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 UALA2009070601914Power Supply · faultyFLOOR MOUNTED EMERGENCY LIGHT FWD OF SEAT 1K INOP. WILL NEED 1K SEAT ASSY MOVED 3 FT AFT OF BULKHEAD TO REPAIR OR REPLACE EMERGENCY LIGHT STRIP. THREE SHIFTS REQUIRED TO ACCESS WIRING. FOUND DOOR 1R AISLE FLOOR LIGHT L901 AND DOOR1 RT LOWER EXIT LIGHT L972SDR UALA2009070101891Module · faultyEICAS MSG STAB TRIM DISPLAYED & STAB TRIM LIGHT ILLUMINATED. STABILIZER TRIM RATE NORMAL. FOUND LT STAB TRIM AIL LOCKOUT MOD FAULT. REPLACED LT SAM. COMPLETED MCDP GRND TEST 65 STAB TRIM AND AIL LOCKOUT TEST, ALL TEST PASS. NO FAULT INDICATIONS.SDR HALA2009070100271Indication Sys · malfunctionedETOPS SIGNIFICANT SYS - BTB L ENG OIL PRESSURE WENT TO ZERO DURING PWR FAILURE AT IDLE. PRESSURE RECOVERED WHEN POWER WAS RESTORED TEMPORARLY. PERFORMED FIM 79-33-00 FIG 105, NO DEFECTS NOTED AND FIM 79-33-00 FIG 104 NO DEFECTS NOTED. ACCOMPLISH ENGINE RUNSDR UALA2009070201899Battery · inoperativeDOOR L1 AND R4 AND LEFT OVERWING SLIDE EMERGENCY LIGHTS INOPERATIVE. DOOR L1 REPLACED BATTERY AND CHECKS GOOD. DOOR R4 CHECKS NORMAL.SDR HALA2009063000268Unknown · warning lightETOPS SIGNIFICANT SYS - FLT 1 DIVERETED TO (ITO) - L ENG OIL FILTER MSG. REMOVED MAIN OIL FILTER ELEMENT, VISUAL CHECK FILTER NO METAL NOTED. REPLACED MAIN OIL FILTER WITH NEW IAW AMM 79-21-05. REPLACED PRESSURE SWITCH, ACCOMPLISHED AUTO EVENT ERASE PROCEDURSDR UALA2009063001882Idg · failedR GEN FAILURE. RTFL. INITIALLY GEN STAYED ON LINE BUT WENT OFF LINE SHORTLY THEREAFTER. IDG WAS THEN DISCONNECTED BY CREW. BPCU HAS MULTIPLE MSGS INCLUDING IDG PMG WIRING, IDG UNDER FREQUENCY, SVC IDG AND IDG HIGH RISE TEMP. REPLACED IDG AND ACCOMPLISHED SDR UALA2009062901846Transceiver · failedNR 1 VHF COMM XMISSION & RECEPTION INOP. REPLACED LT VHF RECEIVER TRANSMITTER, OP CHECKED OKAY.SDR UALA2009062901854Fitting · leakingAPU LEAKING OIL. SERVICED APU WITH 2 QUARTS. LEAK STILL NOT FOUND. RAN APU FOUND T-FITTING 1 O'CLOCK POSITION LEAKING ON FWD SIDE OF GEARBOX. HELICOIL IS STRIPPED OUT. REPLACED APU, RAN APU AND OPS NORMAL.SDR DL76L091091Engine · failedDESENDING THROUGH 22K NOTICED IDG DISCONNECTED AND THEN OIL PRESSURE IN THE RED. N1 AND N2 FAIL BELOW IDLE AND FF WAS LESS THAN 600LBS. TURNED FUEL CUTOFF SWITCH TO OFF. ENGINE SHOWED POSITIVE OIL PRESS THROUGHOUT THE REST OF THE DESCENTAND LANDING. EMERGENCYSDR DL777091090Actuator · malfunctionedRTO/RTB DUE TO MLG STEERING WARNING. FWD TO MCO AND PLAC PER MEL 32-53-01. REPLACED LT MLG STEERING ACTUATOR PER M/M. OPS CK AND LEAK C GOOD. MCO/PLAC REMOVED. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.SDR UALA2009062501797Circuit Board · faultyEQUIP COOLING EICAS AND OVERHEAD. REPLACED EQUIP COOLING INDICATION CIRCUIT BOARD. REMOVED AND CLEANED LOW FLOW SENSORS, HAVE HAD NO FAULTS FOR 1.5 HOURS AT ORD. EQUIP COOLING TEST OKAY.SDR UALA2009062201768Generator · failedL GEN FAILURE. RTFL.SDR UALA2009062201769Idg · failedL GEN FAILURE. RTFL. REPLACED IDG GENERATOR.SDR DL75E091060Gcu · malfunctionedLEFT ENGINE DRIVEN GEN DOES NOT POWER ELECTRICAL SYSTEM AFTER LEFT ENG START APU WAS SHUTDOWN AND ALL ELECTRICAL POWER WAS LOST LT/RT GEN SHOWS GCU ON BPCU. CLEAR BPCU AND RESEAT LT GCU RAN LT AND RT ENG GEN OPS AND INDICATION NORMAL OIL LEVEL NORMAL ON LT IDGSDR UALA2009062201767Probe · faultyL AUX PITOT MESSAGE DISPLAYED AFTER ENGINE START. REPLACED L AUX PITOT PROBE. OP CHECKS OKAY.SDR DL76L091058Circuit Card · failedL ENG SPEED CARD STATUAS MESSAGE. R & R LT ENG SPEED CARD PER AMM. PERFORMED SPEED CARD TESTS.ALL CHECKS NORMAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.SDR UALA2009062301771Controller · failedCABIN CLIMB EXCESS 2000FPM WITH BOTH PACKS OFF. REPLACED CABIN PRESSURE CONTROLLER. OPS CHECKS GOOD. PERFORMED CABIN LEAK CHECK, LEAK CHECKS GOOD.SDR DL76L091054Fmu · malfunctionedNBR 1 ENG SHUTDOWN WHEN THROTTLES WERE ADVANCED FOR TAXI. OPENED LT ENG NO DEFECTS PULLED CHIP DETECTORS ALL CLEAN MOT LT ENG NO PROBLEMS RAN ENG AT IDLE WITH FLIGHT CREW NORMAL START MOVE THROTTLE OFF IDLE NO DEFECTS NOTED RAN ENG T/S P FIM REPLACED FMU ON NSDR UALA2009061701726Pump · faulty'FUEL CONFIG' LIGHT ON WITH 'C' PUMPS ON AND TANK QUANTITIES 40.4-4.1-38.7. ACCOMPLISHED SERVICE TIP. SYSTEM CHECKED GOOD. REPLACED THE RIGHT CENTER OVERRIDE JETTISON PUMP. SYSTEM CHECK FOUND GOOD.SDR UALA2009061601721Coupler · faultyRIGHT HF ISSUE. FLIGHT DIVERTED. REPLACED RIGHT HF COUPLER. SAFTIED ALL CONNECTORS AS REQUIRED. FOUND D4839P AND D4841P LOOSE, MADE WRITE UP. NEED TO ACCOMPLISH OP CK OF LEFT AND RIGHT HF. PERFORMED MM23-11-00 AND MADE CALLS FROM AIRPLANE TO AIRPLANE AND AIRSDR HALA2009061500236Fan Blade · damagedETOPS SIGNIFICANT SYSTEM, RT ENGINE FAN BLADE NR 6 FOUND WITH NICK'S ON THE LEADING EDGE, 2 1/2 INCHES FROM THE TIP. LEADING EDGE AREA "A"-3/16 INCHES BY 1/4 INCHES LONG. PERFORMED BLENDING ON RT ENGINE FAN BLADE NR 6 IAW B7
67 AMM 72-31-02.SDR DL76L091028Oil System · unknownNR 2 ENGINE HIDING OIL. UNABLE TO CURE PROBLEM. REPLACING NR 2 ENGINE. NR 2 E/C PER TRANS 1T149ADSDR UALA2009061501684Oxygen Bottle · low pressureDOOR 2R O2 BOTTLE LOW PRESSURE. REPLACED O2 BOTTLE.SDR UALA2009061501679Acoustic Liner · crackedNR 1 ENGINE ACOUSTIC LINER HAS A 1.25 INCH CRACK LOCATED 0.25 INCH FWD OF THE FAN RUBSTRIP AT THE 10 O'CLOCK POSITION. THE DAMAGED CRACKED AREA IS ALSO DENTED FROM CRACK AFT TO RUBSTRIP JOINT. CRACK MUST BE CHECKED PRIOR TO EACH DEPARTURE AND INLET COWL MUSTSDR UALA2009061501680Slide · faultyINSTALL RT OFF WING SLIDE. REPLACED THE RT OFF WING SLIDE TO COMPLETION.SDR UALA2009061201670Line · leakingEVIDENCE OF HYDRAULIC FLUID LEAK ON RT ENG PYLON AREA. RT HYDRAULIC SYS QTY 0.75 DISPLAYED ON EICAS. FOUND RT EDP PRESSURE LINE DAMAGED ON STRUT AREA. ACCOMPLISHED INTERIM REPAIR. TUBE REPLACED BY FLEXIBLE HOSES. ACPD ENG RUN CHECKED, NO LEAKS. NEED TO RSDR UALA2009061201676Keeper · shearedFOUR (4) LATCH KEEPERS SHEARED FROM RIGHT OVERWING SLIDE DOOR. ALSO HAS 3 BROKEN HINGES. REPLACED RT OVERWING SLIDE DOOR.SDR DL76L091019Engine · hung startRT ENG HUNG START AT 52 PERCENT N2, MAX EGT 487. STARTED ENGINE AT GATE. ALL INDICATIONS NORMAL.SDR UALA2009061001649Panel · damagedRIGHT L/E NR 7 SLAT CLOSURE PANEL HAS DAMAGE. NR 7 LEADING EDGE SLAT REPAIRED BY SFO SHOP ON R&R R42774, REINSTALLED ORIGINAL SLAT WITH NO ADJUSTMENTS DISTURBED DURING REMOVAL OR INSTALL. CHECKED FIT & FAIR AFTER INSTALLATION AND SOLD TO INSPECTION. INSPECTSDR HALA2009061000230Fire Warning · false activationETOPS SIGNIFICANT SYSTEM, CREW CALLED RT ENGINE FIRE LOOP 2 AND RT ENG O/H EICAS MESSAGE OCCURRED AFTER POWER TRANSFER. PERFORMED FIRE WARNING TEST, ALL FIRE WARNING ANNUN LIGHTS ILLUMINATED AND FIRE WARNING MESSAGE SHOWED ON EICAS SCREEN. ENDED FIRE WARNINGSDR HALA2009061000231Start Valve · failedETOPS SIGNIFICANT SYSTEM - RIGHT ENG START VALVE LIGHT CAME ON STAYED ON, NO ENG ROTATION. RT STARTER VALVE EICAS MESSAGE. NO N2 DUCT PRESSURE. REMOVED AND REPLACED NR 2 ENGINE STARTER AND START VALVE PER AMM 80-11-01. OPS AND LEAK CHECK OK. OK FOR SERVICSDR UALA2009060901640Module · failedSTAB TRIM LIGHT AND EICAS DISPLAYED. ABLE TO ISOLATE WITH THE CUTOUT SWITCHES, TO FAIL WITH THE RT STAB-TRIM AILERON MODULE. REPLACED RT STAB TRIM-AILERON LOCKOUT MODULE, CHECKS OKAY.SDR DL76L091012Starter · inoperativeAPU DUCT PRESSURE NORMAL. LEFT ENG N2 SHOWS ZERO DURING START. START VALVE INDICATED OPEN. NO OIL PRESSURE RISE. LEFT ENG STARTER MOTOR REPLACED AND OIL SERVICED IAW M/M. NOW OPS NML.SDR HALA2009060800228Warning Light · false activationETOPS SIGNIFICANT SYSTEM, R FMC FAIL ON L ENG START. PERF FIM 34-61-00 FIG 108A. PERF ENGINE START AT GATE. OPS NORMAL.SDR DL76L091008Line · leakingLEFT ENGINE OIL QTY DROPPING, PRESS AND TEMP GOOD DIVERTED TO LHR. LANDING UNEVENTFUL, ENGINE NOT SHUTDOWN. FOUND OIL PUMP LINE LEAKING IN THE FLEX PORTION. NOT A 'B' NUT LEAK REF IPC 79-21-05-05 NR 36. FOUND LEAK ON MAIN OIL SUPPLY TUBE BETWEEN OIL FILTERSDR DLM88091009Skin · corrodedLT EXTERNAL FUSELAGE AFT LAV SERVICE DOOR AREA SKIN LWR FWD CORNER HAS EVIDENCE OF CORROSION. REPAIRED SKIN FROM STA 1278-1338 L18L-23L IAW ERA 475018-14 REV ORIG DATED 6/6/09.SDR UALA2009060501610Oil Filter · faultyLEFT ENGINE HAS OIL FILTER BYPASS WARNING MSG HISTORY. REPLACED FILTER. CHECKED MAGNETIC CHIP DETECTORS.SDR UALA2009060201590Actuator · faultyAILERON LOCKOUT MESSAGE. REMOVED & REPLACED RT OUTBOARD AILERON LOCKOUT ACTUATOR. OPS CHECK GOOD.SDR UALA2009060301598Battery · faultyRECEIVED "MAIN BATTERY CHARGER" STATUS MSG. REPLACED MAIN BATTERY & CHARGER. CHECKS OKAY.SDR UALA2009060101575Fuel Tank · leakingWEEP HOLE INSIDE OF NR 2 ENGINE ON WING LEAKING FUEL AT 80 DROPS PER MINUTE. ACP TANK 2 AND RT WING TANK ENTRY FOUND FUEL SEEPING INTO DRY BAY FROM LOWER FWD O/B SECTION. RESEALED AND LEAK CHECKED WITH 19K FOB. ALL CHECKS OKAY.SDR UALA2009060101584Shutoff Valve · faultyNR 1 ENGINE BLEED INOPERATIVE. BITE MONITOR FAULTED PRV, PRVC, PRESS SENSOR, HPSOV AND WIRE FAULT. REPLACED CARD M859, NO HELP. INOPED PRSOV. REPLACED HPSOV AND HP CONTROLLER. REACTIVATED PRSOV, RAN ENG. NO BLEED PRESSURE FROM NR 1 ENG INOP'D PRSOV.SDR DL76P090972Engine · malfunctionedAT COMMENCEMENT OF TAKEOFF ROLL AT 40KTS L EEC MODE STATUS MSG ILLUMINATED. RETURNED TO GATE. ACT- T/S PER FIM. PERFORMED BITE ON L PIMU AND CYCLED EEC SWITCHES. CLEARED MSG AND RAN ENGINES AT IDLE. MSG DID NOT REAPPEAR. ALL INDICATIONS NORMAL.SDR HALA2009053000211Blade · nickedETOPS SIGNIFICANT SYSTEM - FOUND NR 1 ENG BLADE NR 34 HAS SMALL NICK ON LEADING EDGE 2 INCHES FROM TIP (AREA A). INSP AND BLENDED BLADE PER AMM 72-31-02. EDDY CURRENT CK OK.SDR UALA2009060101562Wire · disconnectedDURING G4 GALLEY CHILLER CIRCUIT BREAKER INSP, FOUND BUS WIRE DISCONNECTED AT C-B C9032 A1 POSITION. INSTALLED BUSS WIRE. OPS CHECKS GOOD.SDR UALA2009060101563Skin · corrodedEXT FUSELAGE SKIN STA 1542, BL 0 IS CORRODED AROUND DRAIN HOLE STR 39L - 39R. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER TRIPLER REPAIR.SDR UALA2009060101564Stringer · damagedMAIN CABIN STA 1307, STR 17R DRILL DAMAGE IN RADIUS OF STRINGER. MAJOR REPAIR ACCOMPLISHED: BLENDED BEAR STRAP DAMAGE AND INSTALLED STRINGER SPLICE REPAIR.SDR UALA2009060101565Light · inoperativeLEFT AFT DOOR EMERGENCY LIGHT (EXTERNAL) IS INOP. RELAMPED AND OPS CHECKS GOOD.SDR HALA2009052900207Unknown · unknownETOPS SIGNIFICANT SYSTEM - RIGHT ENGINE START DUCT PRESSURE LOW AT R DUCT 17 PSI L DUCT 19 PSI MAX MOTORING N2 AT 19 PERCENT. LEFT ENGINE START DUCT PRESSURE AT L DUCT 20 PSI, R 22 PSI MAX MOTORING 21 PERCENT, FRM CODE 80030502. STARTED BOTH ENGINES, RAN AT SDR UALA2009060101552Splice · defectiveDURING INSPECTION OF APU GEN POWER CABLES, FOUND EVIDENCE OF OVERHEATING AT SPLICE AREAS. DAMAGE AT STA 1809 BULKHEAD BELOW RT HORIZ STAB PIVOT PIN. REMOVED OLD APU GENERATOR SPLICES. INSTALLED NEW SPLICES REF BSWPM 20-30-13 AND INSTALLED STAR SPACERS. OPSSDR UALA2009060101553Feeder Cable · deterioratedNR 1 ENG IDG FEEDERS ARE DETERIORATED. INSTALLED NEW FEEDER IDG CABLES. OPS CHECKS GOOD.
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