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 UALA2012081304364Gauge · inoperativePOTABLE WATER GAUGE CHECKED FULL BEFORE DEPARTURE. FLIGHT ATTENDANT NOTICED LATER THAT GAUGE WAS AT ZERO. REPLACED MISSING SCREW TO GAUGE.SDR UALA2012081304472Battery Pack · malfunctionedFLIGHT DECK EMERGENCY EXIT LIGHT ILLUMINATED WITH EMERGENCY LIGHTS OFF (DISARMED). RESET BATTERY PACK, ACCOMPLISHED OPS CHECK. LIGHT OPS CHECKS SATISFACTORY.SDR UALA2012081304443Actuator · faultyRIGHT ENGINE EEC C1 STATUS MESSAGE DISPLAYED. FOUND ACTUATOR FAULTY.SDR UALA2012081504532Actuator · faultyRIGHT ENGINE EEC C1 STATUS MESSAGE DISPLAYED. REPLACED NR 2 ENGINE TCC AIR VALVE ACTUATOR PER MM 75-24-05-401. OPS AND LEAK CHECKED GOOD.SDR UALA2012081304449Tire · failedNR 3 FWD TIRE WITH TREAD SEPARATION DUE TO RAN FLAT. REPLACED TIRE IAW AMM.SDR UALA2012081304416Brake · fireNR 6 BRAKE FIRE REPORTED. ACCOMPLISHED INSPECTION AND CLEAN UP REF ECRA 0551-01032. NO DAMAGE NOTED. WHEEL ASSY'S 1 ,2, 5 AND 6 REPLACED REF AMM 32-45-01. BRAKE ASSY'S 5 AND 6 REPLACED.SDR UALA2012081004339Indicator · faultyALTIMETER FAULT, RTFL. CAPT'S AIRSPEED IND WENT TO ZERO KTS. ALTIMETER AND ALL OTHER LT SIDE AIR DATA INSTRUMENTS NORMAL. WHEN CAPT SELECTED ALTN AIR DATA, LT SIDE ALL NORMAL REPLACED CAPTAINS AIRSPEED INDICATOR AND LT CADC.SDR UALA2012081004350Controller · faultedFWD CABIN TEMP EICAS ON. VALVE CLOSED PER PROCEDURE 1, ALSO VISUALLY VERIFIED CLOSED. REPLACED LEFT PACK CONTROLLER BOX PER MM, OPS CHECK NORMAL.SDR UALA2012081004353Connector · dirtyOFF FLAG IN CAPTS VSI. LEFT VSI ELECTRICAL CONNECTOR CLEANED. LEFT AND RIGHT VSI INSTALLATION TEST CARRIED OUT SATISFACTORY AS PER AMM. NO FURTHER FLAGS DISPLAYED.SDR UALA2012080904316Bracket · crackedAT DEPARTURE TIME, CAPTAIN UNABLE TO SECURE SLIDING COCKPIT WINDOW. SUPPLEMENTAL DATA UPDATE, ADJUSTED NR 2 CAPTAIN WINDOW, CHECK NO LEAK. LOWER CARRIAGE BRACKET ITEM NR 365 P NR 141T4883-501, -9, OR -15 IS CRACKED AT CAPTAIN'S SLIDING WINDOW. SEE IPC 56-11SDR UALA2012080904331Actuator · leakingDURING WALK AROUND, MECH NOTICED SIGN OF HYD LEAK FROM APU ACCESS DOOR. ON REMOVAL OF RUDDER ACCESS PANEL, FOUND LOWER PCA LEAKING AT THE ACTUATOR STATIC SEAL. THE LEAK IS APPROX 5 DROP PER MIN AND FOUND WITHIN LIMITS IAW AMM.SDR UALA2012081004338Bellcrank · damagedELEVATOR PCA BELLCRANK FUNCTIONALLY CHECK RIG OF ELEVATORS TO IDENTIFY ANY OUT OF RIG CONDITION CAUSED BY SHEARED OR PARTIALLY SHEARED RIVETS IN THE ELEVATOR POWER CONTROL ACTUATOR INPUT LINKAGE ASSEMBLIES. FOUND SHEARED RIVET IN LT OTBD ELEV BELLCRANK. REMOSDR UALA2012081304397Gauge · inoperativePOTABLE WATER GAUGE CHECKED FULL BEFORE DEPARTURE. FLIGHT ATTENDANT NOTICED LATER THAT GAUGE WAS AT ZERO. DEFERED FOR TIME PER MEL VERIFIED TANK FULL.SDR UALA2012081004351Window · stuckAT DEPARTURE, CAPTAIN UNABLE TO SECURE SLIDING COCKPIT WINDOW. ADJUSTED NR 2 CAPTAIN WINDOW, CHECKED, NO LEAKS.SDR UALA2012080804302Controller · malfunctionedBLEED LT RT SIDE AND RT ENG HPSOV EICAS AND STATUS MESSAGE. REPLACED HPC PER AMM. ALL PRESSURES & INDICATIONS NORMAL HIGH POWER RUN.SDR UALA2012080804304Control Panel · stuckAIRSPEED SELECTOR ON MODE CONTROL PANEL SPEED DIGIT STUCK. REPLACED MODE CONTROL PANEL PER AMM.SDR UALA2012080804292Structure · dentedBULK CARGO DOOR DENTED AT FWD LWR CORNER. EVALUATED DENT AND FOUND OUT OF SRM LIMITS. CUT OUT DAMAGE AND ACCOMPLISHED HFEC OF CUT OUT AND HOLES COMMON TO REPAIR REF EA PT67-52-001 AND ECRA 5230-01875. NO CRACKS. ACCOMPLISHED INSURANCE CUT. FABRICATED AND SDR UALA2012080804293Bellcrank · damagedLEFT ELEVATOR OUTBOARD PCA BELLCRANK SHOWS INDICATION OF SHEARED RIVET. REMOVED RIVETS FROM LT OTBD BELLCRANK AND REPLACED WITH SOLID RIVETS PER SB767-27-0186. BELLCRANK REMOVED AND THE REWORKED BELLCRANK INSTALLED ON NR CARD 5232N00169.SDR UALA2012081304395Fitting · damagedTOW FITTING ASSY TORN OUT OF NG. REMOVED DAMAGED FITTING PER MM32-21-12 STOPPED AT ITEM 2 D-3 PAGE 401.SDR UALA2012081304399Bellcrank · damagedELEVATOR PCA BELLCRANK FUNCTIONALLY CHECK RIG OF ELEVATORS TO IDENTIFY ANY OUT OF RIG CONDITION CAUSED BY SHEARED OR PARTIALLY SHEARED RIVETS IN THE ELEVATOR POWER CONTROL ACTUATOR INPUT LINKAGE ASSEMBLIES. REFERENCE AMM 27-31-98 PAGE SERIES 601. MANDATED BYSDR UALA2012080804294Failsafe · corrodedBS 1562 FAILSAFE BETWEEN STR 39L-39R FOUND CORRODED. ACCOMPLISHED CLEAN-UP, DVI AND NDT OF OPEN HOLES COMMON TO REPAIR. NO CRACKS FOUND. FABRICATED AND INSTALLED REPAIR FILLER, ANGLE, SPLICE WEB AND SHEAR TIE.SDR UALA2012080804303Connector · dirty80 KTS A RT HYD QTY EICAS ILLUMINATED AND HYD QTY SHOWED .57 AND RAPIDLY DECREASING. CLEANED CONNECTOR. PRESSURIZED RH HYDRAULIC SYSTEM. CHECKED HYDRAULIC QUANTITY. SAME QUANTITY IN COCKPIT AND AT RESERVOIR.SDR UALA2012080804306Isolation Valve · faultyNR 2 ENGINE THRUST REVERSER FAULT. REPLACED NR 2 THRUST REVERSER MOTORIZED ISOLATION VALVE IAW.SDR UALA2012080604197Adc · malfunctionedCAPT'S ELECTRIAL ALTIMETER IS FAULTY, RETURNED TO FIELD. SELECTED ALTERNATE STATIC FIXES PROBLEM. FL340 CAPTAIN'S ALTIMETER FLUCTUATES + OR - 20 FT WHILE FIRST OFFICERS READS 34240 FT STEADY. FL280 CAPTAIN'S ALTIMETER STILL FLUCTUATES + OR - 20 FT AND FIRSSDR UALA2012080804312Line · leakingLEFT HYD SYSTEM LOW. FOUND LEFT ENG HYD PRESSURE LINE LEAKING NEAR DISCONNECT. TORQUED, NO HELP. REPLACED HYD LINE FROM RACEWAY TO ENGINE DRIVEN HYD PUMP. TORQUED B-NUTS, PERFORMED DRY SPIN NO LEAKS FOUND. PERFORMED ENG RUN AS PER JRH FOR 5 MIN AND INSPESDR UALA2012080704239Actuator · brokenLEFT HYD SYS PRESSURE EICAS, RTFL. FOUND NR 6 SPOILER ACTUATOR HOUSING BROKEN. REPLACED ACTUATOR AND LT CASE RET FILTERS. SERVICED LT HYD FLUID. OPERATIONAL CHECKED OK.SDR UALA2012080704248Warning Light · false activationRT ENG BLEED LGT AND R ENG HPSOV EICAS MSG DURING DESCENT WITH ENG BLEED SW ON, AND ENG RUNNING. DUCT PRESSURE IS 15PSI. ACCOMPLISHED AIR SUPPLY CONTROL SYSTEM TEST PER AMM TASK 36-23-00-715-001. NO FAULTS NOTED ON AIR SUPPLY BITE MODULE.SDR UALA2012080604226Knob · looseFIRST OFFICER'S RADAR AND HSI DIMMING KNOB LOOSE AND CAN BE LIFTED VERTICALLY OUT OF DETENT. REPLACED THE UNIT.SDR UALA2012080704242Connector · failedWINDOW NR 2 RT FAILS THE HEAT TEST. REPLACED "WW1156 A-A AND A-B" TERMINAL CONNECTION PLUG AND HARNESS - D1906, REF WD30-41- 11 PG 1. OPERATIONAL TEST OF RIGHT SIDE (R-2) WINDOW HEAT SYS OK.SDR UALA2012080304154Stringer · corrodedCORROSION FOUND IN AFT CARGO COMPARTMENT AT BS 1540 AT STRINGER 39R. REMOVED DAMAGED STRINGER SECTION. FABRICATED AND INSTALLED NEW STRINGER SECTION AND STRINGER SPLICE REPAIR PARTS REF SRM53-00-03 FIG 201 REPAIR 2 DETAIL IV.SDR UALA2012080604155Shear Tie · corrodedAFT CARGO COMPARTMENT SHEAR TIE ATTACHMENT BETWEEN FRAME AT BS 1280 AND BL 0 FOUND CORRODED. REMOVED CORRODED SHEAR TIE AND FOUND MATERIAL LOSS OUT OF SRM LIMITS. FABRICATED AND INSTALLED NEW SHEAR TIE SRM 51-40-02. MAJOR REPAIRSDR UALA2012080604211Connector · damagedAPU GENERATOR FEEDER CABLES BULKHEAD CONNECTOR DISCONNECTED. WIRES FOUND BURNED AND WELDED TOGETHER. APU GCU CIRCUIT BREAKER COLLARED. INSTALLED APU GEN CABLE 6F16610-501 HARNESS FROM GEN TO BULKHEAD REF MM 24-21-01-409. DISCONNECTED HARNESS IN STAB COMPARSDR UALA2012073104126Engine · unknownAT FL360, IN SMOOTH AIR, FOR ABOUT 15 MINS, BOTH ENG HAD FLUCTUATING PARAMETERS. LEFT ENG EPR RAPIDLY CHANGED FM LESS THAN 1.0 TO 1.45, N1 +--4%, EGT +-- 6, FF +--.4. CHECKED LEFT PIMU EEC CH A REVERSER RNG FAIL DISPLACED CHECKED ASSOCIATED WIRING PLUGS AND SSDR HALA2012073000186Idg · malfunctionedRIGHT ENG "FIELD OFF" LEFT ILLUMINATED ON P61 PANEL. R & R NR 2 RIGHT ENGINE IDG REF AMM 24-11-01. RAN ENG 5 MIN ID L/E OPS CHECKED GOOD, DISCONNECTED IDG - CONNECTED IDG - RAN ENG 5 MIN IDLE, OPS - LEAK CHECKED GOOD - OK FOR SERVICE.SDR UALA2012073004118Indicator · inoperativeLOST RT UPPER CRT, RTFL. RIGHT UPPER CRT DEAD. REPLACED FIRST OFFICERS EADI IAW AMM.SDR UALA2012073104120Connector · damagedEMERGENCY LIGHT CONNECTOR BROKEN AT SEAT 36B. REPAIRED EMERGENCY LIGHT CONNECTOR AT SEAT 36B. OPS CHECKED GOOD.SDR UALA2012080604204Fmu · faultedAFTER BOTH ENGINES STARTED, NR 1 ENGINE FUEL VALVE LIGHT FLICKERING DIMLY. NO EICAS MSG. SAMC TEXT: SHUT ENG DOWN, CYCLED CIRCUIT BREAKER P11-4 D25. ACCOMPLISHED NORMAL START, LIGHT STARTED FLICKERING AGAIN. REPLACED NR 1 ENGINE FMU REF MM. RAN ENGINE, OPSDR UALA2012080804271Switch · dirtyRT RECIRCULATION FAN LIGHT FAILS TO TEST. LIGHT WORKS BY OPERATING THE RECIRCULATION FAN SWITCH. THE LIGHT DID NOT WORK WHEN USING THE LIGHT TEST SWITCH. CLEANED SWITCH, OPS CHECK NORMALSDR HALA2012072900187Switch · looseAPU FAILED TO START ON GROUND. FOUND APU START SWITCH VERY LOOSE, CAN NOT SELECT PROPER START POSITION, SECURED START SWITCH. STARTED NORMAL IAW AMM 49-21-00.SDR UALA2012080604206Transmitter · leakingNR 1 ENG OIL PRESSURE INDICATION FAULT, TEMPERATURE AND QUANTITY NORMAL; OIL PRESSURE FLUCTUATING OR INTERMITTENT. WENT TO 400 PSI AFTER CLIMB POWER SELECTED INTERMITTENT NORMAL TO 400 PSI. NO LEAKS FOUND AFTER OIL PSI TRANSMITTER REPLACED. STATIC RUN CHESDR UALA2012080804272Chiller · failedGALLEY CHILLER INOPERATIVE AT C62. CIRCUIT BREAKER TRIPPED. REPLACED FAILED CHILLER PER AMM.SDR UALA2012080604205Fmu · faultedNR 1 ENGINE 'ENG EEC C1' MESSAGE APPEARED ON EICAS. ENGINE OPERATION NORMAL. CREW COMMENTS: AUTOTHROTTLE OPERATING NORMALLY. DEFERRED AS PER MEL. PIMU FAULT 352-25 AND 353-25 OCCURRED ON FLT 909-08JUL. RANG OUT WIRING. W1P7 PIN G TO -A 241 OHMS. H TO F 302 OHSDR UALA2012080804273Chiller · vibrationCHILLER AFT GALLEY VIBRATS AND IS NOISY. REPLACED FAILED CHILLER PER AMM.SDR UALA2012072704067Oxygen Mask · misinstalledALL LEFT O2 MASKS IMPROPERLY PACKED. REPACKED ALL LEFT O2 MASKS PER AMM.SDR UALA2012072504039Bulb · inoperativeRIGHT EMERGENCY ESCAPE SLIDE RIGHT TEST ONE INOPERATIVE. RESEATED BULB IN TEST PANEL, OPS CHECKED GOOD.SDR UALA2012072504036Stator · brokenON WALKAROUND, FOUND PARTS OF NR 7 BRAKE UNIT STATOR BROKEN. NR 7 MAIN WHEEL BRAKE ASSY REPLACED AS PER AMM. INSPECTED MAIN AXLE ASSY NO DAMAGE OR FAULTS FOUND MAIN WHEEL ASSY REMOVED AND REFITTED AS PER AMM. WHEEL INSPECTED, NO DAMAGE FOUND.SDR UALA2012072303982Duct · damagedAPU COOLING AIR DUCT DAMAGED. REPLACED COOLING AIR DISCHARGE DUCT AND SECURED WITH CLAMPS PER AMM.SDR UALA2012072303980Amplifier · faultySATCOM SYSTEM INOPERATIVE. REPLACED SDU, OPS NORMAL. SATCOM STARTED WORKING AGAIN. REPLACED HIGH POWER AMPLIFIER (LGA).SDR UALA2012072404020Computer · inoperativeCAPTAIN'S FLIGHT DIRECTOR INOPERATIVE. REPLACED LT FCC PER AMM.SDR UALA2012072303977Hose · unsecureR BLD DUCT LEAK EICAS AND DUCT LEAK ON OVERHEAD. SECURED RADIATOR HOSE IN AREA OF WATER CONDENSOR LEAK CHECKED OK..
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