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 CALA2026083119023Outflow Valve · faultedCABIN ALT AUTO 1 EICAS M THE AUTOMATIC PRESSURIZATION CONTROLLER 1 BITE FOUND A FAILURE. CABIN ALT UP TO APPROX 13000 FEETAS PER TOMC REQUEST REPLACED CABIN AUTO 1 PRESSURE CONTROLLER IAW AMM 21-31-02-004-00 & AMM 21-31-02-404-005 UP TO SECTION 3(D)1. REPLACESDR CALA2026083119025Relief Valve · faultedTHUMPING NOISE AT DOOR 1R INFLIGHT. DURING A DETAILED VISUAL INSPECTION OF R1 DOOR, FOUND LOWER DOOR BUSTLE DETACHED & LOOSE ON FWD SIDE. BUSTLE RESECURED IAW AMM 25-66-01-416-010. WHILE CARRING OUT THE EXCESSIVE CABIN PRESSURE LEAKAGE TEST IAW AMM 05-51-2SDR CALA2026083119076Skin · puncturedPUNCTURE BETWEEN AFT CARGO DOOR AND R3 ENTRY DOOR ON THE RIGHT SIDE OF ACFT. DAMAGE LOCATED BTWN BS 1439 & 1461 IAW SRM 53-00-00-0G-0. FOUND DAMAGE TO BE 5.4 INCH LONG BY 2.6 INCH WIDE, ON BS 1439 - 1461, STR 21-22R. DAMAGE IS OUT OF LIMITS IAW SRM 53-00-SDR CALA2026090119173Lens · missingWHITE EMERGENCY LIGHT LENS MISSING AT SEAT 32F. REMOVED AND REPLACED WITH A NEW EMERGENCY LIGHT AT ROW 3 F. OPS CHECKED GOOD IAW CMM 25-21-53 & AMM 33-51-00.SDR CALA2026083119068Computer · faultedLT NAV WILL NOT ENGAGE, MODE CONTROL PANEL HAVE TO BE REPLACED, AUTO THROTTLES DISENGAGED OFF GATE RESET TO THRUST MANAGEMENT COMPUTER, FCC CENTER REPLACED IAW AMM 22-11-01/401-001, REV 148, NOW TESTS OK.SDR CALA2026083119003Lens · brokenEXTERIOR EMERGENCY LIGHT L396 IS WITH LENS BROKEN. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT LENS IAW AMM 33-51-06-960-801. GOOD FOR SERVICE.SDR CALA2026083119005Light · brokenESCAPE PATH LIGHT ASSEMBLY ON SEAT 42D AND 30F ARE BROKEN. R & R ESCAPE PATH LIGHT ASSEMBLY ON SEAT 30F AND 42D IAW AMM 33-51-10-962-104. ESCAPE PATH LIGHT SYSTEM, GOOD FOR SERVICE.SDR CALA2026083119036Smoke Goggles · contaminatedCAPTAIN`S SMOKE GOGGLES COMPT FILLED WITH 1/4 OF COFFEE, GOGGLE BAG SATURATED, GOGGLES UNUSABLE. CAPTAIN SMOKE GOGGLES COMPARTMENT AND BAG HAD ALREADY BEEN CLEANED IAW AMM 25-64-96-860-801-C1.NO DAMAGE FOUND.SDR CALA2026082618923Lamp · inoperativeSEAT 43AB CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS, OPS CHECK CARRIED OUT GOOD IAW AMM 33-51-04-002-001.SDR CALA2026082518904Oven · odorOVEN 109 IN FWD GALLEY HAD LIGHT SMOKEY ODOR WHEN PLATES CAME OU T GALLEY OVEN 109 HEAVILY CONTAMINATED, CLEANED IAW AMM 25-05-03-100-801-C1. OVEN OPERATED FOR 10MINS. SMELL NO LONGER PRESENT.SDR CALA2026082418860Controller · faultedVIBRATION ON RT SIDE OF ACT, DID NOT FEEL IT BEHIND FIRST CLASS. WHILE STARTING BOTH ENGINES, FELT VIBRATION ONLY ON FIRST OFFICER`S SIDE OF THE FLT DECK. VIBRATION WENT AWAY DURING TAXI & TAKEOFF. IN CLIMB, FELT VIBRATION ON F/O SIDE OF FLT DECK ONLY. VISDR 2026FA0000657Oil System · faultedHAD AN AIR RETURN FLIGHT, IN GENEVA, WITH CUSTOMER UNITED. THE AIRCRAFT FLIGHT NUMBER UA957. AIRCRAFT EXPERIENCED AN ABNORMAL INCREASE IN ENGINE 1 OIL PRESSURE, ACCOMPANIED BY ABNORMAL ENGINE NOISE, A BURNING ODOR, & SMOKE IN THE CABIN. THE FLIGHT CREW SUBSEQSDR CALA2026082118777Wire · shortedEMERGENCY LIGHTS TEST WITH TEST SWITCHES. GALLEY G2(8X) AND G2A (4X) EMERGENCY ESCAPE PATH LIGHTS INOP. WIRING CHECK AS PER 767-N0624-D74, SSM SUPPLEMENT 25-00-00, FOUND SHORTED. DISCONNECTED AND REMOVED ALL 12 EMERGENCY LIGHT ASSY FROM G2 & G2A, FOUND ONE OFSDR CALA2026082118796Lens · brokenEMERGENCY ESCAPE PATH LIGHTING SYSTEM PERFORM AN OPS CHK, LIGHT LENSES AT POSITIONS 33D, 34D, 39D AND 41F BROKEN. REMOVED AND REPLACED THE LENSES IAW AMM 33-51-10/201, ITEM GOOD FOR SERVICE.SDR CALA2026083119059Engine · failedLEFT ENGINE FAILED DURING CLIMB, ENG1 SN. (TSI= , CSI= CYC). CREW REPORTED THAT ENG1 WAS SHUTDOWN DUE TO THICK SMOKE IN THE CABIN (L/P 3038084). OIL PRESS IN RED WHILE IN IDLE. EGT 715, FLIGHT ATTENDANTS REPORTED THAT LEFT ENG WAS SHAKING VIOLENTLY ON THE WINSDR CALA2026081918738Proximity Switch · faultedLEFT WING SLIDE EICAS MESSAGE AND EMER DOORS ANNUNCIATOR LIGHT ON MOMENTARILY IN CRUISE. LT WING SLIDE DOOR ON WING TO BODY FAIRY INSPECTED. FOUND LATCHED PROPERLY. SUSPECT PROX SWITCH GIVING FALSE READING. NOT POSSIBLE TO REPRODUCE. FAULT CLEARED. IAW AMM 52SDR CALA2026082018758Access Panel · misinstalledDURING TOWING, LT FUEL LEAKAGE FROM LT SURGE TANK, ACCESS PANEL 541XB. FOUND PANEL HAD BEEN INSTALLED 180 DEGREES OUT OF ALIGNMENT, WITH MISPOSITIONED ALIGNMENT DOWEL THE LIKELY CAUSE FOR FUEL LEAK. FOD CHECK BEFORE PANEL. NO FOD NOTED. INSTALLED THE TANKSDR CALA2026081818706Controller · faultyAT 30000 FT BOTH PACK TEMP AND PACK OFF LIGHTS ILLUMINATED, EICAS AUTO EVENT RECORDED. PERF. PACK TEMP. CONTROLLER BITE REF. FIM 21-51 FAULT TREE 803. NO FAULTS. OPERATED BOTH PACKS WITH APU BLEED AIR FOR 1 HOUR REF. AMM 21-00-00. UNABLE TO DUPLICATE FAULTS. PSDR CALA2026081918727Light · brokenESCAPE PATH LIGHT ASSEMBLY ON SEAT 33D, 40F AND 50F ARE BROKEN. REMOVED AND REPLACED ESCAPE PATH LIGHT ASSEMBLY ON SEATS 40F AND 50F REF AMM 33-51-10-962-104. ESCAPE PATH LIGHT SYSTEM IS GOOD FOR SERVICE.SDR CALA2026082418864Brake · overtempBRAKE TEMP MONITORING SYS, BRAKE TEMP DISPLAYED. NR 7=1, 8=2, 9=3, 10=4, 11=5, 12=6, 13=7, 14=8, BRAKE TEMPS HIGH. MAX LEVEL 01 ON TAKEOFF. BRAKE TEMP LIGHT ON WHEEL 7 AT TEMP 7 LANDED WHEEL 7 BLOWN. PERFORMED HIGH ENERGY STOP CONDITIONAL INSPECTION IAW SDR CALA2026090219196Slide Raft · unraveledPASSENGER CABIN, AT DOOR 843 THE SLIDE- RAFT ASSEMBLY LT SIDE WAS FOUND DISENGAGED.WO MRO 550062620. TASK 64-2566-1-0012. ACCOMPLISHED REMOVED AND REPLACED IAW AMM 25-66-01-004-001 AND 25-66-01-404-072, REV 148, REV-.SDR CALA2026081218514Access Panel · misinstalledFUEL LEAK FROM LT WING SURGE TANK DOOR ASSY, PRESSURE RELIEF VALVE ACCESS PANEL LEAKING FUEL. SUMPED SURGE TANK VIA PIDDLE DRAIN, REMOVED ACCESS PANEL 542AB DUE TO VISIBLE FUEL LEAK. PANEL REMOVED IAW AMM 28-11-01-004-013, AND REF ECRA 2810-10336. FOUND SDR CALA2026081418625Actuator · faultyCABIN ALTITUDE EICAS WARNING. CABIN ALTITUDE 10000 FT PILOTS REPORT EICAS WARNING AT FL330. AT THE TIME CABIN PRESSURE SHOWED 10000 WITH DIFFERENTIAL PRESSURE AT 7. ON DESCENT TO FL320 CABIN PRESSURE SHOWED 8500 WITH DIFFERENTIAL REMAINING AT 7. PERFORMED BSDR CALA2026081418626Buss · trippedGALLEY POWER WAS NOT RESTORED AFTER LOAD SHED AFTER DEPARTING LHR TURNED OFF ALL GALEY USERS INCLUDING IFE SYSTEM. PROCEEDED TO RESET R UTILITY BUS REF FM 2.60.45 ALL GALLEY MONUMENTS POWER RESTORED.SDR CALA2026081118454Wire · detachedOPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM. EMERGENCY EXIT SIGN OVER OVERWING EXIT 20A NOT ILLUMINATING. WIRE HAS COME AWAY FROM RING TERMINAL X1. NEW RING TERMINAL CRIMPED ON WIRE W834-012-18 OF L700 EXIT SIGN, LEFT OVER-WING HATCH STA 916, WL 260, LBL SDR CALA2026081018423Light · detachedSEAT 41F FLOOR EMERGENCY LIGHT ASSY FOUND DETACHED FROM SEAT. EMERGENCY LIGHT ASSY REPLACED. CHECKED OPS. ALL NORMAL. WRT AMM 33-51-10-972-104.SDR CALA2026081118450Window · crackedLEFT FWD SIDE WINDOW CRACKED ON TAXI OUT, FOUND L2 WINDOW WITH CRACK PLUS DELAMINATION ON RT UPPER CORNER, EXTENDS TO HEATING ELEMENT WITH APROX 13 IN. MEASURED HEATING ELEMENT J8 & FOUND OPEN IAW SSM 30-42-02-101.1, AMM 56- 11-00-216-016, FIG 607. REMOVEDSDR CALA2026080918414Hinge Pin · out of positionF/A REPORTED PAX AT OVERWING EMERGENCY ESCAPE HATCH SEATS 20BA, EXPERIENCED NOISE & VIBRATIONS COMING FROM THE FLOOR AREA. LASTED FOR 15 MINS & ABRUPTLY STOPPED. FLT CREW MISINTERPRETED REPORT LOCATION AS AROUND THE LT ENG AREA. PERFORMED EXTERIOR GVI OF LT SDR CALA2026081118465Aileron · contaminatedPERFORMING THERMOGRAPHY INSPECTION ON LT WING, OTBD AILERON LOWER SURFACE, NOTICED MOISTURE UNDER THE LIGHTNING FRAME AT THE OTBD END OF THE AILERON. LT OTBD AILERON WAS REPAIRED. THIS REPAIR IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS PER PART 2 OFSDR 2026F00138Carbon Seal · leakingDURING CRUISE THE A/C FACE RT OIL PRESSURE LT INTERMITTENT ILLUMINATION AND RT ENG QTY INDICATION 0. OIL PRESS FLUCTUATES DOWN 1 TO 27 TEMP NORMAL. CREW REPORTED THAT APPROXIMATELY TWO HOURS PRIOR TO ARRIVAL, INTERMITTENT ENG2 OIL PRESSURE WARNING INDICATIONSSDR ABXA20260519215Engine · faultedDURING ENGINE START, LT ENG NO ROTATION DURING X-BLEED START - RT ENG BLEED NEVER OPENED - TRIED MULTIPLE BLEED ISOLATION VALVE COMBINATIONS WITH NO ROTATION. CREW RETURNED TO THE GATE (BTB). MTC INSPECTED LEFT ENGINE ISOLATION VALVE AND CYCLED. STARTED LEFT ESDR CALA2026052716563Engine · faultedRT ENG OIL PRESS ZERO SHUT DOWN IN FLIGHT HAD COMP STALLS AND FLAMES REPORTED REFERENCE LOG PAGE 9027944 FOR # 2 ENGINE REPLACEMENT REMOVED AND REPLACED # 2 ENGINE AS PER TASK CARD 64-7100-1-0011 AND 76-0571-8-0015. RAN ENGINE, ALL CHECKS GOOD AND NO LEAKS NOTSDR CALA2026051316216Oil System · leakingPOWER PLANT OIL QUANTITY (01=L ENG, 02=R ENG) ZERO, ENGINE OIL P RESSURE WAS (ZERO, LOW) R ENG OIL QUANTITY AND PRESSURE AT 0 AFTER START. ENGINE OIL WAS 22 PRIOR TO START ENG 2 CREW REPORTED THAT RIGHT ENGINE WAS STARTED WITH NORMAL OIL PRESS / QTY, BUT OIL WSDR ABXA20260510192Proximity Sensor · defectiveDURING PUSH. WHEN WE STARTED THE RIGHT ENGINE, "R ENG CONTROL" AND "R ENG MODE EEC EICAS" SHOWED.AND A/C RETURNED TO GATE (BTB),MTX GROUNDED A/C AND TROUBLESHOT TO LEFT GEAR TILT SENSOR "S267" FAULTED. REMOVED & REPLACED THE SENSOR, REF B767 AMM 32-09-02. ALL SDR CALA2026042415693Igniter · faultedON FIRST ENGINE START ATTEMPT ON LEFT ENGINE WITH ENGINE START IGNITER IN NO. 2 POSITION. NO ENGINE VALVE LIGHT WITH NO RISE IN EGT. ABORTED START WITH CHECKLIST FUMES DETECTED IN CABIN. SECOND START WITH IGNITORS IN BOTH WAS GOOD BUT WITH MORE FUMES IN CABIN SDR DALA2026041702451Heat Exchanger · leakingDIVERTED TO HND FOR LEFT ENGINE OIL QUANTITY DECREASED TO ZERO WITH STABLE TEMPERATURE AND PRESSURE. RIGHT ENGINE ALSO HAD OIL QUANTITY DECREASING WITH STABLE TEMPERATURE AND PRESSURE. REPLACED BOTH LEFT AND RIGHT ENGINE AIR OIL HEAT EXCHANGER FOR LEAKING.(8SDR CALA2026030914408Fmu · unserviceableEGT REACHED 597C DURING ENGINE START NR 2 PILOT DEBRIEFED UPON RTB EVENT, THEY CONFIRMED THAT START PROCEDURE WAS NORMAL UP UNTIL THE LATER STAGE WHEN THEY NOTICED THE EGT WAS GETTING OUT OF PARAMETERS, LIGHT UP WAS WITHIN SECONDS AS PER NORMAL, THEY CONFIRM TSDR CALA2026030214137Engine · hung startLEFT ENGINE HUNG ON 1ST. GOOD START ON IGN BOTH. LIGHT OFF. STARTED ON STRONG ODOR IN CABIN PREFORMED ENGINE START AND RUN, WALKED CABIN AND VERIFIED NO ODORS PRESENT IAW AMM 71-00-00. LEFT ENGINE HUNG ON 1ST ATTEMPT. GOOD START ON BOTH IGNITIONS. AFTER LIGHSDR CALA2026020413545Idg · faultedAFTER TAKEOFF LOST L GEN. CREW FOLLOWED FM AND DISCONNECTED IDG .BPCU READ OUT DISPLAYED L IDG HIGH DELTA TEMP. NR 1 ENG C DUCTS OPENED TO INSPECT IDG FOUND NO LEAKS OR EXTERNAL DEFECTS, FOUND DURING IDG SERVICING 1,5 QT OF OIL ON OVERFLOW CAME OUT. NO OTHER SDR CALA2026012913421Blades · shingledRIGHT N1 VIBRATION OF 5.0 OR HIGHER WITH NOTICABLE VIBRATION. DEBRIEFED CREW. STATED N1 VIBE WAS AT 5.0 THROUGHOUT CRUISE. VIBE DECREASED WHEN POWER ADDED TO ABOUT 3.0 & INCREASED BACK TO AROUND 5.0 WHEN POWER REMOVED. CREW STATED VIBRATION NOTICEBLE PHYSICALSDR NACA2026012100001Hpc · faultedNUMBER 2 ENGINE BLEED LIGHT ILLUMINATED DURING ENGINE RUN WITH HSPOV MESSAGE DISPLAYED ON ICAS. REMOVED AND REPLACED NR 2 ENG HPC IAW AMM 36-11-18-04-005-008 AND 36-11-08-04-0050-008 OPS CHECK GOOD.SDR NACA2026012000001Pressure Switch · leakingNUMBER 1 ENGINE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH LEAKING. REMOVED AND REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH IAW AMM 73-34-01-004-001 AND AMM 73-34-01-404-016 NO LEAK NOTED.SDR CALA2026012113128Engine · faultedFL320 EPR ON RT ENGINE WENT TO 0. FUEL FLOW 0. N1 & N2 AND EGT NORMAL. DESENDED FL260 REF LOGPAGES 7585195, 7585208, 7585331, 7585968 DUE TO ENG 2 EXCEEDENCES AND DAMAGE FOUND, REPLACED ENG 2 PER JOB CARD 76-0572-8-0015.SDR NACA202601060001Blades · damagedNR 2 ENGINE, SIX FAN BLADES WERE DAMAGED DURING INSTALLATION OF INLET COWL AT 12 O'CLOCK POSITION. THE ENGINE WAS R & R FOR REPAIR. RECEIVED SERVICEABLE ENGINE. ENGINE WILL BE REINSTALLED ON W/O 4677 NR 21605SDR NACA2025122200001Blades · mechanic errorNUMBER 2 ENG. SIX FAN BLADES WERE DAMAGED DURING INSTALLATION OF INLET COWL AT 12 O'CLOCK POSITION. ENGINE R & R FOR REPAIR. RECEIVED SERVICEABLE ENGINE. ENGINE WILL BE REINSTALLED ON W/O 4677 NR 21605SDR CALA2025121212072Controller · failedCREW REPORTED NOISE/BANG/SHUTTER COMING FROM LT ENGINE IN TWO OCCASIONS DURING FLIGHT, AT 35K FT & THEN ON DESCENT. IN BOTH OCCASIONS N1 SPOOLED DOWN & EPR REDUCED, 0.91 OPPOSITE 1.07, EGT WAS APPROX 70 DEG HIGHER. L ENG SURGE DET MAINT MSG ON ARRIVAL. NOTEDSDR CALA2025120811899Duct · crackedBELOW 50 PERCENT THRUST LT ENG ANTI ICE VALVE CAME ON A FEW TIMES THEN RESOLVED PERFORMED L ENG IDLE RUN FOUND LT ENG ANTI-ICE VALVE LIGHT INTERMITTENTLY ILLUMINATED, C/W AMM 36-11-00-715-149, ASPCU OPERATIONAL TEST. FOUND ASPCU SHOWING LT HPSOV FAULT. FOUSDR CALA2025120811863Wire Harness · damagedDAMAGE FOUND TO NR 2 ENG ON LOOM FROM PYLON DISCONNECT TO EEC CONNECTOR D11686. HARNESS DISCONNECTED FOR FURTHER TROUBLESHOOTING. FOUND BENT PIN T ON CONNECTOR D11686. FOUND DAMAGE TO EEC CONNECTOR F THAT CONNECTES TO D11686. EEC REPLACEMENT CARRIED OUT ON SDR CALA2025120511795Eec · faultedCAPTAIN REPORTED MOMENTARY NOISE/BANG/SHUTTER DESCENDING THROUGH 37K, ENG PARAMETERS NORMAL. FELT LIKE GEAR COMING OUT BUT GEAR NOT DOWN. POSSIBLE CARGO SHIFT? NORMAL THROUGH REST OF DECENT.C/O GVI OF STAB, CONTROL SURFACES, GEAR & BAY PER AMM 05-41-07, 05-41-SDR DALA2025120308836Oil System · low pressureDIV/IFSD- DIVERTED TO LAX DUE TO RIGHT ENGINE OIL PRESSURE LOSS. ENGINE OPERATED AT ZERO OIL PRESSURE. REPLACED NUMBER 2 ENGINE, OPS CHECK NORMAL.(8171678)
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