GE CF6-6K

Service difficulty reports · 54

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'CF66K'
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SDR FDEA202105271414Engine · malfunctionedAT FL380 ALL ENGINES WERE OPERATING NORMALLY. AS WE BEGAN OUR DESCENT AND THROTTLES CAME BACK TOWARDS IDLE ECS SURGED FOLLOWED BY A LEVEL 2 AIRSYS 2 PRES LO AND CONFIRM ENG OUT PROMPT. AIR PRESSURE OUT OF THE NUMBER 2 ENGINE WAS 9 PSI. THE NUMBER 2 THROTTMay 27, 2021 · N550FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA2020042730686Engine · malfunctionedCLIMBING 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 FDEA2019081291831Engine · failedAPPROXIMATELY 500 FEET AFTER TAKEOFF. WE RECEIVED A LEVEL 1 ENG 1 EXEEDANCE. TEMP SHOWED 1010, THROTTLE 1 WAS PULLED BACK AND TEMP DECREASED INTO A NORMAL RANGE. WAS OVERTEMP FOR APPROXIMATELY 2 SEC. ENGINE OPERATED NORMAL FOR THE REMAINDER OF FLIGHT RETAug 9, 2019 · N360FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA2019122089831Engine · overtempPDIS 360 77-20 6391 09AUG19 MEM OPEN U LOGPAGES:2977480 APPROXIMATELY 500 FEET AFTER TAKEOFF. WE RECEIVED A LEVEL 1 ENG 1 EXEEDANCE. TEMP SHOWED 1010?, THROTTLE 1 WAS PULLED BACK AND TEMP DECREASED INTO A NORMAL RANGE. WAS OVERTEMP FOR APPROXAug 9, 2019 · N360FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201803200740Engine · failedENG FAILURE NR 1 ENG CLIMBING THRU 5K. YAW, LOUD BANG RAPIDLY RISING EGT. ENG EXCEEDANCE 942 DEG. THROTTLE TRIMMED POSITIONED TO IDLE. ENG SHUT DOWN. FIRE BOTTLE DISCHARGED. REPLACED NR 1 ENGINE.Mar 20, 2018 · N372FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR 2013FA0000705Engine · seizedNR 2 ENGINE HAD SUDDEN SEIZURE, NO FIRE INDICATION, PRECEDED BY LOAD BANG, PERFORMED EMERGENCY PROCEDURES.Aug 15, 2013 · N450AX · Doug DC1010 · Engine (Turbine/Turboprop)SDR 06FDEA03705Door Frame · misrepairedMAIN CABIN R3 PASSENGER DOOR JAMB AT STA 1305 LONGERON NR 27 EXISTING REPAIR. INSPECTION OF EXISTING REPAIR CARRIED OUT IAW ED 8-5100-7-5001 P2. FOUND 2 FASTENERS NOT INSTALLED ( SEE JPF N00742). FASTENERS INSTALLED IAW SRM 53-30-00 FIG 19. PERFORMED INSPEOct 19, 2006 · N567FE · Doug DC1010F · Fuselage Main, StructureSDR 06FDEA03707Door Frame · misrepairedINTERNAL FUSELAGE CAC AREA AT STA 1156 TO 1158 BETWEEN LONGERONS 31 TO 28 LT SIDE EXISTING REPAIR. PERFORMED INSPECTION IAW EO NR 8-5100-7-5001 P2 CRITERIA FOUND INSTALLED BOLTS INSTEAD OF HI-LOCKS IAW SRM 53-30-00 FIG 7 VOL 1. INSTALLED FASTENERS IAW SRM 53Oct 19, 2006 · N567FE · Doug DC1010 · Fuselage Main, StructureSDR 06FDEA0902Skin · crackedDISCREPANCY EXISTING DOUBLER FUSELAGE SKIN STA 383 AND 410 Z-30 FOUND EXT DOUBLER REPAIR. REMOVED OLD SKIN INSTALLED NEW SKIN P/N ABA7049-3 IAW DWG ABA7049/ABA7035 AND SRM 53-40-00 FIG 15 VOL 1. ON EXISTING HOLES AT SKIN ABA7048-3 7EA HOLES INSTALLED RIVETSMar 2, 2006 · N563FE · Doug DC1010 · Fuselage Main, Plate/SkinSDR 06FDEA0901Skin · dentedDISCREPANCY EXT FUSELAGE LOWER DEEP DENT ON EXT SKIN AT STA 1970 FROM LONG.38 LT TO LONG 39LT. REFORMED DENT AND NDI INSP. NO CRACK FOUND IAW SRM 53-20-00 FIG 13 VOL 1. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW SRM 53-20-00 FIG 13 SHT 14 FABRICATED PARMar 2, 2006 · N563FE · Doug DC1010 · Fuselage Main, Plate/SkinSDR 06FDEA0894Skin · dentedDISCREPANCY LWR FUSELAGE RT SIDE FOUND MANY DENTS ON SKIN STA 979 LONG 39 TO 42. REMOVED DENT IAW SRM 53-20-00 FIG 13 SHT 14 NOTE (C) VOL 1 PERFORMED INSP IAW SRM 53-20-00 VOL 1 NO CRACK FOUND BLENDED AND POLISH NICKS IAW SRM 53-20-00 FIG 13 SHT 2B VOL 1 ORIGMar 2, 2006 · N563FE · Doug DC1010 · Fuselage Main, Plate/SkinSDR 05FDEA04003Skin · damagedLT IB FLAP SKIN UPPER SIDE ACCIDENTALLY DAMAGED DURING STRIPPING ACTIVITIES. REMOVED FLAP SECTION IAW SRM 51-31-01. REFORMED RIB IAW DPS 3.69. PERFORMED INSPECTION, NO CRACK FOUND. PERFORM DOUBLER REPAIR IAW SRM 57-10-00 FIG 85.Nov 29, 2005 · N571FE · Doug MD1010F · Trailing Edge FlapsSDR 05FDEA04004Skin · damagedDURING STRIPPING ACTIVITIES, RR IB FLAP SKIN UPPER SIDE ACCIDENTALLY DAMAGED CAUSING CRACK 3 INCHES LONG. REMOVED FLAP SECTION IAW SRM 51-31-01. PERFORMED INSPECTION, NO CRACK FOUND. PERFORMED DOUBLER REPAIR IAW SRM 57-10-00 FIG 85.Nov 29, 2005 · N571FE · Doug MD1010F · Trailing Edge FlapsSDR 05FDEA04005Doubler · corrodedDURING PRE-PAINT INSPECTION FOUND CORROSION WITH EXFOLIATION ON BEVER/TAIL OF RT WING AT STA XORS 284. REPAIRED IAW EA 8-5710-93818.Nov 29, 2005 · N571FE · Doug MD1010F · Wing, Plate/SkinSDR 05FDEA04006Doubler · corrodedDURING PRE-PAINT INSPECTION FOUND CORROSION WITH EXFOLIATION ON BEVER/TAIL OF LT WING AT STA XORS 284. REPAIRED IAW EA 8-5710-93818.Nov 29, 2005 · N571FE · Doug MD1010F · Wing, Plate/SkinSDR 05FDEA03465Skin · dentedLWR FUS RT SIDE ON SKIN: BTW LONG 37 AND LONG 38 FOUND AT STA 1009 NR 1EA DENT (LENGTH 1,063 INCH X DEPTH 0,082 INCH) AND AT STA 1006 FOUND 1EA DENT (DEPTH 0,161 INCH X LENGTH 2 INCH) BTW LONG38 AND LONG 39 AT STA Y=1007 FOUND NR1 DENT (LENGTH 1.57 INCH X DEOct 21, 2005 · N556FE · Doug DC1010 · Fuselage Main, Plate/SkinSDR 05FDEA03475Rib · corrodedLT HORIZ STAB LEADING EDGE OB FOUND CORROSION BETWEEN SKIN AND RIB. REMOVED CORROSION AND REPAIRED WITH NR 2EA DOUBLER IAW SRM 55-13-01 FIG 1 VOL3.Oct 21, 2005 · N556FE · Doug DC1010 · Horizontal Stabilizer, Spar/RibSDR 05FDEA02603Frame · wornAIR COND COMPT LT SIDE FOUND WORN FRAME AT STA 588 X=64. TRIMMED WORN AREA AND REPAIR IAW SRM.Aug 24, 2005 · N556FE · Doug DC1010 · Fuselage Main, FrameSDR 05FDEA02604Skin · dentedLT WING LOWER SURFACE ON IB AILERON: FOUND NR 1 DENT ( LENGTH 0.87 INCH ; DEPTH 0.094 INCH) AND FOUND NR 1 DENT (LENGTH 0.63 INCH ; DEPTH 0.027 INCH) AT STA XW 343 CUT DAMAGED PORTION OF LOWER SKIN AND REPAIRED IAW SRM.Aug 24, 2005 · N556FE · Doug DC1010 · AileronsSDR 05FDEA02605Rib · crackedRT WING L/E AT XORS 526 FOUND RIB CRACKED. ACCOMPLISHED WING OB EDGE FORMER REPAIR IAW SRM.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02606Skin · crackedRT WING FIXED L/E AT SLAT TRACK NR 7 FOUND NR 1 CRACK 1 INCH LONG ON SKIN AT XORS 372. CUT DAMAGED AREA AND REPAIRED WITH DOUBLER IAW SRM.Aug 24, 2005 · N556FE · Doug DC1010 · Leading Edge DevicesSDR 05FDEA02607Structure · damagedMAIN CABIN INTERNAL FUSELAGE FOUND NR 2 HOLES DIAM. 0.25 INCH TOO CLOSE AT STA 1561, LONGERON 8 LT SIDE. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM.Aug 24, 2005 · N556FE · Doug DC1010 · Fuselage Main, StructureSDR 05FDEA02608Fastener · wrong partAIR COND COMPT LT SIDE FOUND EXISTING REPAIR WITH WRONG FASTENERS (CHERRY AND BOLT) ON NLG BLKHD. REMOVED EXISTING REPAIR, TRIMMED OUT DAMAGED AREA AND REPAIRED IAW SRM.Aug 24, 2005 · N556FE · Doug DC1010 · FastenersSDR 05FDEA02609Rib · crackedRT WING FIXED LEADING EDGE AT STA XORS 936 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER, FILLER AND DOUBLER REPAIR IAW SRM.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02614Rib · crackedRT WING FIXED LEADING EDGE AT STA 750 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND REPAIR ANGLE.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02615Rib · crackedRT WING FIXED LEADING EDGE AT STA XORS702 FOUND NR 1 RIB CRACKED. ACCOMPLISH FORMER REPAIR IAW SRM AND REPAIR ANGLE.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02616Rib · crackedRT WING FIXED LEADING EDGE AT XORS 696 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND REPAIR ANGLE.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02617Rib · crackedRT WING FIXED LEADING EDGE AT XORS 733 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02618Rib · crackedRT WING FIXED LEADING EDGE AT XORS 742 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02619Rib · crackedRT WING FIXED LEADING EDGE AT XORS 831 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02620Rib · crackedRT WING FIXED LEADING EDGE AT XORS 598 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02621Rib · crackedRT WING FIXED LEADING EDGE AT XORS 615 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02622Rib · crackedRT WING FIXED LEADING EDGE AT XORS 490 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02623Rib · crackedRT WING FIXED LEADING EDGE AT XORS 485 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02624Rib · crackedRT WING FIXED LEADING EDGE AT XORS 454 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02625Rib · crackedRT WING FIXED LEADING EDGE AT XORS 402 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02626Rib · crackedRT WING FIXED LEADING EDGE AT XORS 352 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/BulkheadSDR 05FDEA02447Skin · unknownFOUND REPAIR AT STA 1159 - 1139 LONGERON 41-48 RT. REPAIRED IAW FEDEX 8-5330-84091A.Aug 12, 2005 · N564FE · Doug DC1010 · Fuselage Main, Plate/SkinSDR 05FDEA02449Structure · corrodedCTR WING LWR BARREL STA 1216 LONGERON 48 REWORK OF CORROSION 40 PERCENT. MATERIAL LOSS TO STANDING LEG. CUT OUT CORRODED SECTION OF LONGERON IAW SRM 53-00-01 FIG 7 VOL I GN 16.Aug 12, 2005 · N564FE · Doug DC1010 · Wing, Center BoxSDR 05FDEA01680Engine · malfunctionedNR 1 ENGINE REMAINED AT FLIGHT IDLE DURING DESCENT AND WOULD NOT FOLLOW THROTTLE. N1 AND N2 SLOWLY STARTED DECAYING UNTIL GEN, AIR, HYDRAULIC ALERTS STARTED COMING ON. EGT WAS BELOW OTHER ENGINES 150-200 DEG FF WAS APPROX 500 PPH. FIRST NOTED PROBLEM FL220Jun 24, 2005 · N565FE · Doug MD1010F · Engine Indicating SystemSDR 05FDEA00287Engine · vibrationAT FL 340 EXPERIENCED NR 1 ENGINE VIBRATION, N1 ROLLED BACK TO 34%, N2 62% FF 690 LBS. EXECUTED ENG FIRE SEVERE DAMAGE CHECKLIST, FUEL DUMP ABOUT 3000 LBS, DECLARED EMERGENCY LANDING 18C. INSPECTED INTAKE AND EXHAUST. NO DEFECTS NOTED. BOROSCOPE INSPECTEFeb 14, 2005 · N399FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR HALA0100292Fcu · malfunctionedFLT 481 - PPT - NR 3 ENGINE FLAMED OUT ON APPROACH. ENGINE HAD BEEN AT IDLE POWER 5 MINUTES. REMOVED AND REPLACED FUEL CONTROL. OPS AND LEAK CHECK GOOD. (M)Dec 11, 2001 · N128AA · Doug DC1010 · Fuel Control/Turbine EnginesSDR HALA0100204Mec · failedFLT 938 - INBOUND TO ANC, HAD NR 2 ENGINE QUIT AT 15,000 FT, ATTEMPTED RESTART, NO SUCCESS. DECLARED EMERGENCY. REMOVED AND REPLACED MEC AND FUEL PUMP. TRIM RUN CHECKS OK. (M)Aug 8, 2001 · N135AA · Doug DC1010 · Fuel Control/Turbine EnginesSDR CNMA200100029Bearing · failedDURING CLIMBOUT #3 ENGINE OIL STRAINER CLOGGED LIGHT CAME ON AND THROTTLE WAS REDUCED AND LIGHT WENT OUT. SHORTLY THERE AFTER OIL QTY DROPPED TO "0" AND ENGINE WAS SHUT DOWN PER COM PROCEDURES. ACCOMPLISHED FUEL DUMP INFLIGHT. REMOVED AND REPLACED RADIAL MID Aug 6, 2001 · N360AX · Doug DC1010 · Turbine Engine Accessory DriveSDR CNMA200100025Lever · stuckAT FLIGHT LEVEL 360 NR 2 ENG THROTTLE BECAME JAMMED AT A POWER SETTING OF 94 PERCENT N1. REPEATED ATTEMPTS WERE MADE TO FREE THROTTLE LEVER, NONE SUCCESSFUL. AFTER ENGINE SHUTDOWN N1 READ 10-13 PERCENT, N2 READ .7 TO 0 PERCENT 2 ENGINE. APPROACH AND LANDINGJun 6, 2001 · N450AX · Doug DC1010 · Power LeverSDR CNMA200100012Filter · cloggedNR 2 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED IN FLIGHT. PERFORMED OIL STRAINER CLOG LIGHT ABNORMAL CHECKLIST. CLOG LIGHT REMAINED ILLUMINATED. ENGINE WAS SHUTDOWN BY FLIGHT CREW. MX REPLACED OIL STRAINER FILTER AND OIL CLOG LIGHT SWITCH.Apr 14, 2001 · N450AX · Doug DC1010 · Turbine Engine Oil SystemSDR AALA20001213Engine · failedSFO - FLT 39 - DURING TAKEOFF, IN EXCESS OF 100 KNOTS, THE NR 2 ENGINE FAIL LIGHT ILLUMINATED, REJECTED TAKEOFF, ENGINE NR 2 FLAMED OUT AFTER CLEARING THE RUNWAY. REMOVED AND REPLACED NR 2 ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)Jul 22, 2000 · N133AA · Doug DC1010 · Engine (Turbine/Turboprop)SDR 00FDEA00124Engine · malfunctionedON ROTATION AIRCREW HEARD LOUD NOISE, SEEMING TO ORIGINATE FROM LEFT SIDE OF A/C. NR 1 EGT AMBER O/H LIGHT ILLUM ON LANDING (AFT LAND). MEM TOWER SAW 2-3 ORANGE FLAMES COMING OUT OF NR 1 ENGINE. REPLACED ENGINE.Mar 1, 2000 · N375FE · Doug DC1010 · Engine (Turbine/Turboprop)SDR AALA990882Fuel Control · defectiveLAX - FLT 162 - DURING APPROACH LAX AT APPROX 1,006 FEET, THE NR 1 ENGINE FLAMED OUT. FUEL PRESSURE WAS ZERO. FUEL PUMPS WERE ON, HAD 5200 LBS OF FUEL IN NR 1 TANK. ENGINE RELIT AT ABOUT 100 FEET AGL. LANDED LAX WITHOUT INCIDENT. REPLACED MAIN ENGINE FUELJun 16, 1999 · N133AA · Doug DC1010 · Fuel Control/Turbine EnginesSDR HALA9900079Engine · failedGEN 3 OFF AND GEN FAIL LIGHTS BOTH ILLUMINATED AND NR 3 AC LOAD INDICATED ZERO. NR 3 CSD OIL PRESS LOW LIGHT ILLUMINATED CSD OIL OUTLET TEMP NORMAL AND RISE TEMP NORMAL FOLLOWED BY INCREASE IN OUTLET TEMP AFTER SEVERAL MINUTES. OUTLET TEMP REDUCED AFTER CSD Mar 19, 1999 · N171AA · Doug DC1010 · Engine (Turbine/Turboprop)
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