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 08FDEA03747Wire · chafedNR 2 ENGINE SHUTDOWN IN FLIGHT. ON CLIMB-OUT PASSING FL 250 HAD A LEVEL 1 NR 2 ENGINE EGT EXCEEDANCE. PER CHECKLIST BROUGHT POWER BACK. TEMP CAME DOWN WITHIN LIMITS BUT SHORTLY CLIMBED BACK ABOVE REDLINE AND HAD A NR 2 EGT HIGH LEVEL 2. SHUT ENGINE DOWN ANSep 5, 2008 · N399FE · Doug MD1010F · Engine Indicating System WiringSDR 08FDEA00519Throttle Cable · failedNR 2 THROTTLE STUCK AT HIGH POWER SETTING AT CRUISE ALTITUDE. ALL ATTEMPTS TO THAW LINKAGES WERE UNSUCCESSFUL. NR 2 ENGINE WAS SHUT DOWN ON APPROACH TO KMEM. AFTER LANDING THROTTLE OPERATED NORMALLY. REMOVED AND REPLACE NR 2 ENGINE THROTTLE CABLE AND THROTFeb 20, 2008 · N560FE · Doug DC1030F · Power LeverSDR FDEA200712115024Frame · crackedMAIN CABIN FOUND 1 CRACK ON FRAME STA 1741, STR 14, RT. REPAIRED AREA IAW SRM 53-30-00 FIG 5 VOL I AND EA NR 8-5310-111521, 8-5330-111563.Dec 11, 2007 · N371FE · Doug MD1010F · Fuselage Main, FrameSDR 07FDEA04381Engine · damagedCLIMBING THROUGH FL190 AIRCRAFT SHUDDERED TWICE WITH SLIGHT YAW TO LEFT. LOOKED DOWN AND "ENG 1 EXCEEDENCE" ALERT AND RED BOXED ENG 1 EGT "951". PULLED ENG 1 TO IDLE AND RAN ENG FIRE SEVERE DAMAGE CHECKLIST. SHUTDOWN NR 1, PULLED NR 1 FIRE HANDLE AND RTBED Sep 29, 2007 · N386FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR ARWA20070902Engine · flamed outNR 1 ENGINE FLAMED OUT; ENGINE FAILED/SHUTDOWN IN FLIGHT CHECKLIST COMPLETED (ENGINE VIBRATION STOPPED) SHUTDOWN O505Z; WINDMILLING O.P. 10 PSI. TROUBLESHOOT FUEL SYSTEM AND FOUND METAL DEBRIE IN FUEL FILTER. REMOVED AND REPLACED FUEL PACKAGE IN ACCORDANCE WSep 25, 2007 · N68041 · Doug DC1010 · Engine (Turbine/Turboprop)SDR 07FDEA02439Mec · failedNR 1 ENGINE FLAMED OUT ON ROLLOUT. FIRST INDICATION WAS GEN 1 OFF FOLLOWED BY AIR SYS 1 LOW PRESS. REMOVED AND REPLACED FUEL PUMP AND MEC.Jul 10, 2007 · N377FE · Doug MD1010F · Fuel Controlling SystemSDR 07FDEA01672Seat Track · bentMAIN CABIN SEAT TRACK BENT SEVERAL AREAS BETWEEN STA. 625 AND STA. 775, BL107.5. REMOVED BENT AREAS IAW EA NR 8-5310-11060411, (FUSELAGE MAINFRAME-SEAT TRACK BETWEEN STA. 635-765/X=107.25. TRIMMED SEAT TRACK LOBES), ALODINED AND PRIMED IAW SRM 51-21-01 PG.1 Apr 30, 2007 · N68050 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04310Engine · making metalSHUT DOWN NR 3 ENGINE IN FLIGHT BECAUSE OF LEVEL 2 ALERT, ENG NR 3 OIL FILTER. BEFORE SHUT DOWN OIL PRESS WAS NORMAL. OIL TEMP WAS 20 PERCENT HIGHER THAN OTHER ENGINES. AFTER SHUT DOWN IT WIND MILLED FOR 25 MIN WITH SOME OIL PRESS. CHECKED AIU FAULTS LASDec 22, 2006 · N68057 · Doug MD1010F · Engine (Turbine/Turboprop)SDR ARWA20061101Engine · malfunctionedNR 1 ENGINE FAILED TO ACCELERATE PASS 80 PERCENT N1; ABORTED TAKEOFF AT 75 KTS. REMOVED AND REPLACED MAIN FUEL PUMP AND FUEL CONTROL ASSEMBLY IN ACCORDANCE WITH M/M 73-12-01; PERFORMED LEAK CHECK, NO LEAKS NOTED; PERFORMED ENGINE RUN AND TRIM IN ACCORDANCE WINov 3, 2006 · N68041 · Doug DC1010 · Engine (Turbine/Turboprop)SDR 06FDEA03686Seat Track · gougedFOUND CABIN STA 1154 LBL 27 SEAT TRACK SCALLOP GOUGED, W/O 33777, N00393. REMOVED GOUGE IAW SRM 51-21-01 VOL. 2. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5 SHEET 2. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1.Oct 18, 2006 · N10060 · Doug DC1010 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03608Skin · crackedHORIZONTAL STAB UPPER LT SKIN PANEL 7439-1 CRACKED 3.5 INCHES. VERIFIED END OF CRACK WITH HI-FREQ E/C. REFERENCE E/A 8-5510-102053 FOR INTERIM REPAIR AND FERRY FLIGHT, AND REFERENCE E/A 8-5510-102054 FOR PERMANENT REPAIR. A/C FERRIED TO LAX FOR PERMANENT REOct 10, 2006 · N399FE · Doug MD1010F · Horizontal Stabilizer, Plate/SkinSDR 06FDEA03439Cylinder · failedRT MAIN GEAR DOWN ON RETRACTION AFTER T/O. LIGHT WENT RED AND STAYED RED UNTIL GEAR HANDLE PLACED DOWN. RECYCLED, SAME THING. LANDED @ KOAK. PER CREW DEBRIEF, APPARENTLY THE RT MLG NEVER MOVED FROM THE DOWN AND LOCKED POSITION. SUSPECT RT MAIN DOWNLOCK CYCSep 26, 2006 · N68057 · Doug MD1010F · Main Landing GearSDR ARWA20060601Engine · erraticDURING INITIAL CLIMBOUT OF MIAMI, ENGINE NR 1 EGT BECAME VERY ERRATIC AND FLUCTUATED INTO AN OVERTEMP CONDITIONS; RESET C/B, NO HELP. REMOVED AND REPLACED NR 1 ENGINE IAW ARROW AIR MSG-3 DC10 J/C 141R7101M. OPERATIONAL CHECK NORMAL IAW M/M 72-00-00.Jun 4, 2006 · N68041 · Doug DC1010 · Engine (Turbine/Turboprop)SDR 06FDEA1312Engine · failedON CLIMBOUT TO CRUISE ALTITUDE PASSING 28,000 FT HEARD A THUD & EXPERIENCED AIRCRAFT YAW TO THE RIGHT. ENGINE INSTRUMENTS INDICATED NR 3 ENGINE FAILURE. SHUT DOWN ENGINE IN ACCORDANCE WITH QRH. FIRED NR 3 ENGINE FIRE EXTINGUISHER PER QRH. RETURNED TO MEM, Apr 5, 2006 · N386FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR 06FDEA1310Engine · failedON CLIMB-OUT TO CRUISE, ALTITUDE PASSING 28000' HEARD A "THUD" AND EXPERIENCED AIRCRAFT YAW TO THE RIGHT. ENGINE INSTRUMENTS INDICATED NR 3 ENGINE FAILURE. SHUT DOWN ENGINE IN ACCORDANCE WITH QRH. FIRE EXTINGUSHING AGENT TO NR 3 ENGINE PER QRH, RETURNED TO Apr 4, 2006 · N386FE · Doug DC1010 · Turbine Engine Reduction GearSDR ARWA20060301Pump · failedDURING CLIMB FIRST OFFICER NOTICE OIL QUANTITY AND OIL PRESSURE DROP TO ZERO; FOLLOWED BY OIL PRESSURE LIGHT. SHUTDOWN ENGINE NR 2 IN ACCORDANCE WITH ABNORMAL PROCEDURES AND DUMPED 6 MINUTES OF FUEL, DECLARED EMERGENCY LANDING AND LANDED IN MHLM WITH OTHER ABMar 8, 2006 · N68047 · Doug DC1010 · Turbine Engine Oil SystemSDR 06FDEA0900Repair · unknownDISCREPANCY LT WING OB FLAP UPPER SKIN AT STA XOF 458 HAS DOUBLER REPAIR. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-35-01 VOL 1 AND PERFORMED NEW REPAIR. DOUBLER IAW SRM 57-10-00 FIG 9 VOL 1.Mar 2, 2006 · N68054 · Doug DC1010 · Standard Practices/StructuresSDR 06FDEA0899Doubler · damagedDISCREPANCY RT WING OB FLAP UPPER SKIN XOFH 599 EXTERNAL DOUBLER. REMOVED AND REPLACED FASTENERS IAW SRM 57-10-00 VOL 1.Mar 2, 2006 · N68054 · Doug DC1010 · Trailing Edge FlapsSDR 06FDEA0898Bulkhead · crackedDISCREPANCY CLG SPACE FOUND 1EA CRACK 1 INCH LONG ON SKIN OF BLKHD AT STA 1501 X30 RT. PERFORMED REPAIR DOUBLER IAW SRM 53-00-00 FIG 10 VOL 1 AND REPLACED FIITING IAW SRM 51-33-01 PAR 6-10 VOL 2.Mar 2, 2006 · N68054 · Doug DC1010 · Fuselage Main, BulkheadSDR 06FDEA0897Intercostal · crackedDISCREPANCY MAIN CABIN INT FWD DOOR JAMB NR 3 RT FOUND NR1 EA CRACK 2 INCH LONG ON INTERCOSTAL PLANE JAMB ST STA 1256 Z-19. REMOVED DOUBLER AND TRIMMED OUT CRACK ON WEB FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW SRM 53-10-01 FIG 10 AND SRM 51-33-01 PAR Mar 2, 2006 · N68054 · Doug DC1010 · Fuselage Miscellaneous StructureSDR 06FDEA0896Skin · wornLT 1R REF FOUND LE FWD WEAR ON SKIN. PERFORMED REPAIR DOUBLER IAW SRM 57-00-01 FIG 4 SHT 2 VOL 1 FABRICATED PART IAW SRM 57-00-01 FIG 4 AND DETAIL PART TRAVELER F166343/N00343.Mar 2, 2006 · N68054 · Doug DC1010 · Wing, Plate/SkinSDR 06FDEA0893Splice · damagedMAIN CARGO COMPT STA 1129-1169 X-75.25 SEAT TRACK SPLICE REPAIR. PERFORMED VISUAL INSP OF SEAT TRACK SPLICE REPAIR FUS STA 1129-1169 X-75.25 FOLLOWING CRITERIA OF EO NR 8-5100-7-5001 P2.Mar 2, 2006 · N68054 · Doug DC1010 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA0921Doubler · incorrectR/W IB FLAP IB LOWER FAIRING FWD EDGE SIDE AFT OF FWD END MARKED NR 49. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCCOMPLISHED USING FAA APPROVED DATA. N00717, EVALUATED DOUBLER FAA APPROVED DATA, FOUND DOUBLER WAS NOT IMar 2, 2006 · N68057 · Doug MD1010F · Wing Miscellaneous StructureSDR 06FDEA0923Doubler · out of limitsREPAIR LT WING IB FLAP IB LWR FAIRING FWD END MARKED NR 51. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. N00719, EVALAUATED REPAIR IAW FAA DATA FOUND REPAIR WAS NOT IN COMPLIANCE. FAMar 2, 2006 · N68057 · Doug MD1010F · Wing Miscellaneous StructureSDR 06FDEA0924Repair · unknownREPAIR LT OB FLAP UPPER SKIN,STA.XOF 587 MARKED NR 71. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED REPAIR AT LT OB FLAP UPPER SKIN, FOUND TO BE WITHIN SRM 57-20-00 FIMar 2, 2006 · N68057 · Doug MD1010F · Standard Practices/StructuresSDR ARWA20060204Engine · leakingCLIMBING TO FL 360 AT FL 240, OIL QUANTITY AT ENGINE NR 2 DROPPED TO 1.5 QUARTS AND OIL PRESSURE STARTED TO FLUCTUATE; FOLLOW BY ENGINE NR 2 OIL PRESSURE LO LIGHT; PROCEEDED WITH ABNORMAL ENGINE SHUTDOWN CHECK LIST (OIL TEMPERATURE 115 CELSIUS) AND RETURN TO MFeb 22, 2006 · N68047 · Doug DC1010 · Turbine Engine Oil SystemSDR 06FDEA0799Repair · unknownFLUSH REPAIR LT WING NR1 SLAT STA. XORS 60, LE, MARKED NR 93. REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED REPAIR L/W NR 1 SLAT STA. XORS 60 L/E, MARKED NR 93. FOUND TOFeb 21, 2006 · N68050 · Doug MD1010F · Wing StructureSDR ARWA20060101Engine · stalledLOG PAGE NR 117483. NR 3 ENGINE COMPRESSOR STALLED. SHUTDOWN ENGINE. (SEE LOG PAGE NR 117486) REMOVED NR 3 ENGINE DUE TO COMPRESSOR STALLED AND REPLACED NR 3 ENGINE IAW ARROW AIR MM CHECK CARD NR 143-R7101; RUN UP CHECK GOOD. ACCOMPLISHED RED BORDER NR 18948Jan 11, 2006 · N68041 · Doug DC1010 · Turbine Engine Compressor SectionSDR 06FDEA0066Engine · damagedON T/O ROLL AT ORD AT ABOUT 120KT, RECEIVED ENGINE FAIL ALERT ON NR 2 ENG, NOTED EGT EXCEEDANCE AT 1052DEG, REJECTED. CLEARED RUNWAY, QRH. SHUTDOWN NR 2 ENGINE ON TAXIWAY. RETURNED TO RAMP. DUE TO THE FOD DAMAGE DONE TO THE FAN AND METAL IN THE TAIL PIPE WJan 7, 2006 · N391FE · Doug DC1010F · Engine (Turbine/Turboprop)SDR 06FDEA00059Floor Support · crackedAFT CARGO COMPARTMENT, FLOOR SUPPORT STRUCTURE AT FS1521, L46L-44L, SUPPORT ANGLE CRACKED. FABED NEW ANGLE IAW DAC DRAWING AEA0341-15. REPLACED IAW SRM 51-35-01 VOL II. ALODINED AND PRIMERED IAW SRM 51-1-21 VOLII. SEE SNRM N00525 OF WORK ORDER 00031297.Jan 6, 2006 · N359FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR ARWA20051203Fitting · brokenLOG PAGES NR 116686 AND NR 116688. ON SERVICE CHECK FOUND LT MAIN LANDING GEAR DOOR ROLLER ASSEMBLY LOWER SUPPORT FITTING BROKEN. REMOVED AND REPLACED LT MAIN LANDING GEAR DOOR IAW MM 32-14-01. OPERATIONAL CHECK NORMAL IAW MM 32-10-01.Dec 21, 2005 · N68041 · Doug DC1010 · Landing Gear Door Retract SectionSDR 05FDEA04150Doubler · noneDISCREPANCY FOUND EXTERNAL DOUBLER BETWEEN STA 735 AND 755 AND LONGERONS 34 AND 35 LT SIDE, WHERE POTABLE WATER SERVICE PANEL USED TO BE LOCATED. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 6 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-Dec 6, 2005 · N68056 · Doug DC1010 · Aircraft StructuresSDR 05FDEA04151Frame · crackedCAC LOWER LOBE BILGE FOUND 1EA CRACK, 3 INCHES LONG ON LT FRAME AT STA 1159 CLOSE TO PRESSURE PANEL FWD CENTER WING. REMOVED ATTACH ANGLE IAW SRM 51-33-01 PAR 6-10 VOL 2 REPAIRED FRAME IAW SRM 53-30- 00 FIG 7 VOL 1 REINSTALLED ATTACH ANGLE IAW SRM 51-33-01 PDec 6, 2005 · N68056 · Doug DC1010 · Fuselage Main, FrameSDR 05FDEA03577Frame · corrodedIN THE FWD CARGO COMPT SUMP AREA AT STA 919 FOUND SEVERE CORROSION WITH EXFOLIATION ON THE FRAME'S CAP BETWEEN L 51 LH TO L 50 RH. TRIMMED OUT FRAME CAP CORRODED REMOVED REMAINING CORROSION IAW SRM 51-21-01 PAR 34 VOL2 ORIGINAL MATERIAL THK IS .071 INCHES Oct 28, 2005 · N302FE · Doug DC1030 · Fuselage Main, FrameSDR 05FDEA03578Skin · crackedLT WING L/E WING TIP FOUND 1 EA CRACK .50 INCH LONG ON EXISTING REPAIR ON LOWER SKIN AT STA XW99. TRIMED OUT CRACKED PORTION SKIN REPAIR IAW SRM 57-00-01 FIG 4 VOL 2 FAB PART IAW DETAIL PART TRAVELER N00550/F160550.Oct 28, 2005 · N302FE · Doug DC1030 · Wing, Plate/SkinSDR 05FDEA03579Intercostal · crackedRT MAIN LANDING GEAR WHEEL WELL INT CRACK LONG 1.5 INCH ON HORIZONTAL INTERCOSTAL AT STA 1475 Z-103 OB SIDE. FAB PART IAW DETAIL PART TRAVELER F 161131-3 IAW SRM 53-50-00 FIG 2. INSTALLED STRAP DOUBLER F161131-3 IAW SRM 53-50-00 FIG 2 VOL 1.Oct 28, 2005 · N302FE · Doug DC1030 · Fuselage Miscellaneous StructureSDR 05FDEA03580Seat Track · crackedMAIN CABIN AT STA 1029 LT SIDE AT X27.500 ON SEAT TRACK FOUND 1EA CRACK 10 INCHES LONG. CUT OUT CRACKED SECTION OF SEAT TRACK, REPLACED NEW SECTION IAW SRM 53-70-00, FIG 1 SHT1-2, VOL1. FAB PARTS IAW DETAIL PARTS TRAVELER F161689/N01689.Oct 28, 2005 · N302FE · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03581Door Frame · crackedMAIN CARGO COMPARTMENT JAMB DOOR R3 STA 1256 X92 AND Z61 FOUND PLATE IN THE UPPER SECTION OF JAMB CRACK FOR 0.5 INCH LONG. REPAIRED CRACK IAW SRM 53-50-00 FIG 19 VOL1 FAB PART IAW DETAIL PART TRAVELER N01159.Oct 28, 2005 · N302FE · Doug DC1030 · Fuselage Main, StructureSDR 05FDEA03582Floor Panel · crackedCOCKPIT FLOOR SECTION STA 313 CRACK ON MEMBRANE 1 INCH LONG RIF SRM 53-11-01, ITEM 1. REPAIRED MEMBRANE AT STA 313 RIF SRM53-11-01 FIG 4 SHT 2 VOL 1.Oct 28, 2005 · N68056 · Doug DC1010 · Fuselage Floor PanelSDR 05FDEA03584Floor Panel · crackedCOCKPIT FLOOR STRUCTURE FOUND 1 EA CRACK 2 INCHES LONG ON MEMBRANE STA 304 X-12 RT SIDE. REPAIRED CRACK ON MEMBRANE STA 304 X-12 RT SIDE RIF SRM53-11-01, ITEM 1.Oct 28, 2005 · N68056 · Doug DC1010 · Fuselage Floor PanelSDR 05FDEA03585Floor Panel · crackedCOCKPIT FLOOR STRUCTURE FOUND 1 EA CRACK 2 INCHES LONG ON MEMBRANE STA 304 X-27 RT SIDE. REPAIRED CRACK ON MEMBRANE RIF 53-11-01 STA 304 X-27 RT SIDE.Oct 28, 2005 · N68056 · Doug DC1010 · Fuselage Floor PanelSDR 05FDEA03547Warning Light · false activationSOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO DOOR NOT CLOSED. AFT CARGO SW FAULT AND AN AMBER DOOR LIGHT FOR AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE IAW MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 MEL 52-71-01: AFT DOOR CLOSED AND LOCKED INDICAOct 27, 2005 · N412FE · Airbus A310203 · Door Warning SystemSDR 05FDEA03312Tube · looseDURING DESCENT THRU FL200, NOTICED NR 2 ENGINE WOULD NOT SPOOL UP FOR LEVEL OFF. N1 REMAINED AT LESS THAN 35 N1, N2 60 PERCENT. NR 2 THROTTLE HAD A VERY LIGHT TRAVEL FORCE AND FELT DISCONNECTED. ACCOMPLISHED RED TABS AND SHUT DOWN ENGINE DUE TO ENGINE BEIOct 7, 2005 · N391FE · Doug MD1010F · Engine ControlsSDR ARWA20050912Cable · damagedMAIN CABIN L1 DOOR WITH DOOR OPEN, NO WARNING LIGHT. UPON INSPECTION OF DOOR MECHANISM FOUND DAMAGED CABLES AT AFT SECTION OF L1 DOOR. REMOVED DAMAGED SECTIONS IAW M/M 52-10-02; INSTALLED PASSENGER DOOR DRIVE CABLE IAW M/M 52-10-02. OPERATIONAL CHECK OK.Sep 28, 2005 · N68041 · Doug DC1010 · Passenger/Crew DoorsSDR 05FDEA02488Warning Light · illuminatedAT FL 320 (SEL CARGO HEAT OFF) ALERT DISPLAYED AND CTR AND AFT CARGO TEMPS WERE 99 DEGRESS. TURNED OF CARGO HEAT AND TEMP REMAINED AT 99 DEGREES. OAT AT FL 320 -8C. BOTH CARGO TEMPS REMAINED AT 99 DEGREES. DECLARED EMERGENCY. LANDED. MEL 17AUG05 00:23 Aug 16, 2005 · N368FE · Doug MD1010F · Overheat DetectionSDR 05FDEA02448Flange · corrodedCTR WING LWR BARREL AT STA 1216 REWORK TO STR 47 BASE FLANGE TO REMOVE CORROSION MATERIAL PLUS 50 PERCENT. REPAIRED LONGERON IAW SRM 53-00-01 FIG 9 VOL I.Aug 12, 2005 · N564FE · Doug MD1010F · Wing, Center BoxSDR 05FDEA02128Engine · fireNR 1 ENG FIRE ON GROUND-LOUD BANG, FOLLOWED BY SMOKE, FOLLOWED BY NR 1 ENGINE FIRE WARNING ENGINE FIRE AND SEVERE QRH COMPLIED WITH AS WELL AS ALL APPLICABLE CHECKLISTS. NR 1 FIRE BOTTLE FIRED, NR 1 PACK ON-TEMP 38C GOOD FIRE TEST. REMOVED AND REPLACED NR 1 EJul 28, 2005 · N397FE · Doug DC1010 · Engine (Turbine/Turboprop)SDR 05FDEA01681Fuel Line · crackedNR 3 ENGINE FUEL LINE CRACKED ABOVE PYLON AT CONNECTING BRACKET UNDER PANEL 617CT. REMOVED AND REINSTALLED AFTER REPAIR PER TRAVLER T5/527309, NR 3 ENGINE PYLON. MAIN FUEL LINE AT PANEL 617CT IAW MM 20-50-01-2. LEAK CHECK GOOD IAW MM 28-00-02-2.Jun 24, 2005 · N391FE · Doug MD1010F · Engine Fuel DistributionSDR 05FDEA01496Stiffener · gougedCOMPLY WITH EA 8-7254-89506 ENGINE - TURBINE - TMF STRUT NR 1 STIFFENER GOUGE REPAIR. COMPLIED WITH EA 8-7254-89506.May 31, 2005 · N391FE · Doug MD1010F · Nacelle/Pylon Miscellaneous StructureSDR ARWA20050501Igniter · defectiveDURING ENGINE START NR 1 ENGINE IGNITION -A- INOPERATIVE; TRANSFER TO DMI NR 19182 AS PER MEL 74-1-1 CATEGORY-C. REMOVED AND REPLACED NR 1 ENGINE -A- IGNITOR IN ACCORDANCE WITH M/M 74-20-02; OPERATIONAL CHECK NORMAL.May 1, 2005 · N68041 · Doug DC1010 · Spark Plug/Igniter
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