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 2007UALA04632Light · improper partAFT GALLEY (G4) SHORT LIGHT BAR IS WRONG TYPE. INSTALLED CORRECT PART, OPS CHECKS NORMAL.SDR 2007UALA04635Battery · faultyEMERGENCY LIGHTING ON LEFT SIDE OF ECONOMY FLASHES ON AND OFF DURING FLIGHT. REPLACED BATTERY SUPPLY AT 17A. OPS CHECKED OKAY.SDR 2007UALA04634Wire · arcedLEFT WING O/B SURGE TANK WIRES HAS SIGNS OF ARCING AT TERMINAL BLOCK, HARDWARE RUSTED O/B SIDE OF RIB 31. REPLACED LEVEL SENSOR AND TERMINAL BLOCK. AC OK FOR SERVICESDR HALA0700487Cowling · dentedETOPS SIGNIFICANT SYSTEM - NR 2 ENG INLET COWL DENTED AT APPROX 5:30 POSITION AS VIEWED LOOKING FWD DENT MEASURE APPROX: 28"L, 2.5"W, 0.042" DEPTH. REPAIRED PER M105 FILE NR 585114 AND TRANSFERED TO DPM P98977. OK FOR SERVICE.SDR 2007UALA04633Structure · crackedNR 2 PYLON FUEL LINE CUTOUT FWD INBOARD ATTACH HOLE CRACKED.SDR 2007UALA04630Light · inoperativeLEFT MID LAV EEL LIGHT BAR IS INOPERATIVE. REPLACED LIGHT BAR.
SDR UALA2008111304633Structure · crackedNR 2 PYLON FUEL LINE CUTOUT FWD INBOARD ATTACH HOLE CRACKED. SUSPECT ENGINE VIBRATION CAUSE. INSTALLED NEW REPAIR DOUBLER PER REO-G12178 REV B. AC OK FOR SERVICE.SDR 2007UALA04618Floorbeam · crackedSTA 246, LBL 26, FLOORBEAM VERTICAL STIFFENER IS CRACKED. REMOVED & REPLACED VERTICAL STIFFENER.SDR 2007UALA04619Floorbeam · crackedMAIN CABIN FLOORBEAM, ATTACH VERTICAL CHANNEL CRACKED AT BS 1503 LBL 67. MAJOR REPAIR ACCOMPLISHED. REMOVED & REPLACED CHANNEL LBL 67.SDR 2007UALA04654Actuator · faultyAIRCRAFT REQUIRES 4 UNITS LEFT RUDDER TRIM DURING CRUISE. L & R FUEL TANKS BALANCED. SUSPECT RUDDER TRIM ACTUATOR. REPLACED RUDDER TRIM ACTUATOR. ALL SYSTEMS CHECK NORMAL. PERFORM SINGLE HYDRAULIC SYSTEM CHECK OF EACH RUDDER POWER CONTROL ACTUATOR USING EASDR DL76L071416Line · leakingNR 1 ENG LOOSING OIL QTY STEADY DROP DIVERTING TO LGW FOR REPAIRS. OPENED LT ENG FOUND OIL RETURN LINE LEAKING AT TUBE ASSY SCAVENGE PUMP TO OIL FILTER P/N 59T347 IPC 79-21-05-05 ITEM 36 543778. REPLACED TUBE ASSY RETURNED A/C TO NML, PERF ENG RUN/LEAK CHECKSDR 2007UALA04596Pump · leakingCTR ADP HAS HYDRAULIC LEAK. REPLACED AIR DRIVEN PUMP PER MM29-11-03. DURING OPS CHECK OF ADP FOUND PRESSURE REGULATOR VALVE FAILED. OPS CHECK NORMAL. ACFT OK FOR SERVICE.
SDR 2007UALA04565Indicator · faultyRTFL DUE TO STANDBY ATTITUDE INDICATOR PROBLEMS. REPLACED STANDBY ATTITUDE INDICATOR WITH BORROWED UNIT. OPERATIONAL TEST CARRIED OUT SUCCESSFULLY. ACFT CATII-III STATUS NOT ALTERED.
SDR 2007UALA04560Oxygen Bottle · leakingBOTH OXYGEN BOTTLES IN AFT CABIN RIGHT SIDE SHOW BELOW THE GREEN ARC. SUSPECT LEAK AT FILLER VALVE. REPLACED BOTTLES. ACFT OK FOR SERVICE.
SDR 2007UALA04561Pump · unknownRTFL DUE TO CENTER HYDRAULIC PUMP PROBLEM. REPLACED HYDRAULIC AIR DRIVEN PUMP. ALSO REPLACED HYD LINES & PUMP MOUNTS. PERFORMED SYSTEM CHKS. OK FOR SERVICE.
SDR 2007UALA04563Connector · looseBUSINESS CLASS FLOOR LIGHTING INOP ON LEFT SIDE. SECURED CONNECTOR.
SDR 2007UALA04562Battery · faultyFOUND ROWS 15-18 LEFT SIDE OF ACFT EMERGENCY EXIT LIGHTS KEEP COMING ON. REPLACED BATTERY AND FOUND CONNECTOR LOOSE, SYSTEM CHECKED NORMAL.
SDR 2007UALA04498Bulb · inoperativeEMERGENCY FLASHLIGHT AT MID GALLEY CLOSET INOP. SUSPECT FAULTY BULB OR BATTERIES. REPLACED FLASHLIGHT, NOW OPS OK. ACFT OK FOR SERVICE.SDR 2007UALA04499Hose · collapsedHOSE ASSY FOR RAMP SLIDE INFLATION HAS COLLAPSED. SUSPECT HOSE DAMAGED DURING MAINTENANCE. REPLACED HOSE ASSEMBLY. ACFT OK FOR SERVICE.SDR 2007UALA04510Connector · looseEND CAPS MISSING FROM FRONT OF ESCAPE PATH LIGHTING STRIPS IN FIRST CLASS. ALSO CONNECTIONS LOOSE IN SAME AREA. RECONNECTED, OPS CHECK AND INSTALLED END CAPS.
SDR 2007UALA04463Frame · corrodedMAIN CABIN FRAME CAP CORRODED STA 246 BL80R TO BL84R. SUSPECT MOISTURE CONTAMINATION. REMOVED CAP SECTION AND FABRICATED NEW SECTION. ACFT OK FOR SERVICE.SDR 2007UALA04464Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED AT OUTBOARD END BS 287 AT FWD LOWER CORNER OF R-1 DOOR CUTOUT. SUSPECT MOISTURE CONTAMINATION. REMOVED DAMAGED SECTION OF CAP AND FABRICATED CAP SECTION, ANGLES AND STRAPS AND INSTALLED PER SRM 53-00-51. ACFT OK FOR SERVICE.SDR 2007UALA04465Stringer · corrodedMAIN CABIN, RT FUSELAGE INTERNAL, STR 13R HAS SURFACE CORROSION JUST AFT OF STA 1263. SUSPECT MOISTURE CONTAMINATION. REMOVED DAMAGED AND FABRICATED REPAIR AND INSTALLED PER SRM 53-00-03. ACFT OK FOR SERVICE.SDR 2007UALA04438Light · brokenEMERGENCY LIGHTING STRIP BROKEN AT 2B. REPAIRED BROKEN SECTION. OPS CHECK, OK.
SDR 2007UALA04441Angle · corrodedMAIN CABIN AT STA 287 APPROX RBL 80, FLOORBEAM ANGLE P/N 141T5111-45 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE P/N 141T5111-45.SDR 2007UALA04444Engine · vibrationENG 2 VIBRATIONS SHIFTED UP FROM 0.2 TO 0.8 UNITS.
SDR 2007UALA04442Connector · unsecureEMERGENCY FLOOR LIGHTING ON LEFT SIDE OF CABIN AFT OF ROW 15 COMES ON INTERMITTENTLY. SECURED, RESET CONNECTIONS ON EEL STRIP LEFT SIDE OF CABIN. OPS CHECK OK.SDR 2007UALA04443Cap · missingEEL STRIP END CAPS MISSING IN FC AND BC ZONES, 5 EA. REPLACED MISSING EEL STRIP END CAPS.SDR 2007UALA04439Frame · corrodedMAIN CABIN FRAME T-CAP CORRODED STA 303 BL51R TO BL55R. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION OF T-CAP. FABRICATED T-CAP SPLICE. INSTALLED TEE CHORD, ANGLE & SPLICE REPAIR.SDR 2007UALA04440Angle · crackedMAIN CABIN INTERCOSTAL UPPER ANGLE CRACKED BETWEEN STA 1197 + 22 AND 1197 +44, LBL 40. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED ANGLE. INSTALLED NEW ANGLE, P/N 140T2540-9.SDR 2007UALA04449Starter · making metalNR 2 ENG STARTER MAG CHIP DETECTOR SHOWS LARGE FLAKES OF METAL. ALSO THE NR 1 ENG STARTER DRAINED AN INSUFFICIENT AMOUNT OF OIL. ALSO BLACK AND BURNED AND HAS AN ODOR. NR 1 STARTER FOUND WITH LOW OIL AND OIL LOOKS BLACK AND BURNED REPLACED STARTER. AFTER SESDR 2007UALA04410Connector · disconnectedGALLEY EEL STRIP ADJACENT TO DOOR 1R INOPERATIVE. *S/D* RECONNECTED POWER CONNECTOR, OPS CHECKS GOOD.
SDR 2007UALA04378Aileron · damagedRETURN TO GATE DUE TO WING TO WING CONTACT. SUPPLEMENTAL DATA UPDATE RIGHT OUTBOARD AILERON DAMAGED DUE TO RT WING CONTACT WITH LT WING OF 6672.SDR 2007UALA04396Connector · disconnectedEMERGENCY LIGHT PATH IN FRONT OF MIDDLE LT LAVATORY INOP. RECONNECTED PATH CONNECTOR.
SDR HALA0700455Blocker Door · brokenNR 1 ENG THRUST REVERSER BLOCKER DOOR BROKE OFF 6 O'CLK POS. OK TO CONTINUE PER L CDL78-31-3.
SDR HALA0700457Engine · malfunctionedETOPS SIGNIFICANT SYSTEM, AT TOP OF DESCENT W/BOTH THROTTLES BACK THE FOLLOWING ENG READINGS NR 1 N1 50.2 EGT 316 N2 78.5 F/F 1000 NR 2 ENG READING WERE N1 36.2 EGT 306 N2 69.0 F/F 500. AT 19,000 FT TO 18,000 BOTH ENGS READ THE SAME. ENGINES APPROACH IDLE W/SDR 2007UALA04367Light · inoperativeEEL STRIP BY RIGHT SIDE FWD GALLEY AND RIGHT SIDE FC AREA INOP. REPAIRED BROKEN SECTION. OPS CHECK, OK.
SDR DL76L071385Shutoff Valve · malfunctionedUNUSUAL AIR SURGE SOUND DURING TAXI IN LEFT ENG IS 23 PSI AND RT ENG IS 34. REMOVED AND REPLACED LEFT ENG PRSOV, ENG RUN VALVE OP CHECKS GOOD.SDR 2007UALA04338Blade · bent6TH STAGE HPC BLADE HAS BENT AND DISTORTED IMPACT DAMAGE 0.5 INCH FROM BLADE TIP. LENGTH OF DAMAGE 0.5 AND BEND IS .125 INCH.SDR HALA0700452Bleed Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - ATB - LEFT ENG BLEED VALVE CAME ON. DID QRH PROC, NO CHANGE DIVERTED TO SFO FOR MX. NO FURTHER PROBLEMS. (HPSOV LOCKED CLOSED SHORTING PLUG INSTALLED). OK TO CONTINUE PER C 36-11-2.SDR 2007UALA04337Blade · failedECM HAS DETECTED PARAMETERS SHIFT AT BOTH TAKEOFF AND CRUISE. ENGINE REPLACED. SHOP TEARDOWN REVEALED HEAVY HPC BLADE DAMAGE. THE DAMAGE WAS A RESULT OF FAILURE IN A 5TH STAGE DISK KNIFE EDGE. A 5-INCH SECTION OF THE FRONT KNIFE EDGE FRACTURED, CAUSING A 2-SDR HALA0700458Turbine Blades · damagedETOPS SIGNIFICANT SYSTEM, DURING BOROSCOPE INSP LOOKING THROUGH AP-11 ACCESS. PORT FOUND 2 STAGE HIGH STAGE PRESSURE TURBINE BLADE DAMAGE ON NR 2 ENG. ACCOMPLISHED ENGINE INSTALLATION IAW HAL M275-767 NR 2 ENGINE. OPS AND LEAK CHECK GOOD. OK FOR SERVICE. SDR 2007UALA04339Connector · out of adjustEMERGENCY EEL LIGHT TURN ON AND OFF AT SEATS 1AB. ADJUSTED PLUG AT POWER SUPPLY NEXT TO THE SEAT 1AB. CHECKED OK.
SDR 2007UALA04311Unknown · odorELECTRICAL BURNING ODOR IN MID GALLEY AREA AND AIRCRAFT RETURNED TO BLOCKS. INSP GALLEY AREA AND OVERHEAD AREA FOR EVIDENCE OF BURNING NO OBVIOUS SIGHT OF SMOKE OR BURNING. FIRE BRIGADE PERFORMED HEAT DECTECTOR EQUIPMENT NO SIGN FOUND.NO HISTORY () INSP CHILLSDR 2007UALA04269Pump · failedFLIGHT DIVERTED DUE TO LOSS OF RIGHT MAIN FUEL PUMPS. PUMP CONNECTORS WHERE CROSSED. ALSO FOUND FOUND RIGHT AFT BOOST PUMP CKT BK R OUT C371 .REPLACED BREAKER,FOUND WIRE ARCHING ACCOUNT OF SCREW CROSS THREADED. PERFORMED OPS CHECK.SDR 2007UALA04282Starter · faultySPARKS SEEN COMING FROM R ENG DURING START. REPLACED STARTER AND START VALVE. PERFORMED ENG CHK START AS PER JRH AND ALL OPS NOW NORMAL.
SDR 2007UALA04283Battery · faultyAPU WILL NOT START. BATTERY VOLTAGE 16 VOLTS. BATTERY VOLTAGE 16V, REPLACED BATTERY.SDR 2007UALA04271Warning Light · illuminatedCREW REPORT: FLAP-SLAT ELEC LWR EICAS MESSAGE APPEARS AT FLAP POS 5 THEN DISAPPEARS WHEN FLAPS > 20. REPLACED FLAP-SLAT ELECTRONICS UNIT. OPERATION OF FLAP SLAT SYSTEM NORMAL. NO FAULTS OR EICAS MESSAGES DISPLAYED.
SDR 2007UALA04248Toilet · inoperativeFOUR OUT OF EIGHT LAVS INOP THE 4 GOOD LAVS FLUSH CLEAR FLUID. *S/D* AFTER 10 DAYS & CONSIDERABLE TROUBLESHOOTING & TANK SERVICING, DETERMINED LEFT AFT TOILET HAD VALVE PROBLEM WITH CONTINUOUS FLUSHING PROBLEM. REPLACED TOILET ASSEMBLY. LAV SYSTEM CHECKEDSDR HALA0700448Starter · failedETOPS SIGNIFICANT SYSTEM, UPON STARTING THE RIGHT ENGINE, EVERYTHING APPEARED NORMAL AT 26 PERCENT N2. INTRODUCE FUEL, FUEL FLOW NORMAL GOOD LIGHT OFF, N1 READING. AT ABOUT 1 MIN AND 45 SEC N2 STARTING TO DECREASE TO 22% N2. DISCONTINUE START MOTORED FOR 30
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