# GE CJ-610-4 - Type: Engine model (FAA registry) - Registry code: 30034 - Manufacturer (registry): GE - Model: CJ-610-4 - 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: 3 registered aircraft - Page: https://openairdocs.org/engine/ge-cj-610-4 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 (3) - [N711CW](https://openairdocs.org/aircraft/N711CW): [Premier Jets Inc](https://openairdocs.org/faa-owner/PREMIER%20JETS%20INC), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), built 1965, S/N 055 - [N73CE](https://openairdocs.org/aircraft/N73CE): [Yanks Air Museum](https://openairdocs.org/faa-owner/YANKS%20AIR%20MUSEUM), [Baldwin Park, CA](https://openairdocs.org/faa-place/CA/Baldwin%20Park), built 1965, S/N 23068 - [N823LJ](https://openairdocs.org/aircraft/N823LJ): [Artemis Aviation Group LLC](https://openairdocs.org/faa-owner/ARTEMIS%20AVIATION%20GROUP%20LLC), [Kalispell, MT](https://openairdocs.org/faa-place/MT/Kalispell), S/N 23-082A ## NTSB investigations None matched to aircraft with this engine model. ## FAA accident and incident reports (3) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20000108022809I](https://openairdocs.org/incident/20000108022809I), Jan 8, 2000: Lear 24 (N994TD), Fort Wayne, IN. (-23)At 42000 ft. climbing the cabin alt horn sounded. Aircraft descended and horn went off at lower alt. Aircraft landed with no difficulty. - [Incident 19900314011309I](https://openairdocs.org/incident/19900314011309I), Mar 14, 1990: Lear 24 (N711CW), Billings, MT. During landing on icy runway aircraft veered left into a snow berm. Braking action poor. - [Incident 19840613031179I](https://openairdocs.org/incident/19840613031179I), Jun 13, 1984: Lear 24 (N711CW), Hillsboro, OR, Minor damage. Scraped a wing tip on the runway after student and instructor allowed the aircraft to dutch roll on short final. ## Service difficulty reports (10) As reported by operators and repair stations, by the model named in the report. - [SDR CA110125008](https://openairdocs.org/sdr/CA110125008), Jan 15, 2011: PUMP. FAILED. (CAN) OIL PRESSURE LOSS/IFSD WHILE SETTING UP FOR APPROACH, THE OIL PRESSURE WARNING ILLUMINATED AND OIL PRESSURE INDICATION WAS ZERO. THE PILOT IMMEDIATELY SHU - [SDR HAEA200600194](https://openairdocs.org/sdr/HAEA200600194), Sep 22, 2006: ENGINE. FLAMED OUT. RT ENGINE FLAMED OUT ON DESCENT INTO YIP. PILOT REPORTED THAT THE RT ENGINE THROTTLE WAS RETARDED TO LOWER THAN NORMAL IDLE. ENGINE RELIGHT WAS ACCOMPLISHED. AI - [SDR 00116](https://openairdocs.org/sdr/00116), Oct 7, 2003: ENGINE. FLAMED OUT. PILOT REPORTED LT ENGINE FLAMMED OUT WHILE CLIMBING FROM FL420 TO FL430, DECENT TO RELIGHT ALTITUDE, RELIGHT NORMAL AND CONTINUED TO DESTINATION. WILL UPDATE AF - [SDR HAEA200100002](https://openairdocs.org/sdr/HAEA200100002), Oct 5, 2001: FCU. OUT OF ADJ. AIRCRAFT WAS CLIMBING FROM 390 TO 410 AT 410 RIGHT ENGINE FLAMED OUT. DESCEND TO 240, PERFORMED SUCCESSFUL RELIGHT AND CLIMB BACK TO 390. DENSITY SETTING CHANGE - [SDR 2000ZZZX651](https://openairdocs.org/sdr/2000ZZZX651), Feb 3, 2000: FUEL CONTROL. DAMAGED. FLIGHT CREW WAS UNABLE TO REDUCE ENGINE RPM BELOW 97 PERCENT. ENGINE WAS SHUT DOWN AND SECURED AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE REMOVED THE FUEL - [SDR 20000404SH022](https://openairdocs.org/sdr/20000404SH022), Jan 5, 2000: ENGINE. STALLED. LEFT ENGINE COMPRESSOR STALLED ON DESCENT WHILE ADVANCING THROTTLE. UNEVENTFUL LANDING EXECUTED. INSPECTED ENGINE FOR FOD, NONE FOUND. CHECKED THROTTLE AND IGV - [SDR 99ZZZX2312](https://openairdocs.org/sdr/99ZZZX2312), May 13, 1999: ENGINE. FAILED. LEFT ENGINE EXPERIENCED TURBULENCE INDUCED FLAME-OUT AND WOULD NOT RE-LIGHT IN FLIGHT. UNEVENTFUL LANDING ACCOMPLISHED. ENGINE TO BE REMOVED AND REPLACED. ENGIN - [SDR 99ZZZX50](https://openairdocs.org/sdr/99ZZZX50), Sep 12, 1998: ENGINE. MALFUNCTIONED. MKE - AFTER DEPARTING, FLIGHT CREW NOTICED ABNORMAL RT ENGINE INDICATION AND LOSS OF POWER. A PRECAUTIONARY ENGINE SHUT DOWN WAS MADE FOLLOWED BY AN UNEVENTFUL - [SDR 95ZZZX3164](https://openairdocs.org/sdr/95ZZZX3164), May 18, 1995: ENGINE. FLAME OUT. LEFT ENGINE FLAMED OUT AT 40,900 FEET CLIMBING THROUGH BAD WEATHER. PILOT REQUEST DESCENT TO 10,000 FEET AND NEAREST AIRPORT. AIRCRAFT ENGINE RE-LIGHT PROCEDURE - [SDR 95ZZZX675](https://openairdocs.org/sdr/95ZZZX675), Jan 23, 1995: TUBE. FAILED. AIRCRAFT AT LEVEL FLIGHT 41,000 FEET WHEN ENGINE SUDDENLY FLAMED OUT. PILOT REQUESTED DESCENT AND WAS GRANTED. PILOT ATTEMPTED RELIGHT SEVERAL TIMES, UNSUCCESSF ## 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. 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