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 2006UALA02111Light · inoperativeMID-GALLEY CROSS AISLE EMERGENCY FLOOR LIGHT IS INOP. INSTALLED SINGLE LIGHT HARD EEL STRIP, NEEDS DUAL LIGHT HARD EEL. DUAL LIGHT INSTALLED. OP CHKS OK. RETURNED TO SERVICE.SDR 2006UALA02115Warning Light · illuminatedWITH NORMAL CONFIGURATION FORWARD EQUIPMENT VALVE EICAS MESSAGE AND LIGHT. VALVE IDENTIFIED AS E&E COOLING VALVE. CONDUCTED OP CHECK OF VALVE USING A-CHECK JOB CARDS. VALVE AND SYSTEM CHECKED OK.SDR 2006UALA02097Aspirator · leakingASPIRATOR LEAKING BETWEEN SENSING TUBE AND BARREL. SLIDE REPLACED. RETURNED TO SERVICE AFTER VISIT.SDR HALA0600828Heat Exchanger · leakingDURING WALKAROUND FOUND OIL LEAK NR 1 ENG. FOUND NR 1 AIR/OIL HEAT EXCHANGER LEAKING. REPLACED AIR/OIL HEAT EXCHANGER AND VALVE IAW AMM 79-21-09. GROUND RUN UP AND LEAK CHECK OK.SDR 2006UALA02083Pump · failedFAILED HYDRAULIC PUMP. RETURNED TO THE BLOCKS. REPLACED NR 1 ENG ENGINE DRIVEN HYDRAULIC PUMP. LEAK CHECK OK, RETURN TO SERVICE.SDR HALA0600829Engine · leakingETOPS SIGNIFICANT SYSTEM, OIL LEAK FOUND ON ETOPS 2 CHK ON NR 1 ENGINE COMING FROM BOTTOM FWD AREA OF BYPASS DUCT. T/S IAW FIM 71-08-00, AFTER ENG RUN FOUND ENG OIL LEAKING FROM ANGLED GEARBOX COVER BOLTS, RETORQUED BOLTS IAW MFG ENG MAN 72-62-00, LEAK AND OPSDR HALA0600832Cylinder · leakingETOPS SIGNIFICANT SYSTEM, APU VARIABLE VOLUME CHAMBER CYLINDER HAS AIR LEAKING FROM ATTACH POINT GASKET. REMOVED AND REPLACED GASKET VOLUME CHAMBER CYLINDER. RAN APU AIR LEAK CHK OK.SDR 2006UALA02059Angle · crackedNR 1 PYLON MIDSPAR CLOSEOUT ANGLE CRACKED AT BOTH INBD FASTENERS. STOPPED DRILLED CRACK. INSTALLED STRAP AND FILLER REPAIR.SDR HALA0600814Fan · odorFWD EQUIP OVHT DISPLAYED AND OVHT LIGHT ILLUMINATED. LIGHT REMAINED EXTIN. AFTER SELECTOR WAS POSITIONED TO STBY. ELECTRICAL ODOR IN COCKPIT. T/S IAW FIM 21-58-00 CK GOOD.SDR 2006UALA02026Warning Light · illuminatedRETURNED TO JFK UNDER DUE TO LEADING EDGE FLAP INDICATION. ALL CHECKS FOUND NORMAL.SDR 2006UALA02027Switch · shortedFOUND SEAT 8C PCU SHORTING AND CAUSING SMOKE, FUMES IN CABIN. FOUND FAULTY SWITCH. EVIDENCE OF FLUID SPILL. REPLACED THE BACK-CYCLER SWITCH.SDR 2006UALA02008Warning Light · illuminatedTAT PROBE LIGHT ILLUMINATED JUST AFTER TAKEOFF. [5-1-07] REPLACED THE TOTAL AIR TEMPERATURE SENSOR. OP CHECKS OK. CAUSE SUSPECTED TO BE INTERNAL ELECTRICAL SHORT IN SENSOR CIRCUIT.SDR 2006UALA02009Engine · leakingDIVERTED TO BOS DUE TO LOST OF OIL IN THE NR 2 ENGINE. FOUND STARTER TO GEARBOX MOUNTING FLANGE CRACKED AND LEAKING. STARTER HAD BEEN REPLACED PRIOR TO FLIGHT. REPLACED NR 2 ENGINE GEARBOX HOUSING ASSEMBLY.SDR DL76L060853Flange · crackedFOUND CRACKED R FLANGE ON NR 2 ENG OUT OF M/M LIMITS. REPLACED NR 2 ENG PER TRANS 1T149.SDR DL76L060854Mount · crackedDURING ENG EXT HARDWARE INSP, FOUND AFT MOUNT RAILS CRACKED. REPLACED NR 1 ENG.SDR DL76L060855Seat · arcedCAPT SEAT ARCED TWICE DURING ELECTRICAL MOVEMENT. DISCONNECTED SEAT CONNECTOR C/B H-15 ON P6-3 PANEL POPPED. FWD TO MCO C/B PULLED PLACARD INSTALLED. REPLACED CAPTS SEAT ASSY, CHECKS GOOD. MCO/PLAC REMOVED.SDR 2006UALA01994Circuit Card · failedEICAS MSG 'LDG GEAR MONITOR' DISPLAYED WITH LDG GEAR UP AND LOCKED. FOUND ALL EXCEPT 4 CIRCUIT CARDS DISLODGED IN PSEU. REMOVED AND REINSTALLED ALL CIRCUIT CARDS.SDR ANCF200600036Engine · flamed outLT ENG SHUTDOWN, RESTARTING NOT ATTEMPTED DUE TO HIGH EGT (652 DEGREES) HIGH VIBRATION AND NO OIL PRESS, AIRPLANE WAS ON CRZ AT 36000 WITH SPEED MACH 0.79. NO APPARENT REASON FOR FLAMEOUT. WAS PERFORMED VISUAL AND BOROSCOPE INSPECTION AND CHECK, THE DIGITAL FSDR DL76L060832Seal · failedCTR HYD SYSTEM QTY DECEASING .41RF CTR HYD QTY MSG. FOUND FILTER MODULE IN WHEEL WELL LEAKING. REPLACED DPI O-RING LEAK CK OK. OVERWEIGHT LANDNG INSP AND PDC DONE.SDR DL76L060828Projector · overheatedDURING TURN AROUND VIDEO PROJECTOR AT 24CDE CAUSING SMOKE. REPLACED PROJECT AT SEAT 24CDE, OPS CKS NORMAL MCO AND PLAC REMOVED.SDR HALA0600801Fan Blade · damagedDURING ETOPS 2 CHK MINOR L/E FOD, DAMAGE NOTED TO NR 2 ENG FAN BLADE WHERE MARKED. NICK DAMAGE DIMENSIONS ARE 5/16" BY 1/8" DEEP 4" FROM BLADE TIP. MOC CONTACTED. NOT WITHIN DISPATCH LIMITS FAN BLADE BLENDED IAW AMM 72-31-02 IAW AMM 72-31-02 PARA 2 ITEM 4D SDR 2006UALA01951Motor · faulted"AIL LOCK" LIGHT WITH ASSOCIATED "AILERON LOCKOUT" EICAS ADVISORY LEVEL MESSAGE DISPLAYED DURING HIGH SPEED FLIGHT. CONFIRMED RT AILERON LOCKOUT ACTUATOR BAD. REPLACED PER MM27-11-44. FINAL CHECK GOOD. RETURN AC TO SERVICE. DAMAGED ACTUATOR MOTOR. SUSPECSDR DL76L060812Slide · unwanted deployREFERENCE: NR1492, DURING SLIDE ARMING, RT OVERWING SLIDE SYSTEM INADVERTENTLY ACTUATED. REPLACED RT OVERWING SLIDE AND COMPONENTS IAW OPN 7838AD.SDR HALA0600782Fairing · missingNR 2 ENG INTERMEDIATE CASE STRUT FAIRING AT 6:30 POSITION IS MISSING. NR 2 ENG I/B BLOCKER DOOR AT 8:00 POSITION DAMAGED (REMOVED AND PLACED IN W/B). NR 2 ENG I/B REVERSER COWL DAMAGE JUST FWD OF ATTACH LINK FITTING AT 7:00 POSITION (3" LONG, 3/8" WIDE, 1/2"SDR DL76P060811Fan · odorEQUIPMENT COOLING OVHT LIGHT ON OVERHEAD PANEL ACCOMPANIED BY BURNING SMELL IN COCKPIT. FOUND EICAS MSG FWD EQUIP SUPPLY FAN 1 PULLED AND COLLARD C/B H-18 FWD TO MCO AND PLAC 21-58-03B FWD SUPPLY FAN MOTOR BURNED UP NEEDS NEW FAN ASSY. REMOVED AND REPLACED FWSDR HALA0600742Starter · inoperative-BTB- ON STARTING NR 1 ENG N2 DROPPED TO ZERO AFTER REACHING 22 PERCENT, SUSPECT STARTER FAILURE. FOUND LEFT STARTER INOP, REMOVED AND INSTALLED SERVICEABLE STARTER, INSP AREA & NO DAMAGE NOTED, SERVICE STARTER WITH OIL TO FULL, DRY MOTOR ENG CHK GOOD, SECURSDR DL76L060783Blades · crackedNR 2 ENGINE FAILED BOROSCOPE. 1ST STAGE HPT BLADES HAS CRACKS FORMING. REPLACED ENGINE.SDR HALA0600740Indicator · erraticETOPS SIGNIFICANT SYSTEM, ON ENGINE START NR 2 EGT WAS ERRATIC. TEMP CLIMBED TO ABOUT 200 THEN WENT DOWN TO 14 TO 16 ON THE GAGE. EGT NEEDLE JUMPED AROUND EXCESSIVELY. FOUND NR 2 EGT IND ERRATIC WHEN SHAKING WIRES W354451 W-18 & W354451G-18 NEAR CONNECTOR DSDR 2006UALA01869Computer · failedL EICAS COMPUTER STATUS MSG DISPLAYED. REPLACED LEFT EICAS COMPUTER. A11 FLASH BAD. REPLACED A11U4 AND U10. OPS CHECK NORMAL.SDR 2006UALA01870Wire · damagedEICAS MESSAGE NORM ANTISKID & ALTN ANTI-SKID DISPLAYED. TAKEOFF FOLLOWED BY STATUS MESSAGE :ANTISKID CNTRL SHOWS XDUCR 7 FAULT, REPLACED TRANSDUCER 7. PROBLEM CONTINUED. FOUND WIRE TO PIN 1 IN TRANSDUCER CONNECTOR, D2024, BROKEN IN BACKSHELL CLAMP. REPLACED SDR HALA0600745Fan Blade · damagedETOPS SIGNIFICANT SYSTEM - ON OVERNIGHT CK, FOUND 2 NICKS ON NR 1 ENG, FAN BLADE NR 1. 1ST NICK IS LOCATED IN AREA -A- 2.5 INCHES FROM TIP MEASURING .015 INCH DEEP. 2ND NICK IS LOCATED IN AREA -F- 9.6 INCHES FROM TIP MEASURING .040 INCH DEEP. INSP & FOUND NSDR NOCA13806Target · missingDURING TAKEOFF ROLL AT 60 KNOTS MASTER WARNING AND EICAS (MESSAGE FLAPS). ABORTED TAKEOFF AND PERFORMED LOW ENERGY STOP. PERFORMED T/O WARNING SYSTEM TEST IAW FIM 31-51-00 FIG 107, OPS CHECK. TE FLAPS IAW AMM 27-58-00 PERFORMED PSEU BITE PROCEDURE IAW FIM 32SDR DL76L060820Keelbeam · damagedNR1375 AND ERA 457835-14 KEELBEAM RT DAMAGED AT STA 1192+17 DUE TO SKIN REMOVAL ON NR 952. REPAIRED IAW PRODUCTION PERMIT B767-5326413PA, REF ERA 457835-14.SDR 2006UALA01866Wire · damagedRIGHT WING T/E, WS 410, RIGHT MAIN FUEL QUANTITY WIRE BUNDLE FOR CONNECTOR, AFT SHELL CORRODED. FURTHER INSPECTION FOUND THE CORROSION WAS LIMITED TO THE CN1156 -4 CONNECTOR, HOWEVER, WHILE REMOVING THE CONNECTOR BACK SHELL, THE BACKSHELL BROKE APART INTO SESDR 2006UALA01867Compressor · stalledNR 2 ENG COMPRESSOR STALL IN FLIGHT. ENG RECOVERED AND CONTINUED OPERATING. RECOVERED AND CONTINUED OPERATING. PRIOR TO STALL, ENG POWER WAS DECELERATING. ACCOMPLISHED BOROSCOPE OF NR 2 ENGINE, REPLACED ELECTRONIC ENGINE CONTROL, REPLACED IPCV VALVE, HPSOV,SDR HALA0600733Blade · damagedETOPS SIGNIFICANT SYSTEM, DAMAGE IS IN 'AREA C' PER AMM 72-31-02. REPAIRED BLADE PER AMM 72-31-02-308-003-N00. DAMAGE IS IN 'AREA C' PER AMM 72-31-02. REPAIRED BLADE PER AMM 72-31-02-308-003-N00.SDR 2006UALA01864Latch · wornLT OVERWING SLIDE INTEGRATOR TORQUE CHECK FAILED. SLIDE DOOR LATCHES SHOW DEEP WEAR GROOVES ON LATCH SLIDERS PREVENTING PROPER LATCH MOVEMENT. REPLACED 4 LEFT OVERWING SLIDE DOOR LATCHES.SDR 2006UALA01798Floorbeam · crackedFOUND STA 246 FLOORBEAM ATTACH ANGLE AT RBL 11 IS CRACKED. REPLACED SUPPORT ANGLE 141T5146-5 PER SRM 51-40-2.SDR 2006UALA01801Generator · unknownRETURNED TO IAD DUE TO NR 2 GENERATOR PROBLEM. FOUND OVERFILL PRESSURE FITTING LEAKING OIL. REPLACED FITTING AND SERVICED TO FULL.SDR HALA0600726Valve · malfunctionedETOPS SIGNIFICANT SYSTEM, EICAS MX MSG R NAC VENT VAL DIS PLAYED. REPLACED RT NAC VENT VALVE PER M/M 75-23-02.SDR DL76G060737Video Unit · inoperativeVIDEO EQUIPMENT INOP. RESET IFE COOLING C/B. OPS CKS GOOD.SDR DL76L060736Engine · failedNR 1 ENG FAILED TEST 51-457132-14. NR 1 ENG FAILED 51-457132-14 ON WING TEST 21. REPLACED NR ENG OPN 7128.SDR 2006UALA01863Switch · faultyRT WING SLIDE DOOR SENSOR S219 IS OUT OF LIMITS. REPLACED THE S219 PROXIMITY SENSOR.SDR HALA0600679Line · chafedETOPS SIGNIFICANT SYSTEM., R ENG EEC MODE ALERT ILLUMINATED DURING CLIMB THRU FL 330. PERFORMED ABNORMAL CHECKLIST AND EEC RETURNED TO NORMAL OPS. NOTE: A/T DICONNECTED JUST PRIOR TO EEC ALERT. FOUND P 4.95 LINE CHAFED WITH HOLE BEHIND TVC DUCT,REMOVED TUBE SDR HALA0600667Eec · malfunctionedETOPS SIGNIFICANT SYSTEM - RT ENG EEC MODE AMBER EICAS MSG CAME ON NEAR TOP OF CLIMB. SUCCESSFUL RESET FOLLOWING QRH PROCEDURE. T/S PER FIM 73-21-00, FOUND P5 LINE FAULT CHA/B ON PIMU. INSPECTED PHEUMATIC LINES P5 AND P2, NO DISCREPANCIES FOUND. CLEARED PISDR HALA0600664Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ICAS MSG R ENG EEC MODE DISPLAYED, SYS WAS SUCCESSFULLY RESET. T/S PER FIM 73-21-00 FIG 113, NO MSG IN PIMU CLEARED MTC MSG RUN ENG PER FIM PIMU INDEX 350-22. MSG DID NOT RETURN, SYS OK.SDR HALA0600665Indication Sys · erraticETOPS SIGNIFICANT SYSTEM - NR 2 EGT ERRATIC AND FLUCTUATING BETWEEN 750-350 ON CLIMBOUT FOR APPROX 2 MINS, THAN STABLE. ACCOMPLISHED FIM 77-21-00 FIG 103, NO FAULTS OR DAMAGE. CHECKED ENG WIRING PER WDM 77-21-11 AND SSM 77-00-01 SHOOK HARNESS, NO FLUCTUATIONSDR HALA0600668Starter · malfunctionedETOPS SIGNIFICANT SYSTEM - RIGHT ENGINE SLOW TO START STARTER CUT OUT AT APPROX 47%, 130 SECONDS FROM FUEL ON TO IDLE SPEED. RAN NR 2 ENGINE ON GROUND, STARTER CUTOUT AT 49%, 85 SEC FROM FUEL ONTO IDLE SPEED. OK TO CONTINUE PER HAL M105 FILE 584060.SDR HALA0600653Eec · faultedETOPS SIGNIFICANT SYSTEM - RIGHT ENGINE EEC MODE EICAS MESSAGE DISPLAYED. T/S PER FIM 73-21-00 FIG 113 PIMU FAULTED EEC CHANNEL A/B P2 AND P5 LINE. INSPECTED P2 AND P5 LINES PER FIM 350-21. NO FAULTS NOTED. CLEARED PIMU AND RAN ENG NR 2 TO 1.4 EPR. CONFIRSDR DL76L060819Stringer · gougedFUELAGE EXTERIOR SURFACE FOUND GOUGED AT STRINGER 37R AT APPROX STA 1219. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 1.
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