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 UALA2010111204190Relay · faultyON POWER UP - EICAS MESSAGES EQUIPMENT COOLING AFT FAN - CARGO FIRE DET FAN - BATTERY CHARGER AND HYD QTY DISPLAYED - NO HYD QTY INDICATIONS. ACCOMPLISHED WIRING CHECKS PER WD 24-51-52 PG1A SHT 1 FOUND NO POWER ON K102 PIN A2 WHEN APU OR EXTERNAL CONNECTED ANSDR HALA2010111000529Unknown · unknownETOPS SIGNIFICANT SYS - ON ENG SHUTDOWN, APU DUCT PRESSURE ZERO WITH APU ON. T/S IAW FIM 36-10-00, FIG 117. STARTED APU. DUCT PRESSURE AT 35 PSI. RAN BOTH PACKS. CHECKS OK. MOTORED ENGINE. CHECKS OK. CYCLED APU AIR SUPPLY VALVE SWITCH. VALVE GOES TO COMMANDESDR HALA2010111000533Iru · faultedETOPS SIGNIFICANT SYS - AFTER LANDING "L IRS FAULT" MESSAGE. REPLACED NR1 IRU IAW MM 34-21-01. GND CK OK. PERFORMED MCDP TEST 30. NO FAULTS NOTED. TEST PASSED. ACFT LMP STATUS REMAINS IN LAND 3.SDR HALA2010110900525Connector · dirtyETOPS SIGNIFICANT SYS - INTEREMITTENT STATUS MSG R ENG FIRE LP2. CLEANED CONNECTOR PINS ON ENG FIRE LP2 CONTROL CARD M684 TS IAW FIM 26-1100/101, FIG 106, SYS NOW CHECKS OK. NO FAULTS FOUND.SDR HALA2010110800528Computer · malfunctionedETOPS SIGNIFICANT SYS - TCAS FAIL MESSAGE ON HSI INTERMITTENT. RERACKED TCAS COMP IAW MM34-45-01 GROUND CHECKED OK.SDR CA101110010Latch · failed(CAN) LT THRUST REVERSER COWL BAND LATCH FOUND BROKEN AT THE LOWER LATCH POSITION IPC 78-31-05 ITEM 127.SDR HALA2010110500518Shutoff Valve · failedETOPS SIGNIFICANT SYS - ATO - RT PACK OFF WITH RT ENG BLEED ON ICAS WHEN PWR ADVANCE FOR TAKE-OFF AT 80 KTS. ACCOMP FIM 36-10-00. REPLACED RT BLD AIR CTL CARD (M860). GRND OPS CK PEND. REPLACED RT PACK FLOW CNTL & SHUTOFF VLV IAW AMM 21-51-01. HIGH PWR RAN ENSDR HALA2010110500519Fan Blade · damagedETOPS SIGNIFICANT SYS - NR1 ENGINE 1ST STAGE FAN BLADES NR5, NR10, NR24, NR27,AND NR30 HAVE NICKS, ALL 5 FAN BLADES NICK IN AREA A. BLENDED BLADES IAW AMM 72-31-02 PERFORMED FPI IAW AMM 70-11-06/201 NO CRACKS INDICATED. BLADES THAT WERE BLENDED NR 5,10,24,27 SDR HALA2010110500520Stator · damagedETOPS SIGNIFICANT SYS - _RT ENGINE NR7 AIRFOIL HAS NICK IN AREA A, TIP. BLENDED NR7 AIRFOIL IAW AMM 72-31-02-308 PERFORMED FPI IAW AMM 70-11-06/201, NO CRACK INDICATION.SDR HALA2010110500521Stator · damagedETOPS SIGNIFICANT SYS - NR20 AIRFOIL ON RT ENGINE HAS NICK IN AREA F. BLENDED NR7 AIRFOIL IAW AMM 72-31-02-308. PERFORMED FPI IAW AMM 70-11-06/201 NO CRACK INDICATION.SDR UALA2010110504104Actuator · leakingLT WING AFT OF PYLON SAIL TAIL AREA HAS EVIDENCE OF HYD LEAK. LEAK IS AT LT INBD AILERON INBD ACTUATOR ON ACT ROD SEAL. LEAK IS MEASURED AT 4 DROPS PER MIN. COMPLETED ACTUATOR REPLACEMENT.SDR HALA2010110200509Oil System · leakingETOPS SIGNIFICANT SYS - LWR EICAS MSG -"APU OIL QTY". CHECKED APU OIL QTY. FOUND LOW. PERFORMED APU LEAK CHECK, FOUND APU GENERATOR CASE CRACKED. R & R GENERATOR IAW AMM 24-21-01-424-002. SERVICED APU OIL AS REQUIRED. PERFORMED APU LEAK CHECK IAW AMM 49-21-0SDR HALA2010110200510Element · malfunctionedETOPS SIGNIFICANT SYS - "BODY DUCT LEAK" LIGHT ILLUM EICAS MSG "BODY DUCT LEAK DISPLAYED", LIGHT DID NOT EXTINGUISH AFTER ISOLATION VALVE CLOSED. REPLACED DUCT LEAK DETECTOR ELEMENT TS225, IAW AMM 26-18-01. BODY DUCT LEAK DETECTION BITE CHECK GOOD IAW FIM 26-SDR UALA2010110104040Actuator · bypassingOPERATED HYD & TURNED CONTROL WHEEL LEFT, CAN FEEL SHUTTER, VIBRATION IN COCKPIT AIRFRAME, CONTROL WHEEL & FROM INBD AILERON TO OTBD AILERON WHILE IT STILL HELD IN LT TURN. ISOLATED TO CTR HYD SYS. NO VIB IN RT & LT HYD SYS ON. RT WING AILERON OK NO VIBS. ISDR HALA2010103100507Generator · crackedETOPS SIGNIFICANT SYS - DURING OVERNIGHT CK NOTICED EVIDENCE OF OIL LEAK AT APU. RAN APU. FOUND OIL SPURTING FROM CRACK ON GENERATOR HOUSING. REPLACED APU GENERATOR IAW AMM 24-21-01. OPS NML. LEAK CK GOOD.SDR HALA2010102900508Structure · dentedOPEN - DURING OVERNIGHT CHECK FOUND RT MLG TRUNNION DOOR DENTED LOWER EDGE (DOOR REMOVED). OK TO CONTINUE IAW L CDL32-12-1.SDR HALA2010102800503Bleed Air Sys · malfunctionedETOPS SIGNIFICANT SYS - IAW FLT CREW COMMENTED APU AIR LOW DURING ENG START. PERFORMED ENG START IAW AMM 71-00-00, APU AIR IS ADEQUATE SYS OPS NORMAL.SDR UALA2010102804000Engine · cokedNR1 ENGINE HAS COAKING ON VSV AND COMPRESSOR CASE. REPLACED ENGINE.SDR UALA2010102904015Wire · brokenSMALL PART CAME OFF ABOVE SEAT 6H. FOUND SEAT 6H AFT EMERGENCY LIGHT ON SIDE OF SEAT WIRES BROKEN. TAPED WIRES, TAPED LIGHT STRIP TO SEAT. ALL OTHER EMERGENCY LIGHTS CHECK OK.SDR HALA2010102700492Blade · nickedETOPS SIGNIFICANT SYS - DURING 11K CK RT ENGINE EXTERNAL INSP, FOUND NR 2 ENGINE BLADE NR26 L/E NICKED AREA C. BLENDED OUT DAMAGE TO A DEPTH OF .160 BLADE NR26, NR 2 ENGINE AREA C L/E, NEEDS EDDY CURRENT PRIOR TO 121 HOURS OF OPERATION. REF AMM 72-31-02-308-00SDR HALA2010102700493Wire · brokenETOPS SIGNIFICANT SYS - DURING NR 2 ENG EXTERNAL INSP FOUND NR 3 TERMINAL WIRING BROKEN ON HPSOV. REPAIRED WIRING IAW AMM 70-24-05 HPSOV OPS CHECK NORMAL, OK FOR SERVICE.SDR UALA2010102803999Cable · faultedRT HF RADIO FREQUENCY FAULTY. ANYTIME RT HF RADIO FRQ TUNED WILL CAUSE OVERSPEED MSG ON EADI AND AUTOTHROTTLE BACK TO IDLE, PER CREW. PER CREW, GOT MESSAGE AND THROTTLES WENT TO IDLE, BUT AUTOTHROTTLE DID NOT DISENGAGE. NO PROBLEM USING LEFT HF. FOUND OPESDR UALA2010102904022Battery Pack · inoperativeEMERGENCY EXIT OVERHEAD LIGHT OUT ROW 32-39 LT SIDE. REPLACED BATTERY PACK, OPS CHECKS GOOD.SDR UALA2010102904014Damper · faultyRT YAW DAMPER INOPERATIVE. ACCOMPLISHED YAW DAMPER SYS BITE. SYS TESTED NORMAL. STORED FLIGHT LEG FAULTS IN RT YAW DAMPER MODULE FAULTING RT YAW DAMPER ACTUATOR. LT YAW DAMPER MODULE HAS NO FAULTS.SDR HALA2010102600495A/C Pack · malfunctionedETOPS SIGNIFICANT SYS - BOTH LT & RT PACK SWITCHES HAD TO BE TURNED OFF THEN BACK ON MORE THAN ONCE TO GET THE PACK OFF LIGHTS TO EXTINGUISH (EICAS MESSAGE WAS THE SAME THEY FOLLOWED THE PACK OFF LIGHTS. ACCOMPLISHED BITE LT & RT PACK TEMP CONTROLLER & AIR SUSDR HALA2010102600496Control Valve · malfunctionedETOPS SIGNIFICANT SYS - BOTH PNEUMATIC PRESS DROPS EXCESSIVE WHEN LT & RT PACK SWITCHES ARE TURNED OFF USING BOTH APU OR ENG BLEED AIR (BLEED AIR DOES NOT RETURN TO NORMAL) REPLACED LT FLOW CONTROL VALVE IAW AMM21-51-01 TILL STEP 4A. OPS CK IAW AMM21-51-01 OSDR HALA2010102600500Housing · brokenETOPS SIGNIFICANT SYS - NR 2 IDG CHIP DETECTOR HOUSING BROKEN. REPLACED NR2 IDG CHIP DETECTOR HSG & CHIP DETECTOR.SDR UALA2010102803966Lens · missingEMERGENCY LIGHT LENS MISSING AT SEAT 8A. REPLACED LENS. OPS NORMAL.SDR UALA2010102503955Idg · faultyLOAD SHED ISSUES. DUE TO REPORT OF RT HYD QTY INDICATION DROP TWO TIMES AND FWD AND RT AFT GALLEY POWER WENT OFF NEED TO PERFORM A VISUAL INSPECTION OF RT GEN BREAKER TERMINALS (3 PHASE) C903. REPLACED RELAY & REPLACED NR 2 ENG IDG PER MM.SDR UALA2010102503953Acm · inoperativeFOUND RT ACM INOPERATIVE. TEMP INSTALLED NEW RT ACM. REPLACED ACM PER MM. OPS CHECKED GOOD.SDR UALA2010102503922Panel · looseLOUD BANG IN CABIN, RTFL. PER MM AND CG SUPERVISOR CANS FOUND NOT SECURE IN FWD CARGO PIT CAUSING "BANG". DUE TO VIBRATION HISTORY REMOVED CARGO CEILING AND SIDEWALL PANELS LOCATED UNDERNEATH SEATS 2K AND 6K. NO DEFECTS NOTED. FOUND LARGE PANEL LOCATED BEHIND SDR UALA2010102503927Controller · faultyRT PACK INOP LT WITH EICAS R PACK TEMP. REPLACED RT PACK TEMP CONTROLLER.SDR HALA2010102300489Slide · unwanted deployON CHECK FOUND R-1 DOOR HALFWAY OPEN WITH LEVER IN ARM POSITION. TRIED TO INSTALL SLIDE RAFT BUT WE FOUND OUT THAT THE SLIDE RAFT COVER SNAPPED OUT. RELEASED IAW MEL 52-11-4 TRANSCRIBED TO MIC SHEET. INSTALLED 1R DOOR SLIDE IAW 767-3-205003, TASK CARD CLEARESDR UALA2010102203903Gcu · faultyBPCU FAULT APU GCU. REPLACED APU GCU, NO HELP. REPLACED APU GCU, NO HELP. WHEN LT GEN SELECTED APU GEN OFF LT ILLUM AND WOULD NOT COME BACK ON LINE. FREQS AND VOLTS GOOD. CYCLED CB FOR APU GEN CONT, NO HELP. REPLACED NR 1 ENG IDG AND BPCU. ALL AUTOMATIC SWISDR UALA2010102503930Priority Valve · faultyLT ENG PRV EICAS MSG PRIOR TO ENG SHUTDOWN. REPLACED PRV IAW MM, ACCOMPLISHED ENGINE RUN ALL. OPS AND INDICATION NORMAL.SDR UALA2010102503944Sensor · faultyLEFT WING SLIDE EICAS OCCASIONALLY ILLUMINATES INFLIGHT. FOUND S218 SENSOR FAULTED ON PSEU.SDR UALA2010102103889Lens · brokenSEAT 37J, EMERGENCY LIGHT LENS BROKEN. REPLACED BROKEN EMERGENCY LIGHT LENS SEAT 37J.SDR UALA2010102203902Gcu · faultyLT ENG GEN DID NOT COME ONLINE AUTOMATICALLY AFTER ENG START. HAD TO MANUALLY SELECT GEN ON. REPLACED GCU & BPU FOR NR1 ENG. OPS NORMAL.SDR UALA2010102103896Pressure Switch · faultedLEFT FWD BOOST PUMP LOW PRESSURE LIGHT INOPERATIVE. CLEANED CONNECTOR AND BLEED PRESSURE SWITCH LINE, NO HELP. DEFERRED PUMP INOPERATIVE. REPLACED LT FWD FUEL BOOST PUMP PRESSURE SWITCH (S70) IAW MM. CHECKED GOOD, NO LEAKS.SDR UALA2010102103899Controller · malfunctionedRT ENG BLEED PROBLEM. REPLACED NR2 ENG PRV. REPLACED NR2 ENG PRVC. REPLACED NR2 ENG BLEED AIR CONTROL CARD. REPLACED RT ENG OVERPRESSURE SWITCH, NO HELP. CHECKED AND FOUND FAULT WIRE, PRC ON AIR SUPPLY BITE CHECK. REPLACED CONTROLLER HP VALVE MR36157, CONTROSDR UALA2010102103895Actuator · leakingAFTER ARRIVAL FOUND LT ENGINE FUEL LEAK FROM DRAIN TUBE NR5, VARIABLE STATOR VANE ACTUATOR. PERFORMED ENG RUN UP IAW AMM. LEAK WITHIN LIMIT IAW AMM. REPLACE THE VSV ACTUATOR NOT MORE THEN 50 F HOURS. INSPECT THE LEAK BEFORE EACH DEPARTURE. TO PREVENT IRREG SDR UALA2010101903865Drain Valve · leakingRIGHT TANK FUEL SUMP HAS FUEL SEEP AT OUTER CIRCUMFERENCE. REPLACED RT TANK SUMP DRAIN VALVE. OPS NORMAL.SDR UALA2010101803857Light · inoperativeEMERGENCY LIGHT INOP ON SEAT 1B FWD. R & R EMERGENCY LIGHT ASSY, CHECKED NORMAL ON GROUND.SDR HALA2010101800473Outflow Valve · malfunctionedAIR TURN BACK - DUE TO CABIN AUTO INOP, UPON ARRIVAL MODE SELECTOR ON MAN. POSITION. PERFORMED FIM 21-31-00 MANUAL MODE CTRL TEST-CABIN IAW AMM TASK 21-31-00-705-071, MESSAGE CLEARED, OK FOR FLIGHT. CHECKED OUTFLOW VALVE FOR OBSTRUCTION FOUND NORMAL, IAW AMMSDR HALA2010101800474Slide · unwanted deploy4L DOOR SLIDE DEPLOYED. REPLACED 4L DOOR SLIDE IAW CARD NR 767-3-205003.SDR UALA2010101903868Battery Pack · faultyEMERGENCY EVACUATION LIGHTS COME ON WHEN POWER IS REMOVED FROM AIRCRAFT AFT FIRST CLASS OVERHEAD AISLES AND EXTERIOR AT FWD AND OVERWING DOORS. REPLACED THE BATTERY PACKS PER TASK CARD 2300R284. OPS CHECKED GOOD.SDR HALA2010101700470Eadi · malfunctionedETOPS SIGNIFICANT SYS - CAPT ADI DISPLAY FLICKERS INTERMITTENTLY. SELECT EFI SWITCH TO ALTERNATE DOES NOT HELP. R & R CAPT EADI IAW AMM 34-22-03, OPS, CHECKS GOOD.SDR UALA2010101803849Gearbox · fodON FLAP EXTENSION SELECTED FLAPS 5 AND FLAPS EXTENDED TO 15 WITH HANDLE IN 5 DETENT. OPERATED IN ALT TO FLAPS 20 FOR LANDING. OPENED COVERS AT CONTROL STAND FOR FLAP CONTROL LEVER AND REMOVED 2 PIECES OF PLASTIC TY RAPS AND 1 TRIM SCREW THAT WAS INTERFERING WSDR HALA2010101600471Blade · damagedETOPS SIGNIFICANT SYS - DURING RT ENG INSP FOUND NICK IN L/E OF FAN BLADE 16" FROM ROOT BLADE NR15 MARKED. FOUND NICK TO BE IN AREA C AND BLENDED AREA 16" FROM ROOT TO .30"X1". IAW AMM 72-31-02-308-003-N00. REF LOG 368278 ITEM 62FOR EDDY CURRENT DMI VISUAL INSDR UALA2010101803838Connector · inoperativeEMERGENCY LIGHTS ON SEATS 19AB THRU 24B ARE INOP. SECURED BATTERY CONNECTOR. CHECKS GOOD.
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