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 UALA2009041501090Frame · corrodedAFT CARGO COMPARTMENT FRAME T-CAP, LOWER SURFACE CORRODED AT NUT PLATE, BS 1197+132, RBL 45, S-33R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED T-CAP. INSTALLED NEW T-CAP.SDR HALA2009041100140Fan Blade · nickedETOPS SIGNIFICANT SYSTEM, FOUND NICK ON NR 2 ENGINE 1ST STAGE FAN BLADE. BLENDED AREA, WITHIN LIMITS PER AMM 72-31-02, EDDY CURRENT ACCOMPLISHED.SDR HALA2009041100143Connector · damagedETOPS SIGNIFICANT SYSTEM, ON NR 2 ENG FOUND CONNECTOR TO FUEL FILTER BYPASS SWITCH DAMAGE. REPLACED CONNECTOR D10994 PER AMM 71-51-00. FUNCTIONAL TEST GOOD PER AMM 71-00-00.SDR UALA2009041301048Floor Support · corrodedAFT PIT FLOOR SUPPORT HAS CORROSION AROUND NUT PLATES STA 1219, LBL 20 TO LBL 24. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW UPPER CHORD (P/N 146T1060-2).SDR UALA2009041001035Shear Tie · corrodedAFT BULK COMPARTMENT SHEAR TIE CORRODED FWD AND AFT SIDE BS 1562, BL 0. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW SHEAR TIE AND INSTALLED.SDR UALA2009041001043Panel · damagedRT WING LOWER WING FIXED TRAILING EDGE PANEL 651VB HAS A 1.5 INCH CRACK RUNNING FORE TO AFT. CRACK IS LOCATED 5.5 INCHES FROM INNER EDGE OF PANEL AND 0.75 INCHES OUTBOARD OF NEAREST FASTENER. REMOVED TRAILING EDGE RT WING PANEL. ROUTED PANEL TO SHOP 273. PSDR HALA2009040800131Idg · faultedETOPS SIGNIFICANT SYSTEM, RT GEN DRIVE LIGHT FAILED TO ILLUMINATE UPON ENGINE SHUT DOWN POST MAINTENANCE ENGINE RUN. REPLACED RIGHT IDG IAW AMM 24-11-01-404 AND HAL WORK CARD 767-3-405001. OPERATIONAL TEST OK. LEAK CHECK OK.SDR UALA2009040901022Light · inoperativeEXTERIOR EMERGENCY LIGHT AT DOOR 2L INOP. REPLACED LAMP, CHECKED OKAY.SDR UALA2009040901023Light · inoperativeLT EXTERIOR EMERGENCY LIGHT AFT OF TRAILING EDGE WING INOP. RELAMPED EMERGENCY LIGHT, CHECKED OKAY.SDR UALA2009040901026Battery · dischargedLT EXTERIOR EMERGENCY LIGHT, (2ND FROM TRAILING EDGE OF WING) IS INOP. REPLACED BATTERY ASSY, OPS CHECKED OKAY.SDR UALA2009040901027Connector · defectiveEMERGENCY LIGHTS FROM ROW 27JK-34JK INOP. FOUND CONNECTOR CHECK BAD FOR SEAT 32JK. PIN PUSHED BACK AND WILL NOT LOCK. DISCONNECTED CONNECTOR CK AT SEAT 32JK. ONE LIGHT AT SEAT 32JK WILL BE INOP. ALL OTHER SYSTEM OPS OK.SDR UALA2009040901028Shear Tie · corrodedAFT CARGO COMPARTMENT, BILGE ANGLE SHEAR TIE, CORRODED BS 1241, RBL 0. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SHEAR TIE.SDR UALA2009040901029Shear Tie · corrodedAFT PIT STA 1219, ATTACH ANGLE, SHEAR TIE, HAS CORROSION BETWEEN S-39L AND S-39R BY- 85625. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SHEAR TIE.SDR UALA2009040600988Monitor · faultyENG VIBE BITE STATUS MSG WILL NOT CLEAR. REPLACED ENGINE VIBRATION MONITOR UNIT, RAN BOTH ENGINES. INDICATIONS ARE NORMAL.SDR UALA2009040700993Engine · surgesLOUD VIBRATION ON AIRFRAME AT 1000 FT ON FINAL RIGHT ENGINE INDICATIONS DEGRADED SAMC. ENG 2 S/N 724181, EHM PAGE WRITER MESSAGES FLT 964-05 APR SHOW ENG 2 BOTH CHANNELS DETECTED SURGE, REF AMM-FIM 71-05-00 PG 116 SURGE TROUBLE SHOOTING FOR RING CASE ENGINES.SDR ANCF2009040500040Drain Line · leakingRIGHT ENGINE HIGH FUEL FLOW. OTHER ENG PARAMETERS NORM. FUEL QTY DECREASE DOES NOT CONFIRM HIGH FUEL FLOW, THEN GOES ZERO. RT ENG OIL PRESS WENT TO ZERO, ALL QTY WAS ZERO. RT ENG SHUTDOWN. ENG WINDMILLED WITH OIL PRESS LESS THAN 40 PSI FOR 50 MIN OIL QTY SDR UALA2009040600961Floorbeam · corrodedCORROSION CABIN FLOORBEAM CAP AT STA 287, AT RBL 15. MAJOR REPAIR ACCOMPLISHED: REPLACED PREVIOUS DOUBLER REPAIR. INSTALLED NEW T-CAP SECTION AND SPLICES.SDR UALA2009040600964Shear Tie · corrodedAFT BULK CARGO COMPARTMENT SHEAR TIE CORRODED BS 1540, BL 0. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SHEAR TIE.SDR UALA2009040600989Gauge · leakingLOW PRESSURE. LEAKING FROM TOP OF GAUGE FAC THAT WAS BENT. REPLACED GAUGE.SDR UALA2009040600990O-Ring · leakingLOW PRESSURE. LEAKING AT GAUGE. REMOVED & REPLACED GAUGE O-RING.SDR UALA2009040300950Shear Tie · corrodedEVIDENCE OF CORROSION AT LOWER AFT ATTACH POINT OF BULK COMPARTMENT FLOOR SUPPORT FRAME BS 1540, RBL 39 TO RBL 38. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SHEAR TIE.SDR UALA2009040300951Shear Tie · corrodedAFT BULK CARGO COMPARTMENT SHEAR TIE CORRODED BS 1540, STR 38L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SHEAR TIE.SDR UALA2009040300952Slide · unserviceableLT OVERWING SLIDE FWD LACING CLIP BROKEN OFF AT THE UNLACE BAR. SLIDE NOT LACED AT POINT. REPLACED SLIDE ON SNR 6195 04016.SDR UALA2009040100939Tube · leakingFUEL DRAINING FROM RIGHT WING DRY BAY DRAIN AGAIN AFTER ACFT HAS BEEN REFUELED. FOUND RT NR 4 SLAT OUTBOARD TRACK HOUSING CRACKED. DRY BAYS NOT LEAKING. REMOVED NR 9 SLAT O/B HOUSING. REPLACEMENT ON AOG ALONG WITH SELF SEALING NUTS. WELDED DRAIN TUBE ASSYSDR UALA2009040200940Engine · malfunctionedSMOKE IN CABIN. FLIGHT DIVERTED. ACCOMPLISHED FLIGHT CREW DEBRIEF: R ENG EGT RED, EXCD PAGE 713 FOR 4.14. EICAS MSG R ENG SURGE, R PIMU, OIL 19QTS. LWR CASE AREA OIL WET. NOT NORMAL SHUT DOWN, ENG VIBRATION FELT WITH GRINDING NOISE AND SMOKE IN CABIN. ESDR UALA2009033100934Pump · faultyAFTER 3 HRS IN CRUISE RT FUEL QTY 2000LBS LWR THAN LT QTY. REPLACE CTR RT OVERRIDE PUMP REF RT FUEL TANK QUANTITY IMBALANCE. REPLACED CTR RT OVERRIDE PUMP. NEEDS LEAK AND OPS TEST. ACCOMPLISHED OVERRIDE JETTISON OP'S CHECK. LEAK CHECK GOOD.SDR UALA2009033100936Aspirator · leakingSLIDE ASPIRATOR BARREL LEAKING. CAUSE IS UNKNOWN. REPLACED ASPIRATOR.SDR UALA2009040100938Cable · faultyLT AFT ESCAPE SLIDE STEP AFT CABLE IS WORN AND HAS A KNOT IN CABLE. *S/D* REPLACED AFT STEP CABLE.SDR HALA2009032600107Warning Message · false activationETOPS SIGNIFICANT SYSTEM, MX LEVEL EICAS MSG 'IDG OUT TEMP' DISPLAYED, AT TOP OF CLIMB IDG OUT- L63 DEGRESS, R95 DEGREES. IDG RISE- L9, R9. PERFORMED FIM 24-20-00 FIG 103. BITE CHECK NO FAULTS NOTED. OK FOR SERVICE.SDR HALA2009032500105Filter · contaminatedETOPS SIGNIFICANT SYSTEM, L ENG OIL FILTER LT ON AT TAXI. BTB - C/W FIM 79-35-00 NO CONTAMINATION FOUND IN FILTER OR CHIP DETECTORS. REPLACED MAIN OIL FILTER PER AMM 79-21-05 LEAK CK GOOD, COWL CLOSED AND SECURED.SDR HALA2009032500106Housing · leakingETOPS SIGNIFICANT SYSTEM, FOUND OIL ALL OVER NR 2 ENG COWL. NEED TO CHECK FOR LEAKS. FOUND OIL LEAK AT NR 2 ENG NR 3 BEARING LAST CHANCE OIL STRAINER HOUSING. REMOVED AND REPLACED WORN PACKING. LEAK CHECK GOOD. REF AMM 29-21-16-242.SDR HALA2009032300097Idg · making metalETOPS SIGNIFICANT SYSTEM, ON DURING NR 2 ENGINE EXTERNAL INSPECTION FOUND NR 2 IDG DPI POPPED. INSPECTED NR 2 IDG SCAVENGE FILTER AND IGD OIL FOUND METAL PARTICLES. REMOVED NR 2 IDG PER TASK 767-3-405001. INSTALLATION AND LEAK PENDING (2823692). REMOVED ANSDR HALA2009032300100Warning Message · false activationETOPS SIGNIFICANT SYSTEM, EICAS MSG L ENG CONTROL AND L ENG EEC C1 AFTER LANDING. T/S PER FIM 73-21-00 FIG 112 LT ENG CONTROL EICAS MSG PIMU ERASED, ENG RAN NO MSG EICAS OR PIMU MSG OK FOR SERVICE. REF TO LOGPAGE 301032 NR 87 FOR LT ENG EEC C1 DEFERRAL.SDR UALA2009032300869Socket · shortedFOUND AFT LEFT LAV DOME SOCKET SHORTED, REMOVED POWER WIRE AND SECURED. FOUND AFT LEFT LAV DOME SOCKET SHORTED, REMOVED POWER WIRE AND SECURED. NEEDS SOCKET, NOT STOCKED ORD. REPLACED LIGHT SOCKET, OP CHECKED OKAY.SDR UALA2009032300872Shutoff Valve · faultyRIGHT ENG BLEED LIGHT & RT ENG HPSOV EICAS MSG DURING DESCENT WITH ENG BLEED SW ON & ENGINE RUNNING. REPLACED HPSOV.SDR UALA2009032300863Hydraulic Line · leakingNR 1 ENG, OIL DRIPPING FROM LARGE DRAIN TUBE BOTTOM OF REVERSER COWL. FOUND EVIDENCE OF ACTIVE HYD LEAK INSIDE NR 1 PYLON ACCESS PLATE RT OF PYLON. FOUND TORQUE OF HYD B-NUTS AT INSIDE OF DISCONNECT PANEL OK. APPEARS TO BE COMING FROM ABOVE AND AFT OF ACCESSDR UALA2009031700812Radar · inoperativeWEATHER RADAR INOP. RTFL.SDR UALA2009031800829Relay · faultyLEFT ENG P2-T2 PROBE HEAT CH 'A' AND CH 'B' FAULTED ON LEFT ENG PIMU. REPLACED NR 1 ENG EEC ALTERNATOR. OP'S AND LEAK CHECKED GOOD. HOWEVER, IT WAS NO HELP FOR PROBE HEAT MESSAGE. REPLACED K648, NO HELP. REPLACED K4 02, SYSTEM CHECKS GOOD.SDR DL76L090442Boss · strippedDURING SERVICE CHECK IGNITOR REPLACEMENT FOUND IGNITOR BOSS STRIPPED IN ENGINE CASE. MACHINE SHOP UNABLE TO REPAIR. REPLACED NUMBER ONE ENGINE.SDR DL76L090445Starter · inoperativeNO N2 ROTATION DURING RIGHT ENGINE START UP. RT ENGINE STARTER WAS REPLACED IAW AMM 80-11-01-404-014-N00 80-11-01-404-014-N00. STARTER SERVICED IAW AMM 12-13-02 PB301. DRY MOTORING PERFORMED AMM 71-00-00/201 N2 UP TO 26 PERCENT. LEAK CHECK OK.SDR UALA2009031000738Feeder Cable · deterioratedNR 1 ENGINE GENERATOR FEEDERS ARE DETERIORATED AND RUBBER FEED THRU GROMMET IS DETERIORATED. REPLACED FEEDERS PER BSWPM 20-30-13 AND 20-30-11 AND 20-10-13. ALSO REPLACED RUBBER GROMMET PER BSWPM 20-10-13 AND SRM 51-40-02, OPS CHECKS GOOD.SDR CA090309007Seat · jammed(CAN) DURING CRUISE, THE CAPT`S SEAT BECAME JAMMED IN THE FULL FWD POSITION (THEY HAD DIFFICULTY WITH THE MOTOR, AND THERE WAS NO ELECTRICAL REVERSE). A PHONE PATCH WAS ESTABLISHED WITH MX CONTROL. THE FIRE AXE WAS USED TO DISLODGE THE SEAT AND THE FLIGHT CONTSDR UALA200903100073AFeeder Cable · deterioratedNR 1 ENGINE GENERATOR FEEDERS ARE DETERIORATED AND RUBBER FEED THRU GROMMET IS DETERIORATED. REPLACED FEEDERS PER BSWPM 20-30-13 AND 20-30-11 AND 20-10-13. ALSO REPLACED RUBBER GROMMET PER BSWPM 20-10-13 AND SRM51-40-02, OPS CHECKS GOOD.SDR UALA2009031000727Structure · crackedCRACK FOUND ON FWD RT OUTER CHORD OUTBOARD FLANGE AT STA 1809 BULKHEAD BELOW TENSION FITTING AT S12AR. MAJOR REPAIR ACCOMPLISHED. FLANGE REPAIRED. CUT OUT DAMAGED SECTION AND INSTALLED NEW SECTION OF CHORD AND STRAP REPAIR.SDR DL76L090374Controller · malfunctionedLEFT BLEED NO OUTPUT PRESS UNABLE TO CROSSBLEED START ENG. FOUND LT ENG PRV INOP SWAPPED WITH HPSOV FWD TO MCO PER MEL 36-11-02 HPSOV LOCKED CLOSED. REMOVED AND REPLACED PRV CONTROLLER IAW MM.SDR UALA2009030400713Floorbeam · corrodedFWD PIT STA 65+121 TOP CAP OF PIT FLOOR STRUCTURE CORRODED APPROX LBL 16. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF T-CAP, FABRICATED & INSTALLED REPLACEMENT T-CAP CHORD.SDR UALA2009031000713Floorbeam · corrodedFWD PIT STA 65+121 TOP CAP OF PIT FLOOR STRUCTURE CORRODED APPROX LBL 16. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF T-CAP, FABRICATED & INSTALLED REPLACEMENT T-CAP CHORD.SDR UALA2009030300694Skin · damagedFOUND LIGHTNING STRIKE EXIT DAMAGE ON RUDDER TRAILING EDGE. DAMAGE IS LOCATED APPROXIMATELY 8 FEET UP FROM LOWER EDGE. DAMAGE IS A SEMI CIRCULAR DELAMINATED ARE MEASURING 2 INCH BY 1.25 INCH, CONTAINED IN CENTER IS A .75 BY 1.25 INCH AREA OF EXPOSED AND DAMASDR UALA2009030300698Lens · brokenFUSELAGE EXTERIOR EMERGENCY LIGHT LENS BROKEN RT SIDE APPROX 24 INCHES FWD OF AFT PIT DOOR. REMOVED AND REPLACED EMERGENCY LIGHT LENS.SDR UALA2009030400711Oxygen System · low pressureCREW OXYGEN PRESSURE BELOW 3SVC LIMITS (1.610 PSI). SERVICED CREW OXYGEN SYSTEM. OP CHECKS OKAY.
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