Pratt & Whitney PW4060

Service difficulty reports · 7,186

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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.

SDR UALA2012052702969Oxygen Mask · misinstalledALL CENTER PAX O2 MASKS ARE IMPROPERLY PACKED. REPACKED ALL CENTER PAX 02 MASKS IN REF TO AMM.May 26, 2012 · N654UA · Boeing 767322 · Passenger Oxygen SystemSDR UALA2012052702971Oxygen Mask · misinstalledALL LT PAX O2 MASKS ARE IMPROPERLY PACKED. REPACKED ALL LT PAX O2 MASKS IAW AMM 35-21-14.May 26, 2012 · N654UA · Boeing 767322 · Passenger Oxygen SystemSDR UALA2012052702972Oxygen Mask · misinstalledALL RT PAX O2 MASKS ARE IMPROPERLY PACKED. REPACKED ALL RT PAX O2 MASKS IN REF AMM 35-21-14.May 26, 2012 · N654UA · Boeing 767322 · Passenger Oxygen SystemSDR UALA2012052402909Transmitter · malfunctionedAFTER DEPARTURE LOST LEFT VHF. CAN RECEIVE BUT NOT TRANSMIT. NO WAY TO RESTORE IN FLIGHT. CONTINUING TO DESTINATION. GROUND CHECKED , OPS NORMAL.May 24, 2012 · N659UA · Boeing 767322 · VHF Communications SystemSDR UALA2012052402910Computer · faultyAUTO THROTTLE DISCONNECTED ON SEVERAL OCCASIONS AND UNABLE TO STAY IN ARMED POSITION. REMAINDER OF FLT FLOWN WITH AUTOTHROTTLE OFF. REPLACED THRUST MANAGEMENT COMPUTER AS PER AMM. OPS CHECKED NORMAL.May 24, 2012 · N657UA · Boeing 767322 · Auto Throttle SystemSDR UALA2012052402911Computer · faultyCENTER AUTOPILOT WILL NOT ENGAGE AND FIRST OFFICER FLT DIRECTOR BARS LOST WHEN CENTER FLT DIRECTOR ENGAGED. CENTER FCC INOPERATIVE. REPLACED CENTER FLIGHT CONTROL COMPUTER AS PER AMM. OPS CHECKED NORMAL. ALSO ACCOMPLISHED AUTOPILOT FLIGHT CONTROL TEST AS PMay 24, 2012 · N657UA · Boeing 767322 · Autopilot SystemSDR UALA2012052502925Hinge · looseOXYGEN MASK HANGING DOWN OVER FC FLIGHT ATTENDANT JUMPSEAT. FOUND PANEL HINGE LOOSE FROM PANEL. REGLUED PANEL PER B767 AMM. STOWED MASKS AND CLOSED PANEL. OK NOW.May 24, 2012 · N642UA · Boeing 767322 · Passenger Oxygen SystemSDR UALA2012052102863Starter · faultedAFTER LANDING APU WOULD NOT START. THREE ATTEMPTS MAX EGT 777 N40. PRIOR START IN AIR WAS OK. CLEANED CONNECTORS AT IGV, FCU & FUEL FLOW DIVIDER & SOLENOID VALVE PER AMM & MM(S) RESPECTIVELY, CHECKED ALL MAG CD'S PER MM. FOUND CLEAN AND REPLACED APU STARTERMay 19, 2012 · N657UA · Boeing 767322 · APU Start/Ignition SystemSDR UALA2012051802810Lap Joint · damagedON LEFT SIDE OF AIRCRAFT AT STR 35L AT APPROX STA 1263 3 EACH LOCK FASTENERS ON THE LAP JOINT STRINGER ROW HEADS ARE PULLED OR MISSING. INSTALLED 3 BLIND FASTENERS REF ECRA 5330-04239.May 16, 2012 · N654UA · Boeing 767322 · Fuselage Main, Plate/SkinSDR RYNA201205160025Housing · failedON CLIMBOUT 11,000 FT, NR 2 ENGINE OIL PRESSURE STARTED DECREASING, AT 74 PERCENT PER CPM SHUT DOWN ENGINE (PRECAUTIONARY) RETURNED TO LEJ. PERFORMED DETAILED VISUAL INSPECTION OF NR 2 ENGINE FOUND 2 STUDS ON MAIN ENGINE OIL FILTER HOUSING FAILED. INSPECTED May 16, 2012 · N637TW · Boeing 76733AER · Turbine Engine Oil SystemSDR UALA2012060503115Skin · dentedDENT IN SKIN MEASURES 9.7 5 INCHES BY 5.75 INCHES WITH A DEPTH 0F .149 INCH. THE \A\ OVER \Y\ = 38. THE MAX DEPTH ALLOWED IS .125 INCH. DENT INCORPORATED IN LARGER REPAIR PER ECRA 5360-01202 AND EA PT67-53-011.May 16, 2012 · N654UA · Boeing 767322 · Fuselage Main, Plate/SkinSDR UALA2012051802841Actuator · leakingHYDRAULIC FLUID LEAKING FROM BOTTOM OF TAIL AT 10 DROPS PER SECOND. RUDDER RATIO ACTUATOR LEAKING. REPLACED RUDDER RATIO CHANGER ACTUATOR IAW MM. OPS AND LEAK CHECKED NORMAL.May 16, 2012 · N648UA · Boeing 767322 · Rudder ActuatorSDR UALA2012051602789Battery · inoperativeEMERGENCY LIGHT IN COCKPIT IS INOPERATIVE. REMOVED AND REPLACED BATTERIES IAW AMM 33-51-01. OPS CHECKED GOOD.May 14, 2012 · N649UA · Boeing 767322 · Emergency LightingSDR UALA2012051102732Actuator · leakingPOSSIBLE HYD LEAK RT ELEVATOR. CONTINUE INSTALLATION OF RT OTBD ELEVATOR POWER CONTROL ACTUATOR. REMOVED RT OTBD ELEVATOR PCA PER AMM. COMPLETED REPLACEMENT AND ADJUSTMENT OF RIGHT ELEVATOR OUTBOARD PCA.May 11, 2012 · N653UA · Boeing 767322 · Elevator Control SystemSDR UALA2012051102730Oil System · leakingAPU FAULT TWICE. FOUND NO OIL IN APU TANK, AND APU COMPARTMENT OIL SOAKED. REPLACED APU PER MM.May 11, 2012 · N648UA · Boeing 767322 · APU Oil SystemSDR UALA2012051102731Control Unit · faultyWITH HYD ON, RIGHT INBOARD AILERON BANGING AND SHAKING ACFT. REPLACED RIGHT 3R SCM, TEST PASSED.May 11, 2012 · N648UA · Boeing 767322 · Aileron Control SystemSDR UALA2012051102728Indicator · faultyVHF 1 RIGHT DISPLAY, HUNDREDS DIGIT FAINT. REPLACED NR 1 VHF COMM CONTROL PANEL PER MM, OPS NORMAL.May 10, 2012 · N643UA · Boeing 767322 · VHF Communications SystemSDR UALA2012051102729Valve · faultyRIGHT BLEED LIGHT AND HIGH STAGE (OVERHEAT) LIGHT ILLUMINATED. DESCENDING FROM FL380. ACCOMPLISHED QRH ITEMS. BLEED OVERHEAT AND RT PACK OFF LIGHT REMAINED ON. ACCOMPLISHED AN OPERATIONAL TEST PER MM. ACCOMPLISHED BITE CHECK OF AIR SUPPLY BLEED MODULE IAWMay 10, 2012 · N643UA · Boeing 767322 · Pneumatic Distribution SystemSDR UALA2012051102740Lamp · inoperativeEMERGENCY EXIT LIGHT ABOVE SEAT 36AB IS INOPERATIVE. REPLACED LAMP AT SEAT 36AB. OPS CHECKED GOOD.May 10, 2012 · N649UA · Boeing 767322 · Emergency LightingSDR UALA2012051102755Valve · malfunctionedUNABLE TO CONTROL CABIN TEMP. CYCLED CB C33 PER TOMC AND REGAINED CAB TEMP CONTROL. FOUND MID TRIM MODULATING VALVES IN OPEN POSITION. AS PER DF0690 CLOSED AUX MID AND MID MODULATING VALVES.May 10, 2012 · N652UA · Boeing 767322 · Cabin Temperature Control SystemSDR CA120509004Apu · fire(CAN) APU FIRE ON THE GROUND. FIRE REPORTED FROM TAIL, NO FIRE WARNING. CABIN FILLED WITH SMOKE. FLIGHT OPS AND INFLIGHT CREW MEMBERS WERE ON BOARD ACFT, AND WERE EVACUATED. APU BOTTLE HAD BEEN DISCHARGED, AND MAYDAY DECLARED TO GET IMMEDIATE FIRE RESPONSMay 6, 2012 · Boeing 7673Y0 · Airborne Auxiliary Power Unit (APU) SystemSDR UALA2012050802671Stiffener · crackedBS 246 FLOORBEAM VERTICAL STIFFENER ON FWD SIDE AT RBL 16 CRACKED IN RADIUS. FABRICATED AND REPLACED VERTICAL STIFFENER, REPAIRED AFT MOUNTING BRACKET AND PULLEY BRACKET PER SRM'S. OPS CHECKED GOOD PER AMM. MAJOR REPAIRMay 5, 2012 · N648UA · Boeing 767322 · Fuselage Main, Floor BeamSDR UALA2012050802670Track · wornR1 DOOR UPPER FWD TRACK WORN. REPLACED DOOR UPPER TRACK PER SRM. REPLACED TROLLEY ROLLERS PER AMM. ACCOMPLISHED DOOR ADJUSTMENT AND TEST PER AMM, OPS CHECKED GOOD.May 5, 2012 · N648UA · Boeing 767322 · Passenger/Crew DoorsSDR UALA2012051002707Structure · corrodedCORROSION ON CANTED DECK AT STA 955, RBL 12. REMOVED CORROSION PER SRM. ACCOMPLISHED HFEC OF HOLES PER NDTM 51-00-19, PRT 6, NO CRACKS NOTED. ACCOMPLISHED FHRS FOR THICKNESS PER NDTM 51-00-16, PRT 6. FLAP PEENED AREA PER SRM 51-20-06, ECRA 5710-02234, AND EA May 4, 2012 · N648UA · Boeing 767322 · Fuselage Miscellaneous StructureSDR UALA2012050702651Connector · contaminatedAIR RETURN DUE TO STAB TRIM INDICATION. TROUBLESHOOTING FOUND STAB WOULD RUN AT FULL SPEED IN NOSE UP DIRECTION AND HALF SPEED IN NOSE DOWN DIRECTION. IN BLOCK 6 OF FIM FOUND STAB WOULD NOT GO IN NOSE DOWN DIRECTION 104400 ALSO HAD 0.2 OHMS, AND IN NOSE UP DIMay 4, 2012 · N663UA · Boeing 767322 · Flight Control System WiringSDR UALA2012050302617Feeder Cable · chafedNR 1 ENGINE IDG MAIN FEEDER CABLE IS CHAFED THRU THE INSULATION ABOUT 12 INCHES FROM THE IDG TERMINAL LUGS. THERE ARE SOME SIGNS OF ARCHING ON THE FASTENER THAT CAUSED THE CHAFING. INSPECTED AND FOUND DAMAGE WITHIN LIMITS PER SWPM 20. WRAPPED CABLE WITH CHMay 3, 2012 · N659UA · Boeing 767322 · Electrical Power System WiringSDR UALA2012050302608Bulb · inoperativeEMERGENCY LIGHT CEILING ABOVE SEATS 6AB INOP. REMOVED AND REPLACED LIGHT BULB IAW 33-51-04.May 2, 2012 · N648UA · Boeing 767322 · Emergency LightingSDR UALA2012050202590Shear Tie · corrodedFUSELAGE BS 1562 BETWEEN STRINGERS S-39L-39R SHEAR TIE CORRODED. REMOVED AND REPLACED SHEAR TIE REF SRM51-40-02.May 1, 2012 · N648UA · Boeing 767322 · Fuselage Internal Mounting StructureSDR UALA2012050202591Oxygen Mask · misinstalledPASSENGER CABIN, PAX O2 MASKS IMPROPERLY PACKED. REPACKED ALL PASSENGER O2 MASKS.May 1, 2012 · N648UA · Boeing 767322 · Passenger Oxygen SystemSDR UALA2012050202592Floorbeam · corrodedAFT CARGO BAY, BS 1153, RBL 23 - 42, FLOORBEAM CAP CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-00-07. FABRICATED NEW FLOORBEAM CAP IAW SRM 51-40-05 AND INSTALLED IAW SRM 51-40-02.May 1, 2012 · N648UA · Boeing 767322 · Fuselage Main, Floor BeamSDR UALA2012043002559Lamp · failedE/E COOLING SYSTEM FAILS OPS CHECK. SMOKE LIGHT ON P5 PANEL FAILS TO COME ON WHEN P61 E-C TEST SWITCH IS ACTUATED AND HELD. ALSO, FWD EQUIPMENT SMOKE DETECTION FAILS TO APPEAR ON EICAS DISPLAY. CONFIRMED SMOKE LIGHT DOES COME ON DURING LIGHT TEST. RELAMPEDApr 29, 2012 · N662UA · Boeing 767322 · Smoke DetectionSDR UALA2012043002555Light · inoperativeEMERGENCY EXIT AISLE LIGHT AT SEATS 37-38 RT SIDE IS INOP. REPLACED SEAT EMERGENCY EXIT LIGHT REF AMM 33-51-10. OPS CHECKED GOOD.Apr 27, 2012 · N644UA · Boeing 767322 · Emergency LightingSDR UALA2012043002556Skin · dentedDENT ON FUSELAGE AT BS 331 STRINGER S30L FOUND OUT OF SRM LIMITS. TRIMMED OUT DAMAGE IAW EA PT67-53-005 AND ECRA 5310-05483. ACCOMPLISHED NDT. NO CRACKS FOUND. ACCOMPLISHED INSURANCE CUT PER EA FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FILLER REPAIR REApr 27, 2012 · N644UA · Boeing 767322 · Fuselage Main, Plate/SkinSDR UALA2012043002557Skin · misrepairedEXTERNAL FUSELAGE SKIN AT BS 1430-1461 JUST BELOW CARGO DOOR WAS FOUND MISREPAIRED. REPAIRED SKIN IAW EA PT67-53-003 AND ECRA 5360- 01191. ACCOMPLISHED NDT OF AREA. NO CRACKS FOUND. ACCOMPLISHED INSURANCE CUT. FABRICATED AND INSTALLED EXTERNAL FILLER, DOUBApr 27, 2012 · N644UA · Boeing 767322 · Fuselage Main, Plate/SkinSDR UALA2012043002558Line · damagedPOTABLE WATER SUPPLY LINE RUNNING FROM STA 1375 TO 1550 HAS A BURN MARK ASSOCIATED WITH RIBBON HEATER TAPE B110 AT BS 1420. REMOVED AND REPLACED DAMAGED WATER LINE IAW AMM 38-10-00 AND SRM 51-40-02. PERFORMED LEAK CHECK TEST IAW 38-10-00. CHECKED GOOD. HEAApr 27, 2012 · N644UA · Boeing 767322 · Potable Water SystemSDR UALA2012042602500Lamp · inoperativeEMERGENCY EXIT LIGHT ASSY L-288 AT R1 DOORWAY INOPERATIVE. REMOVED AND REPLACED LAMP. OPS CHECKED GOOD.Apr 26, 2012 · N644UA · Boeing 767322 · Emergency LightingSDR UALA2012042602502Stringer · misrepairedSTRINGER 38 LEFT MISREPAIRED AT BS 1453. FABRICATED AND INSTALLED STRINGER REPAIR, SRM 53-00-03 FIG 201 REPAIR 2 DETAIL 4. MAJOR REPAIRApr 26, 2012 · N644UA · Boeing 767322 · Fuselage Main, Longeron/StringerSDR UALA2012042602506Frame · corrodedAFT CARGO PIT, FRAME AT BS 1241 AND STR 34R, INNER CHORD CORRODED. REMOVED CORROSION & FOUND MATERIAL LOSS OUT OF SRM LIMITS. REMOVED EXISTING TEE. FABRICATED & INSTALLED NEW TEE. MAJOR REPAIR.Apr 26, 2012 · N644UA · Boeing 767322 · Fuselage Main, FrameSDR UALA2012042702511Terminal Block · damagedWINDOW EICAS MESSAGE DISPLAYED. INOPERATIVE LIGHT DID NOT EXTINGUISH WHEN SWITCH WAS RECYCLED TO OFF THEN ON. BITE CHECKED, CONTROLLER FAULTED. FOUND DAMAGED TERMINAL BLOCKS ON WIRE HARNESS, HARNESS BRITTLE, TROUBLESHOOTING FOUND RECESSED PINS 2 AND 3 ON COApr 26, 2012 · N644UA · Boeing 767322 · Ice/Rain Protection System WiringSDR UALA2012042702512Light · inoperativeEMERGENCY EXIT LIGHT AT SEAT 34AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSY FOR SEAT. OPS CHECKED GOOD.Apr 26, 2012 · N644UA · Boeing 767322 · Emergency LightingSDR UALA2012042702513Floorbeam · corrodedFWD CABIN BS 287 FLOORBEAM UPPER TEE CORRODED. REMOVED DAMAGED TEE IAW SRM 53-00-51 NR 1. ACCOMPLISHED NDT, NO CRACKS FOUND. FABRICATED AND INSTALLED UPPER TEE IAW SRM 53-00-51 FIG 201 REPAIR NR 1. MAJOR REPAIR.Apr 26, 2012 · N644UA · Boeing 767322 · Fuselage Main, Floor BeamSDR UALA2012042702514Spar · crackedNR 1 PYLON FWD UPPER SPAR WEB OUTBOARD DRAIN HOLE CRACKED AT OUTBOARD DRAIN HOLE AT NAC STA 156. STOP DRILLED CRACK. ACCOMPLISHED NDT, NO CRACKS FOUND. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 54-53-01 REPAIR 10.Apr 26, 2012 · N644UA · Boeing 767322 · Nacelle/Pylon, Frame/Spar/RibSDR UALA2012042702523Unknown · faultedPREDICTIVE WINDSHEAR SYSTEM DOES NOT TEST CORRECTLY. REPLACED WEATHER TRANSCEIVER PER MM AND ACCOMPLISHED TEST, TEST PASSED. NEWLY INSTALLED RT UNIT FAILED, REINSTALLED ORIGINAL UNIT AND TESTS OKAY.Apr 26, 2012 · N656UA · Boeing 767322 · Wind Shear Detection SystemSDR UALA2012043002552Light · inoperativeEMERGENCY EXIT LIGHT AT SEAT 34AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSY FOR SEAT REF AMM 33-51-10. OPS CHECKED GOOD REF AMM33- 51-00.Apr 26, 2012 · N644UA · Boeing 767322 · Emergency LightingSDR UALA2012043002553Floorbeam · corrodedFWD CABIN BS 287 FLOORBEAM UPPER TEE CORRODED. REMOVED DAMAGED TEE AT BS 287 RBL 37-70 IAW SRM 53-00-51 REPAIR 1. ACCOMPLISHED NDT FOR CRACKS. NONE FOUND. FABRICATED AND INSTALLED UPPER TEE REPAIR REF SRM 53-00-51 FIG 201 REPAIR 1.Apr 26, 2012 · N644UA · Boeing 767322 · Fuselage Main, Floor BeamSDR UALA2012043002554Floorbeam · corrodedFWD CABIN BS 287 AND RBL 20, FLOORBEAM TEE CORRODED. REMOVED DAMAGE AND FABRICATED AND INSTALLED TEE REPAIR REF SRM 53-00-051 FIG 201 REPAIR 1.Apr 26, 2012 · N644UA · Boeing 767322 · Fuselage Main, Floor BeamSDR UALA2012042502493Skin · misrepairedSKIN BS 1447, STR 37L MISREPAIRED. CUT OUT DAMAGE, FABRICATED AND INSTALLED HAT CHANNEL AND ANGLES PER SRM 53-00-03, FIG 201, RPR 2, TYPE IV. PERFORMED HFEC PER NDTM 51-00-16, PRT 6, NO CRACKS NOTED.Apr 25, 2012 · N644UA · Boeing 767322 · Fuselage Main, Plate/SkinSDR UALA2012042502495Frame · corrodedAFT CARGO PIT, FRAME INNER CHORD CORRODED AT BS 1197+88 AND S34L. REMOVED DAMAGE AND FOUND MATERIAL LOSS OUT OF SRM LIMITS. REMOVED DAMAGED UPPER TEE SECTION IN ENTIRETY. FABRICATED AND INSTALLED NEW UPPER TEE REF SRM51-40-02.Apr 25, 2012 · N644UA · Boeing 767322 · Fuselage Main, FrameSDR UALA2012042702520Apu · malfunctionedAPU FAILED TWICE WHEN PNEU WAS IN USE. CHECKED CHIP DETECTORS ON APU, ALL GOOD. SERVICE WITH OIL. REPLACED APU BATTERY CHARGER IAW AMM, OPS CHECKED GOOD. RAN APU UNDER LOAD FOR 1 HALF HOUR RAN GOOD. APU AUTO SHUTDOWN AFTER OPERATING FOR 3 MINUTES. 5TH AUTO SHUApr 25, 2012 · N641UA · Boeing 767322 · Airborne Auxiliary Power Unit (APU) SystemSDR UALA2012042502484Lamp · inoperative4TH EMERGENCY OVERWING EGRESS LIGHT AFT ON LEFT SIDE IS INOPERATIVE. RELAMPED AND SECURED CENTER CONTACT LUG. OP CHECKED NORMAL.Apr 24, 2012 · N642UA · Boeing 767322 · Emergency Lighting
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