# GE CF700-2D - Type: Engine model (FAA registry) - Registry code: 30027 - Manufacturer (registry): GE - Model: CF700-2D - Engine type: Turbo-fan - Power: 4,325 lb thrust - Data sheet: [TCDS E7EA](https://openairdocs.org/tcds/E7EA) (OpenAirDocs) - Holder: General Electric Company - Installed in: 0 registered aircraft - Page: https://openairdocs.org/engine/ge-cf700-2d Model codes come from the FAA registry's reference file. ## ADs that may apply (OpenAirDocs) Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2010-09-08](https://openairdocs.org/ad/2010-09-08): AFT Technologies combustion liners · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective May 28, 2010 - [AD 2001-10-12](https://openairdocs.org/ad/2001-10-12): Unapproved Parts · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Jun 7, 2001 - [AD 98-23-06](https://openairdocs.org/ad/98-23-06): Combustion Liner Assemblies · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Nov 20, 1998 - [AD 97-25-08](https://openairdocs.org/ad/97-25-08): General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Jan 2, 1998 - [AD 97-13-10](https://openairdocs.org/ad/97-13-10): Aft fan disk · General Electric CF700-2C, CF700-2D and CF700-2D-2. Effective Aug 26, 1997 - [AD 85-18-03](https://openairdocs.org/ad/85-18-03): Stage 1 Turbine Disk · General Electric CF700-2D, CF700-2D-2, CJ610-8A and 1 more. Effective Nov 15, 1985 - [AD 80-08-06 R1](https://openairdocs.org/ad/80-08-06-R1): Turbine Disks · General Electric CF700-2D, CF700-2D-2, CJ610-8A and 1 more. Effective Feb 2, 1981 - [AD 75-05-13](https://openairdocs.org/ad/75-05-13): Compound Turbine And Fan Blade · General Electric CF700-2C, CF700-2D and CF700-2D-2. Effective Mar 3, 1976 - [AD 75-19-05](https://openairdocs.org/ad/75-19-05): Horizontal Drive Shaft · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 1 more. Effective Sep 26, 1975 - [AD 78-07-06](https://openairdocs.org/ad/78-07-06): Compressor Disks · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 2 more Historical (superseded or no longer in force): - [AD 2000-01-09](https://openairdocs.org/ad/2000-01-09) (historical): General Electric Aircraft Engines CF700-2C, CF700-2D and CF700-2D-2. Effective Feb 11, 2000 ## Information bulletins (advisory) (2) - [SAIB NE-08-49R1](https://openairdocs.org/saib/NE-08-49R1): Turbine Engine Combustion Section. Issued Sep 17, 2008 - [SAIB NE-08-49](https://openairdocs.org/saib/NE-08-49) (historical): Turbine Engine Combustion Section. Issued Sep 9, 2008 ## Registered aircraft None registered with this engine model now. ## NTSB investigations None matched to aircraft with this engine model. ## FAA accident and incident reports None matched to aircraft with this engine model. ## Service difficulty reports (30) As reported by operators and repair stations, by the model named in the report. - [SDR Y2PA20131002052](https://openairdocs.org/sdr/Y2PA20131002052), Oct 2, 2013: ENGINE. FLAMED OUT. CREW REPORTED THAT DURING LEVEL OFF AT FL340, RT ENGINE FLAMED OUT. DESCENDED TO FL290, NORMAL RELIGHT, DIVERTED. ACFT LANDED WITHOUT INCIDENT. MX WAS SENT TO A - [SDR Y2PA20130729044](https://openairdocs.org/sdr/Y2PA20130729044), Jul 28, 2013: ENGINE. FLAMED OUT. FLIGHT CREW PERFORMED A MAXIMUM ALTITUDE ACCELERATION TEST OF THE RT ENGINE AT FL310 AND FL330. ACFT PASSED TEST AT FL310. DURING TEST PERFORMED AT FL330 THE EN - [SDR Y2PA20130120004](https://openairdocs.org/sdr/Y2PA20130120004), Jan 20, 2013: TURBINE BLADES. FOD. CREW REPORTED ENGINE FLAMEOUT AT FL346 AND REQUESTED DESCENT TO FL290. CREW DECLARED AN EMERGENCY AND WERE VECTORED. CREW RAN ENGINE FAILURE AND RELIGHT CHECKLI - [SDR Y2PA20120618032](https://openairdocs.org/sdr/Y2PA20120618032), Jun 14, 2012: GOVERNOR. BYPASSING. IN CRUISE AT .66 MACH AND FL 350, ADJUSTED EPR FROM 1.44 TO 1.60, AFTER 30 SECONDS FURTHER INCREASED EPR TO 1.75. APPROX 1 MINUTE LATER THE NR 1 ENGINE FLAMED O - [SDR Y2PA20120428021](https://openairdocs.org/sdr/Y2PA20120428021), Apr 28, 2012: GOVERNOR. BYPASSING. NR 1 ENGINE FLAMED OUT AT FL350, NO INDICATION FOR REASON WHY. INSPECTED FUEL FILTERS, BOROSCOPED AND VISUALLY INSPECTED ENGINE, NO DEFECTS FOUND. R & R FUEL PR - [SDR Y2PA20120417013](https://openairdocs.org/sdr/Y2PA20120417013), Apr 17, 2012: TURBINE CASE. RUPTURED. AT 14000 FT, NR 1 ENGINE FIRE INDICATION AND HORN ACTUATED. REDUCED THRUST IAW EMERGENCY CHECKLIST, LIGHT EXTINGUISHED. DECLARED EMERGENCY AND LANDED WITHOUT IN - [SDR KC82007F00000](https://openairdocs.org/sdr/KC82007F00000), Jul 16, 2007: TRANSMITTER. MALFUNCTIONED. THE LT FUEL TRANSFER PUMP STOPPED TRANSFERING FUEL TO THE LT FEEDER FUEL TANK ON THE PREVIOUS LEG. THE TRANSFER PUMP WAS DEFERRED IAW THE APPROVED MEL. DURING T - [SDR 042507N220CA](https://openairdocs.org/sdr/042507N220CA), Apr 25, 2007: ENGINE. STALLED. ON CLIMB-OUT FROM ADS AT FL250, THE NR 2 ENGINE STALLED. THE A/C RETURNED TO ADS. AFTER EXTENSIVE TROUBLESHOOTING THE CAUSE OF PROBLEM WAS NOT FOUND. THE ENGINE - [SDR Y2PA200700022](https://openairdocs.org/sdr/Y2PA200700022), Feb 22, 2007: INLET. DAMAGED. WEATHER CLEAR - VFR - CLIMBING THROUGH 8000' CREW HEARD A LOUD NOISE FROM REAR AND FELT AN IMPACT. CREW NOTICED LEFT ENGINE EPR CLIMB AND OIL PRESSURE DECREASIN - [SDR 5092006N209CA](https://openairdocs.org/sdr/5092006N209CA), May 5, 2006: ENGINE. SHUTDOWN. A/C DEPARTED TUL BOUND FOR OLS, WHILE CLIMBING THROUGH 22,000 FT, A/C WAS STRUCK BY LIGHTNING. THE NR 1 ENGINE ROLLED BACK AND QUIT. THE NR 1 ENGINE WAS RESTART - [SDR KCB2005F00000](https://openairdocs.org/sdr/KCB2005F00000), Sep 29, 2005: ENGINE. FLAMED OUT. RT ENGINE FLAMED OUT DUE TO TURBULANCE. ENGINE WAS RESTARTED AND CONTINUED TO ORIGINAL DESTINATION. CAPTAIN CONTACTED MAINTENANCE DEPARTMENT. ENGINE WAS INSPECT - [SDR Y2PA05014](https://openairdocs.org/sdr/Y2PA05014), Sep 1, 2005: ENGINE. BIRD STRIKE. DURING TAKEOFF, JUST AFTER ROTATION, AIRCRAFT ENCOUNTERED A FLOCK OF BIRDS, RESULTING IN FOD TO BOTH ENGINES AND SUBSEQUENT SHUTDOWN OF BOTH ENGINES. AIRCRAFT H - [SDR Y2PA05009](https://openairdocs.org/sdr/Y2PA05009), Jun 14, 2005: TRANSMITTER. FAILED. DURING DESCENT, CREW NOTICED NR 1 ENGINE OIL PRESSURE GAUGE MAXED OUT. REDUCED NR 1 THROTTLE AND GAUGE DIDN`T MOVE. CREW SHUTDOWN NR 1 ENGINE, DECLARED AN EMERG - [SDR KC82005F00000](https://openairdocs.org/sdr/KC82005F00000), Dec 9, 2004: VALVE. STUCK. AIR CONDITIONING VALVE STUCK PARTIALLY OPEN NOT ALLOWING ENOUGH AIR INTO THE CABIN TO PRESSURIZE. REPLACED VALVE WITH SERVICEABLE VALVE. PERFORED OPS CHECK IAW - [SDR KC82005F00001](https://openairdocs.org/sdr/KC82005F00001), Dec 8, 2004: ENGINE. SHUTDOWN. RT ENGINE ROLLED BACK AND SHUTDOWN WHEN CAPTAIN ADVANCED THE POWER LEVERS. PILOT TAXIED BACK TO HANGAR. PERFORMED ENGINE RUNS AND PERFORMANCE CHECKS IAW GE MANU - [SDR Y2PA04017](https://openairdocs.org/sdr/Y2PA04017), Jul 12, 2004: COMPRESSOR. DAMAGED. DURING RVSM FLT TESTING, IN LEVEL FLT AT FL375, NR 1 ENG FLAMED OUT. CREW DECLARED EMERGENCY, DRIFTED DOWN & ENGINE RE-STARTED AT FL290 USING AIRSTAT CHECKLIST. - [SDR KC82003F00003](https://openairdocs.org/sdr/KC82003F00003), Aug 20, 2003: FAN. DAMAGED. SHORTLY AFTER TAKE OFF THE RT ENGINE ROLLED BACK CLIMBING THROUGH 3000 FT. FOUND RT ENGINE WITH COMPRESSOR FOD. REPLACED RT ENGINE WITH SERVICEABLE ENGINE. - [SDR Y2PA03015](https://openairdocs.org/sdr/Y2PA03015), Jul 8, 2003: STUD. SHEARED. NR 1 ENG FLAMED-OUT AT 32,000 FT, AIRSPEED 64 CLEAR NO TURBULENCE, -20 DEGREES CELSIUS, NR 1 EPR AND NR 1 FUEL FLOW ERRATIC DURING CLIMB. CREW DESCENDED TO FL30 - [SDR Y2PA03001](https://openairdocs.org/sdr/Y2PA03001), Jan 6, 2003: ENGINE. FOD. NR 1 ENG LOST PWR IN FLT, POST FLT INSPECT REVEALED DAMAGE TO COMPRESS. A/C CRUISING AT INTERMEDIATE (12000 FT) ALTITUDE INBOUND (DESCENDING). CREW HEARD/FELT C - [SDR Y2PA02018](https://openairdocs.org/sdr/Y2PA02018), Aug 14, 2002: LINE. FAILED. UPON DESCENT INTO DRT THE NR 1 ENGINE LOST OIL PRESSURE. THE ABNORMAL CHECKLIST FOR LOSS OF OIL PRESSURE WAS EXECUTED AND THE CREW SHUT DOWN THE LEFT ENGINE. CR - [SDR DKAA98008](https://openairdocs.org/sdr/DKAA98008), Jun 10, 1998: COMPRESSOR. FOD. NR 1 ENGINE FLAMED OUT DURING FIRST POWER REDUCTION AFTER TAKEOFF. FOUND NR 1 ENGINE TO HAVE COMPRESSOR FOD. REPLACED NR 1 ENGINE PER RAI CARD NR 1-7100-01 AND - [SDR DKAA97002](https://openairdocs.org/sdr/DKAA97002), Dec 28, 1997: FUEL CONTROL. MALFUNCTIONED. NR 2 ENGINE FLAMED OUT AT FL 33.5 AND FL 27.3. PERFORMED BORESCOPE INSPECTION, NO DEFECTS NOTED. REPLACED NR 2 ENGINE FUEL CONTROL UNIT AND PERFORMED POWER ASSU - [SDR 97ZZZM1212](https://openairdocs.org/sdr/97ZZZM1212), Oct 29, 1997: FUEL PUMP. INOP. YIP - NR 2 ENGINE FLAMED OUT WHILE CLIMBING THROUGH FL325. ENGINE RELIT AT FL290, FLIGHT CONTINUED AT FL270. NO EMERGENCY PROCEDURES WERE NECESSARY. MAINTENANCE - [SDR Y2PA97027](https://openairdocs.org/sdr/Y2PA97027), Oct 29, 1997: FUEL CONTROL. INOP. YIP - NR 2 ENGINE FLAMED OUT WHILE CLIMBING THROUGH FL325. ENGINE RELIT AT FL290, FLIGHT CONTINUED AT FL270. NO EMERGENCY PROCEDURES WERE NECESSARY. MAINTENANCE - [SDR 97ZZZM1082](https://openairdocs.org/sdr/97ZZZM1082), Sep 24, 1997: FUEL CONTROL. OUT OF ADJUST. LEFT ENGINE FLAMED OUT AT FL 310. RESTARTED NORMAL AT FL 280. ADJUSTED FEED BACK CABLE ON FUEL CONTROL TO INSURE POSITIVE BLEED VALVE CLOSURE, IAW MM 73-20. OPE - [SDR 97ZZZX4612](https://openairdocs.org/sdr/97ZZZX4612), Sep 19, 1997: ENGINE. FLAMED OUT. LEFT ENGINE FLAMED-OUT APPROACHING FL 350. ENGINE RE-LIT AT FL 300. PERFORMED VISUAL INSPECTION OF COMPRESSOR/FAN SECTIONS, NO DEFECTS NOTED. ENGINE RUN-UP CHEC - [SDR 97ZZZM960](https://openairdocs.org/sdr/97ZZZM960), Aug 20, 1997: FUEL PUMP. FAILED. LEFT ENGINE FLAMED OUT AT FL230 AND WOULD NOT RELIGHT. LANDED AT SYR. REPLACED NR 1 ENGINE FUEL CONTROL AND PUMP PER SEI-187. OPERATIONAL AND LEAK CHECKS GOOD. - [SDR 97ZZZX2357](https://openairdocs.org/sdr/97ZZZX2357), May 20, 1997: O RING. LEAK. THE PILOT RETURNED AFTER 30 MINUTES DUE TO OIL PRESSURE AND OIL QUANTITY LOSS ON NR 2 ENGINE. AN INVESTIGATION REVEALED THE O-RING SEAL (ACCESS 'C') ON THE DRIV - [SDR Y2PA97014](https://openairdocs.org/sdr/Y2PA97014), Apr 15, 1997: CARBON SEAL. FAILED. YIP - PERFORMED PRECAUTION ENG SHUT DOWN NR 2 ENG DUE TO FLUCT OIL PRESS AND FLICKERING OIL PRESS LIGHT. A/C CONTINUED TO YIP. A/C WAS FLOWN UNDER SPECIAL FLT P - [SDR YIEA96001](https://openairdocs.org/sdr/YIEA96001), Jan 18, 1996: ENGINE. FLAME OUT. PILOT REPORTED WHILE IN A STEADY STATE, CLIMB-OUT FOR FL 330 TO FL 370, LT ENGINE FLAMED OUT AT 34,300 FEET. ACFT FLYING AT .68 MACH. THERE WERE NO CLOUDS AND V ## STCs that may be installed (OpenAirDocs) (5) Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SE976SO](https://openairdocs.org/stc/SE976SO): Installation of an oil tank sight gauge on a G.E. oil tank, P/N6003T09P04. JSF Aviation Services Inc. Lists CF700 Series - [STC SE8674SW](https://openairdocs.org/stc/SE8674SW): Modification of the following engine oil tanks by adding a sight glass: 6002T03P01, 6002T03P03, 6003T09P01, 6003T09P02, 6003T09P03, 6003T09P04, 6003T89P01, 6003T89P02, 6003T03P02, 6002T03P04. Bizjet International Sales & Support Inc - [STC SE966SO](https://openairdocs.org/stc/SE966SO): Manufacture and installation of Axis C gearshaft plugs per Fed Ex Drawing F-72-003, Sheets 1 and 2. JSF Aviation Services Inc - [STC SE1057SO](https://openairdocs.org/stc/SE1057SO): Installation of capacitance type probe with oil quantity indicating system in oil tank. Aircraft Equipment Certification Corporation. Lists CF700 Series - [STC SE949SO](https://openairdocs.org/stc/SE949SO): Installation of an oil level sight gauge. Aircraft Equipment Certification Corporation --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.