR VIBE INDICATOR SHOWED OSCILLATION DURING CLIMB, 2.5 OR 4.0 THEN ZERO. ACCOMPLISHED FIM 77-31 FT 806 AND 807M NO DISCREPANCIES NOTED.SDR NACA2025032900001Start Valve · failedR STARTER CUTOUT EICAS MULTIPLE TIMES IN FLIGHT. REMOVED AND REPLACED RH ENGINE START VALVE IAW AMM 80-11-02SDR NACA2025032800001Igniter · faultedREMOVED AND REPLACED RIGHT ENG #2 IGNITER PLUG AND #2 IGNITION EXCITER OPS CHECK GOOD.SDR CALA2025032803288Engine · failedENG FAIL AT 18000 FEET RIGHT ENGINE SEVERE DAMAGE EGT 668 CREW DEBRIEF. THROUGH 16000FT R ENG HIGH EGT 668, HIGH ENG VIBS, NO N2 ROTATION. ENGINE SHUTDOWN INFLIGHT AND FIRE HANDLE PULLED BUT NO BOTTLES FIRED (NO FIRE WARNING). PASSENGER REPORTED FLAMES FROM RSDR ABXA20250322063Oil System · lowDURING TAXI OUT ON ENGINE START, RT ENGINE QUANTITY WAS 9. A/C RETURNED TO GATE (BTB). SERVICED RT ENGINE IAW B767 AMM 12-13-01. VERIFIED OIL CAP AND ACCESS PANEL WERE CLOSED. RETURNED A/C TO SERVICE.SDR 2025FA0000166Skin · not reportedREPAIR - ENG #1 - L/H CORE COWL INNER SKIN. AFT OF THE PRECOOLER VENT, UNDER THE PANEL 314T3210.SDR 2025FA0000167Skin · not reportedREPAIR - ENG#2 - L/H CORE COWL INNER SKIN, AFT OF THE PRECOOLER VENT, UNDER THE PANEL 314T3210.SDR 2025FA0000175Sleeve · damagedREPAIR - #1 ENGINE EXHAUST NOZZLE OUTER SLEEVE OUTER SKIN DAMGE.SDR ABXA20250205032Oil System · warning messageDURING TAXI WHILE STARTING RH ENGINE ,OIL DROPPED TO 11QTS AFTER START, A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C .CONFIRMED OIL LEVEL AND MTX DEFERRED RH OIL QTY INDICATION IAW MEL ABX-79-31-1-1 PLACARD INSTALLED AND RETURNED A/C TO SERVICE .AC REMASDR CALA2025012301978Engine · bird ingestionREJECTED T/O ENG SRG D2 PSBL BIRD INGEST RT ENG SPEED 160 HIGHE ST BTMS 9+ CREW DEBRIEF: 160 KTS, APPROACHING T/O SPEEDS, SAW BIRD FLY IN F RONT OF ACFT, HEARD A BANG ON E2, OBSERVED MOMENTARY DROP AND RE COVERY OF EPR. CAPT SIMULTANEOUSLY THROTTLED DOWN FOR SDR DALA2024112611241Warning Message · illuminated-ATB- FLIGHT RETURNED TO JFK FOR RIGHT ENGINE OIL FILTER ADVISORY MESSAGE. OVER-WATER CROSSING NOT ALLOWED PER QRH. CHECKED MCD'S AND OIL FILTER, NO ISSUES FOUND. REPLACED OIL FILTER AND DIFFERENTIAL PRESSURE SWITCH. WAITING ON ENGINE RUN. (0676925)SDR NACA2024111400001Blade · nickedLEFT ENGINE #18 BLADE HAS A NICK. REPAIRED LH ENG BLADE PER AMM 72-31-02SDR NACA2024111300001Igniter · failedLEFT ENGINE 2 FAILED START ATTEMPTS WITH #1 STARTER SELECTED. DEFERRED PER MEL 74-00-01B CAT C. REMOVED AND REPLACED LH ENGINE IGNITOR PLUG IAW AMM 74-21-02SDR CALA2024092500690Wire Harness · faultyCREW REPORTED THAT #2 ENG SN. 727337 (TSI= 28340 HRS). E GT RED ON T-OFF. EGT WENT TO 886 WITH EGT RED ON GAUGE. RETRIEVE EGT EXCEEDANCE AS PER FIM 71-08 FAULT TREE 801 (TAKE PICTURE OF EGT ECXD. PG. & ATTACH TO L/P ) REF FIM 71-05 FAULT TREE 810 F OR HIGHT ESDR DALA2024092309350Line · looseSHIP 192 -DIV/IFSD- DIVERTED TO MSP DUE TO RIGHT ENGINE OIL QUANTITY DROPPED TO ZERO. CORRECTIVE ACTION: MAINTENANCE INSPECTED RIGHT ENGINE AND FOUND LOOSE OIL LINE AT LOW OIL PRESSURE WARNING SWITCH TO TEE FITTING. TIGHTENED OIL LINE, NO LEAKS NOTED ON ENGINESDR DALA2024082608450Eec · faultedDIV/IFSD- LEFT ENGINE ROLLED BACK AND SHUTDOWN. MCD AND OIL FILTER CLEAN. PERFORMED PIMU BITE FOUND CHANNEL A/B P5 FAULT. FAULT CONFIRMED ON HIGH POWER RUN. REPLACED LEFT EEC COMPLETED HIGH POWER RUNS. OPS CHECK NORMAL.SDR NACA2024080700001Heat Exchanger · failedREMOVED AND REPLACED RH VALVE AIR/OIL HEAT EXCHANGER ON #2 ENGINE LEAK AND OPS CHECK GOOD IAW 24-11-12 AND AMM 71-00-00. PART IS UNKNOWN TO TRAX.SDR CALA2024072300271Pump · faultedR COMPRESSOR STALLGOT COMPRESSOR STALL AT 2500 FEET SPEED 200KT ON FINAL APPROACH INTO IAD. USE FIM 71-05 TASK 803 FOR TROUBLESHOOTING. WORKED FIM 71-05 THROUGH TO BLOCK 7 WITH NO DAMAGE NOTED.N1 ROTOR SPINS FREELY IN BOTH DIRECTIONS. NO DAMAGE TO FAN CASE RUBSDR CALA2024062400069Chip Detector · missing#2 ENGINE MAGNETIC CHIP DETECTORS (MCD) INSPECTION {B767-72-3-7011} - COMPT NO.4 MCD FOUND MISSING ON INSP SDR AND MATERIAL UPDATE MCD INSTALLED IAW AMM: 79-21-10-424-008-N0.SDR NACA2024060900002Engine · failedLEFT ENGINE CHANGE IS REQUIRED DUE TO BORESCOPE INSPECTION AS UNSERVICEABLE CONDITION ENGINE SN 724732. REMOVED AND INSTALLED LEFT ENGINE IAW AMM 71-00-02, LEAK CHECK AND ENGINE RUN GOOD.SDR NACA2024060500002Eec · faultedL ENG EEC C1. TS PER FIM 73-21 FT 878 FOUND THE EEC CH A/6 ADC TR-CK FAIL MESSAGE. CARRIED OUT THE FIM 71-01 TASK 830 FOUND THE WIRING CONT CHECK IS GOOD. ENG RUN NO ISSUES.SDR NACA2024052000002Anti-Ice Valve · failedL ENG ANTI-ICE DOES NOT ALWAYS CLOSE, VALVE LIGHT STAYS ON, EXTINGUISHES LATER. REMOVED AND REPLACED LH ENGINE INLET TAI VALVE. PER AMM 30-21-03, OPS AND LEAK CHECK GOOD. UNIT UNKNOWN TO TRAX.SDR NACA202404060001Blade · bentDURING DAILY CHECK FOUND BLADE #9 BENT, APPROX 6" FROM THE TIP ON LH ENGINE. INSPECTED PER B767 AMM 72-31-02, FOUND WITHIN LIMITS. ACCOMPLISHED FPI PER AMM 70-11-06, NO DEFECTS NOTED.SDR NACA2024032200002Igniter · wornDURING ENGINE 1 IGNITOR PLUGS INSPECTION FOUND IGNITOR PLUG WORN OUT. REMOVED AND REPLACED IGNITOR PLUG 1 ON ENGINE 1 PER AMM 74-21-02 OPS CHECK GOOD PER AMM 74-00-00SDR DALA2024021602290Idg · faultedSHIP 0172 -ATB- RIGHT GENERATOR DRIVE LIGHT ILLUMINATED. APU STARTED NORMAL. CORRECTIVE ACTION: REPLACED RIGHT IDG PER B767 AMM 24-11. OPS NORMAL. (5726756)SDR CALA2024020200303Clamp · misinstalledL STRUT DUCT LEAK INDICATION DURING CLIMB THRU FL180 DURING TROUBLESHOOTING, FOUND THE NO.1 ENGINE THERMAL ANTI-ICE VALVE AFT CLAMP INCORRECTLY INSTALLED AND NOT MATED PROPERLY TO THE DUCT AND VALVE FLANGE. PHOTO ATTACHED. REMOVED BOTH ANTI-ICE VALVE MOUNTING
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