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 2008UALA05914Light · inoperativeEEL LIGHT BARS INOP AT MID LEFT AND RIGHT LAVS.SDR 2008UALA05915Light · inoperativeEEL LIGHT BAR AT RT FWD G2 GALLEY IS INOP.SDR 2008UALA05916Attach Angle · crackedNR 2 STRUT AFT STRUT BULKHEAD INBOARD ATTACH ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED ANGLE. FABRICATED & INSTALLED NEW ANGLE.SDR 2008UALA05917Spring · weakDOOR R2 DOOR DEPLOYMENT BAR GAS SPRING WEAK. SPRING FOUND INADEQUATE. REPLACED GAS SPRING. OPS OKAY.SDR 2008UALA05918Spring · weakDOOR R1 DEPLOYMENT BAR GAS SPRING WEAK. GAS SPRING DEFECTIVE. REPLACED DEPLOYMENT BAR GAS SPRING. OP CHECKS OKAY.SDR 2008UALA05919Connector · arcedCENTER SYS NR 1 ACMP CONNECTOR D482 SHOWS SIGNS OF ARCHING AND HAS A RECESSED PIN. REPLACED CONNECTOR D482P. OPS CHECKS GOOD.SDR 2008UALA05885Aspirator · leakingLEAKY ASPIRATOR. LEAKING AROUND BARREL SEAL. REPLACED ASPIRATOR.SDR 2008UALA05896Skin · crackedNR 2 STRUT, ONBOARD AFT SKIN CRACKED AT PANEL CUTOUT RADIUS, FORWARD OF AFT BULKHEAD. MAJOR REPAIR ACCOMPLISHED. STOP-DRILLED CRACK. VERIFIED HFEC. INSTALLED -1 & -3 DOUBLERS.SDR 2008UALA05806Pump · damagedL HYD SYS MAINT STATUS MESSAGE. FOUND L EDP SHAFT SHEARED, REPLACED PUMP, OKAY.SDR DL76L081206Eec · malfunctionedAFTER LEFT ENG START, LT ENG CONTROL STATUS MSG APPEARED FOLLOWED BY LT ENG C2 STATUS MSG. PERFORMED LT ENG PIMU READOUT. FOUND BITE MSG CH-A LOST POWER AND CH-B UNIT FAIL. CYCLED EEC C/B AND PIMU RESET. ALL MESSAGES CLEARED. RAN LT ENG IN DLE AND NO FAULSDR DL76P081209Engine · bird ingestionDURING T/O HAD BIRDSTRIKE ON LEFT SIDE OF AIRCRAFT. RETURNED MCO. MTC FOUND DENT IN FUSELAGE FWD OF LEFT PITOT PROBES. AOA VANE SHEARED OFF. PITOT PROBES IMPACTED. LEFT ENGINE HAS 2 FAN BLADES BENT OUT OF LIMITS AND SOME MINOR ACOUSTICAL LINER DAMAGED. VSDR 2008UALA05823Latch · corrodedLT OVERWING COMPARTMENT DOOR LATCHES (4 EA) HAS CORROSION AND EXCESSIVE WEAR MARKS. REPLACED 4 LATCHES AT LT OVERWING SLIDE COMPARTMENT DOOR. INSPECTED AND OPS CHECKED GOOD.SDR DL76L081207Rotor · damagedRT ENG EEC MSG, AUTO THROTTLES INOP, RT CTR FUEL PUMP, NO RT ENG N2 DISPLAY. ALL OCCURRED INFLT EN ROUTE TO CVG. FOUND PMA ROTOR DAMAGED DUE TO DRIVE ASSY FAILURE. BEARING PIECES MISSING AND PRESUMED TO HAVE ENTERED THE GEARBOX WHEN BEARING FAILED. METAL OSDR 2008UALA05802Starter · malfunctionedL ENG START VALVE WON'T OPEN. START VALVE MALFUNCTIONED. REPLACED STARTER AND STARTER VALVE. ALL CHK NORMAL.SDR 2008UALA05815Cover · missingEMERGENCY LIGHTS AT SEAT 14B COVERED BY DUCT TAPE REPAIR IN AREA. FOUND COVER IS MISSING. REPLACED EMERGENCY LIGHT TRACK COVER. LIGHTS OPS CHECK NORMAL.SDR 2008UALA05772Fire Loop · faultyL ENG FIRE LOOP 1 ON STATUS PAGE AND FIRE-OVHT SYS ON EICAS, ABORTED TAKEOFF AT 63 KNOTS. RESISTANCE HIGH AT CARD M681 PINS 19 & 20. CHECKED ENG 1 LOOPS . LOOPS OK. FOUND BAD LUG ON FWD BOTTOM LOOP. REPLACED LUG. RESISTANCE CHECKS NORMAL. SYSTEM TESTED OK.SDR 2008UALA05842Panel · splitRT WING LOWER PANEL 651VB (REAR OF LDG GEAR) HAS 5.5 INCH SPLIT IN FWD EDGE. REPAIRED T/E PANEL ON R&R. COMPLETED GEAR SWINGS FOR ADEQUATE CLEARANCE BTWN RIGHT GEAR FIXED STRUT DOOR & LWR WING PANEL.
SDR 2008UALA05754Inlet Bullet · damagedCRACK AND DELAMINATION FOUND ON INLET CONE (SPINNER) ON RT ENGINE. SPINNER FOUND CRACKED/DELAMINATED. ASSY SENT TO SHOP. REPLACED INLET CONE. NO FAN BLADE DAMAGE FOUND. AFTER VERIFICATION FLIGHT, A/C DETERMINED OK FOR SERVICE.SDR DALA1100880180Attach Fitting · crackedPYLON WING TO STRUT ATTACH FITTINGS, NR 2 PYLON FWD UPPER SPAR BUSHING. REPAIRED IAW ERA 470658-14.SDR 2008UALA05755Light · disconnectedEMERGENCY EXIT LIGHTING STRIP DISCONNECTED NEAR SEATS 10E. LIGHT STRIP FOUND DISCONNECTED. SECURED LOOSE LIGHT STRIP. OP CHECKS OKAY.SDR 2008UALA05731Actuator · leakingNR 2 ENG, TURBINE CASE COOLING ACTUATOR IS LEAKING FUEL AT A RATE OF 30 DROPS PER MINUTE.SDR UALA2008111305731Fmu · faultyNR 2 ENG, TURBINE CASE COOLING ACTUATOR IS LEAKING FUEL AT A RATE OF 30 DROPS PER MINUTE. FOUND CHUNKS OF RUBBER COVERING 10 PERCENT OF STRAINER. PERHAPS O-RING MATERIAL. NO METAL FOUND. CLEANED AND REINSTALLED STRAINER. COMPLETED INSP OF STRAINER INSTALLSDR 2008UALA05671Torque Box · corrodedAFT PIT, PITTING CORROSION IN TOP SURFACE OF TORQUE BOX STA 1345, RBL 8. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS. REMOVED WEB. FABRICATED & INSTALLED NEW WEB.SDR 2008UALA05672Web · crackedNR 2 PYLON NAC STA 180 (APPROX) RIGHT SIDE, UPPER WEB CRACKED INTO RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. REMOVED OLD DOUBLER. INSTALLED NEW DOUBLER REPAIR.SDR 2008UALA05673Shear Tie · corrodedBULK CARGO COMPARTMENT AT STA 1562 BETWEEN STR 39R AND 39L, SHEAR TIE HAS CORROSION AROUND DRAIN HOLE AFT SIDE. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE.SDR 2008UALA05681Feeder Cable · damagedEMERGENCY ESCAPE PATH LIGHTING BESIDE 10FG WON'T COME ON DURING EMERGENCY LIGHT TEST. CABLE REPAIRED USING SPLICE CRIMPER METHOD. IT NOW OPS SATISFACTORY.SDR DL76P081162Door · missingFOUND NR 2 ENG INBD AFT NACELLE STRUT ACCESS DOOR MISSING. FORWARD TO MCO PER CDL 54-53-02.SDR DL738081163Valve · out of toleranceLEFT OUTBD TIRE BURST AFTER LANDING. TROUBLESHOOT ANTI-SKID SYSTEM FOUND LEFT OUTBD ANTI-SKID NORMAL VALVE RESISTANCE OUT OF RANGE PER FIM 32-42-00-810-804. BITE A/S BOX FOUND VLV1 WITH SP-CO-VI. T/S PER FIM 32-42-00-810-804 FOUND NR 1 NORMAL A/S SDR 2008UALA05637Bottle · lowCREW OXYGEN PRESSURE BELOW 3SVC REQUIRED LIMITS (1.620 PSI). UNIT FOUND UNDERSERVICED. SERVICED O2 TO FULL. OPS CHECK GOOD.
SDR DL76G081164Isolation Valve · malfunctionedRT BLEED ISOLATION VALVE LIGHT CAME ON DURING TAXI. RETURNED TO GATE PER MAINTENANCE REQUEST. REMOVED AND REPLACED RIGHT ISOLATION VALVE PER AMM. OPS CHECK OK.SDR 2008UALA05613Shear Tie · corrodedAFT PIT AT STA 1219, LBL 4 - RBL 4, CORROSION ON ANGLE AT FRAME ATTACH TO SKIN. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SHEAR TIE.SDR 2008UALA05614Frame · damagedAFT PIT STA 1197+66 FRAME CAP HAS FLAKED PAINT AND LIGHT SURFACE CORROSION FROM LBL 48 - RBL 10. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW FRAME CAP.SDR 2008UALA05615Structure · corrodedAFT PIT, UPPER CHORD FOR WEB AT STR 33L CORRODED ON THE LOWER SURFACE. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW ANGLE.SDR 2008UALA05616Structure · corrodedAFT PIT CORROSION ON FRAME CAP LOWER SURFACE AT BS 1197+110 AND STR 33L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED "T" CAP.SDR 2008UALA05617Lamp · inoperativeAFT RIGHT EMERGENCY EXIT LIGHT DOOR HANDLE IS INOP. RELAMPED. OPS CHECKS GOOD.SDR 2008UALA05618Connector · damagedRIGHT ACMP CONNECTOR D486P, PIN 'B' IS BURNED, SHOWS SIGNS OF ARCING. REPLACED RIGHT ACMP CONNECTOR D486P PIN "B". OPS CHKS NORMAL.SDR 2008UALA05619Angle · corrodedAFT PIT STA 1394, BL 0, CORROSION ON ANGLE AT FRAME ATTACH TO SKIN. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE.SDR 2008UALA05620Seat Track · corrodedCORROSION ON SHORT SEAT TRACK AT BS 795, LBL 62. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SEAT TRACK SECTION.SDR 2008UALA05640Oil Filter · faultyR OIL FILTER BYPASS LIGHT ON FOR 1 MIN AFTER START. R OIL FILTER STATUS MSG REMAINS ON. REPLACED MAIN OIL FILTER. LEAK CHECKS OK.
SDR DL76P081154Starter · failedNR 1 ENG NO START NO ROTATION, FOUND STARTED AT FAULT. REPLACED STARTER.SDR 2008UALA05587Fmu · malfunctionedRIGHT ENGINE START AT 51% N2 AFTER STARTER CUTOUT RIGHT OIL P EICAS CAME ON. ELECTED TO SHUT DOWN. FOUND FAULTY FUEL METERING UNIT. REMOVED AND REPLACED FMU AND RAN. ENG START NORMAL ALL INDICATIONS & OIL PRESSURE NORMAL.
SDR DL76L081155Switch · failedEMERGENCY LIGHTS WILL NOT TURN OFF. REPLACED EMERGENCY LIGHT PANEL DAL P/N 331702405.SDR 2008UALA05576Control Unit · failedEICAS MSG (L,R) UTIL BUSS OFF DISPLAYED. UTILITY BUSS OFF LGT ILLUM. SYS FAILED TO RESET. BUSS PCU FAILURE. REPLACED BUSS POWER CONTROL UNIT.TESTS OKAY. RAN BOTH ENGINES & RAN ALL ELECTRICAL POWER SYSTEMS USING ALT BUSSES ALL INDICATION & OPS NORMAL.SDR 2008UALA05570Web · crackedNR 1 PYLON STA 156 WEB AT OUTBOARD DRAIN HOLE IS CRACKED, MIGRATED BEYOND EXISTING STOP DRILL. MAJOR REPAIR ACCOMPLISHED. FOUND 2 CRACKS AT INBOARD DRAIN HOLE. STOP DRILLED CRACKS. FABRICATED & INSTALLED A DOUBLER REPAIR.SDR 2008UALA05564Mechanism · underservicedEXIT DOOR 2R ARMING LEVER & BUTTON HARD TO OPERATE. FOUND MECHANISM UNDERSERVICED. CLEANED & LUBED ARMING MECHANISM. OPS CHECKED NORMAL.SDR 2008UALA05556Stiffener · crackedSTA 246 FLOORBEAM FWD SIDE VERT STIFFENER CRACKED AT LBL 26. MAJOR REPAIR ACCOMPLISHED. REMOVED AND INSTALLED NEW STIFFENER.SDR 2008UALA05557Floorbeam · corrodedMAIN CABIN FLOORBEAM T-CAP CORRODED UNDER STEEL SUBFLOOR AT BS 1518 AT BL 0. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED T-CAP SECTION. FABRICATED AND INSTALLED A NEW T-CHORD, SPLICE ANGLES & SPLICE STRAPS.SDR 2008UALA05558Floorbeam · corrodedMAIN CABIN FLOORBEAM T-CAP CORRODED AT BS 1502 AND LBL 28. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF T-CAP. FABRICATED A-1 AND -2 REPAIR ANGLES, -3 STRAP AND 4 EACH SHIM AND INSTALLED.
SDR 2008UALA05559Floorbeam · corrodedCABIN FLOORBEAM FRAME CORRODED STA 284 RBL 17. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF FLOORBEAM TEE AND FABRICATED A NEW TEE REPAIR ANGLE. DAMAGED T-CAP REMOVED BETWEEN RBL 17 - RBL 22 AND WL 208.
SDR 2008UALA05605Wire · damagedFWD CARGO COMP BELOW FLOOR-EQUIP COOLING SUPPLY AIR OVERHEAT SWITCH CONNECTOR WIRE HAS INSULATOR DAMAGE AND BARE CONDUCTOR EXPOSED 19 INCHES UPSTREAM OF CONNECTOR D00644.
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