GE CF6-6D

Service difficulty reports · 1,051

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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 = 'CF66D'
  ORDER BY difficulty_date DESC"

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SDR FDEA201004141187Shear Tie · corrodedFWD CARGO COMPARTMENT BILGE AREA HAS CORROSION ON A FRAME AT BS 879 BETWEEN STRINGER 47L AND STRINGER 48L. REMOVED CORROSION ON SHEAR CLIP REF SRM 51-21-02, VOL II. ORIGINAL THICKNESS 0.071 REF SRM 53-13-01, VOL I. MATERIAL REMOVED 0.040. MATERIAL REMAINApr 14, 2010 · N361FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR FDEA201004141184Shear Tie · corrodedCTR PIT SHEAR TIE IS CORRODED AT FS 1661; LONGERON 48R. REMOVED SHEAR TIE REF SRM 51-31-01, VOL II. REMOVED CORROSION WITH 100 PERCENT MATERIAL LOSS AND IS OUT OF LIMITS REF 53-00-01, VOL I. FABBED NEW SHEAR TIE REF DAC DWG ADA 3677, REV "B". ALODINED, PRIMApr 14, 2010 · N361FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR FDEA201004141189Shear Tie · corrodedCTR PIT SUMP AREA SHEAR TIE CLIP IS CORRODED AT FS 1712; LONGERON 48R. REMOVED SHEAR TIE IN THE CTR PIT FS 1712, DAC DWG AFA 3901, REV F. RECEIVED HEAT TREATED PART TRACKING NR 2010-0149, PO NR 680560. FABBED LOCATED AND DRLLED UP IAW SRM 53-30-00, FIG 10, Apr 14, 2010 · N361FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR FDEA201004131171Stringer · corrodedSTRINGER AFT END IS CORRODED FROM BS 1219 TO 1239 STR 20L. CORROSION ON ORIGINAL STRINGER WAS FOUND OUT OF LIMITS IAW SRM 53-00- 01, PG 8; VOL I. MACHINED NEW STRINGER IAW DAC DWG NR AEA0355, REV "B". ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. INSTALLEApr 13, 2010 · N361FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201004131172Longeron · corrodedMAIN CABIN INTERIOR LONGERON IS CORRODED FROM BS 1381 TO BS 1401; LONGERON 17L TO LONGERON 17L. REMOVED CORROSION IAW SRM 53-00-01, VOL I. ORIGINAL MATERIAL THICKNESS 0.135. REMOVED MATERIAL 0.020. REMAINING MATERIAL THICKNESS 0.115 AND FOUND TO BE WITHIN Apr 13, 2010 · N361FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201004121164Spool · crackedMCD SPOOLS - NR 7 SPOOL LOCATION HAS CRACK INDICATIONS AT A, B, C & D HOLES. REAMED HOLES "A", "B" , "C" AND "D" TO 0.520" IAW SRM 53-50-00, FIG 17, VOL I. FABRICATED AND INSTALLED BUSHINGS IN HOLES "A", "B", "C", "D" IAW SRM 53-50-00, FIG 17, VOL I. REApr 12, 2010 · N361FE · Doug MD1010F · Cargo/Baggage DoorsSDR FDEA201004121165Skin · gougedRT WING INBD AILERON, UPPER INBD EDGE IS WORN AND GOUGED. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS (ORIGINAL 0.040; REMAINING 0.022 IAW SRM 57-00-01, VOL I. REMOVED SKIN PANEL IAW SRM 51-35-01, VOL II. FABRICATED SKIN PANEL IAW DWG ARC 1316, REV "C". PEApr 12, 2010 · N361FE · Doug MD1010F · AileronsSDR FDEA201004121150Beam · crackedMCD SPOOLS - NR 1 SPOOL HAS CRACK INDICATIONS AT C & D HOLES. REAMED HOLES "C" AND "D" TO 0.520 ' IAW SRM 53-50-00, FIG 17, VOL I. NO CRACKS NOTED. FABRICATED AND INSTALLED BUSHING IAW SRM 53-50-00, FIG 17, VOL I.Apr 12, 2010 · N361FE · Doug MD1010F · Fuselage Main, StructureSDR FDEA201004121159Beam · crackedMCD SPOOLS -NR 2 SPOOL HAS CRACK INDICATIONS AT C HOLE. REAMED HOLE "C" TO 0.520 ' IAW SRM 53-50-00, FIG 17, VOL I. NO CRACKS NOTED. FABRICATED AND INSTALLED BUSHING IAW SRM 53-50-00, FIG 17, VOL I.Apr 12, 2010 · N361FE · Doug MD1010F · Fuselage Main, StructureSDR FDEA201004121160Beam · crackedMCD SPOOLS - NR 3 SPOOL HAS CRACK INDICATIONS AT HOLES C & D. REAMED HOLES "C" AND "D" TO 0.520 ' IAW SRM 53-50-00, FIG 17, VOL I. NO CRACKS NOTED. FABRICATED AND INSTALLED BUSHINGS IAW SRM 53-50-00, FIG 17, VOL I.Apr 12, 2010 · N361FE · Doug MD1010F · Fuselage Main, StructureSDR FDEA201004121161Beam · crackedMCD SPOOLS - NR 4 SPOOL HAS CRACK INDICATIONS AT HOLES C & D. REAMED HOLE "C" TO 0.520 ", HOLE "D" TO 0.460" IAW SRM 53-50-00, FIG 17, VOL I. NO CRACKS NOTED. FABRICATED AND INSTALLED BUSHING FOR HOLE "C" IAW SRM 53-50-00, FIG 17, VOL I. NO BUSHING REQUIRApr 12, 2010 · N361FE · Doug MD1010F · Fuselage Main, StructureSDR FDEA201004081101Former · crackedLT WING L/E PANEL SUPPORT IS CRACKED AT WING STA XORS 770. REMOVED FORMER IAW SRM 51-33-01, VOL II. FABRICATED NEW -21 FORMER IAW DAC DWG ARB 1164, REV "M". ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. INSTALLED -21 FORMER IAW SRM 51-33-01, VOL II AND DACApr 8, 2010 · N361FE · Doug MD1010F · Wing Miscellaneous StructureSDR FDEA201004081103Support · crackedLT WING L/E PANEL SUPPORT IS CRACKED AT WING STA XFS 455. REMOVED CRACKED SUPPORT AND INSTALLED NEW SUPPORT IAW SRM 51-35-01, PG 1, VOL II; SRM 51-33-01, PG 1, VOL II AND DAC DWG ARB 1162, REV "S". RECEIVED MATERIAL ID 7075-0 0.050 IAW DAC DWG ARB 1162, REVApr 8, 2010 · N361FE · Doug MD1010F · Wing Miscellaneous StructureSDR FDEA201004061078Floorboard · delaminatedAFT CARGO COMPARTMENT FLOORBOARD 187 CF IS DELAMINATED AND DENTED AT SEVERAL LOCATIONS. FABRICATED NEW AFT CARGO FLOOR PANEL 187 CF IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".Apr 6, 2010 · N361FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201004061082Floorboard · delaminatedAFT CARGO COMPARTMENT FLOORBOARD 187 HF IS DELAMINATED AND DENTED AT SEVERAL LOCATIONS. FABRICATED NEW AFT CARGO FLOOR PANEL, 187 HF IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".Apr 6, 2010 · N361FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201004061083Floorboard · delaminatedAFT CARGO COMPARTMENT FLOORBOARD 187 AF IS DELAMINATED AND DENTED AT SEVERAL LOCATIONS. FABRICATED NEW AFT CARGO FLOOR PANEL, 187 AF, IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".Apr 6, 2010 · N361FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201004061084Floorboard · delaminatedAFT CARGO COMPARTMENT FLOORBOARD 187 EF IS DELAMINATED AND DENTED AT SEVERAL LOCATIONS. FABRICATED NEW AFT CARGO FLOORBOARD, 187 EF, IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".Apr 6, 2010 · N361FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201004061085Floorboard · delaminatedAFT CARGO COMPARTMENT FLOORBOARD 187 GF IS DELAMINATED AND DENTED AT SEVERAL LOCATIONS. FABRICATED NEW AFT CARGO FLOOR PANEL 187 GF IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".Apr 6, 2010 · N361FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201004061088Web · crackedNR 1 RT SLAT DAMAGED AT INBD WEB/RIB STRUCTURE R & R FITTING PN ARB701602 IAW DWG ARB 7016 VIEW CC AND SRM 51-31-01, VOL II. R & R WEB PN ARB7128-24 IAW SRM 51-33-01 VOL II AND DRWN ARB7128-24.Apr 6, 2010 · N362FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201004031050Engine · flamed outENGINE FLAMEOUT AT FL350. RESTART ATTEMPTED DURING DESCENT/DIVERT. DURING RESTART ATTEMPT, OIL PRESSURE WENT TO "0" (ZERO). "ENGINE FIRE, OR SEVERE DAMAGE" CHECKLIST ACCOMPLISHED. DIVERTED. TO PIT. CHECKED MAIN OIL FILTER CHIP DETECTOR. DETECTOR IS VERY CApr 3, 2010 · N68052 · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201003271019Spar Cap · crackedRT WING REAR SPAR REPAIR IAW EA 8-5710-138106, PART 1 INSTRUCTIONS. INTERIM REPAIR ACCOMPLISHED IAW EA NR 8-5710-138106 PART 1, REPETITIVE INSP AT 1650 FLT CYC INTERVALS AND FINAL RESTORATION TO BE ACCOMPLISHED PRIOR TO ACFT REACHING 39357 FLT CYC REF: EA NMar 27, 2010 · N388FE · Doug MD1010F · Wing SparSDR FDEA201003261013Spar Cap · crackedRT WING INBD FLAP; INBD FLAP WEDGE UPPER INBD L/E CORNER "T" CAP IS CRACKED. REMOVED SPAR CAP REF SRM 51-35-01, VOL II. FABBED NEW SPAR CAP REF DAC DWG ARC 2450, REV "K". ALODINED AND PRIMED SPAR CAP REF SRM 51-21-01, VOL II. SPAR CAP AND SKIN REF SRM 51-71Mar 26, 2010 · N570FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201003250993Hinge Fitting · corrodedLT WING; OTBD FLAP, OTBD HINGE FITTING, NR 10 BARREL NUT HOLE IS CORODED. REPAIRED NR 10 BARREL NUT HOLE IAW EA 8-5750-136633 "WINGS - LT WING OTBD FLAP HINGE FITTING" AND DAC CMM 57-44-09.Mar 25, 2010 · N570FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201003251006Skin · damagedRT WING, INBD FLAP, LOWER SURFACE, OTBD WEDGE SECTION, JUST BELOW THE OUTBD HINGE FAIRING, APPROX 14 INCHES FROM THE T/E AT STA XW 273.000 HAS SKIN DAMAGE/ PUNCTURE 9" H X 10" W. REMOVED DAMAGED SKIN IAW MD/DC10-10 SRM 51-31-01, VOL II. FABRICATED NEW SKINMar 25, 2010 · N570FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201003160836Cable · failedNR 2 THROTTLE STUCK AT 93 PERCENT AT FL 340 LOWER ALTITUDE AND STARTING APU AIRBORNE DID NOT UNFREEZE THROTTLE. SHUT NR 2 DOWN IAW QRH WINDMILLED FOR 17 MINUTES. RAN NR 2 ENG FOR A MINIMUM OF 3 MINUTES TO OIL/LUBE BRGS, BECAUSE OF WIND MILLING DUE TO INFLMar 16, 2010 · N398FE · Doug MD1010F · Power LeverSDR FDEA201003090703Skin · gougedNR3 ENG RT THRUST REVERSER COWL FWD HINGE PANEL IS GOUGED AND LOOSE. THRUST REVERSER FWD HINGE PANEL 50 PERCENT MATERIAL LOSS; FOUND TO BE OUT OF LIMITS IAW EM 78-32-12, PG 2. R & R DAMAGED SKIN IAW SRM 51-10-00, VOL II; SRM 51-21-00, VOL II; SRM 51-21-01, VMar 9, 2010 · N570FE · Doug MD1010F · Engine Thrust ReverserSDR FDEA201003070654Skin · misrepairedEXISTING REPAIR - LT WING NR3 SLAT REPAIR PATCH (2 EACH) FOUND ON INBD OUTER SKIN AREA. EXISTING REPAIR (2 EACH) AT LT WING NR 3 SLAT ON INBD OUTER SKIN AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR PATCH (2Mar 7, 2010 · N601FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201003030621Skin · wornNR 1 ENG RT THRUST REVERSER LATCH HANDLE, FWD PANEL, FWD EDGE IS WORN. THRUST REVERSER FWD HINGE PANEL WORN AREA EXCEEDS LIMITS IN 3 AREAS IAW EDGE 0.250 WIDE STATED IN EM 78-32-10. R & R DAMAGED SKIN IAW ASTME 1476-04; SRM 51-10-00, VOL II, SRM 51-21-01, VOMar 3, 2010 · N570FE · Doug MD1010F · Engine Thrust ReverserSDR FDEA201003030626Stiffener · crackedRT WING UPPER L/E PANEL 616 ET INNER SURFACE HAS 3 EA CRACKED STIFFENERS. PANEL 616 ET REQUIRES SRM REPAIR IAW SRM 57-10-00, VOL I. MATERIAL VERIFICATION 7075-0 0.040, PO NR 657517.2. FORMED REPAIR STIFFENERS AND FABRICATED REPAIR STIFFENERS IAW SRM 57-10-Mar 3, 2010 · N570FE · Doug MD1010F · Wing Miscellaneous StructureSDR FDEA201003020592Stiffener · crackedLT WING UPPER L/E PANEL 516 ET HAS 3 EA INNER STIFFENERS CRACKED. RECEIVED MATERIAL ID 7075-0 0.040 TO FORM 3 REPAIR STIFFENERS AND HEAT TREAT TO 7075-T6 0.040 IAW SRM 57-10-00, PG 83, VOL I. FABRICATED 3 REPAIR STIFFENERS IAW SRM 57-10-00, PG 83, VOL I. APMar 2, 2010 · N570FE · Doug MD1010F · Wing Miscellaneous StructureSDR FDEA201001200199Mec · failedNR 3 ENGINE LOST POWER AND WAS UNRESPONSIVE. STARTED TO HANG AT RPM, GOT ENG 3 RPM LOW, THEN NR 3 GEN OFF. ENG WAS STILL RUNNING, OIL PRESS WAS LOW, BUT NO LOW OIL PRESS ALERT. PROGRESSIVELY WORSE RESPONSE. ENGINE WAS SHUTDOWN ON APPROACH. R & R OF MECJan 20, 2010 · N368FE · Doug MD1010F · Fuel Controlling SystemSDR FDEA201001190177Wire · damagedACFT AIR TURNBACK, NR 2 EGT SHOWED AMBER "X"ON CLIMBOUT. SPORADICALLY CAME BACK WITH ERRATIC READINGS. RTB AFTER CONFORMATION WITH MOCC. REMOVED AND REPLACED AIU'S 1 & 3. WAITING HIGH POWER RUN. REPAIRED WIRE 2H2704F22 GOING TO R5-8212 PIN B WITH BLUE SPJan 19, 2010 · N359FE · Doug MD1010F · Engine Indicating System WiringSDR FDEA200912024328Ecu · malfunctionedLEAVING FL 180 ON DESCENT NR 3 ENG RPM LOW INDICATION. N1 20 PERCENT,N2 50 PERCENT, EGT 400. NO OBVIOUS DAMAGE TO ENGINE. ATTEMPTED RE-START AND ENGINE RE-STARTED BUT INDICATIONS ONLY WENT BACK TO N1 20 PERCENT, EGT 400, AND N2 50 PERCENT. ENG HUNG THERE Dec 2, 2009 · N365FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA200909273392Engine · malfunctionedABORT TAKEOFF, 75 KNOTS, ENG 3 EXCEEDANCE ON N2 PEAK 101, .2 RED: 101.0 FOR 2.3 SECONDS NO RESTRICTION, REF: AMM 72-00-00-6, NR 3 ENGINE N2 EXCEEDANCE 101.2 WILL REQUIRE CORE COMPRESSOR AND HPT BORESCOPE WITH IN 10 CYCLES INSPECTED EXHAUST NOZZLES FOR PARTISep 27, 2009 · N366FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA200909263389Sensor · failedFLT 3707. NR 2 ENGINE ROLLED BACK ON TAKEOFF, MAX N1 WAS 84 PERCENT, ENGINE FAIL LIGHT ON. CKED VIA'S AND HAD NR 2 ENG N1 FAILED MSG -PROBABLE CAUSE ENG 2 TACHOMETER. REPLACED NR 2 ENG FAN SPEED SENSOR/N1 TACH PER AMM 77-11-01-2 OPS CKS NRML, RAN ENG TO T/Sep 26, 2009 · N564FE · Doug MD1010F · Engine RPM Indicating SystemSDR FDEA200909173323Relay · malfunctionedREJECTED T/O DUE TO: LEVEL 1 ALERT: REV 1, PRESS FAIL T, DUPLICATED REV 1 PRESS FAULT ON 3 DIFFERENT TAXI/RUN-UP TESTS IAW JRH CHAPT 5 AND CHPT 4-8. REMOVED AND REPLACED NR 1 T/R ACTUATION SYS LOCK RELAY BOX IAW MM 78-33-10-6 AND CHECKED IAW MM 87-33-10-4. Sep 17, 2009 · N362FE · Doug MD1010F · Engine Thrust ReverserSDR FDEA200909053259Lead · failedENG 2 EGT HI" LEVEL ONE ALERT DURING DESCENT. EGT WAS 1092 IN RED.MOVED THROTTLE TO IDLE, APPROX 20 SECONDS LATER ALERT CHANGED TO LEVEL 1 "ENG 2 EXCEEDAMCE", TEMP INDICATION DECREASED TO AROUND 900. APPROX 10 SECONDS LATER TEMP INCREASED ABOVE RED LINE WSep 5, 2009 · N554FE · Doug MD1010F · Engine Indicating System WiringSDR FDEA200907202679Engine · malfunctionedREJECTED T/O PDX 28L NR 2 ENGINE N2 EXCEEDENACE 90KTS. INSPECTED EXHAUST FOR PARTICLES NONE FOUND. ACFT OK FOR SERVICE. REMOVED BOROSCOPE PLUGS FOR INSPECTION AND INSTALLED AND SAFTIED PLUGS AFTER COMPLETION OF INSPECTION REF MM 72-00-00-6.Jul 20, 2009 · N387FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA200907032471Thermocouple · inoperativeDURING CLIMB, ENG CLIMB POWER ENG 1 EGT EXCEEDENCE 993'C MAX. TOTAL EXCEEDENCE TIME APPROX 15 SEC. NO ERRATIC N1, N2, OR F/F. EGT ROSE GRADUALLY & THEN SLOWLY DECLINED AS THROTTLE REDUCED TO IDLE. EGT IN LIMITS WITH THROTTLE REDUCED. NO FIRE WARNINGS. ATJul 3, 2009 · N399FE · Doug MD1010F · Engine Temperature Indicating SystemSDR FDEA200905051541Throttle · bindingON DESCENT NR 2 THROTTLE WAS BINDING AND WOULD NOT RETARD TO IDLE POSITION UNTIL TOUCHDOWN. REMOVED AND REPLACED NR 2 ENGINE THROTTLE PUSH PULL CABLE.May 5, 2009 · N385FE · Doug MD1010F · Power LeverSDR FDEA200904211369Push-Pull Cable · stuckAT FL 360 IN CRUISE NR 1 AND NR 3 THROTTLES RAPIDLY CAME TO IDLE WHILE NR 2 STAYED AT ITS CRUISE SETTING (95.4). DISCONNECTED AUTO THROTTLES AND TRIED TO MARRY THROTTLES. NR 2 WAS FROZEN AND REMAINED FROZEN THROUGHOUT FLIGHT. IN DESCENT HAD TO SHUTDOWN ENGApr 21, 2009 · N395FE · Doug MD1010F · Power LeverSDR FDEA200903060858Line · looseNR 2 ENG OIL QTY DROPPED FROM 12 QTS TO 3 QTS IN 2HRS. TEMP/PRESS NORMAL. DECREASED TO 2 QTS AT IDLE WITH DECREASING PRESSURE. SHUTDOWN NR 2. NR 2 ENG AND FOUND LINE LOOSE FROM NR 2 ENG OIL SCAVENGE FILTER BOWL TO THE OIL STRAINER CLOGGING SWITCH.Mar 6, 2009 · N362FE · Doug MD1010F · Turbine Engine Oil SystemSDR FDEA200902120514Fuel Control · malfunctionedNR 3 ENG ROLLBACK AT FL370, ENG IGN OVERRIDE ON. ENGINE RESTARTED ITSELF AT FL 270 IN CLOUDS -10C WITH ALL ENG ANTI-ICE ON. ROLL BACK RESULTED IN N1 OF 48 PERCENT & FUEL FLOW OF 1000. EGT OF 570. PERFORMED INSPECTION OF NR 3 ENGINE INLET & EXHAUST NO DEFEFeb 12, 2009 · N68050 · Doug MD1010F · Fuel Control/Turbine EnginesSDR FDEA200812085106Sleeve · dentedNR 2 ENGINE LEFT TRANSLATING COWL OUTER SKIN IS DENTED. REPAIRED NR 2 LEFT TRANSLATING SLEEVE/COWL OUTER SKIN BY DRILLING INJECTED HOLES AND INJECTING EA 934 ADHESIVE AND FILLING THE DENT WITH POTTING COMPOUND AND CURING IAW CF6-6 ENGINE MANUAL 78-00-32; REPADec 8, 2008 · N397FE · Doug MD1010F · Engine Thrust ReverserSDR 08FDEA04576Blade · damagedNR 3 ENGINE S/N 451539 10TH STAGE COMPRESSOR BLADE T/E TIP AREA HAS A DING 0.036 INCH WITH 0.020 TEAR ON THE CONVEX SIDE. BLENDED BLADE TIP AND REMOVED THE DAMAGED AREAS AND PERFORMED AN INSPECTION TO ENSURE DEFECTS HAVE BEEN REMOVED IAW MD-10-10 AMM 72-36-00Oct 27, 2008 · N390FE · Doug MD1010F · Turbine Engine Compressor SectionSDR 08FDEA04488Lead · malfunctionedWHEN DESCENDING OUT OF FL240 FOR LANDING, GOT "ENG 3 EGT HI" AND ENG 3 EXCEEDANCE ALERTS EGT 3 INDICATION. SEQUENCED BETWEEN HIGH INDICATIONS (1053) AND AMBER "X", NO SECONDARY INDICATIONS. SHUT DOWN ENGINE IAW QRH, EGT WAS HIGH APPROX 30 SEC ON LANDING CRASOct 22, 2008 · N367FE · Doug MD1010F · Engine Indicating System WiringSDR FDEA200810224488Lead · failedWHEN DESCENDING OUT OF FL240 FOR LANDING, GOT "ENG 3 EGT HI" AND ENG 3 EXCEEDANCE ALERTS, EGT 3 INDICATIONS SEQUENCED BETWEEN HIGH INDICATIONS (1053) AND AMBER "X", NO SECONDARY INDICATIONS. SHUT DOWN ENGINE IAW QRH, EGT WAS HIGH APPROX 30 SEC ON LANDING CRASOct 22, 2008 · N367FE · Doug MD1010F · Engine Indicating System WiringSDR 08FDEA04420Cable · inoperativeNR 2 THROTTLE STUCK DURING CRUISE. ENGINE SHUTDOWN DURING DESCENT. NR 2 THROTTLE MOVED BACK ON SHORT FINAL AFTER LANDING NR 2 THROTTLE COULD BE MOVED TO IDLE. CABLE COMING FROM OAK. REPLACED #2 THROTTLE CABLE PER MM 76-11-01-2, OP'S CHEKS NORMAL. PERFORMEDOct 17, 2008 · N68059 · Doug DC1010F · Auto Throttle SystemSDR 08FDEA04173Fuel Control · malfunctionedNR 3 ENGINE FLAMED OUT ON TAKEOFF ROLL. ENGINE ROLLED BACK TO ABOUT 8% N1; FF INTERMITTENT FROM 0-500. EGT LOWER THAN OTHER 2 AT IDLE. REPLACED THE FUEL CONTROL AND FUEL PUMP.Oct 2, 2008 · N384FE · Doug MD1010F · Fuel Control/Turbine EnginesSDR FDEA200810024173Fuel Control · failedNR 3 ENGINE FLAMED OUT ON TAKEOFF ROLL. ENGINE ROLLED BACK TO ABOUT 8 PERCENT N1; FF INTERMITTENT FROM 0-500. EGT LOWER THAN OTHER 2 AT IDLE. REPLACED THE FUEL CONTROL AND FUEL PUMP.Oct 2, 2008 · N384FE · Doug MD1010F · Turbine Governor
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