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 DL76L060221Engine · damagedFRM CODE SENT 770323020 RIGHT ENG PRIMARY N2 INDICATOR READS INOP. FOUND PMA DAMAGE. REPLACED ENGINE.SDR 2006UALA00571Generator · unknownRETURNED TO IAD DUE TO NR 2 GENERATOR PROBLEM. AFTER EVENT, INITIAL IDG SERVICE AND ENGINE RUN PRODUCED NO FAULTS OR LEAKAGE, AND MONITORING AC REVEALED NO DUPLICATE EVENTS. INDICATION OF LOW OIL PRESSURE FROM INTERNAL CHARGE PRESSURE SWITCH CLOSURE MOST LIKESDR 2006UALA00604Toilet · malfunctionedRETURNED TO IAD DUE TO A WATER LEAK IN THE MAIN CABIN. TOILET OVERFLOWED AND WATER KEPT RUNNING UNTIL CREW CLOSED LAV WATER VALVE.SDR DL76L060189Idg · malfunctionedRIGHT GENERATOR DRIVE LIGHT ILLUMINATED DISCONNECTED IDG IN FLT. REPLACED IDG.SDR 2006UALA00469Angle · crackedCLOSEOUT ANGLE BELOW MID SPAR FITTINGS OF NR 2 PYLON HAS CRACKS FROM INBOARD AND OUTBOARD ENDS. INBD AND OUTBD ENDS ON CLOSEOUT ANGLE BELOW MID SPAR FITTINGS OF NR 2 PYLON WERE FOUND CRACKED. THE CLOSEOUT ANGLE WAS REPLACED USING 767-300 SRM 51-40-02.SDR 2006UALA00470Stiffener · gougedLT WING STIFFENER GOUGED BEYOND LIMITS AT WS 825 REAR SPAR. THE LEFT WING STIFFENER, P/N 112T1237-1, WAS FOUND GOUGED BEYOND LIMITS AT WS 825 REAR SPAR. NO DAMAGE WAS REPORTED ON THE ADJACENT STRUCTURES. THEREFORE, THE GOUGED WAS LIKELY CAUSED BY FOD. REPLSDR 2006UALA00471Fitting · crackedNR 2 PYLON MIDSPAR FITTING LOWER TANG AT INBOARD CLOSEOUT ANGLE HAS 2 EACH CRACKS COMING OUT OF THE INBOARD BOLT HOLE. 2 CRACKS EMANATING FROM INBD BOLT HOLE OF CLOSEOUT ANGLE INSTALLED OVER NR 2 PYLON MIDSPAR FITTING LOWER TANG WAS FOUND. THE CLOSEOUT ANGLE SDR 2006UALA00468Attach Fitting · misdrilledRIGHT WING INBOARD AILERON, INBOARD SECTION LEADING EDGE ATTACH FITTING MISDRILLED. S/D* THE SUBJECT FITTING WAS MISDRILLED DURING INSTALLATION. REPAIRED PER TIMCO REO-G11452.SDR DL76L060176Engine · smokeSMOKE IN FWD HALF OF CABIN AND SOME IN COCKPIT. PERFORMED ENGINE RUN/ DUCT BURNOUT PER MM, NO TROUBLE FOUND. INSPECTED E/E, NO TROUBLE FOUND.SDR 2006UALA00452Failsafe · corrodedCORROSION ON STA 1562 FAIL-SAFE, P/N 146T1223-30, BETWEEN STR 39L & 39R. REPAIRED BL 0 AREA CORROSION AT STA 1562 FAILSAFE CHORD WITH A REPAIR ANGLE AND FILLER PER TIMCO REO(EVA) G11428 AND UA EVA 60127. REPAIR IS FAA APPROVED AND PERMANENT.SDR DL76L060170Valve · failedTAKEOFF ABORTED AT 80 KNOTS DUE TO RT ENG PRV CAUTION WITH A RIGHT ENG BLEED LIGHT. BRAKE TEMPS RANGE FROM A 3 TO A 7 ON RIGHT REAR BRAKE ASSY. FWD TO MCO AND PLACARD PER MEL M36-11-02. PERFORMED BITE CHECK OF BLEED AIR MODULE. NO FAULTS. LOCKED OUT RT ENSDR 2006UALA00448Bulkhead · crackedBS 1809 BULKHEAD RT SIDE, FWD OUTER CHORD, INBD FLANGE HAS A CRACK COMING OUT OF THE FASTENER HOLE. DAMAGE FOUND AS A RESULT OF ROUTINE INSPECTION, MANDATED PER AD 2005-11-02. REPAIRED PER AD REQUIREMENTS.SDR 2006UALA00397Seat Track · brokenMAIN SEAT TRACK OUTBD LT SIDE STA 786-808, LBL 88 INBD NODES BROKEN OFF FROM TRACK. DAMAGED SEAT TRACK REMOVED/REPLACED PER SRM.SDR 2006UALA00398Hinge Fitting · crackedLEFT INBD FLAP-CENTER HINGE FITTING CRACKED ON INBD AND OTBD FLANGES. THE SUBJECT HINGE FITTING WAS FOUND CRACKED ON THE INBOARD AND OUTBOARD FLANGE. REPAIRED PER 767-300 STRUCTURAL REPAIR MANUAL 57-53-02.SDR DL76L060161Engine · leakingINFLIGHT OIL QTY WENT TO 0 WITH DECREASE PRESS AND INCREASE TEMP, OIL PRESS IN RED, ENGINE SHUTDOWN. TIGHTENED TUBE B-NUT ON TOP OF FUEL /OIL HEAT EXCHANGER. PERFORMED NECESSARY INSPECTIONSSDR 2006UALA00353Floorbeam · corrodedAFT PIT FLOORBEAM AT STA 1197 BTWN STR 33L- 33R IS CORRODED TOP AND BOTTOM OF T-CAP, SEVERAL LOCATIONS. CORRODED FLOORBEAM REPAIRED PER SRM. DAMAGE FOUND BY ROUTINE INSPECTION.SDR 2006UALA00354Floorbeam · corrodedAFT PIT FLOORBEAM AT STA 1197+132 BETWEEN STR 33R TO 33L IS CORRODED AT 6 LOCATIONS. CORRODED FLOORBEAM REPAIRED PER SRM. DAMAGE FOUND BY ROUTINE INSPECTION.SDR CA060301002Carrier Assy · burnedGND CREW REPORTED BRAKE FIRE ON RT MAIN GEAR AFTER SHUTDOWN. FIRE EXTINGUISHED. FOUND NR 4 BRAKE PISTONS WORN THROUGH STATORS AND INTO THE ROTORS. AXLE INSPECTED AS PER AMM 05-51-15-212-001 AND 05-51-14 PB201. AXLE OK. BRAKE REPLACED AS PER JC 6-232A. WHSDR 2006UALA00419Flap Track · shearedFRACTURE OF LT OTBD T/E FLAP DETECTION CONTROL TRACK. LT OTBD T/E FLAP DEFLECTION CONTROL TRACK IS COMPLETELY SHEARED JUST AFT OF TIE ROD SUPPORT LUG. PER BOEING, THIS TYPE OF INCIDENT IS UNUSUAL, BUT NOT UNCOMMON. BOEING HAS RELEASE SB 767-27-0184 TO EXAMISDR 2006UALA00541Track · separatedLEFT OUTBOARD FLAP DEFLECTION CONTROL TRACK HAS SEPARATED AT FWD END.SDR 2006UALA00254Frame · corrodedAFT PIT FLOOR FRAME UPPER CHORD AT BS 1153, LBL 24 TO RBL 18 CORRODED ON TOP AND BOTTOM SURFACES. CORRODED FRAME ASSY PIECES REPLACED AND SPLICED PER SRM.SDR 2006UALA00255Stiffener · gougedL-1 DOOR CABLE HAS RUBBED A DEEP GOUGE IN FRAME STIFFENER AFT SIDE OF BS 303 FRAME AT STR 1R. GOUGED SUPPORT MEMBER REPLACED AND INSTALLED PER SRM.SDR 2006UALA00256Attach Angle · crackedFLOORBEAM TO WEB ATTACH ANGLE AT BS 246 APPROX LBL 48, COCKPIT ENTRY STEP IS CRACKED. CRACKED ANGLE REPLACED PER SRM. ANGLE FOUND DURING ROUTINE INSPECTION PROGRAM PER BOEING SERVICE BULLETIN 767-53-0093.SDR 2006UALA00257Bushing · migratedNR 2 ENG PYLON INBOARD MIDSPAR FITTING OUTBOARD LUG BUSHING MIGRATED. NR 2 ENG PYLON INBD MIDSPAR FITTING OUTBD LUG BUSHING WAS FOUND MIGRATED. 4 EACH MIDSPAR BUSHINGS WERE FABRICATED PER SRM 54-53-90, REPAIR 3 & REPLACED PER GN-MM 01-0- 01-013.SDR 2006UALA00199Seat Track · corrodedMAIN CABIN STA 1087, SEAT TRACK RBL 88 IS CORRODED. A 20 INCH SECTION OF CORRODED SEAT TRACK REPLACED WITH NEW, PER SRM.SDR 2006UALA00200Seat Track · corrodedSEAT TRACK IN MAIN CABIN HAS AREAS OF GOUGES AND CORROSION STA 1197 + 142 TO 1213, 88 RBL. GOUGED SECTIONS OF SEAT TRACK REPLACED WITH NEW, PER SRM.SDR 2006UALA00182Seat Track · gougedAFT CABIN SEAT TRACK GOUGED STA 1302 - 1325 LBL 11. SECTION OF AFT CABIN SEAT TRACK GOUGED BY UNKNOWN ORIGIN. REPAIRED PER SRM.SDR DL76L060080Sleeve · displacedON PDC FOUND LT ENGINE REVERSER O/B SLEEVE OUT OF TRACK. ON INSP FOUND O/B REV SLEEVE DETACHED FROM TRACK. REMOVED TRACK FITTING AND REINSTALLED IN GUIDE TRACK. CYCLED THRUST REV, OPS/IND NORMAL. NO DAMAGE TO REV OR TRACK. REVERSER LOCKED IN FWD THRUST PRSDR 2006UALA01186Latch · wornNR 3 LATCH EDGE MARGIN BEYOND LIMITS. REMOVED AND REPLACED NR 3 LATCH IAW B767 MM 25-65-98.SDR NOCA0706Fan · burned outLT RECIRCULATION FAN WRITTEN UP FOR HAVING AN ELECTRICAL BURNING SMELL, FAN WAS DEFERRED IAW MEL 21-25-01.SDR NOCA0406Cable · brokenFOUND L4 GIRT BAR DEPLOYMENT CABLES DISCONNECTED. REPLACED SLIDE ASSEMBLY. STATEMENT PROVIDED BY MECHANIC INDICATES CABLES WERE BROKEN AT THE GIRT BAR ATTACH POINT. THIS WAS DISCOVERED DURING A FLEET CAMPAIGN DIRECTIVE DUE TO OTHER PROBLEMS ON 767 FLEET EMERGESDR 2006UALA01178Latch · failedRT OVERWING COMPT DOOR LATCHES FAILED TORQUE CHECK. REPLACED LATCHES. IAW B767, MM 25-65-98.SDR DL76L060017Sensor · failedLT REVERSER UNLOCKED LIGHT ILLUMINATED DURING TAKEOFF ROLL. EXTINGUISHED AFTER ABORT. REPLACED RT THRUST REVERSER ACTUATOR PROX SENSOR S-1608.SDR DL76L060005Fmu · unknownNR 1 ENG FLUCTUATED LIKE A PULSING AT FL350 MACH .79. EPR 1.36-1.38 FP 203-209 N1 AND N2 +/- .1%. APPLIED ENG A/I WITH NO CHANGE. SWITCHED OFF BOTH EEC SWITCHES AND LEFT FLUCTUATED MORE FF 5820 TO 5960. REMOVED AND REPLACED FMU PER AMM 73-21-01. PERFORMED SDR DL76L050832Engine · failedPASSING THRU 7K FEET ABOUT 4 MINS AFTER T/O, THE RIGHT ENG EXPERIENCED A VIOLENT SURGE WITH VIBRATIONS. THROTTLE PULLEDBACK TO IDLE AND EGT CONTINUED TO CLIMB. ENG SHUTDOWN WITH FUEL CUTOFF SWITCH. EGT REACHED 722 DEGS BEFORE SHUTDOWN AND N1 ROLLED BACK. SDR 2006UALA01185Latch · wornNR 3 LATCH EDGE MARGIN BEYOND LIMITS. REPLACED LATCH, IAW B767 MM 25-65-98.SDR 2005UALA01494Skin · crackedNR 1 PYLON INBOARD FWD STRUT SKIN CRACKED AT PANEL 416BR CUTOUT RADIUS. IT WAS PROBABLY CAUSED BY FATIGUE. THE SKIN WAS REPAIRED PER SRM 54-53-01 WITH -1 AND -2 DOUBLERS.SDR 2005UALA01495Bushing · corrodedNR 1 PYLON UPPER LINK FITTING, OUTBOARD LUG REQUIRES REWORK DUE TO INBOARD LUG REWORKED. BUSHING REPLACEMENT DUE CORRODED BUSHING. BOTH LUGS MUST BE REWORKED AS A PAIR. REWORKED AND BUSHINGS WERE REPLACED DUE TO CORROSION. BUSHINGS WERE REPLACED PER SRM 54SDR DL76L050801Carbon Seal · damagedCREW REPORTED SOMKE/SMELL DURING T/O AND AGAIN ON APPROACH INTO ATL. REPLACED FRONT CARBON SEAL ON NR 1 ENGINE.SDR 2005UALA01448Bushing · looseNR 2 PYLON OUTBOARD MIDSPAR FITTING, INBOARD LUG BUSHING MOVES IN BORE. NR 2 PYLON OUTBD MIDSPAR FITTING, INBD LUG BUSHING MOVED IN THE BORE. BUSHING MIGRATION CAUSE IS UNKNOWN. IT WAS REPLACED WITH AN OVERSIZED BUSHING PER SRM 54-53-90SDR 2005UALA01449Bushing · rotatedNR 1 PYLON DIAGONAL BRACE FITTING AT STRUT ATTACH, FWD INBOARD AND OUTBOARD BUSHINGS HAS EVIDENCE OF ROTATION IN THE BORE. NR 1 PYLON DIAGONAL BRACE FITTING AT STRUT ATTACH, FWD INBD AND OUTBD BUSHINGS HAVE EVIDENCE OF ROTATION IN THE BORE. MIGRATION CAUSE IS SDR 2005UALA01450Bushing · wornNR 1 PYLON UPPER LINK FITTING, INBOARD LUG, OUTBOARD BUSHING LIP FRETTED. NR 1 PYLON UPPER LINK FITTING, INBD LUG, OUTBD BUSHING LIP FRETTED. IT WAS PROBABLY CAUSED BY TOLERANCE BUILD UP. BUSHING WAS REPLACED PER SRM 54-51-93.SDR 2005UALA01420Frame · corrodedFRAME TOP CAP CORRODED AT BS 654+121, LBL42, FWD CARGO PIT. MAJOR REPAIR TO FRAME TOP CAP PER SRM AS PERMANENT REPAIR.SDR 2005UALA01421Bushing · migratedNR 1 PYLON INBD MIDSPAR FITTING, INBD AND OUTBD LUG BUSHINGS MIGRATED. NR 1 PYLON INBD MIDSPAR FITTING, INBD AND OUTBD LUG BUSHINGS WERE MIGRATED. CAUSE OF BUSHING MIGRATIONS IS UNKNOWN. BUSHINGS WERE REPLACED PER MM 54-53-90.SDR 2005UALA01422Bushing · migratedNR 1 PYLON OUTBD MIDSPAR FITTING OUTBD LUG, BUSHING IS MIGRATED. NR 1 PYLON OUTBD MIDSPAR FITTING OUTBD LUG, BUSHING WAS MIGRATED. THE BUSHING MIGRATION IS UNKNOWN. IT WAS REPLACED PER SRM 54-53-90.SDR 2005UALA01423Bushing · migratedNR 2 PYLON DIAGONAL BRACE FITTING FWD-STRUT ATTACH, INBD SIDE BUSHING IS MIGRATED. NR 2 PYLON DIAGONAL BRACE FITTING FWD-STRUT ATTACH, INBD SIDE BUSHING WAS MIGRATED. BUSHING MIGRATION CAUSE IS UNKNOWN. THE BUSHING WERE REPLACED PER SRM 54-53-90.SDR 2005UALA01409Bracket · crackedLT WING KRUEGER FLAP INBD OF NR 1 PYLON, ROTARY ACTUATOR OUTBD SUPPORT BRACKET IS BUCKLED AND CRACKED. BRACKET FAILURE WAS DUE TO FATIGUE. PART WAS REPLACED.SDR 2005UALA01405Spacer · burnedBURNED SPACER BLOCKS BETWEEN APU GENERATOR 3 CABLES. FAILING SPLICE INSTALLATIONS REVEALED A MISMATCH BETWEEN THE SPLICE AND CRIMPER USED. MANUFACTURERS' SPLICES AND CRIMPER DIES MUST BE USED AS A MATCHED SET; IF NOT, AN INCOMPLETE SWAGE WILL RESULT IN HEAT GSDR 2005UALA01318Slide · unserviceableDAMAGED BEARINGS. THIS TYPE OF EVENT HAS HAPPENED BEFORE AND BOEING IS WORKING ON IMPROVED FABRICATION MATERIALS TO ADDRESS THIS CONDITION. SLIDE WAS REMOVED FROM THE AIRCRAFT AND SENT TO THE COMPONENT SHOP WHERE BEARINGS WERE REPLACED.SDR 2005UALA01257Skin · lightning strikeLIGHTNING STRIKE AT LEFT FUSELAGE STA 1587 JUST AFT OF PRESSURE BULKHEAD. *S/D* LIGHTNING STRIKE DAMAGE CUT OUT AND REPAIRED PER SRM.
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