Pratt & Whitney PW4462

Service difficulty reports · 778

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'PW4462'
  ORDER BY difficulty_date DESC"

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SDR WRLA2007007Fuel Tank · corrodedDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND CENTER WING TANK UPPER SKIN CORRODED AT STA Y=1227, X=75 TO X=79 AREA. MECHANIC FOUND CENTER WING TANK UPPER SKIN UPPER SURFACE SEVERAL CORROSION EXIST. REPAIRED CORRODED AREA PER EGAT E1 W2007A57B-047 REV.01 WITH Jan 11, 2007 · N276WA · Doug MD11F · Fuel StorageSDR WRLA2007008Skin · corrodedDURING 2C+12A+150M CHECK, MECHANIC FOUND CENTER ACCESSORY COMPARTMENT LWR SKIN SPLICE SURFACE CORRODED AT STA Y=1165, LONGERON 51L LEFT SIDE. BLEND OUT CORRODED AREA PER MD-11F SRM VOL.II 51-21-01 REV.38. MEASURE REWORK AREA STILL WITHIN ALLOWABLE DAMAGE LIMIJan 11, 2007 · N276WA · Doug MD11F · Fuselage Main, Plate/SkinSDR WRLA2007009Seat Track · corrodedDURING 2C+12A+120M CHECK, EGAT MECHANIC FOUND MAIN DECK CARGO SEAT TRACK FLANGE CORROSION AT STA Y=1321 TO Y=1381, X=27. CUT,FABRICATE REPAIR THE CORRODED SEAT TRACK SECTION & SPLICE HAT PER MD-11F SRM VOL.1 53-70-00 FIG.1 REV.38. 2.CONDITION CHECK NORMAL.Jan 11, 2007 · N276WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2007010Rivet · corrodedDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND MAIN DECK CGO CENTER WING TANK UPPER STRUCTURE SEVERAL RIVETS HAVE CORROSION AT STA Y=1366, X=30 TO X=75. BLEND OUT CORRODED AREA AND MEASURE REMAIN SKIN THICKNESS STILL WITHIN ALLOWABLE DAMAGE LIMITATION PER MD-1Jan 11, 2007 · N276WA · Doug MD11F · Fuel StorageSDR WRLA2007011Skin · corrodedDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND LEFT WING UPPER SURFACE BULGE CORRODED UNDER FIXED PANEL NEAR XORS=1042 REAR SPAR. REPAIR THE DAMAGE AREA PER EGAT E1 NT W2007A57B-060 REV.00 AND APPROVE DOCUMENT BOEING MESSAGE NR 1-276023171-2. CONDITION CHECK NJan 11, 2007 · N276WA · Doug MD11F · Wing, Plate/SkinSDR WRLA2007014Seat Track · corrodedDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND M/D CARGO FLOOR SEAT TRACK CORROSION AT Y=470, X=30. CLEANED UP CORROSION AREA PER MD-11F SRM VOL.II 51-21-01 REF 38. MEASURE REWORK DEPTH=0.009" STILL WITHIN ALLOWABLE LIMIT PER MD-11F SRM VOL.1 53-70-00 FIG.3.Jan 11, 2007 · N276WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2007017Seat Track · corrodedDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND MAIN DECK CARGO SEAT TRACK FLANGE CORRODED AT STA Y=1329, X=29. CUT AND FABRICATE REPAIR THE CORRODED SEAT TRACK SECTION AND SPLICE HAT PER MD-11F SRM VOL 1 53-70-00 REV 38. CONDITION CHECK NORMAL. (MAJOR REPAIRJan 11, 2007 · N276WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2007021Fitting · corrodedDURING 2C+12A+150M CHECK, MECHANIC FOUND CENTER ACCESS COMPARTMENT DOOR FWD AREA LONGERON 51L END FITTING CORRODED AT STA Y=6-74.750 TO Y=6-90. FABRICATED THE NEW PARTS IAW E1 NR W2007P53B-029 REV.00 AND MFG DRAWING NR AAA7088. CONDITION CHECK NORMAL. (EGAT Jan 11, 2007 · N276WA · Doug MD11F · Fuselage Miscellaneous StructureSDR WRLA2007022Fitting · corrodedDURING 2C+12A+150M CHECK, MECHANIC FOUND CENTER ACCESS COMPARTMENT DOOR FWD AREA LONGERON 52L END FITTING CORRODED AT STA Y=6-74.750 TO Y=6-90. FABRICATE THE NEW PARTS IAW E1 NR W2007P53B-029 REV.00 AND MFG DRAWING NR AAA7088. CONDITION CHECK NORMAL. (EGAT NJan 11, 2007 · N276WA · Doug MD11F · Fuselage Miscellaneous StructureSDR WRLA2007025Rib · brokenITEM:DURING 2C+12A+150M CHECK, MECHANIC FOUND RT HORI STAB UPPER TO BODY FAIRING PANEL SUPPORT RIB BROKEN AT INTERSECTION STA 2025.00. FABRICATE FAIRING PANEL SUPPORT RIB IAW EGAT E1 NO.W2007P55B-075 REV.01. AND APPROVED DOCUMENT MFG CONTROL NR PO209380. INSJan 10, 2007 · N276WA · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2007002Unknown · smokeTO+15 MIN SMOKE & FUMES IN COCKPIT, UNKNOWN SOURCE. COCKPIT DOOR POWER & RECIRC FANS TURNED OFF. SMOKE DISSIPATED SOME. RETURN TO ORIGIN. CHECKED RECIRC FANS, ALL CHECKED GOOD, CHECKED MUX SYSTEM OPS CHECK GOOD. CHECKED WIRING IN OVERHEAD, FOUND NO PROBLEJan 8, 2007 · N277WA · Doug MD11 · Air Distribution SystemSDR WRLA2007004Rib · crackedDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND LEFT WING L/E RIB CRACKED AT FRONT SPAR APPROXIMATELY AT XORS840. REPAIREDTHE DAMAGED AREA PER MD-11F SRM VOL1 57-00-01 FIG 10 REV 38. CONDITION CHECK NORMAL. EGAT NRC NO U05067.Jan 8, 2007 · N276WA · Doug MD11F · Wing, Rib/BulkheadSDR WRLA2007012Longeron · corrodedDURING 2C+12A+150M CHECK, EGAT MAINT FOUND CORROSION AT STA 630 - STA 670 LONGERON L51. CUT & FABRICATE REPAIR THE DAMAGED AREA PER MD-11F SRM 53-10-00 REV.38 FIG.1 & FIG.2. CONDITION CHECK NORMAL.Jan 8, 2007 · N276WA · Doug MD11F · Fuselage Main, Longeron/StringerSDR WRLA2007013Longeron · corrodedDURING 2C+12A+150M CHECK, EGAT MAINT FOUND CORROSION AT STA 630-670 LONGERON L52. CUT & FABRICATE REPAIR THE DAMAGED AREA PER MD-11F SRM 53-10-00 REV.38 FIG.1 & FIG.2. 2.CONDITION CHECK NORMAL.Jan 8, 2007 · N276WA · Doug MD11F · Fuselage Main, Longeron/StringerSDR WRLA2007020Stiffener · corrodedDURING 2C+12A+150M CHECK, EGAT MECHANIC FOUND FUSELAGE LT WING TO BODY FAIRING SUPPORT STIFFENER CORRODED AT STA Y=5-30,X=80 TO 100 AREA. ACCOMPLISHED REPAIR, THE STIFFENER CORROSION IAW EGAT E1 NR W2007P53B-054 REV 00 AND IAW MD-11F SRM 51-35-01 REV.38 AND APJan 6, 2007 · N276WA · Doug MD11F · Fuselage Miscellaneous StructureSDR WRLA2006101Slide · no testDURING 4C CHECK IN TPE, L4 DOOR SLIDE DEPLOYMENT FAILED DURING TESTING. REMOVED AND REPLACED SLIDE PER AMMNov 2, 2006 · N277WA · Doug MD11 · Escape SlideSDR WRLA2006094Structure · corrodedITEM: DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 7. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION IAW EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATED REPASep 22, 2006 · N275 · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006095Structure · corrodedDURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4, FOUND CORROSION ON HST LH BARREL NUT HOLE NR 4. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION IAW EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATED REPAIR BUSSep 22, 2006 · N275 · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006096Floorbeam · corrodedDURING 2C+12A+150M CHECK FOUND UPPER DECK CARGO FLOORBEAM CHANNEL CORROSION AT STA 496.5 X=22.5. REPLACED FLOORBEAM CHANNEL IAW SRM 51-33-01 VOL II REV 38, CONDITION CHECK ALL NORMAL.Sep 22, 2006 · N275 · Doug MD11F · Fuselage Main, Floor BeamSDR WRLA2006082Barrel Nut · corrodedITEM: DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 3. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRSep 12, 2006 · N275 · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006083Barrel Nut · corrodedDURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 6. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATEDSep 12, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006085Barrel Nut · corrodedDURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 9. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATEDSep 12, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006081Barrel Nut · corrodedITEM: DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 1. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATED REPASep 11, 2006 · N275 · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006086Barrel Nut · corrodedDURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 17. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATESep 11, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006087Barrel Nut · corrodedDURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 21. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATESep 11, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006089Barrel Nut · corrodedDURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 34. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATESep 11, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006091Barrel Nut · corrodedDURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST RT BARREL NUT HOLE NR 4. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATEDSep 11, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006092Barrel Nut · corrodedDURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST RT BARREL NUT HOLE NR 4. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATEDSep 11, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006093Barrel Nut · corrodedDURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST RT BARREL NUT HOLE NR 12. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATESep 11, 2006 · N275 · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006084Barrel Nut · corrodedDURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 8. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATEDSep 11, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006080Spar · corrodedDURING 2C+12A+150M CHECK, FOUND CORROSION ON LT WING REAR SPAR UPPER CHORD UPPER SURFACE XORS 780 TO XORS 790.Sep 8, 2006 · N275 · Doug MD11F · Wing SparSDR WRLA2006088Barrel Nut · corrodedDURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 32. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABRICATEDSep 8, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006090Barrel Nut · corrodedITEM: DURING 2C+12A+150M CHECK WHILE COMPLYING WITH EO 02-5510-098 REV 4 INSPECTION, FOUND CORROSION ON HST LT BARREL NUT HOLE NR 35. ACCOMPLISHED BARREL NUT REMOVAL AND INSPECTION PER EO 02-5510-098 SEC06, REMOVED CORROSION AND OVERSIZED BARREL NUT HOLE, FABSep 8, 2006 · N275WA · Doug MD11F · Horizontal Stabilizer StructureSDR WRLA2006075Skin · corrodedDURING 2C+12A+150M CHECK, FOUND CORROSION ON LEFT WING UPPER SKIN AT XORS 97 TO XORS 1070 BETWEEN FRONT SPAR TO REAR SPAR.Sep 3, 2006 · N275 · Doug MD11F · Wing, Plate/SkinSDR WRLA2006076Skin · corrodedDURING 2C+12A+150M CHECK FOUND CORROSION ON RIGHT WING UPPER SKIN AT XORS 97 TO XORS 1070 BETWEEN FRONT SPAR AND REAR SPAR.Sep 3, 2006 · N275 · Doug MD11F · Wing, Plate/SkinSDR 06FDEA03098Trunnion · corrodedCENTER LANDING GEAR, RT TRUNNION AFT HOLE UPPER SURFACE FOUND CORRODED. COMPLIED WITH FEDEX E.A 1-5340-103487, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 27, 2006 · N621FE · Doug MD11F · Main Landing Gear Attach SectionSDR WRLA2006039Seal · blownRCH764/14 KGTB/KGTB DURING CLIMB (HYD 3 ELEV OFF) LEVEL 1 ILLUMINATED. HYD 3 WENT TO 3.8GAL. CONFERED WITH MX AND ACCOMPLISHED AIR RETURN TO KGTB. AFTER GEAR DOWN HYD 3 QUANTITY WENT TO 2.1 AND THE (HYD 3 QTY LOW) LEVEL 1 ALERT ILLUMINATED. FOUND HYD SYSTEM SAug 14, 2006 · N272 · Doug MD11 · Hydraulic System, MainSDR WRLA2006038Switch · inoperativeRCH964/10 EDDR/OKBK SH0RTLY AFTER ARRIVAL NOTICED SMOKE SMELL IN FORWARD GALLEY. PULLED C/B'S AND DEACTIVATED NR 3 OVEN. FOUND NR 3 OVEN SW VERY HOT, WITH AIRCRAFT POWER ON CB POPPED. ISOLATED PROBLEM TO THE SWITCH. PULLED CB'S, PLACED ITEM ON DMI AND INSTALLAug 10, 2006 · N271 · Doug MD11 · Buffet/GalleysSDR WRLA2006019Engine · flamed outNR 2 ENG FLAMED OUT APPROX 30 MINS INTO FLIGHT. PRECEDED BY A LEVEL 2 SELECT FADEC ALTN ALERT NR 2 EPR OBSERVED WITH AN AMBER X EGT DECREASING. FUEL OFF INDICATION IN THE FUEL FLOW DISPLAY. FADEC ALT SELECTED AND ENG RESTARTED. ALT TIME OF OCCURRENCE 360 DAug 1, 2006 · N272 · Doug MD11 · Engine (Turbine/Turboprop)SDR WRLA2006016Motor · leakingWOA8198/01 BGR/BGR AIR TURNBACK. ABOUT 10 MINS AFTER DEPT, HYD 3 OFF ALERT DISPLAYED (FLUID LOSS). RETURNED TO BGR WHEN SLATS WERE EXTENDED, HYD 3 FAIL ALERT DISPLAYED 0 FLUID. FOUND NR 1 STAB TRIM MOTOR LEAKING. REMOVED AND REPLACED STAB TRIM MOTOR. LEAK ANDJul 18, 2006 · N277 · Doug MD11 · Stabilizer ActuatorSDR WRLA2006015Charger · failedAIR TURNBACK DUE TO BATTERY DISCHARGING LEVEL 1 ALERT, INTERMITTENT BATTERY VOLTAGE 29V WHEN ALERT OFF. REPLACED BATTERY CHARGER AND BOTH AIRCRAFT BATTERIES, PERFORMED TEST ALL CHECK NORMAL PER MD11 AMM.Jul 4, 2006 · N272 · Doug MD11 · Battery/Charger SystemSDR WRLA2006012Adc · malfunctionedON DEPARTURE LOST FLT DIRECTOR PITCH BAR, GOT AMBER AUTO PILOT BOX, AND IAS AND ALT COMPARATOR ON BOTH SIDES. LOST AUTO THROTTLES. ACCOMPLISHED -AIRSPEED LOST, SUSPEND- CHECKLIST. DETERMINED CADC 2 WAS SUSPECT. DIVERTED TO ATLANTA. REMOVED AND REPLACED NRJun 6, 2006 · N272 · Doug MD11 · Air Data ComputerSDR WRLA2006013Pitot Tube · obstructedON DEPARTURE, FLIGHT DIRECTOR INOP BOTH SIDES AMBER A/P AND ATS BOXES IAS COMPARATOR BOTH SIDES. FA USING AIRSPEED LOST, SUSPECT ERROR. CHECKLIST DETERMINED. DETERMINED CADC NR 1 WAS AT FAULT. DIVERT TO ATL. FOUND FOD NR 1 PITOT TUBE. ALSO TUBE L/E ERODEJun 6, 2006 · N272 · Doug MD11 · Pitot/Static SystemSDR WRLA2006014Slide · deployedSLIDE BLOWN ON ARRIVAL. DH CREW MEMBER (1 OF 2) INADVERTANTLY PULLED WRONG HANDLE ATTEMPTING TO DISARM R1 DOOR FROM EMERGENCY ARM STATUS. NO ADVERSE EFFECTS. REMOVED BLOWN SLIDE RAFT AS PER MEL 52-10-3-2. R1 DOOR RESET. DMI'D M52JU0406-24 CAT C DUE 06/14/Jun 4, 2006 · N276 · Doug MD11F · Escape SlideSDR WRLA2006011Engine · flamed outDURING DESCENT NR 3 ENGINE FLAMED OUT. CONFIRMED ENGINE OUT ON MCDU NR 3 FUEL FLOW DROPPED TO 900 LBS AND DROPPING. IGNITION OVERRIDE ON ENGINE RETURNED TO NORMAL. TROUBLESHOT AS PER FIM 71-01-11 AND 71-01-01, FOUND TT2 NO SIGNAL FOR EECB AND GROUND ENGINE May 30, 2006 · N275 · Doug MD11F · Engine (Turbine/Turboprop)SDR WRLA2006010Control Cable · damagedAILERON BECAME JAMMED DURING CRUISE FLIGHT. FOUND RIGHT INBOARD AILERON TRIM CABLE DAMAGED SECTION 206 AND PULLEY DAMAGED. REMOVED TRIM CABLE AND PULLEY PER MM 27-10-00. INSTALLED NEW TRIM CABLE AND PULLEY, ADJUSTED TRIM CABLE PER MM 27-10-00. OPS CHECK GOMar 13, 2006 · N276 · Doug MD11F · Aileron Control SystemSDR WRLA2006007Actuator · malfunctionedAFTER TAKEOFF FROM SNN AND DURING CLIMB, WHEN FLAPS/SLATS WERE RETRACTED, A DEFLECTED AILERON DISAGREE ALERT MESSAGE WAS DISPLAYED ON THE SD ALONG WITH LEFT OUTBOARD AILERON INDICATING DEFLECTED. FLIGHT CREW FOLLOWED PROCEDURES AND RETURNED TO SNN, WHERE THE Mar 1, 2006 · N271 · Doug MD11 · Aileron Control SystemSDR WRLA2006008Fire Loop · defectiveAPPROXIMATELY ONE HOUR AFTER TAKEOFF FROM KWI, ENGINE-2 FIRE DETECTOR FAIL ALERT INTERMITTENTLY APPEARED ON THE SD. (NOTE SYSTEM 2-B FIRE DETECTION SYSTEM PREVIOUSLY ON MEL). FLIGHT CREW FOLLOWED PROCEDURES AND RETURNED TO KWI. EXPECTED FIX: REPLACE DEFECTMar 1, 2006 · N271 · Doug MD11 · Fire DetectionSDR WRLA2006005Tire · flatUPON TOUCHDOWN SPOILERS DEPLOYED AUTOMATICALLY, ONCE DEPLOYED ABS FAIL ALERT DISPLAYED AND AIRCRAFT WAS SLOWING NORMALLY. WHEN BRAKES WERE APPLIED CAPTAIN AND F/O FELT NO PRESSURE AND AIRCRAFT WAS HOLDING ON THE TAXIWAY JUST AT THE END OF RUNWAY. AIRCRAFT OVFeb 10, 2006 · N272 · Doug MD11 · TireSDR WRLA2006001Wire Harness · burnedREADING LIGHTS WENT OUT AFTER TAKEOFF, PAX SAW SPARKS, BURNING SMELL. FOUND OVERHEAD DECODER AND ONE WIRING HARNESS BURNED. REMOVED DECODER AND HARNESS RUNNING FORWARD TO READING LIGHTS, DEFERRED ITEM TO DMI M25JA1806-131 PER MEL 25-22-1 AND COLLARED CIRCUITJan 18, 2006 · N271 · Doug MD11 · Light System Wiring
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