# GE CJ610-5 - Type: Engine model (FAA registry) - Registry code: 30121 - Manufacturer (registry): GE - Model: CJ610-5 - Engine type: Turbo-jet - Power: 2,950 lb thrust - Data sheet: [TCDS 1E16](https://openairdocs.org/tcds/1E16) (OpenAirDocs) - Holder: General Electric Company - Installed in: 0 registered aircraft - Page: https://openairdocs.org/engine/ge-cj610-5 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 78-07-06](https://openairdocs.org/ad/78-07-06): Compressor Disks · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 2 more - [AD 73-23-05](https://openairdocs.org/ad/73-23-05): First Stage Turbine Discs · General Electric CF700-2C, CJ610-1, CJ610-4 and 2 more ## 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 (8) As reported by operators and repair stations, by the model named in the report. - [SDR KC82005F00008](https://openairdocs.org/sdr/KC82005F00008), Nov 14, 2005: SERVO. DEFECTIVE. AFTER TAKEOFF, GEAR WAS SELECTED UP, NOSE STEERING SERVO DRIVE NOSE WHEEL 90 DEGREES. NOSE GEAR WOULD NOT RETRACT INTO THE WHEEL WELL. GEAR WAS SELECTED DOWN AN - [SDR KC82005F00003](https://openairdocs.org/sdr/KC82005F00003), Jan 24, 2005: SQUAT SWITCH. FAILED. AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT. PILOT RETURNED TO DEPARTURE. FOUND LT MAIN GEAR SQUAT SWITCH FROZEN AND THE INTERNAL MICRO SWITCHES REMAINED - [SDR KC82002F00005](https://openairdocs.org/sdr/KC82002F00005), Oct 23, 2002: GASKET. MISINSTALLED. THE LEFT AIRCRAFT LOW PRESSURE FUEL LIGHT CAME ON AS THE ENGINES WERE POWERED UP. TROUBLE SHOT LEFT FUEL SYSTEM AND FOUND THAT THE LOW PRESSURE FUEL FILTER GASK - [SDR 8292001N39CK](https://openairdocs.org/sdr/8292001N39CK), Aug 31, 2001: SWITCH. FAILED. LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO AIRPORT. UNEVENTFUL LANDING ACCOMPLISHED. REPLACED RIGHT MAIN GEAR TRUNNION SWITCH WITH NEW AND ADJUSTED IN - [SDR 20010312CW016](https://openairdocs.org/sdr/20010312CW016), Jan 24, 2001: CONNECTOR. DAMAGED. LANDING GEAR WOULD NOT EXTEND NORMALLY. PERFORMED EMERGENCY GEAR EXTENSION. UNEVENTFULL LANDING ACCOMPLISHED. REPLACED LOOSE SOCKET AT GEAR SELECTOR SWITCH CONN - [SDR GXPA99002](https://openairdocs.org/sdr/GXPA99002), May 29, 1999: BELLOWS. LOOSE. LEFT ENGINE FLAME-OUT CLIMBING FROM FL 370 TO FL 390. ENGINE RE-LIGHT AT 5,000 FEET. FOUND 'P2' BELLOWS LOOSE AT FUEL CONTROL ENGINE. GROUND RUN GOOD AFTER RE-S - [SDR 97ZZZX3447](https://openairdocs.org/sdr/97ZZZX3447), Jul 17, 1997: HOSE. LOOSE. RIGHT ENGINE FLAMED OUT AT FL 370. ENGINE RE-STARTED IAW AFM AIR START PROCEDURES. ENGINE INSPECTED AND NO DAMAGE NOTED. TIGHTENED LOOSE T2 SENSE HOSE. C/W ALTI - [SDR GXPA96004](https://openairdocs.org/sdr/GXPA96004), Oct 21, 1996: ENGINE. FLAME OUT. A/C WAS EN ROUTE, A/C ALT 33,000 FEET SKIRTING THUNDERSTORMS EXPERIENCED SEVERE TURBULENCE, NR 2 ENGINE FLAMED OUT. STARTED DESCENT, AIRSTART ON, NR 1 ENGINE FL ## 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 CJ610 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 SE1057SO](https://openairdocs.org/stc/SE1057SO): Installation of capacitance type probe with oil quantity indicating system in oil tank. Aircraft Equipment Certification Corporation. Lists CJ610 Series - [STC SE949SO](https://openairdocs.org/stc/SE949SO): Installation of an oil level sight gauge. Aircraft Equipment Certification Corporation - [STC SE6CE](https://openairdocs.org/stc/SE6CE): Installation of slotted disc magnetic pickup on overspeed fuel control. Woodward Governor Co --- 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.