GE CF6-6D

Service difficulty reports · 1,051

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Query with SQL
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"

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 UIEA2026010300003Plug · leakingDIVERSION ENGINE 3 OIL QUANTITY LOSS. INSPECTED #3 ENG AND FOUND OIL LEAKING FROM #3 IDG. DEACTIVATION BLANKING PLATE, REMOVED BLANKING PLATE AND FOUND DRIVE SEAL PLUG MISSING & INSTALLED DRIVE SEAL PLUG PER MEL 24-11-01A. RAN ENG IAW AMM 71-00-00, LEAK CHECKJan 3, 2026 · N476MC · Boeing 74747UF · Turbine Engine Oil SystemSDR KRDY2025061714786Engine · fireN476MC FLT 5Y 8208 AFTER T/O ENGINE # 1 WAS FIRE, SO CREW TAKE THE DECISION TO DIVERT TO GYE. PLS SEE ALSO MSR-14785.Jun 13, 2025 · N476MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR KRDY2025061714785Engine · fireACFT N476MC FLT 5Y8208 B747C DEPARTED FROM UIO, AFTER DEPART ENG #1 WAS FIRED SO CREW TOOK THE DECISION TO DIVERT TO GYE. ACFT LAND ON GYE, TOWED TO POSITION 13. A RIDING MECHANIC FROM ATLAS IS IN CHARGE OF THE TECHNICAL RELEASE AND WE PROVIDE MECHANIC ASSIJun 12, 2025 · N476MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR IXXA20241002002Retainer · gouged#1 ENGINE OB TR UPPER BIFURCATION FWD SEAL RETAINER CHANNEL IS WORN. HAECO WO 320008 NON ROUTINE 40293Aug 23, 2024 · N491AZ · Boeing 767323 · Engine Thrust ReverserSDR NACA2023013020001Shutoff Valve · failedENG BLEED OFF LIGHT DOESNT ILLUMINATE WITH ENGINE NOT RUNNING. REMOVED LH ENG PRSOV PER M2, INSTALLED LH PRSOV PER AMM 36-11-09 OPS CHECKS AND LEAK CHECKS GOOD. PART UNKNOWN TO TRAX.Jan 26, 2023 · N321CM · Boeing 767323 · Engine Bleed Air SystemSDR MK1Y01292021003Cowling · unknownUNDOCUMENTED REPAIR DOUBLERS FOUND AT LT ENGINE ON OUTBOARD CORE COWL OUTER SKIN.Jan 29, 2021 · N394AN · Boeing 767323 · Engine Cowling SystemSDR FDEA202010102523Door Frame · gougedNR 2 ENGINE LT SIDE, APPROXIMATELY STA YTN 133, 6 O`CLOCK POSITION, GOUGED METAL ON FWD LT FAN COWL LAND. MARKED DOT NR 45. REMOVED GOUGED DOOR JAM & REPLACED WITH FABRICATED DOOR JAM, REF SRM 51-31-01, DWG AJC 7415.Oct 10, 2020 · N562FE · Doug MD1010F · Nacelle/Pylon, Main FrameSDR FDEA2020040630686Engine · unknownCLIMBING THRU FL340 WITH ENGINES ALL AT CLIMB POWER WE FELT A BUMP LIKE MINOR TURBULENCE. THEN ANOTHER AND ANOTHER. WE SAW ENG 2 N1 FLUCTUATING SO WE SUSPECTED A COMPRESSOR STALL. AS WE WERE RUNNING THE QRH FOR ENG COMPRESSOR STALL WE RECEIVED LEVEL 2 ENGApr 3, 2020 · N550FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201905291179Engine · failedPDIS 560 72-57 4731 29MAY19 CLT OPEN U LOGPAGES:3089200 ENGINE 2 FIRE WARNING ON DEPT FROM CLT FACT 15JUN19 18:57 CLT R & R`D #2 ENGINE PER W/C 71T1701 SYSTEM CHECKS NORMAL. PER SDR REQUIREMENTS, ENGINE P/N CF6-6D, S/N 451447.May 29, 2019 · N560FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201902286504Wire Harness · damagedNR 3 ENGINE HAS HAD A SHIFT IN EGT TRENDS WITH ALL OTHER PARAMETERS STABLE. THIS NORMALLY INDICATES AN IMPENDING EGT INDICATION SYSTEM FAILURE. TESTED NR 3 ENG EGT INDICATION SYSTEM PER E.O. 8-7720-E0330327. R & R LT UPPER, RT UPPER AND LT LOWER HARNESFeb 26, 2019 · N560FE · Doug MD1010F · Engine Indicating System WiringSDR FDEA201811163266Lead · defectiveAS AUTO THROTTLES WENT TO CLIMB TRUST, NR 1 EGT WENT TO 1018' WITH "ENG 1 EXCEEDANCE" ALERT. C/W MTSI, R&R ALL NR 1 EGT THERMOCOUPLE PROBES AND FWD AND AFT LEADS I/R/T MM 77-21-01-2. RAN ENGINE NR 1 AND NR 3 FOR COMPARISON. ENGINE NR 1 START EGT 560, EGT 375 ANov 16, 2018 · N550FE · Doug MD1010F · Engine EGT/TIT Indicating SystemSDR FDEA2018102653006Engine · fireMDIS 566 78-10 5297 24OCT18 MEM OPEN U ENG 2 TAIL PIPE FIRE DURING START. INSTRUCTED FLT CREW TO USE ENG FIRE PROCEDURES. BOTH BOTTLES DISCHARGED. PER FLT CREW DEBRIEF NO FIRE IND IN COCKPIT, NO EGT LIMIT EXCEDED FIRE DEPT CALLED. FIRE DEPT DISCHARGED FOAM INTOct 25, 2018 · N566FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201805221271Heat Exchanger · failedDURING CLIMBOUT, THE NR 2 ENGINE OIL TEMP PEAKED AT 184 DEGREES IN THE RED BAND AND ALSO RECEIVED A LEVEL 2 ALERT FOR NR 2 ENG OIL TEMP HIGH. SHUTDOWN THE NR 2 ENGINE ALL OTHER ENGINE PARAMETERS NORMAL. NO VIBRATIONS. COMPLETED INSTALLATION OF THE NR 2 May 22, 2018 · N383FE · Doug MD1010F · Engine Oil TemperatureSDR FDEA201710243035Pump · malfunctionedNR 2 ENGINE WOULD NOT ACHIEVE CLIMB POWER. THE THROTTLE WAS FIRE WALLED DURING CLIMB, ALL INDICATIONS CONSISTANTLY LESS THAN 1 & 3. REMOVED AND REPLACED THE NR 2 ENGINE FUEL PUMP IAW AMM 73-12-01-2. REMOVED AND REPLACED MEC IAW AMM 73-20-01-2. PREFORMED Oct 24, 2017 · N375FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201708052122Wire Harness · damagedDURING CLIMBOUT, NOTICED THE NR 2 ENGINE EXCEEDENCE LEVEL 1 ALERT. EGT GAUGE FOR NR 2 SHOWED MAX 998. NORMAL EGT AT REDUCED POWER FOR LEVEL FLIGHT AT 7000 FT. ON ADVANCING POWER FOR CLIMB, NR 2 EGT CLIMBED RAPIDLY. PERFORMED GVI OF THE VSV FEED BACK CABLE Aug 5, 2017 · N394FE · Doug MD1010F · Engine Indicating System WiringSDR FDEA201704041065Compressor · stalledAT FLT LEVEL 370, HEARD A LOUD BANG AND NOTICED THE NR 2 ENGINE STALLED & N1 DECREASED TO 30%. DESCENDED TO FL 310 & RAN QRH FOR ENGINE COMPRESSOR STALL & WAS ABLE TO REGAIN NORMAL ENGINE OPERATION FOR APPROXIMATELY 5 MINUTES, WHEN THE NR 2 ROLLED BACK AGAIN TApr 4, 2017 · N383FE · Doug MD1010F · Turbine Engine Compressor SectionSDR FDEA201702210606Fuel Control · failedAFTER SHUTTING DOWN THE NR 1 ENGINE FOR A FUNCTIONAL CHECK. FUEL FLOW EGT AND N2 PROGRESSED NORMAL DURING START, BUT THE N1 WOULD NOT ADVANCE PAST 28%. ADVANCING THROTTLE DID NOT CHANGE ANY NR 1 ENGINE PARAMETERS UNTIL REACHING 10,000 FT, AT WHICH TIME THE Feb 21, 2017 · N389FE · Doug MD1010F · Fuel Control/Turbine EnginesSDR UIEA2017021600195Receptacle · damagedFOUND THE NR 1 ENGINE FUEL TRANSMITTER RECEPTACLE AND CONNECTOR DAMAGED. IAW SWPM 20-60-06 REV.63 AND WDM 73-33-11 REV.41 REPLACED THE TRANSMITTER RECEPTACLE AND CONNECTOR. IAW AMM 73-33-01-000-801 REV.88 AND AMM 73-33-01-400-801 REV.88 REPLACED FUEL PRESSUREFeb 15, 2017 · N476MC · Boeing 74747UF · Engine Fuel System WiringSDR FDEA201701310285Throttle Cable · inoperativeAT TOP OF DESCENT , NR 2 THROTTLE WAS STUCK AT 85% N1. SHUT DOWN NR 2 ENGINE AT 10.000. NORMAL LANDING, WAS ABLE TO MOVE NR 2 THROTTLE TO IDLE DURING TAXI TO CHOCKS. REMOVED AND REPLACED THROTTLE CABLE.Jan 31, 2017 · N363FE · Doug MD1010F · Power LeverSDR AALA20161215022Fuel Control · faultyLEFT ENGINE WOULD NOT SHUT DOWN WITH FUEL CONTROL IN OFF POSITION. CYCLED SWITCH AND ENGINE SHUT DOWN. ENGINE VALVE LIGHT REMAINED ON. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED LEFT MAIN ENGINE CONTROL IAW WC 73-94-02 AND 71-95-20. OPERATIONAL CHECKED GDec 14, 2016 · N398AN · Boeing 767323 · Fuel Control/Turbine EnginesSDR FDEA201610153643Engine · failedLEVEL FLIGHT, HEARD BOOM NOISE, FELT MOMENTARY HEAVY RUMBLE, AND YAW TO THE RIGHT. NR 3 ENGINE FAILED. COMPLIED WITH QRH. DURING DESCENT, N1-21 EGT-30 N2-10.5 FF - 0 OIL PRESS - 1 OIL TEMP - 60 OIL QTS - 16. FAILED BORESCOPE, REPLACED THE ENGINE.Oct 15, 2016 · N358FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201607162482Engine · failedUPON ADVANCING POWER FOR TAKEOFF, FELT A RUMBLING IN THE RUDDER PEDALS. ABORTED T/O AT AT 10 KTS. TURNED OFF RUNWAY, ANOTHER ACFT ADVISED SEEING FLAMES FROM THE NR 2 ENGINE. SHUTDOWN ENGINE, BLEW BOTH FIRE BOTTLES. REMOVED NR 2 ENG PER WORK CARD 71T1101Jul 16, 2016 · N564FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201603230995Mec · inoperativeON APPROACH, NR 1 THROTTLE WOULD NOT GO BELOW 65% N, AT THE IDLE STOP F FLOW 2350 RAN THE ENG. SHUTDOWN IN FLIGHT CHECK LIST. R&R THE ENGINE NR 1 MEC PER AMM 73-20-01-2 AND ADJUSTMENT AND TEST PER EO 8-7320-7-5000 C. RAN ENGINE PER JRH CHPT 7.7. ENGINE LEAMar 23, 2016 · N383FE · Doug MD1010F · Fuel Control/Turbine EnginesSDR AALA20160219014Controller · failedAIRCRAFT WAS NOT GNDED. AIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, RT ENG HPSOV, EICAS MSG DISPLAYED & BLEED LIGHT REMAINED ILLUMINATED. ACCOMPLISHED PNEUMATIC SYS HEALTH CHECK IAW AMM 36-00-21 WITH RT HIGH PRESSUFeb 19, 2016 · N398AN · Boeing 767323 · Pneumatic Distribution SystemSDR FDEA201601160166Nose Cowl · crackedNUMBER 3 ENG INLET NOSE COWL APPROX 6:00 POSITION HAS HORIZONTAL CRACK UNDER BOLTS. R & R NR 3 ENG NOSE COWL IAW MM 71-11-00-2.Jan 16, 2016 · N560FE · Doug MD1010F · Engine Cowling SystemSDR FDEA201601100105Engine · bird ingestionMULTIPLE FAN BLADES DAMAGED ON NR 3 ENG DUE TO BIRD STRIKE. DURING BORESCOPE OF NR 3 ENG FOR BIRD STRIKE, FOUND LARGE TEAR ON LE 10TH STAGE THROUGH PORT B1-10. REPLACED NR 3 ENG.Jan 10, 2016 · N554FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201601090091Anti-Ice Valve · failedNR 1 ENG ANTI-ICE DISAGREE DURING CLIMB WITH ENG ANTI-ICE SELECTED ON. R & R ANTI-ICE VALVE IAW AMM 30-22-02-0-0. OPS CHECKED NORMAL, OK FOR SERVICE.Jan 9, 2016 · N10060 · Doug MD1010F · Engine Anti-Icing SystemSDR FDEA201601050044Attach Bolt · looseNUMBER 3 ENG LT THRUST REVERSER, UPPER LATCH ATTACH BOLTS LOOSE, 5 EACH. TORQUED UPPER LATCH ATTACH BOLTS IAW AMM 78-32-11-2.Jan 5, 2016 · N560FE · Doug MD1010F · Engine Thrust ReverserSDR FDEA201601050045Bolt · looseNUMBER 3 ENG LT THRUST REVERSER, MOUNTING RING LATCH ASSEMBLY HAS 16 LOOSE BOLTS. QUALITY CONTROL REQUESTS, TORQUE CHECK, ON ALL MOUNTING RING ATTACHMENT FASTENERS. TIGHTENED AND TORQUE CHECKED ALL BOLTS ON MOUNTING RING LATCH ASSY IAW AMM 78-32-11-2.Jan 5, 2016 · N560FE · Doug MD1010F · Engine Thrust ReverserSDR FDEA201510163252Cable · damagedREJECTED TAKEOFF DUE TO NR 3 ENGINE NOT SPOOLING UP TO TAKEOFF POWER. REJECT SPEED LESS THAN 80 KIAS NR 1 & 2 APPROX 103% N1, NR 3 STOPPED ACCELERATING AT APPROX 96 % N1 WHERE THROTTLE POSITION HAD NO FURTHER EFFECT. TROUBLESHOT IAW FIM 71-00-00-2 FIM AND IOct 16, 2015 · N68053 · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201510143211Engine · faultyDURING CLIMB OUT PASSING FL 260, NR 3 N1 WENT TOWARD ZERO WHILE ACFT EXPERIENCED MODERATE VIBRATION. MOVED THROTTLE TO IDLE EGT & N2 APPEARED NORMAL & WERE SIMILAR TO 1 & 2 ENG, WHEN NR 3 THROTTLE WAS ADVANCED FROM IDLE, MODERATE VIBRATIONS WERE FELT. RAN Oct 14, 2015 · N567FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR UIEA2015101300577Fuel Filter · faultyINFLIGHT DIVERT DUE TO QRH 7.16, REF TO LP 733225 01 & LP 733226 4. NR 1 & NR 4 FUEL FILTER WERE REPLACED, FUEL LEAK CHECKED SATISFACTORY. ENG 1 & 4 GND IDLE RUN CUT OUT NIL PLF & EXISTING FAULT NOTED IAW AMM 71-00-00.Oct 12, 2015 · N476MC · Boeing 74747UF · Engine Fuel DistributionSDR UIEA2015101300576Fuel Filter · faultyENG 4 FUEL FILT IN CRUISE, SELF-CLEAR WITHIN 10 - 15 SECONDS STATUS MSG. ENG 4 FUEL FILT NR 4 ENG FUEL FILTER ELEMENT REPLACED. FUEL LEAK CHECKED CUT OUT & SATISFACTORY IAW AMM 73-11-02. ENG NR 4 GND IDLE RUN TEST PERFORMED IAW AMM 71-00-00. NIL PLF & EXISOct 12, 2015 · N476MC · Boeing 74747UF · Engine Fuel DistributionSDR FDEA201508062490Unknown · malfunctionedLEVEL 2 ENG 1 OIL FILTER ALERT DURING CLIMB PASSING FL 200. ALL OIL PRESS & TEMP INDICATIONS WERE NORMAL, NO VIBRATION. REDUCED THROTTLE TO IDLE. LEVEL 2 ALERT REMAINED. SHUTDOWN NR 1 ENG IAW QRH GUIDANCE, NO OTHER INDICATIONS. ENG 1 CONTINUED TO WINDMILLAug 6, 2015 · N564FE · Doug MD1010F · Engine Oil Indicating SystemSDR FDEA201503040646Wire Harness · damagedIN FLIGHT GOT EGT 2 HI 997 DEG ENG 2 EXCEEDANCE. PULLED TO IDLE TEMP DROPPED BELOW LIMITS ON LEVEL OFF WITH THROTTLE AT IDLE. TEMP EXCEEDED LIMITS AGAIN. SHUTDOWN NR 2 ENG & RAN APPROPRIATE CHECKLISTS. REMOVED AND REPLACED BOTTOM LT, BOTTOM RT HARNESSES, AMar 4, 2015 · N358FE · Doug MD1010F · Engine Indicating System WiringSDR FDEA201411233868Cowling · wornNUMBER 3 ENG LT FAN COWL AFT EDGE AT 10:00 HAS BEEN DAMAGED, WORN THROUGH TO HONEYCOMB. DAMAGE APPEARS TO HAVE BEEN CAUSED BY RIDING CONDITION WITH STRUCTURE. REPAIRED IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02 VOL II.Nov 23, 2014 · N550FE · Doug MD1010F · Engine Cowling SystemSDR FDEA201410083007Seat Track · wornMAIN DECK FLOORS STATION 1741 LBL 47 TWO EACH SEAT TRACK WORN. REMOVED AREA OF DAMAGED SEAT TRACK IAW SRM 53-70-00 VOL 1.Oct 8, 2014 · N40061 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201410052972Frame · chafedNUMBER 2 ENG LT CORE COWL 2ND FRAME FROM AFT HAS CHAFE MARK. REPAIR ACCOMPLISHED IAW EA 8-7113-T0312063 REV NO PS P1. TITLE POWER PLANT COWL NR 2 END LT PYLON CORE COWL CHAFE. WELD ACCOMPLISHED ON T14 1096831. MINOR REPAIR.Oct 5, 2014 · N10060 · Doug MD1010F · Engine Cowling SystemSDR FDEA201409092547Duct · crackedNR 2 NOSE COWL INLET DUCT, CRACKED THROUGHOUT CIRCUMFERENCE. R & R WITH NEW NOSE COWL ASSEMBLY IAW AMM 54-22-01-2.Sep 9, 2014 · N390FE · Doug MD1010F · Engine Air Intake SystemSDR FDEA201407051633Wire · damagedDURING CLIMB OUT AT 11,000 FT THE NR 1 ENG EGT WAS AMBER, XED OUT THEN CAME BACK ON & EXCEEDED THE EGT LIMIT ABOVE 965 DEGREES C. THE EGT RETURNED TO NORMAL AFTER PULLING TO IDLE. SECOND TIME AFTER THROTTLE MOVED HALF WAY FWD EGT SPIKED TO 1089 DEGREES C WIJul 5, 2014 · N399FE · Doug MD1010F · Engine Indicating System WiringSDR FDEA201406151464Power Supply · no testEMERGENCY LIGHT BATTERY 1 LOW ILLUMINATED DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01-4Jun 15, 2014 · N372FE · Doug MD1010F · Emergency LightingSDR FDEA201406141452Skin · crackedWHILE PERFORMING FCD, FOUND A CRACK ON NR 1 INBD SLAT TRACK SKIN CUT OUT LT WING. VERIFIED CRACK USING HFEC IAW NDTSPM 06-10-01. CRACK 1/2 INCH IN LENGTH. REMOVED CRACK. COMPLIED WITH HFEC INSPECTION, NO CRACKS FOUND. REPAIRED IAW EA 8-5710-F0308207. Jun 14, 2014 · N370FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201406141448Skin · crackedFOUND A CRACK ON RT WING SKIN AT NR 3 SLAT TRACK BETWEEN NR 1 & 2 SLATS. TRIMMED OUT DAMAGED AREA. PERFORMED INTERNAL & EXTERNAL VISUAL INSPECTION WITH NO ADDITIONAL DAMAGE NOTED. HFEC INSPECTION DONE WITH NO CRACKS NOTED. REPAIRED IAW EA 8-5730-T0308776Jun 14, 2014 · N68057 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201406141450Skin · crackedDURING POST FLIGHT, FOUND A CRACK ON THE LT WING LE AT NR 4 SLAT, OTBD TRACK CUT OUT, LOWER, INBD RADIUS. HFEC INSPECTED SUSPECTED IAW NDTSPM 06-10 01 & VERIFIED THE CRACK TO BE A 3/8 - 1/2 INCH LONG. CUT OUT DAMAGED AREA IAW SRM. VERIFIED CRACK REMOVED USJun 14, 2014 · N370FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201404010605Wire Harness · damagedDURING DEPARTURE, NR 1 ENGINE EXCEEDED EGT 932 DEGREES WITH MOMENTARY SPIKE IN N1, RETARDED NR 1 THROTTLE, N1 STEADY AT 93 & EGT 700 - 750 AT FL310. FOUND ENG 1 EXCEEDANCE MESSAGE DISPLAYED & NR 1 EGT INDICATOR WAS FLAGGED AT 999. OPENED NR 1 CORE COWL & SHOApr 1, 2014 · N383FE · Doug MD1010F · Engine Indicating System WiringSDR FDEA201403200538Wire Harness · damagedRTO AT 110KTS FOR, ENG 3 EXCEEDANCE, LVL 1 ALERT. NR 3 EGT SHOWED YELLOW, 1011, FOR EXCEEDANCE, ESTIMATE EXCEEDANCE WAS MOMENTARY. PULLED UP VIA NR 3 ENG EXCEEDANCES. THE ACARS EXCEEDENCE SHOWS IT WAS AN EGT INDICATION PROBLEM. R & R NR 3 ENG TOP LT EGT THMar 20, 2014 · N371FE · Doug MD1010F · Engine Indicating System WiringSDR FDEA201403190532Shutoff Valve · failedDURING CLIMB, RECEIVED ECAM WARNING NR 2 THRUST REVERSER PRESSURIZED. ECAM LASTED FOR SEVERAL SECONDS THEN WENT OUT, REAPPEARED. THROTTLE WAS BROUGHT TO IDLE IAW ECAM & WARNING AGAIN WENT AWAY. MANUAL THRUST USED & EACH TIME NR 2 THROTTLE WAS MOVED ABOVE IDLMar 19, 2014 · N656FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA201403190535Shutoff Valve · inoperativeABORTED TAKEOFF DUE TO NR 2 ENG MASTER CAUTION. NR 2 ENGINE THRUST REVERSER LIGHT 60KTS AS STANDARD POWER COMING UP. R & R PRSOV IAW MM 78-31-05-04, OPS CHECKED GOOD ON GROUND ENG RUN IAW JRH. FAN COWL CLOSED & LOCKED IAW MM 71-13-02. CLOSED & LOCKED THRUMar 19, 2014 · N656FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA201403020430Push-Pull Cable · malfunctionedON TOP OF DESCENT NR 2 THROTTLE FROZE AT 92% N1 FROM FL 370 TO 10,000 FT NO MOVEMENT, SHUTDOWN ENG. CREW REPORTED THAT AFTER ARRIVAL AT GATE & SHUTDOWN NR 2 THROTTLE OPERATED NORMALLY. R & R NR 2 ENG THROTTLE PUSH PULL CABLE. RIG & OPERATIONS CHECKED OK IAWMar 2, 2014 · N371FE · Doug MD1010F · Power LeverSDR FDEA201402140315Wire · damagedNR 2 ENGINE EGT 1018 DEGREES DURING CLIMB OUT. EGT STAYED HIGH AT REDUCED POWER SETTING. EGT HIGH ALERT, SHUTDOWN ENGINE. DUMPED 8500 LBS FUEL PRIOR TO LANDING. WIRE FOUND DAMAGED, WIRE REPLACED.Feb 14, 2014 · N360FE · Doug MD1010F · Engine Indicating System Wiring
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