Pratt & Whitney PW4462

Service difficulty reports · 778

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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 = 'PW4462'
  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 WLDA200495Structure · damagedIMMEDIATELY UPON BRAKE RELEASE DURING TAKEOFF, NOSE RAPIDLY BEGAN TO RISE, RESULTING IN TAIL STRIKE. REPAIRED THE DAMAGE PER DELTA ERA 094364-14 AND 094561-14. PERFORMED AIRCRAFT WEIGHT, ALL CHECKED NORMAL.Oct 9, 2004 · N275 · Doug MD11F · Fuselage Main, StructureSDR WLDA200494Compressor · stalledAIR TURNBACK DUE TO NR 2 ENGINE COMPRESSOR STALLED WITH ANTI-ICE ON THROUGH 11000 FEET. TEMPERATURE APPROX 620 DEG. BROUGHT THROTTLE TO IDLE, NR 2 EGT WAS APPROX 70 DEG HOTTER THAN NR 1 AND NR 3, FF 900LBS HIGHER THAN NR 1 AND NR 3. ADVANCED THROTTLE WITH AOct 7, 2004 · N275 · Doug MD11F · Turbine Engine Compressor SectionSDR WLDA200490Engine · leakingAIR TURNBACK DUE TO LOSS OF NR 2 ENGINE OIL QUANTITY. INDICATION BOXED "0", PERFORMED CHECKLIST NOTED OIL PRESSURE DECREASING; ENGINE WAS SHUTDOWN PERFORMED. REMOVED AND REPLACED NR 2 ENGINE PER WOA T/C 0105 AND MD-11 MM PROCEDURES. ACCOMPLISHED ENGINE RUN UAug 25, 2004 · N271 · Doug MD11 · Turbine Engine Oil SystemSDR 04FDEA02550Longeron · crackedRT SIDE STA 5-113-1541, LONGERON 25 FOUND CRACKED. REMOVED AND FABRICATED PER SRM 53-10-00 TYPE 1 VOLUME I. FABRICATED REPAIR PARTS AND EXISTING SPLICE INSTALLED PER SRM 53-10-00 TYPE 1 VOLUME I AND SRM 53-33-01 VOLUME II.Aug 23, 2004 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 04FDEA02544Longeron · corrodedCENTER CARGO, CORROSION OBSERVED ON LONGERON 48L SPLICE DOUBLER AT STA 5-113 TO STA 1541. REMOVED PER SRM 51-33-01 VOLUME II. THREE (3) EACH SPLICE DOUBLERS P/N A5A7124-1, A5A7124-2 AND A5A7125-501 FABRICATED PER DWG A5A7124 AND A5A7125; AND PART MARKEAug 22, 2004 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 04FDEA02545Longeron · corrodedCENTER CARGO CORROSION OBSERVED ON LONGERON 51R SPLICE BETWEEN AT STA 1701 TO STA 172. LONGERON 51R AND SPLICE REMOVED PER SRM 53-10-00 FIGURE 2 VOLUME 1. LONGERON AND SPLICE FABRICATED PER SRM 53-10-00 FIGURE 2 VOLUME 1 AND INSTALLED PER SRM 51-33-01 VOLUMAug 22, 2004 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 04FDEA02546Longeron · corrodedCENTER CARGO, CORROSION OBSERVED ON LONGERON 48R SPLICE DOUBLER AT STA 5-116 TO STA 1541. DOUBLERS REMOVED PER SRM 51-33-01 VOLUME II. SPLICE DOUBLERS AFA7124-1, AFA7124-2, A5A7125-501 FABRICATED PER DWG AFA7124 AND A5A7125. PART MARKED AS PER FEDEX GMMAug 22, 2004 · N578FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 04FDEA02525Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AT XORS 600 TO XORS 650 FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-31-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR.Aug 19, 2004 · N578FE · Doug MD11F · Wing SparSDR 04FDEA02526Spar · corrodedRT WING, REAR SPAR, LOWER CHORD AT XORS 650 AREA FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR.Aug 19, 2004 · N578FE · Doug MD11F · Wing SparSDR 04FDEA02527Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AREA AT XORS 680 TO XORS 690 FOUND WTH CORROSION. CORROSION REMOVED PER SRM 51-31-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR.Aug 19, 2004 · N578FE · Doug MD11F · Wing SparSDR 04FDEA02528Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AREA AT XORS 730 TO XORS 755 FOUND WTH CORROSION. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR.Aug 19, 2004 · N578FE · Doug MD11F · Wing SparSDR WLDA200488Warning Light · illuminatedAIR TURNBACK DUE TO AILERON DEFLECTED DISAGREE ALERT DISPLAYED AFTER TAKEOFF. DEACTIVATED TAKEOFF DEFLECTED AILERONS IAW MEL 27-13-2 CAT (C), ENTERED IN DMI M27AU1904-106.Aug 18, 2004 · N273WA · Doug MD11 · Aileron Control SystemSDR WLDA200489Computer · inoperativeUNCOMMANDED ELEV MOVEMENT. CONSIDERABLE CONTROL COLUMN PULL FORCE REQUIRED DURING INITIAL ROTATION TO ATTAIN REQUIRED T/O CLIMBOUT PITCH ATTITUDE UNTIL 500-800 FT AGL. AFTER FLAP RETRACTION, FORCE REQUIRED RETURNED TO NORMAL, CNTRL COLUMN OSCILLATED(TWICE) BEAug 16, 2004 · N275WA · Doug MD11 · Autopilot SystemSDR WLDA200443Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 29. PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 29 Aug 12, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200439Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 34.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 34 FOAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200444Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 25.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 25 FOAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200446Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 23.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 23 FOAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200447Panel · corrodedITEM: DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 21. PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE Aug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200448Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 20.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 20 FAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200449Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 19.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 19 FOAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200450Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 18.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 18 FOAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200451Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 17.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 17 FOUAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200452Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 16.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 16 FOUAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200453Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 14.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 14 FOAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200454Panel · corrodedDURING 4-C CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 10.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 10 FOAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200455Panel · corrodedITEM: DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 6. PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NRAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200457Panel · corrodedDURING 4-C CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 4.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 4 FOUAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200460Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 3.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 3 FOUNAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200464Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 33.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 33 FOAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200466Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 31.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 31 FOUAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200473Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 22.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 22 FOUAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200474Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 20.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 20 FOUAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200477Structure · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 15.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE 15 FOUND Aug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer StructureSDR WLDA200479Structure · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 13.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 13 FOUAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer StructureSDR WLDA200480Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 6.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 6 FOUNAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200481Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 4.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 4 FOUNAug 2, 2004 · N278 · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200482Panel · corrodedITEM: DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 3.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR Aug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200483Panel · corrodedDURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 1.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 1 FOUAug 2, 2004 · N278WA · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR WLDA200484Skin · puncturedDURING 4C-CHECK, WHILE PERFORMING J/C NR WA5740 FOUND A PUNCH HOLE ON RT WING LEADING EDGE SLAT NR 3 AT STA XOS435. PERFORMED REPAIR OF RT WING LEADING EDGE SLAT NR 3 IAW EGAT EI NR W2004A53B. CONDITION CHECK SATISFACTORY.Aug 2, 2004 · N278WA · Doug MD11 · Leading Edge DevicesSDR WLDA200433Aileron · malfunctionedAIR TURNBACK DUE TO AILERON DEFLECTION DISAGREE LEVEL 2 ALERT ON FLAP/SLAT RETRACTION. DEFERRED ITEM TO DMI M27JL2404-122 IAW MEL 27-13-2 CAT (C). NOTE: NO EMERGENCY DECLARED AND NO FUEL DUMPED.Jul 24, 2004 · N273 · Doug MD11 · Aileron Control SystemSDR WLDA200430Tire · separatedNR 8 TIRE CAP SEPARATION: ON ARRIVAL FOUND NR 8 TIRE CAP SEPARATED AND RT IB FLAP OB EXTENSIVE DAMAGE. REMOVED AND REPLACED NR 8 MWA AND SERVICED TO CORRECT LEVEL. LEAK CHECKED IAW MM32-42-01. REMOVED AND REPLACED RT IB FLAP AND RT IB VANE ASSEMBLY IAW MM PJul 20, 2004 · N277 · Doug MD11 · TireSDR WLDA200431Actuator · defectiveLEVEL II ALERT AFTER SLAT RETRACTION, AILERON DEFLECTION DISAGREE AFTER T/O. A/C DIVERTED TO JFK. INSPECTED QUAD RINGS & ASSOCIATED LINKAGE, RAN FLIGHT CONTROLS. CHECKED FOR FLAIRING, PERFORMED RTS ON FCC 1&2 AILERON SYSTEM. ALL TESTS PASSED. DEFERRED AILJul 4, 2004 · N273 · Doug MD11 · Aileron Control SystemSDR WLDA200432Charger · defectiveFRA/NKT AIR TURNBACK DUE TO LEVEL I BATTERY CHARGING ALERT ILLUMINATED DURING NORMAL CRUISE FLIGHT. ELECTRIC SCHEMATIC SHOWED 40V. BATTERY APPEARED TO BE CONTINUOUSLY CHARGED WITH NO DRAW. REMOVED & REPLACED BATTERY CHARGER IAW MM PROCEDURES. PERFORMED EMEJun 26, 2004 · N271 · Doug MD11 · Battery/Charger SystemSDR WLDA200429Tire · separatedTIRE CAP SEPARATION: NR 6 TIRE CAP SEPARATED AFTER LANDING AND HIT LT IB FLAP. REMOVED AND REPLACED NR 6 MAIN TIRE ASSEMBLY. SERVICED WITH DRY NITROGEN TO NORMAL LEVEL IAW MM. INSPECTED LT IB FLAP DAMAGE, FOUND NEGLIGIBLE IAW SRM 51-00-00.Jun 18, 2004 · N277 · Doug MD11 · TireSDR WLDA200427Controller · failedFLIGHT NR WOA8743 ACCORDING TO THE FLIGHT CREW (ENGINE 1 FUEL PUMPS OFF) LEVEL ONE ALERT IMMEDIATELY AFTER POWER FOR TAKEOFF, CAPT DISCONTINUED THE TAKEOFF EXITED THE RUNWAY, SWITCHED FUEL CONTROLLERS THE FUEL SYSTEM OP'S NORMALLY, TAXIED BACK FOR A NORMAL TAKJun 14, 2004 · N279WA · Doug MD11 · Fuel Controlling SystemSDR WRLA200412Engine · vibrationENGINE NR 2 HAS LEVEL 2 VIBRATION HI ALERT, ENGINE SHUTDOWN INFLIGHT AS A PRECAUTIONARY MEASURE FLIGHT FROM RKSI TO PANC, NR 2 ENGINE WILL BE CHANGE ON PANCMar 22, 2004 · N274WA · Doug MD11F · Engine (Turbine/Turboprop)SDR WRLA200408Fan Blade · shingledENGINE 1 VIBRATION HIGH ALERT DISPLAYED ON TAKEOFF, ABORTED TAKEOFF AT 15 KNOTS. INSPECTED NR 1 ENGINE IAW FIM 77-32-01 FOUND FAN BLADES SHINGLED, FREED BLADES, NO DAMAGE NOTED, LUBED FAN SHROUDS AND ROOTS. OPS CHECKED GOOD ON GROUND RUN.Jan 23, 2004 · N278WL · Doug MD11 · Turbine Engine Compressor SectionSDR WRLA200404Fan Blade · damagedON TAKEOFF ROLL, ENGINE 2 EVM COMP READ 5.0 UNITS WITH STRONG VIBRATION. TAKEOFF ABORTED BELOW 80 KNOTS. REMOVED AND REPLACED FOUR EACH FAN BLADES ON NR 2 ENGINE PER MM 72-31-02 PERFORMED ENGINE RUN AT 95 PERCENT N1 EVM COMP 7 READING, OPS CHECK GOOD. REPLAJan 11, 2004 · N274WA · Doug MD11F · Turbine Engine Compressor SectionSDR WRLA200402Engine · leakingTAKEOFF PLUS 30 LEVEL OFF FL310 NR 2 ENGINE OIL TEMP HIGH 165 DEGREES FOR 15 MINUTES 170 DEGREES MOMENTARY OIL QUANITY DROPPED TO 7 QUARTS DESCEND TO FL230 STABILIZED 234 PSI, 142 DEGREES, 7 QUARTS. AIRCRAFT DIVERTED TO LAWANDA. REMOVED AND REPLACED ENGINE. Jan 2, 2004 · N278WA · Doug MD11 · Engine (Turbine/Turboprop)SDR WRLA200323Engine · malfunctionedENGINE 3 OIL PRESSURE LOW LEVEL 2 ALERT. TEMPERATURE AND QUANTITY STABLE. ENGINE SHUTDOWN IAW PROCEDURE. REPLACED NR 3 ENGINE IAW PAPER WORK CARD 0104 COMPLIED WITH PREFLIGHT HANDBOOK MM 71-00-01. REPLACED ENGINE. (M)Nov 23, 2003 · N278WA · Doug MD11 · Turbine Engine Oil System
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