# GE CJ610-1 - Type: Engine model (FAA registry) - Registry code: 30120 - Manufacturer (registry): GE - Model: CJ610-1 - Engine type: Turbo-jet - Power: 2,850 lb thrust - Data sheet: [TCDS 1E16](https://openairdocs.org/tcds/1E16) (OpenAirDocs) - Holder: General Electric Company - Installed in: 1 registered aircraft - Page: https://openairdocs.org/engine/ge-cj610-1 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 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 (1) - [N1965L](https://openairdocs.org/aircraft/N1965L): [Museum Of Flight Foundation](https://openairdocs.org/faa-owner/MUSEUM%20OF%20FLIGHT%20FOUNDATION), [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle), built 1965, S/N 012 ## 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 (22) As reported by operators and repair stations, by the model named in the report. - [SDR KC82005F00004](https://openairdocs.org/sdr/KC82005F00004), Nov 18, 2004: STARTER GEN. VIBRATION. CREW FELT VIBRATION IN AIRCRAFT DURING CRUISE FLIGHT. FOUND RT STARTER GEN WAS CAUSING VIBRATION. REPLACED STARTER GEN WITH REPAIRED ASSEMBLY. PERFORMED ENGINE - [SDR 1013041](https://openairdocs.org/sdr/1013041), Oct 13, 2004: CONTROL MODULE. MALFUNCTIONED. ON A FLIGHT, THE FLIGHT CREW NOTICED THAT THE PRESSURIZATION SYSTEM WAS NOT INCREASING CABIN PRESSURE AT A RATE TYPICAL TO NORMAL AIRCRAFT OPERATION. AT 17,000 - [SDR KC82004F00000](https://openairdocs.org/sdr/KC82004F00000), Jan 12, 2004: LINE. FAILED. COMPLETE HYDRAULIC FAILURE OF THE NORMAL SYSTEM AFTER GEAR EXTENSION. AUXILIARY SYSTEM WORKED NORMALLY. FOUND HYDRAULIC LINE FROM LT ENGINE DRIVEN HYDRAULIC PUM - [SDR 00120](https://openairdocs.org/sdr/00120), Nov 6, 2003: UPLOCK SWITCH. DIRTY. AIRCRAFT DEPARTED YIP FOR RWI SHORTLY AFTER TAKEOFF LT UNSAFE GEAR LIGHT ILLUMINATED, CREW CYCLED GEAR SEVERAL TIMES WHEN GEAR WAS FULLY EXTENDED GEAR LIGHT WOU - [SDR 2004F00326](https://openairdocs.org/sdr/2004F00326), Sep 24, 2003: ENGINE. FLAMED OUT. ON A TEST FLIGHT AFTER ENGINE INSTALL. ENGINE BEING TESTED FLAMED OUT AT 42,500 FT. AT A LOWER ALTITUDE OF 23,000 FT ENGINE RESTARTED AND RAN WITH NO FURTHER TR - [SDR X5E2003F00000](https://openairdocs.org/sdr/X5E2003F00000), Sep 15, 2003: WINDSHIELD. FAILED. LEFT WINDSHIELD WAS REPLACED WITH A PMA PART ON 12/8/1999. ON 7/3/2001 A BLISTER/ BUBBLE HAD FORMED IN THE INNER PLY AND WAS POLISHED OUT BY THE WINDOW MANUFACT - [SDR EA11200202951](https://openairdocs.org/sdr/EA11200202951), Oct 22, 2002: INDICATOR. MALFUNCTIONED. RT THRUST REVERSER ILLUMINTED IN FLIGHT, SYSTEM OPERATED CORRECTLY IWA MFG MM. VISUAL INSPECTION REVEALED STICKY LATCHES AND DEFECTIVE T/R ACCUMULATOR. AWAITING - [SDR X5C2002F00000](https://openairdocs.org/sdr/X5C2002F00000), Oct 17, 2002: O-RING. NICKED. LOW HYDRAULIC PRESSURE ON APPROACH, AIRCRAFT RETURNED, MAINTENANCE BASE. FOUND HYDRAULIC LEAK AT LT MAIN GEAR ACTUATOR FITTING, HYDRAULIC FLUID LEVEL LOW. LEAK - [SDR X5C2002F00001](https://openairdocs.org/sdr/X5C2002F00001), Oct 17, 2002: O-RING. FAILED. LOW HYDRAULIC PRESSURE DURING LANDING APPROACH. REPLACED O-RING AT LEFT MAIN LANDING GEAR ACTUATOR FITTING, OPS CHECK GOOD. - [SDR ECA2002F00002](https://openairdocs.org/sdr/ECA2002F00002), Oct 1, 2002: ACCUMULATOR. LEAKING. RT THRUST REVERSER ARM LIGHT ILLUMINATED IN FLIGHT ON LEG NR 2. A/C RETURNED TO BASE. GROUND OPS CHECK WAS PERFORMED, SYSTEM WAS OPERATING CORRECTLY IAW MM. VIS - [SDR ESUA116380](https://openairdocs.org/sdr/ESUA116380), Sep 14, 2002: ACCESS PANEL. DEPARTED. AFTER DEPARTURE , PASSING THROUGH 13000 FEET, PILOT HEARD A LOUD BANG FOLLOWED BY A NOTICEABLE VIBRATION. PILOT DECLARED AN EMERGENCY, RETURNED TO AIRPORT. MAIN - [SDR KC82002F00003](https://openairdocs.org/sdr/KC82002F00003), Aug 26, 2002: OUTFLOW VALVE. OBSTRUCTED. CREW HAD DIFFICULTY MAINTAINING CABIN ALTITUDE. FOUND DEBRIS ON SEAT OF OUTFLOW VALVE. CLEANED OUTFLOW VALVE, CLEANED JET PUMP FILTER, AND PERFORMED OPERATIONAL - [SDR QH52002F00001](https://openairdocs.org/sdr/QH52002F00001), Apr 6, 2002: WHEEL. CRACKED. WHEEL CRACKED AT BOLT HOLES. - [SDR ECA2002F00000](https://openairdocs.org/sdr/ECA2002F00000), Apr 1, 2002: SEAL. TORN. CABIN ALTITUDE REACHED 10,000 FT MAX., AIRFLOW WAS APPLIED AND CABIN WAS RESTORED. DECENT FOLLOWED WITH FLOW ON UNTIL 1500 FT PRIOR TO LANDING. REQUIRED MAX AIR - [SDR ECA2002F00001](https://openairdocs.org/sdr/ECA2002F00001), Apr 1, 2002: SEAL. TORN. CABIN ALTITUDE REACHED 10,000 FT MAXIMUM AIRFLOW WAS APPLIED AND CABIN WAS RESTORED. DECENT FOLLOWED WITH FLOW ON UNTIL 1500 FT PRIOR TO LANDING. REQUIRED MAX A - [SDR KC82002F00000](https://openairdocs.org/sdr/KC82002F00000), Feb 13, 2002: CONNECTOR. LOOSE. PRIMARY PITCH TRIM WILL NOT PITCH UP. TIGHTENED LOOSE CONNECTOR PLUG AT TWO SPEED TRIM BOX AND RE-SAFTIED. FUNCTIONAL CHECK OF TRIM SYSTEM COMPLIED WITH PER MFG - [SDR 20010525CW003](https://openairdocs.org/sdr/20010525CW003), May 7, 2001: ENGINE. FLAMED OUT. RIGHT HAND ENGINE FLAMED OUT DURING MAX ACCELERATION CHECK. ENGINE WAS RESTARTED AND UNEVENTFUL LANDING ACCOMPLISHED. COMPLIED WITH LEARJET SSK959 REPLACEMENT O - [SDR 2401N813JW](https://openairdocs.org/sdr/2401N813JW), Feb 6, 2001: SQUAT SWITCH. INOPERATIVE. LANDING GEAR WOULD NOT RETRAACT. AIRCRAFT RETURNED TO BASE. REPLACED RT SQUAT SWITCH WITH NEW. OPERATIONAL CHECK OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM - [SDR 20010213CW009](https://openairdocs.org/sdr/20010213CW009), Jan 10, 2001: CONTROL UNIT. MALFUNCTIONED. AC COULD NOT MAINTAIN PRESSURIZATION AND INCREASE IN CABIN ALTITUDE RESULTED IN OXYGEN MASK DROP AND AURAL WARNINGS, AS APPROPRIATE. AC DESCENDED TO FL220 AND C - [SDR 20010213CW008](https://openairdocs.org/sdr/20010213CW008), Jan 5, 2001: INDICATOR. INOPERATIVE. LEFT ENGINE OIL PRESSURE GAGE NOTED TO HAVE DROPPED AND STUCK AT 12 PSI, OIL PRESSURE ON TAXI FOR TAKEOFF. AC WAS RETURNED TO MAINTENANCE AND A SERVICEABLE OIL - [SDR 20010213CW010](https://openairdocs.org/sdr/20010213CW010), Dec 15, 2000: ACTUATOR. SLUGGISH. RT MAIN LANDING GEAR DOWN AND LOCK (SAFE) LIGHT WAS SLOW TO INDICATE ON GEAR EXTENSION. REPLACED RT MAIN GEAR ACTUATOR AND INDICATING SYSTEM WAS NORMAL. SENT SU - [SDR 20010208CW003](https://openairdocs.org/sdr/20010208CW003), Dec 4, 2000: SERVO. INOPERATIVE. DURING TAXI OUT FOR TAKE OFF AT ERI, NOSE STEERING BECAME INOPERATIVE. FOUND NOSE STEERING SERVO MOTOR INOPERATIVE. ## 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.