Pratt & Whitney PW4060
Service difficulty reports · 7,186
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 UALA2011122107051Rub Strip · damagedNR 2 ENG O/B REV RUBSTRIP DAMAGED AND LOWER GUIDE CHANNEL WORN. REPLACED NR 2 ENG OTBRD REV RUBSTRIP. WAITING ON GUIDE CHANNEL ON AOG. REPLACED NR 2 ENGINE OUTBOARD GUIDE CHANNEL. GUIDE CHANNEL REQUIRES SEALANT APPLICATION.SDR UALA2011122107052Indicator · defectiveCABIN PRESSURIZATION VSI RATE GOING FROM 0 TO 2000 FPM RAPIDLY. REPLACED CABIN PRESS INDICATOR, OPS NORMAL.SDR UALA2011121906928Warning System · activatedR ENG FUEL FILT EICAS MSG, RTFLSDR UALA2011121906968Controller · faultyAPU NO START. REPLACED APU CONTROLLER PER AMM, OPS CHK OK. SECURED CONNECTOR TO APU DOOR ACTUATOR. STARTED APU. SATISFACTORY OPERATIONS.SDR UALA2011121906967Slide · detachedR1 DOOR SLIDE WAS PARTIALLY DEPLOYED. DOOR CHECK PERFORMED. FOUND DOOR SLIDE PARTIALLY DETACHED. REPLACED DOOR SLIDE PER MM.SDR UALA2011121906969Actuator · unknownAILERON LOCKED LIGHT ON AT HIGH SPEED. EICAS MESSAGE AILERON LOCKOUT DISPLAYED. OUTBD AILERONS INDICATED NORMAL - LOCKED OUT. ANNUNCIATION DISPLAYED FOR APPROX 10 SECONDS. ACCOMPLISHED FIM 27-11-00 F104 AND FAULT BALLS FOR 'ADC' ON RIGHT SAM AND 'R AIL LOCKSDR UALA2011122107005Pump · failedLEFT ELECTRIC HYDRAULIC PUMP SHOWS NO PRESSURE INDICATED WHEN IN AUTO OR ON, ENGINE RUNNING OR NOT. REPLACED LT ENGINE EDP PRESSURE CASE DRAIN FILTER MODULE PER MM, OPS CK IS NORMAL.SDR UALA2011122107039Controller · failedECM HAS PARAMETER SHIFTS DETECTED AT CRUISE & TAKEOFF. NO MESSAGES DOWNLINKED. REPLACED CONTROLLER PER MM 36-11-08. BITE CHECKED GOOD PER MM.SDR UALA2011121906930Panel · looseFOUND DURING WALK AROUND THE RT ANTI-ICE DUCT FAIRING PANEL JUST OUTSIDE OF THE ENGINE REAR PART HANGING DOWN. REMOVED PER CDL 57EE. DOOR ASSY IS LOST. REPLACED PANEL.SDR UALA2011121906959Relay · faultyDUE TO REPORT OF EXTERNAL POWER CONTACTOR NOT OPENING AFTER EXTERNAL POWER WAS DE-SELECTED AND EXTERNAL POWER WAS REMOVED REPLACED EXTERNAL POWER CONTACTOR K114 PER MM. RPL'D EXTERNAL PWR CONTACTOR, CKS OKAY PER MM TEST. RAN ENGINES TO DUPLICATE DF680, PWR WSDR UALA2011121906971Door · openAT DEPARTURE CENTER FUEL PUMPS REMAINED ON WHEN THEY SHOULD HAVE SHUTOFF. FOUND FUELING DOOR AJAR SECURED FUELING DOOR, OPS CKS OKAY.SDR UALA2011121906972Anti-Ice Valve · malfunctionedRIGHT ENG ANTI ICE ILLUMINATED. FOLLOWED CHKLIST KEPT VALVE OPEN PER QRH. SAMC TEXT: PER CREW COMMENT THE RT ENG ANTI ICE VLV IS STUCK IN THE OPEN POSITION. RT ENG ANTI ICE VLV CHK FOR FREE MOVEMENT, ALL NORMAL. ELECTR CONNECTOR CLEANED. FOR REF USED SERSDR UALA2011121906970Latch · brokenEMERGENCY FLASHLIGHT COMPARTMENT DOOR BELOW JUMPSEAT 260, CENTRE SEAT AT MID CROSS AISLE,HAS RIGHT DOOR LATCH BROKEN. DOOR SECURED CLOSED. LATCH TIE ROD BROKEN.SDR UALA2011121906952Connector · not seatedONE AREA OF EMER EXITS LIGHTS FLASHED ON AND OFF DURING DESCENT REPORTED BY PSGRS IN 19&20AB. RESEATED CONNECTOR ON AREA POWER SUPPLY, EMERGENCY LIGHTS OPS OK.SDR UALA2011121906951Power Supply · malfunctionedEMERGENCY LIGHTS CAME ON DURNG FLIGHT WITH SWITCH ARMED. OFF WHEN SWITCH IS OFF. FA REPORTS EMERGENCY LIGHTS ILLUMINATED CONTINUOUSLY AT 2R AND IN THE FWD PART OF AFT GALLEY. REPLACED POWER SUPPLY PER 33-51-07, OPS CHECKED OK.SDR UALA2011121606921Selector Panel · inoperativeRADIOS INOPERATIVE. REPLACED SECOND OBS AUDIO SELECTOR PANEL PER MM.SDR UALA2011121606922Connector · dirtyIN CRUISE FLIGHT STATUS-MSG CAME ON L ENG EEC1. SAMC TEXT: ACTUAL FAULT CODE DOWNLINKED IS E352 BIT-14 FOR N1 RANGE FAIL CH-B. MAINT TEXT: PER TOMC ENG DOWNLOAD FAULTS 270A, 270B, 350A, 350B & 352B. ENG EEC NR 1 C1 & ENG NR 1 EEC C2 MSG. CLEANED ENG NR 1 SDR UALA2011121606923Transceiver · defectiveHF TRANSMISSION & RECEPTION ARE INOP, WEAK, GARBLED INTERMITTENT, ETC. AT ALL CREW STNS. (1 = L HF, 2 = R HF) CREW COMMENTS: UNABLE TO XMIT. CAN RECEIVE OK. LONG SIDE TONE WHEN TUNING. COMPLIED WITH MEL. REMOVED AND REPLACED RIGHT HF TRANSCEIVER.SDR UALA2011121506903Shear Tie · corrodedCORROSION ON SHEAR TIE ON FWD AND AFT SIDE AT BS 1562 BETWEEN S38L - 38R. MAJOR REPAIR ACCOMPLISHED, REPAIRED FRAME SHEAR TIE IAW PD 67-53- 034 AND ECRA 5360-01170.SDR UALA2011121406859Audio Panel · faultyFIRST OFFICERS VHF L SELECTOR BUTTON STICKS AND IS HARD TO DEPRESS. REPLACED F/O'S AUDIO SELECT PANEL, OP CHECKS NORMAL.SDR UALA2011121406868Control Valve · malfunctionedRIGHT PACK OFF-RIGHT BLEED OFF PROBLEMS. ACCOMPLISH RIGHT PACK LOW LIMIT VALVE TEST PER MM. ACCOMPLISH PACK TEMP CONTROLLER BITE PROCEDURE PER MM. IF NO FAULTS FOUND WITH THE LOW LIMIT VLV OR PACK TEMP CONT BITE, REPLACE THE RIGHT PACK FLOW CONTROL VLV PCSDR UALA2011121406870Thrust Reverser · damagedFOUND RT ENG INB TR DAMAGED AND STRUT FAIRING COVER MISSING AT THE 9 O'CLOCK POSITION. DAMAGE IS APPROX 7"X .5" WIDE WITH A DEPTH OF .5". PER AVO #1103 COMPLETED REPAIR STEPS 1-5. SEALANT NEEDS TO BE CONFIRMED CURED AND STEP 6 & 7 NEED TO BE COMPLETED. REF ESDR UALA2011121406869Controller · failedRT ENG BLEED OFF AND NO AIR AVAILABLE FOR RT ENGINE ANTI ICE, ACCOMPLISHED PNEUMATIC HEALTH CHECK ON RT ENG PRIORITY VALVE PER MM. FOUND WIRE W3508-009-18 CHAFED TO GROUND APPROX 14" AWAY FROM D11116P. REPAIRED INSULATION PER SWPM. ALSO PRC FAILED HEALTH CHECSDR UALA2011121506890Unknown · unknownON DESCENT GOT STATUS R ENG CONTROL AND R ENG EEC C1. PIMU SHOWS CH A AND CH B B25 TR-CK FAIL. 2.5 BLEED VALVE ACTUATOR CONNECTION CHECKED AND CLEANED, TEST 15 EEC GROUND TEST OF ENGINE CONTROL SYSTEM ACTUATORS CARRIED OUT IAW AMM PAGE 586D AND FIM 71 PIMU MESDR UALA2011121406839Hose · crackedONE HOSE TO THE ANTI SKID SHUT OFF VALVE MODULE IS CRACKED. BRAKE POS 6 HAS BEEN DEACTIVATED. REPAIRED, PRESSURIZED LINE TO 6K PSI, NO LEAKS NOTED. FOUND BAD UNION PACKING. REPLACED PACKING, OPS NORMAL.SDR UALA2011121406843Linkage · unsecureON WALKAROUND FOUND STEERING LINK AT NLG WITH ONE BOLT LOOSE AND THE OTHER ONE NOT INSTALLED. REPLACED MISSING BOLT AND CHKD IAW MM, CKD OKAY. BOLT REPLACED IS IAW ECRA3251-01031 INSTALLED SUBSTITUTE BOLT NAS67004U15 AND TWO EXTRA WASHERS CKD OK AS PERMANENTSDR UALA2011121206795Light · unknownEMERGENCY LIGHT AFT CABIN FLICKERS ROW 38 TO AFT GALLEY - ACCOMPLISHED CHECK OF LIGHTS AND CONNECTORS. ACCOMPLISHED OPS CHECK REF MM AND ALL OK.SDR UALA2011121206790Priority Valve · faultedCREW REPORTED NO RT HIGH STAGE BLEED AT 80 PERCENT N1. RT BLEED DUCT OSCILATES BETWEEN 20-40 PSI DURING CLIMB. IN DESCENT RT DUCT 20 PSI LESS THAN LEFT. VALVE IN LOCKED IN INTERMEDIATE POSITION. FAULTING FAN AIR TEMP SENSOR. ON TAKEOFF AND CLIMBOUT RIGHT DSDR UALA2011121206782Shutoff Valve · leakingRIGHT BLEED ISSUE, RTFL. PRSOV LEAKING. REPLACED PRSOV. LEAK CHECKED LINE TO PRSOV, OK. COMPLETED RUN UP BLEED SHIFT, OK. ALL PRESSURES NORMAL.SDR UALA2011121206789Pressure Switch · malfunctionedCENTER HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED WITH EICAS AND ADP LOW PRESSURE LIGHT. REPLACED CENTER HYD SYSTEM LOW PRESSURE SWITCH PER MM, OPS NORMAL.SDR UALA2011121206824Control Panel · malfunctionedCAPTAIN'S AUDIO PANEL TRANSMIT LIGHTS INOPERATIVE. REPLACED CAPTS AUDIO CONTROL PANEL.SDR UALA2011121206825Power Supply · inoperativeINTERIOR EMERGENCY AISLE LIGHTS AND EXIT SIGN LIGHT ARE INOPERATIVE. REPLACED POWER SUPPLY, LIGHTS CHECKED OK.SDR UALA2011120906767Controller · faultyFWD CABIN TEMP EICAS DISPLAYED. NO FAULTS ON GRD, BITE OKAY. REPLACED ZONE TEMP CONTROLLER PER MM, BITE OK. ALSO CLEANED FWD ZONE TEMP SENSOR.SDR UALA2011120906773Controller · faultedRIGHT BLEED DUCT OSCILLATES B-W 20-40 PSI DURING CLIMB. IN DESCENT RT DUCT 20 PSI LESS THAN LEFT. VALVE IN LOCKED INTERMEDIATE POSITION. FAULTING FAN AIR TEMP SENSOR. ON TAKEOFF AND CLIMBOUT RIGHT DUCT PRESSURE RAPIDLY FLUCTUATED BETWEEN 20 AND 40 PSI, PER CSDR UALA2011120906764Mirror · missingVIEWING MIRROR FOR DOOR 1RT SLIDE PRESSURE ON AFT SIDE OF BUSTLE IS COMPLETELY MISSING. SLIDE PRESSURE GAUGE IS STILL VIEWABLE, PRESSURE CHECKS OK. NEEDS NEW VIEW PORT DOOR ASSEMBLY. REPLACED, OPS CHECKED GOOD.SDR UALA2011120906765Wire · chafedLT ENG BLD OVERHEAT ON DURING TAXI. NEED TO REPLACE M859 LT BLEED AIR CONT CARD FOR LT BLEED OVERHEAT LIGHT AND EICAS MESSAGE. REPLACED M859 CARD PER MM. ACCOMPLISHED ENGINE RUN, NO HELP. LEFT OVERHEAT LIGHT STILL ON. FOUND WIRE W376-046-18 CHAFING AGAINSSDR UALA2011120906768Heat Exchanger · faultyRIGHT IDG VALVE STATUS MESSAGE DISPLAYED AT TOP OF DESCENT. PERFORMED BPCU BITE CHECK PER FIM 24-20-00. LAST FLT LEG NR 2 SHOWS COOLER VALVE WIRING FAULT. REPLACED NR 2 ENGINE IDG AIR OIL HEAT EXCHANGER AND VALVE PER MM.SDR UALA2011120906774Actuator · leakingRUDDER RATIO CHANGER ACTUATOR LEAKING. REPLACED RUDDER RATIO CHANGER ACTUATOR. INSTALLED RRCA FAILED TEST. REINSTALLED ORIGINAL RUDDER RATIO CHANGER ACTUATOR PER MM. OPS CHECKED GOOD, NO FAULTS.SDR UALA2011120806748Valve · faultyRIGHT DUCT PSI FLUCTUATES +-25 PSI ON CLIMB & DESCENT. ACCOMPLISHED AIR SUPPLY BITE MODULE PROC PER MM. RIGHT PRV FAULT INDICATED. REPLACED NR 2 ENG PRV PER MM & ACCOMPLISHED GRD RUN PER JRH, ALL OPS & INDS NOW NORMAL. AIR SUPPLY MODULE BITE PROC.SDR UALA2011120806750Transmitter · erraticIN CRUISE AT FL 360 WITH EPRS, N1 AND N2 BASICALLY MATCHED, NR 2 FF SHOWS ANYWHERE FROM 400 TO 1200#S HIGHER BURN THAN LEFT ENGINE. FF IS VERY ERRATIC ON RT ENGINE, BUT SEEMS TO BE VALIDATED BY THE HIGHER BURNOUT FROM THE RIGHT MAIN TANK. RT ENGINE FUEL FLOWSDR UALA2011120806751Warning Message · false activationSTAB TRIM EICAS MESSAGE ON CLIMBOUT. APPEARS TO WORK NORMALLY. NO EICAS MESSAGE PRESENT ON ARRIVAL CHECKED BOTH STAB TRIM AND AILERON LOCKOUT MODULES FOR FAULT BALLS. NONE PRESENT.SDR UALA2011120706725Floorbeam · damagedFLOORBEAM AT BS 654.121 LBL 54 TO 88 HAS DRILL BIT PILOT HOLES PART WAY INTO UPPER CHORD SURFACE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED FLANGE & FABRICATED REPAIR PARTS IAW B767 SRM 53-00-51. INSTALLED PARTS ON FLOORBEAM AT BS 654 LBL 54 TO LBL 88. NDSDR UALA2011120606699Ratio Changer · leakingLEFT SYSTEM HYDRAULIC QUANTITY DROPPED TO 0.47 OVERNIGHT. HYDRAULIC FLUID EVIDENT BELOW REAR OF AIRCRAFT. FOUND LEAK FROM RUDDER RATIO CHANGER. REPLACED RUDDER CHANGER AS PER MM AND PERFORMED LEAK CHECK ALL OK. RUDDER RATIO CHANGER IS A BRITISH AIRWAY 7 DASDR UALA2011120606701Line · leakingNR 2 ENGINE TCC ACTUATOR PRESSURE HARD LINE REF IPC 75-32-00-002 ITEM 1 AND MANIFOLD OIL COOLER INLET RETURN HARD LINE REF IPC 75-32-00-002 ITEM 70 BOTH CHAFING THROUGH AT CLAMPS AND PRESSURE LINE LEAKING FUEL. REPLACED BOTH LINES REF STATED IPC (PCN 280-4075SDR UALA2011120606720Controller · faultyAFT CABIN TEMP EICAS MESSAGE WITH INOP LIGHT ON. RESET ZONE TEMP CONTROLLER - NO HELP. CW MEL. REPLACED ZONE TEMP CONTROLLER PER MM, OPS CHECK GOOD. NO EICAS MESSAGES OR FAULTS.SDR UALA2011120506650Intercostal · crackedCABIN FLOOR STA 334, LBL 40 INTERCOSTAL CRACKED. MAJOR REPAIR ACCOMPLISHED. FABBED AND REPLACED INTERCOSTAL PER SRM.SDR UALA2011120506651Floorbeam · corrodedCORROSION IN VARIOUS LOCATIONS ON FLOORBEAM AND T-CAP STA 287, FROM BL 0. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM, ANGLES AND STRAPS PER SRM ON PEMCO NR 3363N00555.SDR HALA2011120200560Blades · damagedETOPS SIGNIFICANT SYS - NR 2 ENGINE FAN BLADE 21 HAS A NICK IN AREA A. MARKED .030 DEPTH. BLENDED FAN BLADE IAW AMM 72-31-02. PERFORMED EDDY CURRENT, IAW AMM 72-31-02. NO TROUBLE FOUND.SDR HALA2011120200561Blades · damagedETOPS SIGNIFICANT SYS - NR 2 ENGINE FAN BLADE NR 23 HAS A NICK IN AREA A. MARKED .030 DEPTH. BLENDED FAN BLADE IAW AMM 72-31-02. PERFORMED EDDY CURRENT IAW AMM 72-31-02. NO TROUBLE FOUND.SDR HALA2011120200562Blade · damagedETOPS SIGNIFICANT SYSTEM - NR 2 ENGINE FAN BLADE NR 29 HAS A NICK IN AREA A. MARKED .030 DEPTH. BLENDED FAN BLADE IAW AMM 72-31-02. PERFORMED EDDY CURRENT IAW AMM 72-31-02, NO TROUBLE FOUND.
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