GE CF6-50E2

Service difficulty reports · 401

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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 = 'CF650E2'
  ORDER BY difficulty_date DESC"

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SDR UIEA201000072Skin · crackedDURING C-CHECK, CRACKING WAS FOUND IN THE 65B94052-1, NR3 PYLON RT SKIN ASSY AT THE NAC STA 248 PRECOOLER EXHAUST. THE CRACK WAS REPAIRED BY TRIMMING OUT THE DAMAGE AND RESTORING THE SURFACE FINISH IAW RFTA 00664-0006, REV A AND REA MF00664R0006, REV A (FIG 1 Mar 26, 2010 · N540MC · Boeing 747243F · Nacelle/Pylon, Plate/SkinSDR UIEA201000077Beam · damagedDURING C-CHECK, DAMAGE WAS FOUND IN THE 65B04721-2 AFT LOWER CARGO DOOR LOWER BEAM WEB BETWEEN BS 1840 TO 1852. DAMAGE WAS TRIMMED OUT AND REPAIRED IAW NRC 786 AND SRM 51-40-03, FIG 1. THE 65B04721-2 WEB IS MADE FROM 0.125 INCH THICK 7075-0 SHEET IAW QQ-A-25Mar 26, 2010 · N540MC · Boeing 747243F · Fuselage Main, StructureSDR UIEA201000078Skin · damagedDURING C-CHECK, DAMAGE WAS FOUND IN THE 65B04144-3 SKIN AT BS 1790, S-38R. THE DAMAGE WAS TRIMMED OUT AND REPAIRED IAW NRC 732 AND SRM 53-30-03, FIG 1. THE 65B04144-3 SKIN IS MADE FROM 0.100 INCH THICK 2024-T3 CLAD ALUMINUM SHEET IAW QQ-A-250/5. THE REPAIR COMar 26, 2010 · N540MC · Boeing 747243F · Fuselage Main, Plate/SkinSDR UIEA201000069Bulkhead · crackedDURING C-CHECK, CRACKING WAS FOUND IN THE 65B94107-19 NAC STA 270 BULKHEAD UPPER WEB ASSY ON THE NR1 PYLON. THE WEB ASSY WAS REPLACED IAW DWG 65B94107 WITH MINOR DEVIATIONS IAW REA 00664R0002. THIS EO DOCUMENTS THE REPLACEMENT OF THE WEB IAW DWG 65B94107 AND Mar 25, 2010 · N540MC · Boeing 747243F · Nacelle/Pylon, Bulkhead/FirewallSDR UIEA201000070Stringer · crackedDURING C-CHECK, CORROSION AND CRACKING WAS FOUND IN THE 65B04161-17, STR 49L BETWEEN BS 2180 AND 2200. DAMAGE WAS TRIMMED OUT AND A NEW STR SECTION WAS INSTALLED IAW REA MF00664R0004. THE 65B04161-17 STRINGER IS MADE FROM BAC1498-144 EXTRUSION IN 7075-0 SHEEMar 25, 2010 · N540MC · Boeing 747243B · Fuselage Main, Longeron/StringerSDR UIEA201000075Cargo Track · damagedTHIS EO DOCUMENTS A MAJOR REPAIR. DURING C-CHECK, DAMAGE WAS FOUND TO THE AFT CARGO COMPARTMENT - BS1900 - BS1920, LBL24.75 CARGO TRACK WITH A CRACK (REF FIG 1) IAW SRM 53-10-23, FIG 5 (ITEM 3) THE CARGO TRACK IS MADE OF BAC1520-1682 (7178-T6511) EXTRUSION. PMar 20, 2010 · N540MC · Boeing 747243B · Fuselage, Seat/Cargo Attach FittingsSDR UIEA201000081Seat Track · crackedTHIS EO DOCUMENTS A MAJOR REPAIR. DURING C-CHECK, DAMAGE WAS FOUND TO THE MAIN DECK - BS1980, LBL98 - SEAT TRACK WITH A CRACK (REF FIG 1) IAW SRM 53-10-23, FIG 4C (ITEM 1) CARGO TRACK IS MADE OF BAC1520-1566 (7178-T6511) EXTRUSION. PERMANENT REPAIR WAS PERFORMar 20, 2010 · N540MC · Boeing 747243B · Fuselage, Seat/Cargo Attach FittingsSDR Q2S2010F00022Frame · corrodedWORKSHEET NR 0819, WORKCARD NR 53-176-02-01, LOWER FUSELAGE LT BODY FAIRING SUPPORT AT STA 880 FOUND CORROSION. REPLACED FRAME ASSY IAW SRM 51-30-02, REV 116.Mar 1, 2010 · N760SA · Boeing 747230B · Fuselage Main, FrameSDR Q2S2010F00020Strap · corrodedWORKSHEET NR 0628, WORKCARD 57-830-01-01. LT WING L/E FRONT SPAR UPPER CHORD STRAP AT APPROX OLES 1481 FOUND CORROSION. CORRODED STRAP REPLACED IAW SRM 51-30-02 REV 116. PN ON: 65B016877.Feb 26, 2010 · N760SA · Boeing 747230B · Wing SparSDR Q2S2010F00021Mount · corrodedWORKSHEET NR 0435, WORKCARD NR 71-012-01-03, ENGINE NR 3 AFT UPPER MOUNT FOUND WITH CORROSION. REPLACED ENGINE NR 3 AFT UPPER MOUNT IAW AMM 71-21-03, REV 142. PN ON: 65B94349-1, SN ON: SA-982.Feb 25, 2010 · N760SA · Boeing 747230B · Engine Mount SectionSDR UIEA201000018Fuel Filter · dirtyNR 3 ENGINE AT DESCENT NOTICED LOW POWER AND SHUT DOWN. LOW FUEL FLOW. ENGINE FAILURE/SHUT DOWN CHECK LIST ACCOMPLISHED NO ABNORMAL INDICATIONS SO ATTEMPTED RESTART WITH INFLIGHT START. LOW FUEL FLOW 200KGS, LESS THAN 26 PERCENT N1 LESS THAN 30 PERCENT N2, Feb 17, 2010 · N523MC · Boeing 7472D7B · Fuel Controlling SystemSDR UIEA201000068Skin · damagedDOORS - RT AFT MLG BODY DOOR SKIN DAMAGE - REPAIR. APPLIED A CHEMICAL CONVERSION COATING TO THE BARE SURFACES OF THE SKIN. REFER TO SRM 51-10-02. APPLY ONE LAYER OF BMS 10-79, TYPE II PRIMER TO THE BARE SURFACES OF THE SKIN. REF TO SOPM 20-44-04. INSTALLED TFeb 10, 2010 · N540MC · Boeing 747243B · Landing Gear DoorsSDR UIEA2010020400005Nozzle · crackedDURING AN ENGINE CHANGE AT AN A-CHECK, MX FOUND 3 EA CRACKS ON THE NR 4 ENG FIXED COWL EXHAUST NOZZLE FWD FLANGE COWL SUPPORT ASSY. THE CRACKS CAN BE REPAIRED IAW THE ESM TASK 78-33-05. REPAIR 002. THE REPAIR CALLS FOR A POST WELD HEAT TREATMENT AND THERMAL SPFeb 4, 2010 · N523MC · Boeing 7472D7B · Engine Collector/Tailpipe/NozzleSDR UIEA201000154Skin · corrodedDURING C-CHECK, CORROSION WAS FOUND BETWEEN BS 2020 AND 2040 AT S-46L IN THE 65B04151-2 FUSELAGE SKIN. THE DENT WAS TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-30-03, FIG 19. THE 65B04151-2 SKIN PANEL IS MADE FROM 0.063 INCH THICK 2024-T3 CLAD AJan 31, 2010 · N522MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA201000021Angle · corrodedCORROSION ON ANGLE AFT TO BULK CARGO BEAM BS 2200 S38-40R. DAMAGED AREA TRIMMED OUT AREA REINFORCED WITH DOUBLER IAW SRM 51-40-03, FIG 1.Jan 18, 2010 · N517MC · Boeing 747243B · Fuselage Miscellaneous StructureSDR UIEA201000026Floorbeam · crackedCRACK ON AFT CARGO FLOORBEAM UPPER CHORD BS 1860, LBL 47-48. TRIM THE UPPER FLANGE DAMAGED IAW SRM 51-40-04, FIG 3, REF EO 4753B236.Jan 18, 2010 · N517MC · Boeing 747243B · Fuselage Main, Floor BeamSDR UIEA201000027Frame · crackedPERFORMED BOROSCOPE INSP AND FOUND CRACK ON FRAME BY LENGTH 3" AT BS 360, S-2R END OF CRACK STOPPED BY STOPPING HOLE. REINFORCED AREA WITH DOUBLER & ANGLE PN N517MC-NRC677-1/2 IAW SRM 53-10-04, FIG 18. PERMANENT REPAIR PRIOR TO 20,000 CYCLES IAW EO 4753B240 PAJan 18, 2010 · N517MC · Boeing 747243B · Fuselage Main, FrameSDR UIEA201000028Stringer · crackedCRACK ON FWD CARGO STR 38 BS 480-500 RT. CRACKED AREA TRIMMED OUT, REINFORCED AREA WITH STRINGER SEGMENT PN N517MC-NRC624-1, IAW SRM 53-10-03 FIG 3 USING FASTENERS IAW SRM 51-30-02.Jan 18, 2010 · N517MC · Boeing 747243B · Fuselage Main, Longeron/StringerSDR UIEA201000029Stringer · damagedLIGHTING STRIKE ON FASTENER HEAD BS 340-440 STR-32AL. DRILLED OUT AND INSTALLED HI-LOCK HL63PB6-4 B/N 36457-01 IAW SRM 51-30-02, PERFORMED HFEC IAW D67170 PART 651-00-00 T-16 AND 23 NO CRACKS FOUND.Jan 18, 2010 · N517MC · Boeing 747243B · Fuselage Main, Longeron/StringerSDR UIEA201000030Skin · damagedEXTERIOR FUSELAGE SKIN EXT. B/O BY 09" X 0.6" X 0.039" ON EXT FUSELAGE SKIN BETWEEN STA 540-560 AT STR 37/R. A SKIN REPAIR WAS ACCOMPLISHED AT DAMAGED IAW REA: MF00656R0010 REV A. REPEAT INSP PRIOR TO 20,000 CYCLES.Jan 18, 2010 · N517MC · Boeing 747243B · Fuselage Main, Plate/SkinSDR UIEA201000153Stringer · corrodedDURING C-CHECK, CORROSION WAS FOUND ON THE 65B04483-13 STRINGER 51 LT AT BS 1918-1927. PART 1 - INTERIM REPAIR DO NOT SCHEDULE; THIS EO DOCUMENTS AN INTERIM REPAIR ACCOMPLISHED DURING THE JANUARY 2010 C-CHECK AT 14,764 TFC AND 87,026 TFH. INITIAL AND REPEAT Jan 18, 2010 · N517MC · Boeing 747243B · Fuselage Main, Longeron/StringerSDR Q2SA753006Mec · failedNORMAL THRUST TAKEOFF WAS ESTABLISHED ON RUNWAY AT EBLG. UPON INITIAL CLIMB AT APPROXIMATELY 2100 FT NR 2 ENGINE, FLAMED OUT. ADDITIONAL SHUTDOWN PROCEDURES WERE ACCOMPLISHED PER COMPANY GUIDELINES IN ADDITION TO THE DUMPING OF FUEL TO REDUCE LANDING WEIGHT.Dec 4, 2009 · N753SA · Boeing 747228F · Fuel Control/Turbine EnginesSDR EIAA200900126Pressure Switch · malfunctionedDURING CRUISE APPROX 7 HOURS INTO FLIGHT NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED FLASHING. RETARDED NR 2 THRUST LEVER, LIGHT CONTINUED TO FLASH. ACCOMPLISHED INFLIGHT ENGINE FAILURE AND SHUTDOWN PROCEDURE. FILTER BYPASS LIGHT REMAINED ON STEADY AFTENov 3, 2009 · N489EV · Boeing 747230B · Engine Oil PressureSDR Q2SA765001Duct · rupturedON TAKEOFF ROLL OUT OF VHHH ENGINE NR 4 HAD EXHAUST GAS TEMPERATURE OVERTEMP AS WELL AS NACELLE TEMPERATURE RISE. CREW CONTINUED TAKE OFF SUCCESSFULLY BUT ELECTED TO TERMINATE FLIGHT, DUMPED 137,000 LBS OF FUEL, RETURNED AND LANDED SAFELY AT VHHH. AFTER LANDNov 2, 2009 · N765SA · Boeing 7472F6B · Engine Bleed Air SystemSDR Q2SA760001Flex Duct · crackedON TAKEOFF CLIMBOUT OF EBLG ENGINE FIRE WARNING CAME ON FOR ENGINE NR 2, CREW ELECTED TO SHUTDOWN ENGINE NR 2, DUMPED 77,000 LBS OF FUEL, RETURNED TO AND LANDED SAFELY AT EBLG. AFTER LANDING MAINTENANCE CREW IN EBLG INSPECTED ENGINE NR 2 AND FOUND A CRACKED POct 30, 2009 · N760SA · Boeing 747230B · Pneumatic Distribution SystemSDR Q2SA795001Turbine Blades · nickedON TAKEOFF CLIMBOUT OF OAKN ENGINE NR 1 EXHAUST GAS TEMPERATURE REACHED 999 DEG CELSIUS FOR MORE THAN 90 SECONDS, CREW OPTED TO SHUTDOWN ENGINE NR 1 IN FLIGHT IN ACCORDANCE WITH QUICK REFERENCE HANDBOOK. CONTINUED FLIGHT TO OMSJ AND LANDED SAFELY. AFTER LANDOct 25, 2009 · N795SA · Boeing 747243F · Turbine SectionSDR Q2SA758007Fuel Filter · failedON TAKEOFF CLIMBOUT OF KJFK, ENGINE NR 1 AND ENGINE NR 4 FUEL FILTER BYPASS INDICATION LIGHTS CAME ON AND STAYED ON, CREW ELECTED TO TERMINATE FLIGHT, DUMPED 156,000 LBS OF FUEL, RETURNED TO KJFK AND LANDED SAFELY. AFTER LANDING MAINTENANCE CREW IN KJFK REPLAOct 24, 2009 · N758SA · Boeing 747281F · Engine Fuel DistributionSDR Q2SA754006Clamp · looseIN CRUISE, ENGINE FIRE WARNING ACTUATED FOR ENGINE NR 2, CREW BROUGHT ENGINE NR 2 TO IDLE POWER AND OPTED TO SHUTDOWN THE ENGINE IN ACCORDANCE WITH QUICK REFERENCE HANDBOOK. NO ENGINE FIRE EXTINGUISHING DEVICE WAS USED, CREW CONTINUED FLIGHT TO DGAA AND LANDEOct 23, 2009 · N754SA · Boeing 747228F · Engine Bleed Air SystemSDR UIEA201000184Skin · damagedDURING JACKING OF DATUM AIRPLANE, MX DAMAGED THE FUSELAGE SKIN SECTION 48 - BS2594.5 AT S-26R (ABOVE THE TAIL JACK PAD). MEASURING 2.5 IN. D AND 0.437 IN DEPTH. THE DAMAGE IS LOCATED APPROX 3.5 IN FWD OF BS 2598 BUTT JOINT. "INTERIM REPAIR PERFORMED AS DESCRIBOct 17, 2009 · N540MC · Boeing 747243B · Fuselage Main, Plate/SkinSDR Q2SA746011Fairing · inflt separationON POST-FLIGHT INSPECTION, FOUND SECTION 44 UPPER RT WING-TO-BODY FAIRING PANEL (NR 292DR) MISSING, WITH BROKEN ATTACH BRACKETS ON ACFT STRUCTURE. REPLACED DAMAGED PANEL AND SUPPORT BRACKETS IN ACCORDANCE WITH B747 SRM 51-30-02 AND 51-20-01.Apr 27, 2009 · N746SA · Boeing 747206B · Aerodynamic FairingsSDR UIEA201000182Nozzle · damagedPUNCTURE ON THE LONG FIXED CORE EXHAUST NOZZLE (LFCEN) ON THE NR 2 ENGINE. THE PUNCTURE IS APPROX 0.25" WIDE, APPROX 5.0 INCHES FROM THE T/E OF THE EXHAUST SLEEVE AT THE 3:00 POS. SMOOTH THE EDGES OUT USING STANDARD PRACTICES AND ELEMENTARY OPERATIONS. REPLACEApr 21, 2009 · N523MC · Boeing 7472D7B · Engine Collector/Tailpipe/NozzleSDR Q2SA758006Slide · unwanted deployPRIOR TO DEPARTURE FROM KJFK, LEFT UPPER DECK EMERGENCY EXIT SLIDE INADVERTENTLY DEPLOYED. REMOVED SLIDE IN ACCORDANCE WITH AMM 25-68-02. TRANSFERRED TO DEFERRED MAINTENANCE ITEM NR 18844 PER MEL 25-11, CAT. C. PLACARD INSTALLED.Apr 20, 2009 · N758SA · Boeing 747281F · Escape SlideSDR EIAA20090055Oil System · low pressureDURING CRUISE AT FL 310, NR 4 ENGINE OIL PRESSURE ILLUMINATED. CHECKED OIL QUANTITY GAUGE IT READ ZERO, AND OIL PRESSURE READ 10 PSI. SHUTDOWN ENGINE USING IN-FLIGHT FAILURE AN SHUT DOWN CHECKLIST. WINDMILL FOR 76 MIN, NOTIFY ATC AND DISPATCH, DUMPED FUEL AApr 20, 2009 · N489EV · Boeing 747230B · Engine Oil Indicating SystemSDR Q2SA748009Door · crackedDURING CRUISE INBOUND TO KMIA, CREW REPORTED MAIN DECK WINDOW 850R SOUNDED LIKE AIR LEAK. FURTHER INSPECTION ON GROUND REVEALED 9 INCH CRACK IN MAIN ENTRY DOOR 2R SIDE FRAME. DOOR ASSEMBLY REMOVED AND REPLACED IN ACCORDANCE WITH AMM 52-11-01/PG 401.Apr 17, 2009 · N748SA · Boeing 747206B · Passenger/Crew DoorsSDR Q2SA746010Slide · unwanted deployINADVERTENTLY DEPLOYED LEFT UPPER DECK SLIDE WHILE AIRCRAFT WAS ON GROUND AT KMIA. REMOVED SLIDE IN ACCORDANCE WITH AMM 25-68-02. TRANSFERRED TO DEFERRED MAINTENANCE ITEM NR 18822 PER MEL 25-11 (3). PLACARD INSTALLED.Apr 15, 2009 · N746SA · Boeing 747206B · Escape SlideSDR Q2SA758005Pms · inactiveCLIMB-OUT OF EBLG, PERFORMANCE MANAGEMENT SYSTEM (PMS) LIGHT ILLUMINATED IN FLIGHT AND AUTOPILOTS "A" AND "B" WOULD NOT FOLLOW FLIGHT MANAGEMENT SYSTEM (FMS) COMMAND. AIR TURN BACK TO EBLG. NO FUEL DUMPED. OPERATIONALLY CHECKED IN ACCORDANCE WITH DELCO OPERMar 17, 2009 · N758SA · Boeing 747281F · Flight Management Computing Hardware SystemSDR Q2SA748008Wire Harness · chafedON TAXI-OUT AT SKBO, WIND SHEAR LIGHT CAME ON WHEN THROTTLE ADVANCED. MULTIPLE FAILURES, WIND SHEAR LIGHT FLICKERED AND WENT OFF, THEN SMOKE CAME UP THROUGH THROTTLE QUADRANT; LOST GEAR DOWN GREEN LIGHT, AND ANTI-SKID LIGHT ILLUMINATED ON FWD PANEL; LOST ANTIMar 14, 2009 · N748SA · Boeing 747206B · Light System WiringSDR Q2SA748007Battery Pack · dischargedDURING PRE-FLIGHT FROM KMIA, FOUND FORWARD AND AFT UPPER DECK EMERGENCY EXIT SIGNS INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS IN ACCORDANCE WITH AMM 33-51-04.Mar 5, 2009 · N748SA · Boeing 747206B · Emergency LightingSDR Q2SA746009Panel · detachedON TOP OF CLIMB-OUT, CREW EXPERIENCED AIRFRAME VIBRATION, SUBSEQUENTLY PERFORMING FUEL DUMP (30,000 LBS) AND AIR TURN BACK TO KMIA. ON INSPECTION AFTER LANDING, FORE AND MID-FLAP DAMAGE WAS FOUND ON RIGHT WING, RESULTING FROM RIGHT WING FLIGHT PANEL HAVING DEJan 15, 2009 · N746SA · Boeing 747206B · Trailing Edge FlapsSDR UIEA200900002Blades · missingDURING DESCENT CREW REPORTED SIGNIFICANT VIBRATION FROM NR 1 ENGINE. INSPECTION FOUND MISSING BLADES IN THE LPT AREA. ENGINE CHANGE IS IN PROGRESS.Dec 30, 2008 · N809MC · Boeing 747228F · Turbine SectionSDR Q2SA753005Sensor · failedON TAKE-OFF FROM LEIGE, BELGIUM (EBLG), NR 2 ENGINE FLAMED OUT. LOUD NOISE HEARD AND AIRCRAFT YAWED LEFT. IGNITION AND ENGINE ANTI-ICE IN USE. ENGINE RELIGHT AT 3000' AGL, ALL PARAMETERS NORMAL. AIRCRAFT CONTINUED TO DESTINATION AT DOHA, QATAR (OTBD). NO Dec 25, 2008 · N753SA · Boeing 747228F · Fuel Controlling SystemSDR Q2SA758004Thrust Reverser · deployedON CLIMB-OUT FROM ADDIS ABABA, ETHIOPIA (HAAB), AIRCRAFT PERFORMED AN AIR TURN BACK DUE TO INDICATION OF NR 4 ENGINE THRUST REVERSER TRYING TO DEPLOY IN FLIGHT. CREW WAS ALERTED BY THRUST REVERSER VALVE LIGHT AND TRANSIT LIGHT ILLUMINATING. CREW RETURNED TO Dec 21, 2008 · N758SA · Boeing 747281F · Engine Thrust ReverserSDR Q2SA751007Rod End · shearedAFTER DEPARTURE FROM LAGOS, NIGERIA (DNMM), RIGHT BODY GEAR DOOR WOULD NOT INDICATE CLOSED WITH GEAR RETRACTED. FLIGHT CREW FOLLOWED QRH. UNABLE TO CONTINUE TO DESTINATION DUE TO INCREASE FUEL BURN. AIR TURN BACK. NO FUEL DUMP PERFORMED. INSPECTION CONFIRDec 16, 2008 · N751SA · Boeing 747228F · Landing Gear ActuatorSDR Q2SA783002Pitot Line · brokenON DEPARTURE FROM KJFK, CAPTAIN'S POSITION LOST ALL PRIMARY INSTRUMENTS (AIRSPEED, ALTITUDE, IVSI INDICATORS). AIR TURN BACK TO KFJK, NO FUEL DUMP PERFORMED. CADC REPLACED AND BROKEN PITOT LINE FOUND BEHIND CAPTAIN'S ALTIMETER.Dec 15, 2008 · N783SA · Boeing 747281F · Pitot/Static SystemSDR Q2SA753004Pump · defectiveON CLIMB-OUT FROM EBLG (LIEGE, BELGIUM), NR 2 ENGINE FILTER BYPASS LIGHT ILLUMINATED, THEN WENT OUT. APPROXIMATELY 3 MINUTES LATER, NR 2 ENGINE FLAME OUT OCCURRED. IN FLIGHT ENGINE START COMPLETED. 3 HOURS, 20 MINUTES LATER AT FL350, FILTER BYPASS LIGHT ILLNov 23, 2008 · N753SA · Boeing 747228F · Engine Fuel PumpSDR UIEA200800340Connector · defectiveAIR TURN BACK. NR 1 ENGINE OIL TEMP OFF SCALE HIGH FOR AT LEAST 10 MINUETS . ENGINE SHUT DOWN. WIRING CHECKS ACCOMPLISHED AND FOUND NR 1 OIL TEMP SENSOR CONNECTOR DEFECTIVE . CONNECTOR REPLACED AND ALL OPERATIONS NORMAL. ENGINE RUN UP NORMAL. NR 1 ENGINE OIL Nov 13, 2008 · N524MC · Boeing 7472D7B · Engine Oil System WiringSDR CNMA20080010Engine · malfunctionedNR 2 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED AT TOP OF CLIMB (29,000) INTERMITTENTLY. LIGHT BECAME SOLID AFTER 3 MINUTES. ENGINE SHUTDOWN IN FLIGHT IAW QRH PROCEDURE 4-1-2-19 AND CORRESPONDING CHECKLISTS. COMPLETED WORTAN 08-0368 R&R NR 2 ENGINE OIL STRANov 2, 2008 · N270AX · Doug DC1030 · Engine (Turbine/Turboprop)SDR UIEA200800333Element · false activationDURING CLIMBOUT AT 17000 FEET NR 2 ENGINE FIRE WARNING BELL AND LIGHT CAME ON. ACCOMPLISHED CHECKLIST, BOTH FIRE BOTTLES WERE DISCHARGED, HYD PUMP SUPPLY OFF FOR 1 HOUR AND 30 MINUTES NR 2 FIRE WARNING LIGHT AND NACELLE TEMP STAYED AT 7.9 AND 8.9 AFTER BLOCK Oct 11, 2008 · N540MC · Boeing 747243B · Fire DetectionSDR Q2SA789001Compressor · stalledEN ROUTE FROM SPIM TO KMIA DURING CLIMB AND CRUISE, NR 2 ENGINE EXPERIENCED HIGHER EGT READING (70 DEG) THAN OTHER ENGINES. REDUCED THRUST SETTINGS ON NR 2 ENGINE LOWERED HIGHER EGT READING TO 30 DEG ABOVE OTHER ENGINES, WITH NO ROUGHNESS OR APPARENT ENGINE IOct 10, 2008 · N789SA · Boeing 747341 · Turbine Engine Compressor SectionSDR Q2SA758003Engine · damagedDURING TAKEOFF AFTER V1 FROM HAAB, BIRD INGESTION INTO NR 3 ENGINE. AIR TURNBACK TO HAAB. FUEL DUMP OF 50,000 LBS. INSPECTION AFTER LANDING CONFIRMED DAMAGE TO NR 3 ENGINE FAN BLADES, AS WELL AS EVIDENCE OF BIRD STRIKE ON NR 2 ENGINE. NR 1, 3, 4, 6, 11, 13Oct 9, 2008 · N758SA · Boeing 747281F · Engine (Turbine/Turboprop)
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