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 UALA2012022401112Bulkhead · damagedSTA 1809 BULKHEAD RIGHT SIDE INBOARD HORIZ HINGE DEFECT INDICATION NOTED ON 2 EA HOLES, 1 LOCATED ON HINGE SECOND ONE DOWN AND 1 LOCATED ON BRACE FIRST INBOARD HOLE. RESULTS FROM NDT, RMV'D FASTENERS, REAMED HOLES, ACCOMP NDT NO CRACKS NOTED, INSTALLED NEW FASDR UALA2012022401113Stiffener · crackedSTA 1809.5 AFT BULKHEAD STIFFENER CRACKED, BENT AT RBL 8. MAJOR REPAIR ACCOMPLISHED. RMV'D AND RPL'D AFT BULKHEAD STIFFENER STA 1809.5.SDR UALA2012022701196Display · inoperativeP-R LOWER ECAM AND F/O DISPLAY UNIT NOT OPERATING. RMV'D & RPLC'D LOWER ECAM DISPLAY UNIT.SDR UALA2012022301099Line · burnedPOTABLE WATER SUPPLY LINE HAS BURN DAMAGE AT STA 1495. RMV'D & RPLC'D POTABLE WATER SUPPLY LINE.SDR UALA2012022401105Frame · bentSTA 1725.5 FRAME CHORD BENT-PUSHED IN FWD SIDE OF FRAME STR 30L. REPAIRED FRAME CHORD AT STA 1725.5, STR 30L.SDR UALA2012022401106Fastener · looseSTA 1725.5 FRAME FWD SIDE OF FRAME STR 30L HAS RIVETS LOOSE, PUSHING ON ATTACH FITTING. REMOVED FASTENERS AT STA 1725.5, STR 26L AREA, ACCOMPLISHED NDT OF HOLES NO CRACKS NOTED, INSTALLED NEW FASTENERS.SDR UALA2012022401110Bulkhead · bentSTA 1809.5 AFT BULKHEAD WEB CREASED BENT AT STR 36L TO 36R. MAJOR REPAIR ACCOMPLISHED. RMV'D AND RPL'D STA 1809.5 AFT LWR BULKHEAD WEB.SDR UALA2012022201068Skin · corrodedAFT OF CARGO BAY AT BS 1544, BL 0 INTERNAL SKIN IS CORRODED AROUND DRAIN VALVE. MAJOR REPAIR ACCOMPLISHED, REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS OF SRM. TRIMMED OUT DAMAGE AND ACCOMPLISHED NDT OF REPAIR AREA AND OPEN HOLES FOR CRACKS. NONESDR UALA2012022401126Tape · peelingRT ENG STATOR VANES METAL SPEED TAPE PEELING. APPEARS TO INTERFERE W/ REQUIRED SMOOTH AIRFLOW. SMOOTHED LIFTED TAPE AS MUCH AS POSSIBLE BUT SOME FURTHER TAPE REPAIR REQUIRED. INTERIM -REPAIR TAPE NEEDS TO BE RESTORED WITHIN THE NEXT 50 FLIGHT HRS PER MM. RSDR UALA2012022301096Skin · damagedSTA 1725.5 EXTERNAL SKIN TORN-BENT AT LAP JOINT AND BUTT JOINT STR 32L. ACCOMPLISHED EXTERNAL SKIN REPAIR PER ECRA 5380-01078.SDR UALA2012022201066Slide · unwanted deployDURING MANUAL OPERATION OF THE DISARM FEATURE FROM THE EXTERNAL HANDLE OF THE L2 DOOR IAW TASKCARD 683301410, THE SLIDE DEPLOYED. REMOVED AND REPLACED SLIDE ASSEMBLY REF AMM. OPS CHECKED GOOD.SDR UALA2012022301104Computer · failedCAPTIN FLT DIRECTOR NO ROLL MODE SEL RT FLT DIR ROLL MODE RETURNS NO LAND 3 BOTH POSITIONS. REPLACED LEFT SIDE FLT COMPUTER PER MM. NO LAND 3 ON AUTOLAND STATUS ANNUNCIATOR. REPLACED LEFT FLIGHT CONTROL COMPUTER IAW MM. ACP'D TEST PER MM. GRND CK NORMAL. SDR UALA2012022001006Web · crackedNR 2 PYLON FWD UPPER SPAR DRAIN WEB AT NAC STA 175.5 COMMON TO FUEL TUBE CUTOUT IS CRACKED AT NUT PLATE HOLE. TRIMMED OUT DAMAGE & ACP NDT FOR CRACKS, NONE FOUND. FABRICATED AND INSTALLED DOUBLER REPAIR PER EA PD67-54-020 & ECRA 5453-01048.SDR UALA2012022101059Valve · faultyEICAS MESSAGE FOR COCKPIT TEMP DISPLAYED AND COCKPIT TEMP INOPERATIVE LIGHT ILLUMINATED IN AUTO. MANUAL OPERATION NORM. FOUND COCKPIT TRIM AIR VALVE SLOW TO MOVE. REPLACED TRIM AIR VALVE.SDR UALA2012022000998Rvdt · misriggedT/E FLAP DISAGREE EICAS ON FLAP EXTENSION FOR LANDING. FOUND ON INITIAL EVALUATION ON FSEU M603 FLAP LEVER RVDT MISRIG SEC1 AND M548 OUTBD SLAT PDU RVDT MISSRIG, RAISED FLAPS UP ELECTRICALLY, CHECKED NR 2 OUTBD SLATS PDU INDICATOR ALL NORMAL AS PER MM. PERFOSDR UALA2012022000988Guard · corrodedCORROSION ON FASTENER HOLES CREASE BEAM AT L1 DOOR FROM BS 192-345 AT LBL 82. (N-R 3811N00437). MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION REF SRM 51-10-02 & FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED & REPLACED EXISTING CREASE BEAM SPLASH GUARD WITH A NESDR UALA2012022000989Crease Beam · corrodedCORROSION AROUND FASTENER HOLES ON CREASE BEAM AT L1 DOOR FROM BS 292-345 LBL 82. WORK ACP ON PTT SEQ 7152119. CREASE BEAM REPAIRED ON BASE N-R 3811N00437.SDR UALA2012022001016Splash Guard · damagedDOOR 1LT CREASE BEAM SPLASH GUARD REPAIR MUST RECEIVE A NEW 8100-9 SHOWING COMPLIANCE TO 14 CFR 25.571 & 26.43(D) AND THE DAMAGE TOLERANCE INFORMATION INCORPORATED IN THE AIRCRAFT MAINT PROGRAM WITHIN 24 MONTHS FROM 15FEB2012 FOR THE REPAIR APPROVAL TO REMAINSDR UALA2012022001017Fastener · faultyFUSELAGE CROWN STA 218.9 LBL 12.5 & STA 233.9 LBL 14.4 HAS 1 EACH BLIND FASTENER INSTALLED IN EACH LOCATION. BLIND FASTENERS REMOVED AND REPLACED WITH BLIND FASTENERS DUE TO NO ACCESS PER REO(EVA) G11456 AND UA-EVA-60126. CUT ACCESS HOLES IN DRIPSHIELD & INSSDR UALA2012022001024Shim · migratedLEFT WING AT RIB NR 9, STR 18L, WS 404, SHIM HAD MIGRATED. ACCOMPLISHED PERMANENT REPAIR 85625 REPLACED DISCREPANT FASTENER AND MIGRATED SHIM. REMOVED SEALANT TO ACCESS SHIM AND FOUND ADDITIONAL MIGRATION. TRIMMED SHIM AND DETERMINED DIMENSIONS. FABRICATESDR UALA2012022001018Bolt · damagedLT WING BOLT LOCATED AT WS 416.2, STR 18L COMMON TO RIB NR 9 AND P-N 112T5373-9 FITTING HAS THREAD DAMAGE, REF EVA IMC-00713 AND IMC-00733 FOR HISTORY. REMOVED AND REPLACED BOLT WITH NEW ONE.SDR UALA2012022000976Cable · damagedEEL STRIP INOP AT CROSS AISLE IN FWD GALLEY. RPR'D RIBBON CABLE IN LEFT AISLE NEAR SEAT 1A, OPS CHECKS NORMAL.SDR UALA2012022101058Controller · inoperativeCOCKPIT AUTO TEMPERATURE CONTROL INOPERATIVE, WORKS IN MANUAL. FOUND CABIN TEMP CONTROLLER FAILED BITE. REPLACED CONTROLLER AS PER AMM. ALL OPS NORMAL, BITE TEST AND OPS CHECKED OKAY.SDR UALA2012022001035Union · leakingNR 1 ENG HYDRAULIC LEAK FROM DRAIN. ACCOMPLISHED AMM 71-71-00 P61, HYDRAULIC LEAK IN LT PYLON VIA STRUT DRAIN FROM CTR MOUNT DRAIN LINE. AREA CHECKED. FOUND UNION OF LT HYDRAULIC SYSTEM BETWEEN HYDRAULIC BAY AND PYLON LEAKING UNION RETIGHTENED AND LEAK CHESDR UALA2012022001027Failsafe · damagedRIGHT BS 955 FAILSAFE STRAP DAMAGED. ACCOMPLISHED REPAIRE ON FAILSAFE STRAP ON TASKCARD 3872N00715.SDR UALA2012022001034Generator · crackedAPU SHUT DOWN ON ITS OWN. FAULT LIGHT ON. FOUND LARGE CRACK IN APU GENERATOR CASING, CAUSING APU OIL LOSS. APU GENERATOR REPLACED AS PER AMM, ALL CHECKED OKAY.SDR UALA2012022001026Failsafe · damagedLEFT BS 955 FAILSAFE STRAP DAMAGED. ACCOMPLISHED SMC038 FAILSAFE STRAP REWORK ON TASKCARD 3872N00714.SDR UALA2012021600945Flap · malfunctionedTRAILING EDGE FLAP DISAGREE AT POSITION ONE USED ALTERNATE FLAP EXTENSION. ON ARRIVAL FSEU DISPLAYS FAULTS M548 OUTBD SLAT PDU RVDT MISRIG AND M603 FLAP LEVER RVDT MISRIG. RESET FLAPS TO SOWED USING ELECTRICAL SYSTEM AND CARRIED OUT MULTIPLE FLAP SLAT FUNCTISDR UALA2012021700960Control Valve · vibrationVIBRATION STILL FELT ON 6 MINUTE CYCLE. CAN BE FELT IN COCKPIT FLOOR. ALL CRUISE ALTITUDES. FWD CARGO HEAT DUCTING IN RT AC BAY IS SECURED. WILL NEED TO INSPECT PICCOLO DUCT IN FWD CARGO PIT FLOOR. NOT ENOUGH TIME TO DISASSEMBLE FWD CARGO PIT FLOOR PANELSSDR UALA2012021700963Engine · vibrationDUE TO REPEAT VIB IND HIGHER THAN NORMAL TO PREVENT IRREG OPS, ACCOMPLISH FAN BLADE ROOT LUBE. `WILL REQUIRE VIBRATION SURVEY (HIGH POWER RUN), TEST NR 8 PER AMM. ACP'D TEST NR 8 VIBRATION SURVEY. TEST FAILED, (N1 VIB) INDICATES 4.2 AT 78% N1 AND (BB VIB) WSDR UALA2012021600949Indicator · faultyAIRFRAME VIBRATION FELT EVERY 6 MIN, LASTING 1 MIN. CABIN RATE -500FPM AT BEGINNING & CONT. REPLACED CABIN PRESS INDICATOR PER AMM. VERIFIED REMOTE DIFFERENTIAL PRESS SENSOR WAS COMPATIBLE.SDR UALA2012021500932Fmu · faultyRT ENG FUEL FILTER IND, RTFL. PUMP METERING VALVE READY TO BE RMV'D. NR 2 ENG FUEL PUMP & FUEL METERING UNIT RMV'D FOR LOG2. ACCMP'D REMOVAL REF MM 73-11-01 PAGE 412 PARAGRAPH 3A AND MM 73-21-03 PARAGRAPH 3 E 2. INSTALLED NEW FUEL PUMP AND FUEL METERING USDR UALA2012021500891Floor Support · corrodedAFT LEFT ENTRY DOOR HAS CORROSION INBD OF THRESHOLD ON FLOOR SUPPORT AT BS 1510. FABRICATED AND INSTALLED FILLERS, ANGLE AND PLATE PER ECRA 5360-01178 AND EA PD67- 53-045.SDR UALA2012021500892Guard · corrodedL2 DOOR SPLASH GUARD CORRODED AT THE DOOR SILL. FABRICATED AND INSTALLED FILLERS, ANGLE AND PLATE PER ECRA 5360-01178 AND EA PD67- 53-045.SDR UALA2012021400877Battery · dischargedEMERGENCY LIGHT SIGN AT 19A AND EMERGENCY LIGHT STRIP, BY LT MID LAV CAME ON FOR ABOUT 30 MIN IN FLT THEN FLICKERED AND WENT OUT. DISCONNECT AND RECONNECTED EMERGENCY BATTERY PACK PER MM AND TESTED PER MM. ACP FIM 33-51-00-108 SYS PASSED OK, NO FAULTS FOUND.SDR UALA2012021400886Hydraulic Line · leakingPIN HOLE IN LT MLG RETRACT LINE NEAR ACTUATOR. P/N 272T1200-316 TUBE. REMOVED LINE, HAD TO CUT ATTACHING LINE OFF AT LOWER AFT OUTBD END, LINE IS IN SHOP BEING MANUFACTURED, ALSO ORDERED ELBOW FOR UPPER FWD END TO LSVC DESK. REPAIRED LINE WITH RYNGLOCK AND SDR UALA2012021400867Hydraulic System · unknownHYDRAULIC FLUID DRIPPING FROM NR 2 ENGINE. OPENED RT NACELLE, HYD FLUID WETNESS IN AREA OF EDP AND HYD LINES. CLEANED & DRIED. RAN ENGINE 5 MINS, REINSPECTED, NO LEAKS NOTED. HYD QTY CHECKED GOOD.SDR UALA2012021300814Idg · faultyRT GEN DRIVE & OFF LIGHT. DUE TO REPEAT GRIPES OF RIGHT GEN DRIVE LIGHT AND GEN OFF LIGHT AND GCU ALREADY REPLACED, REPLACE THE RIGHT IDG. VERIFY EFFECTIVITY WITH ON-LINE IPC. REPLACED RIGHT ENGINE IDG PER MM. OPS AND LEAK CHECK NORMAL.SDR UALA2012021300855Controller · faultyAPUC FAILED TO RESET OR TEST AFTER FIRE BOTTLE WAS ARMED AT NLG. REPLACED APUC.SDR UALA2012021300820Battery · dischargedR EMER ESCAPE LIGHT NOT TESTING. ACCOMPLISHED TROUBLESHOOTING PER MM AND RESEATED CONNECTOR ON RT OFF WING ESCAPE SLIDE SQUIB AND STILL TEST BAD. TRIED NEW PANEL AND STILL NO GOOD AND NOW TEST 1 INOP. PER FIM FIG 103 REPLACED BATTERY AND 25-65-17 AND TEST NSDR UALA2012021300822Battery Pack · dischargedREF RT OFF WING ESCAPE SLIDE TROUBLESHOOTING REMOVED BATTERY FROM RT EMERGENCY BATTERY PACK M00732. INSTALLED BATTERY PACK FROM OFF WING ESCAPE SLIDE POSITION PER MM. EMERGENCY LIGHT TEST NORMAL. CARRIED OUT INSPECTION OF ITEM REF MM, ALL SATIS. ACCOMPLISHSDR UALA2012021300815Gcu · faultyEICAS MSG R GEN OFF DISPLAYED. GEN OFF LIGHT ILLUM. OPERATED NORM AFTER RESET. REPLACED THE RIGHT ENG GCU PER MM. RAN NR 2 ENG ALL INDICATIONS NORMAL FOR RIGHT GEN.SDR HALA2012020900057Blade · damagedNR 1 ENGINE HAS TIP CURL ON ONE BLADE. .250" ON L/E THRU .100 ON OUTER EDGE TIP OF BLADE. REMOVED DAMAGED AREA REF AMM 72-31-02. PERFORMED FPI AND EDDY CURRENT IAW AMM 72-31-02, NO FAULTS.SDR UALA2012020900772Power Supply · inoperativeTHE 19AB, 20AB EMER LIGHTS FLASH - *FIX DN. REPLACED POWER SUPPLY AND BATTERY ASSYS M1559 AND M737 AT SEAT 21A PER MM, TESTED AND OPS NORMAL.SDR UALA2012020900777Connector · burnedNR 1 PYLON CONNECTOR TO MOTORIZED ISOLATION VALVE IS BURNED BETWEEN PINS. REMOVED & REPLACED CONNECTOR & BACKSHELL REF BOEING SWPM20-61-00 AND WDM78-34-11. PERFORMED OPS CHECK OF SYSTEM. CHECKS GOOD.SDR UALA2012020800754Thrust Reverser · damagedNR 2 ENG LT REVERSER DAMAGED. THREE DAMAGED AREAS, TWO IN SLEEVE ACCOUSTICAL SKIN AND ONE ON INNER BARREL ACCOUSTICAL SKIN, MOST LIKELY DAMAGED FROM PREVIOUS BLOCKER DOOR OR FAIRING DEPARTURE. DENT IN SLEEVE 1.375" X 1.875" X .125" A-Y=11, CREASE IN SLEEVE 1SDR UALA2012020800755Actuator · leakingLT OUTBOARD ELEVATOR PCA HAS RUNNING LEAK FROM SHAFT SEAL. SHOULD READ LEAKING FROM LT CENTER ELEVATOR PCA. PCA REMOVED. COMPLETED INSTALLATION OF LT CTR ELEV PCA.SDR UALA2012020700740Actuator · intermittentRUDDER TRIM INTERMITTENT, FLIGHT DIVERTED. REPLACED RUDDER TRIM ACTUATOR PER MM. REPLACED RUDDER TRIM CONTROL MODULE PER MM. OPS CHECKS GOOD.SDR UALA2012020600724Pump · unknownNR 2 ENG FUEL PUMP REPLACEMENT.SDR UALA2012020600703Pcu · out of adjust5 UNITS LEFT RUDDER TRIM NEEDED IN CLIMBOUT. FOUND LEFT RUDDER PCU OUT OF ADJUSTMENT. ADJUSTED PER MM. CHECKED ADJ OF CENTER AND RIGHT PCU. CHECKS NORMAL.
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