GE CF6-50C2

Service difficulty reports · 719

Newest first. General aviation reporting is voluntary.

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 = 'CF650C2'
  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 22AA201000050Longeron · crackedDURING "C" CHECK, NR 1 ENG LT CORE COWL LOWER LONGERON FOUND CRACKED. NON-ROUTINE NR 0124, CRACK AREA AT NR 1 ENGINE LT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1016-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000051Longeron · crackedDURING "C" CHECK, NR 1 ENG, RT CORE COWL LOWER LONGERON AND STRAP FOUND CRACKED. NON-ROUTINE NR 0125, CRACKED STRAP AND LOWER LONGERON AT NR 1 ENGINE RT CORE COWL AREA REPAIRED IAW EN 1016-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000052Longeron · crackedDURING "C" CHECK, NR 3 ENGINE LT CORE COWL LOWER LONGERON AFT SECTION FOUND CRACKED. NON-ROUTINE NR 0159, CRACK AREA AT NR 3 ENGINE LT CORE COWL LOWER LONGERON AFT SECTION REPAIRED IAW EN 1018-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000053Longeron · crackedDURING "C" CHECK, NR 3 ENGINE RT CORE COWL LOWER LONGERON CRACKED AT APPROX AT MID AND AFT FRAME SECTION. NON-ROUTINE NR 0163, CRACK AREA AT MID AND AFT SECTION OF LOWER LONGERON AT NR 3 ENGINE RT CORE COWL AREA REPAIRED IAW EN 1018-10 WORK INSTRUCTIONS AND FFeb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000054Rib · wornDURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT MOST RIB FOUND WITH WEAR MARK. NON-ROUTINE NR 0195, WORN AREA AT NR 2 ENGINE LT CORE COWL AFT MOST RIB AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/RibSDR 22AA201000055Longeron · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL LOWER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0196, CRACK AREA AT NR 2 ENGINE LT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000056Longeron · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0197, CRACK AREA AT NR 2 ENGINE LT CORE COWL UPPER LONGERON AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000057Skin · wornDURING "C" CHECK, NR 2 ENG LT CORE COWL UPPER AFT RUB STRIP FOUND WORN TO COWLING SKIN. NON-ROUTINE NR 0198, WORN COWLING SKIN AREA AT NR 2 ENG LT CORE COWL UPPER AFT RUB STRIP AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Plate/SkinSDR 22AA201000058Rib · wornDURING "C" CHECK, NR 2 ENG RT CORE COWL AFT MOST RIB FOUND WITH WEAR MARK. NON-ROUTINE NR 0201, WORN AREA AT NR 2 ENGINE RT CORE COWL AFT MOST RIB AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030 · Nacelle/Pylon, Frame/Spar/RibSDR 22AA201000059Longeron · crackedDURING "C" CHECK, NR 2 ENG RT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0202, CRACKED UPPER LONGERON AT NR 2 ENGINE RT CORE COWL AREA REPAIRED IAW 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FROM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000060Rib · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0296, CRACK AREA AT NR 2 ENGINE LT CORE COWL AFT RIB LOWER SIDE AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/RibSDR 22AA201000061Rib · crackedDURING "C" CHECK, NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE FOUND WITH CRACK. NON-ROUTINE NR 0297, CRACK AREA AT NR 2 ENGINE RT CORE COWL AFT RIB LOWER SIDE AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030F · Nacelle/Pylon, Frame/Spar/RibSDR 22AA201000062Skin · corrodedDURING "C" CHECK, CABIN CORROSION FOUND ON CTR WING SECTION SURFACE AT STA 1156 TO STA 1221 X = 107.5 (RT). NON-ROUTINE 0220, CTR WING SECTION SURFACE AT STA 1156 TO STA 1221 X = 107.5 (RT) CORROSION REMOVED AND REPROTECTED IAW SRM 51-21-01 VOLUME II AT S 21 FFeb 24, 2010 · N478CT · Doug DC1030F · Wing, Center BoxSDR 22AA201000063Intercostal · corrodedDURING "C" CHECK, CTR CARGO COMPARTMENT BILGE, INTERCOASTAL FOUND CORRODED AFTER SIDE GUIDE RAIL, REMOVED TO FACILITATE FOR STRUCTURE REPAIR AT STA 1764, L42 TO L43L (REFER CNTRL NR 0425). NON-ROUTINE NR 0449, CTR CARGO COMPARTMENT BILGE, INTERCOASTAL REPAIR Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage Miscellaneous StructureSDR 22AA201000064Seat Track · corrodedDURING "C" CHECK, CABIN CORROSION FOUND ON INNER SURFACE OF SEAT TRACK AT STATION 1139 TO STATION 1156, X= 47.5. NON-ROUTINE NR 0314, SEAT TRACK FROM STATION 1129 TO STATION 1169, X= 47.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIGURE 1 VOLUME 1 REVISION 96.Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 22AA201000065Roller Tray · corrodedDURING "C" CHECK, CTR CARGO COMPARTMENT LT OTBD CARGO ROLLER TRAY FOUND CORRODED AFTER CARGO SIDE GUIDE RAIL REMOVED TO FACILITATE FOR STRUCTURE REPAIR AT STA 1697 TO STA 1781. NON-ROUTINE NR 0450, CTR CARGO COMPARTMENT LT OTBD CARGO ROLLER TRAY REPAIR CARRIEFeb 24, 2010 · N478CT · Doug DC1030F · Fuselage Floor PanelSDR 22AA201000066Skin · crackedDURING "C" CHECK, LOWER FUSELAGE, ALONG LONGERON 44L, ALONG STA 1701 FUSELAGE SKIN FOUND CRACKED THROUGH. NON-ROUTINE NR 0425, CRACK AREA AT LONGERON 44L ALONG STATION 1701 FUSELAGE SKIN REPAIRED IAW SRM 53-20-00 FIGURE 6 VOLUME I REVISION 96.Feb 24, 2010 · N478CT · Doug DC1030F · Fuselage Main, Plate/SkinSDR FDEA201002230494Clamp · looseBASED ON MX REPORT, DECIDED TO GIVE A LITTLE EXTRA TIME FOR ACCELERATION . IT WAS NECESSARY TO GO FULL QUADRANT TO GET CLOSE TO TAKEOFF POWER. WHEN THE AUTOFLIGHT TILE WAS PRESSED ENG 1 AND 2 REACHED TAKEOFF POWER, ENG NR 3 WAS LAGGING ABOUT 15 PERCENT BELOWFeb 23, 2010 · N314FE · Doug DC1030F · Compressor Bleed ControlSDR FDEA201002180447Skin · dentedRT HORIZONTAL STAB EXTERIOR SURFACE FOUND DEEP NICK ON SKIN. (REMOVED PART). REPAIRED EDGE FWD SKIN IAW SRM 55-10-00 FIG.13 VOL.1, REPAIRED LEADING REAR SKIN IAW SRM 55-00-01 FIG.3 SH.2 VOL.1Feb 18, 2010 · N320FE · Doug DC1030F · Horizontal Stabilizer, Plate/SkinSDR FDEA201002170439Engine · failedTEST FLIGHT-UNABLE TO RESTART NR 1 ENGINE AIRBORNE AFTER SHUTDOWN WHEN FUEL LEVER SELECTED ON N1 INDICATION WENT TO "0", AFTER 20 SECS, WHEN FUEL LEVER SELECTED OFF, N1 INDICATION CAME BACK AFTER 15-20 SECS, START ATTEMPT WAS AT FL 240- 250, 240 KNOTS-280 KNOTFeb 17, 2010 · N306FE · Doug MD1030F · Engine (Turbine/Turboprop)SDR 22AA201000038Skin · crackedDURING "C" CHECK, LT WING FIXED L/E AT APPROX STA XFS 675 UPPER INTERNAL SKIN FOUND CRACK. NON-ROUTINE NR 372, LT WING FIXED L/E AT APPROX STA XFS 675 UPPER INTERNAL SKIN REPAIR IAW EN 1003-10 AND FAA APPROVED FORM 8110-3 DATED 24 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Wing, Plate/SkinSDR 22AA201000039Fairing · crackedDURING "C" CHECK, NR 3 PYLON FWD FAIRING FOUND WITH CRACKED AT 02 LOCATIONS. NON-ROUTINE NR 227, 02 EACH CRACK LOCATIONS AT NR 3 ENGINE PYLON FWD FAIRING AREA REPAIRED IAW 1004-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3, DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Main FrameSDR 22AA201000040Skin · crackedDURING "C" CHECK, NR 2 ENGINE RT CORE COWL FWD LOWER SKIN FOUND WITH CRACK. NON-ROUTINE NR 439, CRACK AREA AT NR 2 ENGINE RT CORE COWL FWD LOWER SKIN AREA REPAIRED IAW EN 1009-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Plate/SkinSDR 22AA201000041Fairing · crackedDURING "C" CHECK, NR 1 ENGINE PYLON FWD FAIRING FWD SIDE FOUND WITH CRACK. NON-ROUTINE NR 224, CRACK AREA AT NR 1 ENGINE PYLON FWD FAIRING FWD SIDE AREA REPAIRED IAW EN 1004-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Main FrameSDR 22AA201000042Skin · wornDURING "C" CHECK , NR 2 ENGINE LT CORE COWL UPPER SKIN FOUND WITH WEAR MARKS. NON-ROUTINE NR 440, WEAR MARKS ON NR 2 ENGINE LT CORE COWL UPPER SKIN AREA REPAIRED IAW EN 1007-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Plate/SkinSDR 22AA201000043Longeron · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL FOUND UPPER LONGERON WITH CRACK. NON-ROUTINE NR 393, CRACK AREA AT NR 2 ENGINE LT CORE COWL UPPER LONGERON AREA REPAIRED IAW ENGINEERING NOTE (EN) 1006-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000044Longeron · crackedDURING "C" CHECK, NR 3 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 323, CRACKED LONGERON AT NR 3 ENG LT CORE COWL UPPER AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000045Longeron · crackedDURING "C" CHECK, NR 1 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 324, CRACKED NR 1 ENG LT CORE COWL UPPER LONGERON AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000046Longeron · crackedDURING "C" CHECK, NR 2 ENG RT CORE COWL UPPER LONGERON FOUND WITH CRACK AT 02 LOCATIONS. NON-ROUTINE NR 392, CRACKED LONGERON 02 EACH LOCATIONS AT NR 2 ENGINE RT CORE COWL UPPER AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000047Longeron · crackedDURING "C" CHECK, NR 2 ENG RT CORE COWL LOWER LONGERON AND STRAP FOUND CRACKED. NON-ROUTINE NR 394, CRACKED LONGERON AND STRAP AT NR 2 ENG RT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030F · Nacelle/Pylon, Longeron/StringerSDR 22AA201000048Frame · corrodedDURING "C" CHECK , AFT CARGO COMPARTMENT BILGE AREA FRAME (STA 1996) LOWER CHORD CORRODED AT LBL 15 TO RBL 15 AS MARKED. NON-ROUTINE NR 0610, AFT CARGO COMPARTMENT BILGE AREA FRAME (STA 1996) LOWER CHORD, LBL 15 TO RBL 15 CORROSION, REMOVED AND REPROTECTED IAWFeb 13, 2010 · N524MD · Doug DC1030F · Fuselage Main, FrameSDR WRLA20091228328Battery Pack · dischargedEMERGENCY EXIT LIGHT TEST - "A" ZONE EMERGENCY LIGHTS REMAINED ON WOULD NOT TURN OFF. REPLACED FWD EMERGENCY EXIT LIGHT BATTERY PACK.Dec 28, 2009 · N136WA · Doug DC1030 · Emergency LightingSDR 22AA200900029Oil System · lowENG NR 3 ESN NR 455-780 IN FLIGHT SHUT DOWN DUE TO OIL / PRESS, QTY DROP & COMPRESSOR STALL AND CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 3 ENG. ON ENGINE RUN UP, OPS CHECKED NORMAL.Oct 16, 2009 · N478CT · Doug DC1030 · Turbine Engine Oil SystemSDR FDEA200909163308Sensor · malfunctionedDURING T-OFF, WHILE SETTING POWER TARGET 114.4 WHEN N1 REACHED APPROX 98-99 PERCENT (70KTS) N2 EXCEEDENCE ON NR 01 ENGINE, RESET T-OFF AT 70KTS AMBER ENG 1 EXCEDENCE DISPLAYING, AMBER 109,9 N2 DISPLAYED VCP R NO RESTRICTION REF: 72-00-00-6 1, NR 1 ENGINE,Sep 16, 2009 · N318FE · Doug DC1030F · Turbine GovernorSDR FDEA200909083267Longeron · corrodedLT AIR CONDITIONING COMPT FOUND SEVERE CORROSION WITH EXFOLIATION ON LONGERON. REPAIRED AREA IAW SRM 53-30-00 FIG 4 & SRM 53-40-00 FIG 15 VOL I.Sep 8, 2009 · N321FE · Doug DC1030F · Fuselage Main, Longeron/StringerSDR FDEA200909053260Transcowl · departedTOWER INFORMED US WE DROPPED SOMETHING ON ROLLOUT. SMOOTH LANDING, REVERSERS STOWED BY 65-70KTS. A LARGE PIECE OF NR 2 REVERSER CAME OFF AT END OF LANDING, ROLL INITIALLY GOT ALL 3 ENGINES SHOWING REV STOWED THEN NR 2 U/L LIGHT CAME ON. SHUTDOWN NR 2 AND TSep 5, 2009 · N306FE · Doug DC1030F · Engine Thrust ReverserSDR CA090811006Bolt · shearedWHILE PERFORMING A GENERAL VISUAL INSP OF THE MAIN GEAR WELLS, FOUND SHEARED BOLT IN THE RT WHEEL WELL FWD BULKHEAD OTBD DOOR SUPPORT CASTING. BOLT WAS REPLACED AND RETURNED TO SERVICE.Aug 10, 2009 · Doug DC1030 · Fuselage, Landing Gear Attach FittingsSDR FDEA200907262807Wire Harness · damagedCLIMB 320 TO 340 AUTO THROTTLES ENGAGED NR3 ENG EXCEEDANCE HIGH EGT 1021, REQUIRED THROTTLE REDUCTION TO MAINTAIN EGT LIMITS. COMPLIED WITH EO 8-7720-7-5001. EGT PROBES ON NR 3 CHECKED GOOD. OPENED BORESCOPE PLUGS B3-1 AND B3-2 FOR QA ON NR 3 ENG. COMPLIEJul 26, 2009 · N302FE · Doug MD1030F · Turbine Engine System WiringSDR 22AA200900002Engine · stalledNR 2 ENGINE COMPRESSOR STALLED ABRUPTLY AFTER TAKEOFF. REDUCED POWER AND PROCEEDED WITH ABNORMAL CHECK LIST. ENGINE SHUTDOWN AT 03:18Z. SHUT DOWN NR 2 ENGINE DUE TO SEVERE COMPRESSORS STALLS, EVEN AT FLIGHT IDLE. ENGINE SHUTDOWN OCCURED AFTER TAKEOFF DURING INJun 21, 2009 · N524MD · Doug DC1030 · Engine (Turbine/Turboprop)SDR DHLA200900036Oil Filter · cloggedFILTER CLOG LIGHT ILLUMINATED ON MWP. FILTER NR 2 OIL CLOG LIGHT ILLUMINATED ON S/O PANEL AFTER TAKEOFF. REMOVED AND REPLACED MAIN ENGINE OIL FILTER P/N AC9380F4010 IAW MM 79-22-01. OPS AND LEAKS CK GOOD IAW JRH 18.1.Jun 16, 2009 · N364DH · Airbus A300B42C · Turbine Engine Oil SystemSDR DHLA200900032Switch · failedENGINE NR 2 "OIL CLOG" LIGHT ILLUMINATED INFLIGHT ENGINE 2 WAS SHUTDOWN WITH INFLIGHT ENGINE SHUTDOWN ABNORMAL PROCEDURE ALL ENG IND NORMAL. REPLACED NR 2 ENG OIL FILTER CLOGGING SWITCH PER MM 79-35-11. RAN NR 2 ENG PER JRH 16.5. SYS OPS TEST NORMAL. FOLLOMay 26, 2009 · N364DH · Airbus A300B42C · Engine Oil System (Airframe Furnished)SDR WRLA2009118Fluid · leakingEDDP-KBWI ON LANDING AIRCRAFT BOUNCED A BIT ON BOTH MAINS AND BECAME SLIGHTLY AIRBORNE AGAIN AT WHICH TIME, THE GROUND SPOILERS DEPLOYED CAUSING A RAPID DESCENT AND SUBSEQUENT HARD IMPACT, WHICH CAUSED ANOTHER TRIP INTO THE AIR. AT SOME POINT THE SPOILERS CYCMay 6, 2009 · N139WA · Doug DC1030 · Hydraulic System, MainSDR CNMA20090003Oil System · malfunctionedUPON DECENT PRESS DROPPED BELOW 10PSI AND ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED PERFORMED INFLIGHT ENGINE SHUTDOWN IAW QRH 20 MIN PRIOR TO LANDING.May 6, 2009 · N603AX · Doug DC1030 · Turbine Engine Oil SystemSDR FDEA200905061557Throttle Cable · bindingPDX - MEM ON INITIAL DESCENT CLEARANCE, THE NR 2 THROTTLE WOULD NOT RETARD, N1 WAS APPROX 80 PERCENT ON N2. THROTTLE REMAINED FROZEN DURING ARRIVAL AND ENGINE WAS SHUTDOWN PER QRH ON DOWNWIND AT 4000 FT NR 2 THROTTLE DID FREE UP ON SHORT FINAL AND NO FURTHERMay 6, 2009 · N302FE · Doug MD1030F · Power LeverSDR DHLA200900022Engine · leakingSTRONG OIL ODOR FROM PACK NR 2 WHEN THROTTLE AT IDLE AND HP VALVE ON ENGINE NR 2 OPEN. ALL PRESS AND TEMPS NORMAL. PLACED NR 2 PACK ON DMI LIST PER MEL 21-51-01, CAT C, DDD 4-14-09. CONTROL NR 34715. PLACARD INSTALLED. BOROSCOPE ENGINE FOUND OIL WETTING, Apr 4, 2009 · N364DH · Airbus A300B42C · Turbine Engine Oil SystemSDR DHLA20090020Coalescer Bag · contaminatedFLT 165 OIL ODOR WITH NR 2 PACK OPERATING. DEFFERED NR 2 PACK IAW MEL 21-51-01 CAT C ASSIGNED DMI 34713 PLACARDS INSTALLED. R/R NR 2 COALESCAR SOCK IAW MM 21-51-16 NO ODOR NOTED WHEN OPERATING NR 2 PACK, THIS CLEARS DMI 34713 PLACARD REMOVED P/N 20D10-3. AIRCRApr 3, 2009 · N364DH · Airbus A300* · Humidity Control SystemSDR WRNA2009002Compressor · stalledSEVERE COMPRESSOR STALLS (2) DURING TAKEOFF AT ABOUT 100 KTS ON NR 2 ENGINE. TAKEOFF WAS REJECTED (ABORTED) AT ABOUT 100KTS, DURING BRAKING ACTION THE TOWER REPORTED FIRE IN NR 2 ENG, FIRE CK LIST WAS PERFORMED, DISCHARGING ONE (1) FIRE BOTTLE. AFTER LEAVINGApr 1, 2009 · N821 · Airbus A300* · Turbine Engine Compressor SectionSDR CNMA20090001Engine · power lossNR 2 ENGINE COMPRESSOR STALL CLIMBING THRU 320 NO THROTTLE MOVEMENT SMOOTH WEATHER. N1 DROPPED TO 90%, EGT 850 WITH VIBRATION. CORRECTIVE ACTION REPLACED ENGINE.Mar 28, 2009 · N612AX · Doug DC1030 · Engine (Turbine/Turboprop)SDR 22AA20090303Oil System · leakingLOG PAGE NR 126111. NR 2 ENGINE STARTED LOOSING OIL RAPIDLY. ACCOMPLISHED ENGINE FAILURE SHUTDOWN IN FLIGHT CHECK LIST. SHUTDOWN ENGINE AT 05:52Z AND REST OF FLIGHT UNEVENTFULL. REMOVED AND INSTALLED ENGINE IAW W/C 142R7101M. OPERATION TEST ON ENGINE RUN UMar 26, 2009 · N526MD · Doug DC1030F · Turbine Engine Oil SystemSDR 22AA20090501Mount · damagedFOUND AT AFT SECTION EXTENSIVE DAMAGE IN AFT PYLON AND NACELLE STRUCTURE, BY DEBRIS FROM ENGINE. REMOVED AND REPLACED AT AFT ENGINE MOUNT, TAIL PYLON TORQUE BOX IAW DC-10 DRAWING AVB7050 AND AVB 7326. REPLACED FASTENERS IAW DC-10 SRM 51-31-00 PAGE 1 TO 15 REMar 26, 2009 · N526MD · Doug DC1030 · Engine Mount Section
Back to GE CF6-50C2