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 UALA2011080804134Cable · inoperativeSEAT MOUNTED EEL INOP AT 30JK. REPLACED SEAT CABLE, OPS CHECK OK.SDR UALA2011080804146Control Quadrant · dirtyCREW ACCOMPLISHING CONTROL CHECK CONTROL WHEEL BINDS WHEN TURNING TO THE LEFT AT APROX 4 UNITS. ACP AILERON CONTROL CHECK PER MM. ALSO CLEANED AND LUBED RIGHT AND LEFT LCCA QUADRANT. OPERATED SEVERAL TIMES, OP CHECKS OKAY.SDR UALA2011080804122Pump · faultyGEAR VERY SLOW TO RETRACT. BOTH CENTR ELEC PUMPS LOW PRESS ILLUM AND GEAR DISAGREE EICAS. FOUND DURING TROUBLESHOOT ADP PER FIM 29-11-00 FIG 109 ADP AUTO FUNCTION INOP. DEFERRED PER MEL. ADP MANUAL FUNCTION CHECKED GOOD. 06AUG IAD INF- :REPLACED OVERSPEEDSDR UALA2011080404063Cdu · malfunctionedF/O FMC CDU BLANK RTFL, HAPPENED ON PREFLIGHT AND RESET CB E29. CDU WORKED OK UNTIL NOW. REPLACED F/O'S FMC CDU IAW MM 34-61-02. OPS CHECK NORMAL.SDR UALA2011080504085Nozzle · obstructedFIRE EXT NOZZLE PARTIALLY COVERED WITH PIT TAPE. AFT NOZZLE IN AFT PIT. TAPE PARTIALLY BLOCKING NOZZLE TRIMMED PER MM, OTHER NOZZLES CHECKED IN FWD, AFT & BULK PITS. ALL OKAY.SDR UALA2011080504086Nozzle · obstructedFWD SIDEWALL FIRE EXT NOZZLE PARTIALLY COVERED WITH PIT TAPE. REMOVED TAPE COVERING NOZZLE AND RETAPED.SDR UALA2011080504087Nozzle · obstructedBULK PIT CEILING FIRE EXT NOZZLE NEEDS RETAPING DUE PARTIALLY BLOCKING NOZZLE. REMOVED DAMAGED TAPE AND RETAPED.SDR UALA2011080804117Valve · faultyL ENG PRV EICAS. SAMC TEXT: ON LT ENG START WENT OUT THEN BACK ON, ON RT ENG START. REPLACED PRV ON NR 1 ENG.SDR UALA2011080304041Switch · faultySTANDBY POWER SWT ON OVERHEAD PANEL DOES NOT HAVE DETENT FROM AUTO TO OFF. INSTALLED SWITCH, TESTED STNDBY PANEL ACCORDING TO AMM. SWITCH PCN (586-2220) PN 3600-5478. NO TAG ATTACHED ACCORDING SAMC.SDR UALA2011080304059Idg · failedELEC GEN DRIVE R RIGHT IDG FAULT (LOW INTERNAL OIL PRESSURE). REPLACED IDG PER MM AND ALSO REPLACED IDG DRIVE SEAL.SDR UALA2011080404074Windshield Wiper · defectiveF/O WINDSHIELD WIPER WON'T STOP. ALSO THE CAPT'S OUTER PORTION OF WINDSHIELD WIPER DOES NOT CLEAN RAIN FROM WINDOW. REPLACED F/O WIPER ARM ASSY IAW MM. REPLACED CAPT'S WIPER BLADE. OPS CHECK NORMAL.SDR UALA2011080304050Autothrottle Sys · malfunctionedAUTOTHROTTLE FAIL AT STATUS ON ADI IS BLANK. TMC APPEARS OK. LEG FAULT A-T DISC TMC 01310800 AND TEST FAILURE OF MCDP-TMC. REPLACED TMC. AUTOLAND TEST 02, 30, 40 PASSED.SDR UALA2011080304013Fairing · missingDURING RAMP CHECK FOUND PANEL MISSING ON AFT TOP OF RIGHT LANDING GEAR BODY DOOR AREA. ACCOMPLISH REPAIRS PER EVA 81169. RT WING MLG SIDE STRUT SWIVEL FAIRING ASSEMBLY TEMPORARY FAIRING INSTALLED AS PER EVA-8 1169. VERIFICATION REQUIRED BEFORE EACH FLIGHT SDR UALA2011080304053Relay · failedCAPT SIDE PRIMARY FLIGHT INSTRUMENTS ALL BLANK. REPLACED RELAY K862. CAPT'S EFIS OP CHECKED NORMAL.SDR UALA2011080304052Heat Shield · failedNR 2 ENG OIL TANK HEAT SHIELD HAS DETERIORATED. REPLACED HEAT SHIELD.SDR UALA2011080103961Monitor · defectiveHYDRAULIC QUANTITY MONITOR UNIT NEEDS REPLACEMENT. REPLACED HYD QTY MONITOR.SDR UALA2011080103965Warning System · activatedL ENG HPSOV EICAS & BLEED LT AFTER ENG START.SDR UALA2011080103925Idg · failedPER INBOUND CREW, LEFT BUSS TRIPPED ON THROTTLE ADVANCE DURING T/O. RESET AS REQUIRED. ITEM HAS HISTORY. DUE HISTORY OF THIS FAULT, THIS ITEM IS GENERALLY CAUSED BY A DEFECTIVE IDG. SUSPECT IDG INSTALLED BY PREVIOUS STATION FOR ANOTHER TYPE FAULT, NEEDS RPSDR UALA2011080204004Idg · defectiveRT IDG RED DIFFERENTIAL PRESSURE INDICATOR POP. REPLACED IDG WITH NEW ONE, LEAK CHECKED AND OPS CHECKED NORMAL.SDR UALA2011080204005Idg · failedCREW REPORT: JUST PRIOR TO TAKING RUNWAY L AC BUS FAILED. ACP TROUBLESHOOTING PER TABLE 102 REF MM P163 FOR DP TRIP AND MAIN BUS-OVERLAP. ALL WIRE CHECKS SAT. CREW ALSO REPORTED THE LEFT GENERATOR CONTROL TRIPPED AND THE LEFT TIE BUS ALSO FAILED. BOTH THESDR UALA2011080103977B-Nut · leakingFLAP SLAT HYDRAULIC SHUTOFF VALVE IN RT MAIN GEAR WHEEL WELL LEAKING 20 DROPS PER MINUTE FROM PRESSURE PORT B-NUT. ACCOMPLISHED RINGLOCK REPAIR TO PRESSURE PORT END OF TUBE PER GNMM. LEAK CHECK OKAY.SDR UALA2011080103982Actuator · leakingRAMP REPORTED FLUID LEAK NR 2 ENGINE. FOUND NR 2 ENGINE INBOARD UPPER REVERSER ACTUATOR LEAKING 5 DROPS PER MINUTE.SDR UALA2011080103978Battery · failedAPU WILL NOT CRANK. REPLACED BATTERY PER MM, OPS CHECKED NORMAL.SDR UALA2011080103924Idg · disconnectedLEFT GENERATOR DRIVE EICAS & DRIVE LIGHT ON DRIVE DISCONNECTED. REPLACED NR 1 ENGINE IDG, OPS CHECKED NORMAL.SDR UALA2011080103922Battery Pack · faultyEXIT SIGN DOOR 1R AS WELL AS FLOOR LIGHTING STRIP BY SAME DOOR ARE FLASHING ON AND OFF. REPLACED POWER SUPPLY BATTERY PACK M1552, OPS CHECKED OKAY.SDR UALA2011080103923Ignition Sys · failedAPU WILL NOT START. REPLACED IGNITION UNIT.SDR UALA2011072903916Pump · malfunctionedRIGHT CENTER TANK FUEL PUMP INOPERATIVE AND DEACTIVATED. CIRCUIT BREAKER POPPED ON P-6 PANEL. RAN NR 2 ENGINE FOR 5 MIN, OPS CHECKED RIGHT CENTER TANK FUEL PUMP. NO CIRCUIT BREAKER POP, CENTER TANK FUEL PUMP CHECKED NORMAL PER JRH.SDR UALA2011072903903Battery · faultedA CABIN APPEARANCE TEAM FOUND DURING AN INTERIOR SWEEP 2 EMERGENCY EXIT LIGHTS INOP AT DOORS 2L AND R. REPLACED BATTERY AND CHARGER ASSY PER MM, LAMPS OP NORMAL.SDR UALA2011072803881Duct · crackedFOUND RT PACK INBOARD LWR DUCT BETWEEN REHEATER AND HEAT EXCHANGER CRACKED. RIGHT PACK OUTPUT TEMP 58 DEG WILL NOT GO COLDER TEMP VALVE SHOWS 0.00 POSITION DCT PRSS 31. REPLACED DAMAGED DUCT ASSY.SDR UALA2011072703855Warning Light · illuminatedLEFT HYD QTY INDICATION.SDR UALA2011072803894Actuator · leakingNR 1 ENG VSV ACT HAS HISTORY OF FLUID LEAKS. NEED TO REPLACE THE VSV. REPLACED PER MM.SDR UALA2011072703838Transmitter · failedLEFT HYD QTY INDICATION. REPLACED LT HYD QTY TRANSMITTER AMM 29-33-02. R AND E WORKING SIGNAL WIRE OF PTU. AFTER TRANSMITTER WAS REPLACED FOUND DIODE BLOCK R397 WITH BRUNDY TERMINAL JAMMED IN POSITION "C". WIRE TO POSITION "C" WAS BROKEN OFF AND TIED BACK. SDR UALA2011072703839Lamp · inoperativeFWD MED EXTERNAL SLIDE LIGHT INOPERATIVE. RELAMPED (767) AND OP CKD GOOD.SDR UALA2011072703840Battery Pack · inoperativeENERGENCY LIGHT STRIP AT CTR RT LAV AND EXIT IDENTIFIERS AT RT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK PER MM, OP CHECKED NORMAL.SDR UALA2011072703841Lamp · inoperativeTWI REAR RIGHT OVERWING EMERGENCY SLIDE LIGHTS INOPERATIVE. RELAMPED, OP CHECKED GOOD.SDR UALA2011072703837Slat System · malfunctionedEICAS MESSAGE LE SLAT DISAGREE DISPLAYED, LEADING EDGE LIGHT ILLUM WITH THE FLAP LEVER IN 1. BOTH FLAP POINTERS ARE CORRECT. NO EICAS MESSAGE OR L/E LIGHT UPON GATE ARRIVAL, L/E FLAP SYSTEM T/S IAW AMM, PSEU TARGETS NO FAULT, FSEU NO FAULTS, FLAPS CYCLED SEVSDR UALA2011072703869Fseu · malfunctionedEICAS MESSAGE FLAP SLAT ELEC. FIM PERFORMED WITHOUT SUCCESS. SEVERAL RESET PERFORMED. NOT OK. FSEU RERACK NOT OK. BITE TEST SHOWS M545 AMBER LIGHT. FLAP SLAT ELEC FULLY DEPLOYED AND RETRACTED OKAY. EICAS MSG NOT RESETABLE. FSEU REPLACED AS PER AMM.SDR UALA2011072703875Indicator · failedDURING FUELING LOST POWER TO UNDER WING FUEL STATION. AFTER RESET RIGHT TANK GAUGE FAULTED. DEFERRED RIGHT TANK UNDERWING FUEL GAUGE INOP PER MEL 2841G. REPLACED RIGHT UNDER WING GAUGE.SDR UALA2011072503813Check Valve · surgesSILENT SURGE. REPLACE IP CHECK VALVE BEFORE FURTHER FLIGHT DUE TO PREVIOUS REPORT OF A SILENT SURGE. REPLACED IP CHECK VALVE PER MM. NO LEAKS NOTED.SDR UALA2011072503787Module · malfunctionedSTABILIZER TRIM EICAS WITH ASSOCIATED TRIM LIGHT ILLUMINATED. ACCOMPLISHED CK OF STABILIZER TRIM SYSTEM AND FOUND LEFT CHANNEL FAULT. LEFT SAM SHOWED STCM AND PRESS SWITCH FAULTS. RESET BOTH SAMS, NO HELP. ALSO REPLACED LEFT SAM NO HELP. LEFT NEW UNIT INSSDR UALA2011072503788Pressure Switch · faultedRIGHT AUTOPILOT INOP DUE TO RIGHT STABILIZER TRIM CHANNEL FAULT. REPLACED PRESSURE SWITCH ON RT STCM.SDR CA110725002Compressor · failed(CAN) CREW REPORT A FOUL ODOR EMANATING THROUGH CABIN ON CLIMB, ODOR DISSIPATED IN CRUISE. ON DESCENT/APPROACH, A TOXIC SMELL PERMEATED THROUGHOUT CABIN. SOME CREW MEMBERS WERE REPORTING SORE THROAT ASSOCIATED WITH THE TOXIC ODOR AND WANTED TO USE OXYGEN MASSDR UALA2011072503769Valve · stuckONE TRIM AIR VALVE APPEARS STUCK. AUX FWD VALVE STUCK OPEN, DEFFERED PER MEL PROCEDURE 2. REPLACED TRIM AIR VALVE. OPS NORMAL.SDR UALA2011072503802Detector · faulted"FWD CARGO DET 2" STATUS MESSAGE. WILL NOT CLEAR. COMPLIED WITH MEL. REPLACED DETECTOR PER MM.SDR UALA2011072203733Aileron Sys · bindingCREW REPORTS DURING THE FLIGHT CONTROL CHECK BOTH CAPT AND F/O FELT BINDING IN THE LEFT AND RIGHT AILERON CONTROL CHECK. AILERON CONTROL BINDING. MM INSPECTED CABLES AND BEARINGS PER MM. LUBED LEFT FEEL AND CTR MECH AND LEFT OUTBOARD AILERON PER MM. DISCONSDR UALA2011071903655Fitting · missingSTRANGE NOISE AROUND ROW 19A. SOUNDS LIKE OBJECT FLAPPING IN WIND STREAM CLOSE TO FUSELAGE. FOUND LEFT AFT OVERWING DOOR STEP CHORD DISCONNECTED, REPLACED MISSING CIRCLIP AND SECURED CHORD TO STEP, ALL CHECKS NORMAL.SDR UALA2011071903667Pressure Switch · faultyL ENG OIL FILTER EICAS, RTFL. ALL OTHER (OIL QTY, OIL PRESS, OIL TEMP AND LOW OIL PRESS) INDICATIONS NORMAL, OIL FILTER LIGHT WENT OUT INITIALLY BUT CAME BACK ON NOW STEADY. SAMC TEXT: L ENG S/N 727897. REF AMM 79-35-00 PG 106 FOR OIL FILTER MESSAGE T-SHOOTISDR UALA2011071903653Pca · out of adjustPLANE NEEDS EXCESSIVE RT RUDDER TRIM, 3.5 UNITS. FFS MATCHED, L-EPR 1.27, R-EPR 1.22. ADJUSTED UPPER, MIDDLE AND LOWER PCA'S PER MM. ACCOMPLISHED INSPECTION OF THREE RUDDER ACTUATOR ADJUSTMENTS FOR SAFETY AND SECURITY, RIGS. ALL CHECKS OKAY.SDR UALA2011071903681O-Ring · leakingNR 4 BEARING MCD OIL LEAKAGE BEYOND ALLOWABLE LIMITS WITH MAG PROBE. REMOVED ON NR 1 ENGINE (APPROX 90 DROPS PER MINUTE, MAX ALLOW 10 DROPS). REPLACED O-RING CHECKS GOOD.SDR UALA2011071903674Window · unserviceableCAPTAIN'S FIXED SIDE-AFT WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS, REPLACE FIRST AVAILABLE. CREW COMMENTS: IN SUN VISIBILITY IS AFFECTED. NR 3 LT WINDOW NEEDS REPLACEMENT. WINDOW REPLACED.
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