# GE CJ610-8

- Type: Engine model (FAA registry)
- Registry code: 30123
- Manufacturer (registry): GE
- Model: CJ610-8
- Engine type: Turbo-jet
- Power: 3,100 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-cj610-8

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

## 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)

- [N564CL](https://openairdocs.org/aircraft/N564CL): [David Copperfield Project Magic Fund](https://openairdocs.org/faa-owner/DAVID%20COPPERFIELD%20PROJECT%20MAGIC%20FUND), [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas), built 1976, S/N 25-060

## 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 20070301002479I](https://openairdocs.org/incident/20070301002479I), Mar 1, 2007: Lear 31A (N181PA), Fort Smith, AR, Minor damage. (-23) Aircraft received maintenance at the springdale, AR facility prior to flight. Maintenance crew did not secure left engine cowling properly, PIC did not…
- [Incident 19900425020589I](https://openairdocs.org/incident/19900425020589I), Apr 25, 1990: Lear 25 (N564CL), Van Nuys, CA. On single engine approach instructor took over and made go around. Left wing tip tank hit runway.
- [Incident 19800518052729I](https://openairdocs.org/incident/19800518052729I), May 18, 1980: Lear 25 (N564CL), Van Nuys, CA, Minor damage. Nose steering malfunctioned on landing. Aircraft ran off runway.

## Service difficulty reports (24)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2016FA0000151](https://openairdocs.org/sdr/2016FA0000151), Mar 22, 2016: TUBE. FAILED. DURING A ROUTINE FLIGHT THIS TUBE RUPTURED AT THE BASE OF THE FLARE SLEEVE FOR THE B-NUT. THE RUPTURE WAS APPROXIMATELY 50 PERCENT AROUND THE TUBE. THE RUPTURED
- [SDR ZP7A2010F00117](https://openairdocs.org/sdr/ZP7A2010F00117), May 26, 2010: ENGINE. BIRD INGESTION. BIRD WAS INGESTED INTO LEFT ENGINE JUST AFTER V-1. ENGINE FLAMED OUT, TAKE OFF WAS CONTINUED TO A SAFE ALTITUDE. CREW DECLARED AN EMERGENCY ON CTAF AND RETURNED
- [SDR CJP2006F00000](https://openairdocs.org/sdr/CJP2006F00000), Nov 17, 2006: BALL JOINT. OUT OF ADJUST. NR 1 ENGINE FLAMED OUT WHEN THROTTLED TO IDLE FOR DESCENT. ENGINE WAS SUCCESSFULLY AIR STARTED. UPON LANDING THROTTLES WERE RETARDED AND NR 1 ENGINE FLAMED OUT 
- [SDR 2005FA0000188](https://openairdocs.org/sdr/2005FA0000188), Feb 3, 2005: PUMP. FLAKING. THE INTERNAL COATING IN THE GEAR SECTION OF THE FUEL PUMP STARTED FLAKING OFF AND GOT INTO THE HIGH PRESSURE FUEL LINE THAT GOES TO THE JET PUMPS IN THE RT WING
- [SDR 4019](https://openairdocs.org/sdr/4019), Aug 13, 2004: WARNING LIGHT. ILLUMINATED. ON APPROACH INTO CLT RIGHT ENGINE FIRE LIGHT CAME ON, FIRST STARTED FLICKERING THEN CAME ON STEADY. REDUCED POWER LIGHT WENT OUT, THEN CAME BACK ON AND STAYED O
- [SDR 4020](https://openairdocs.org/sdr/4020), Aug 13, 2004: WARNING LIGHT. ILLUMINATED. ON APPROACH INTO CLT RIGHT ENGINE FIRE LIGHT CAME ON, FIRST STARTED FLICKERING THEN CAME ON STEADY. REDUCED POWER LIGHT WENT OUT, THEN CAME BACK ON AND STAYED O
- [SDR YDB2004FBBB](https://openairdocs.org/sdr/YDB2004FBBB), Jul 21, 2004: TUBE. UNSERVICEABLE. PILOT REPORTED BRAKES WERE VERY WEAK ON LANDING ROLL OUT. FOUND LARGE AMOUNT OF HYDRAULIC FLUID ON AFT PORTION OF AIRCRAFT BELLY. T/S AND FOUND LT ENGINE HYDRAU
- [SDR 2004F00045](https://openairdocs.org/sdr/2004F00045), Jan 13, 2004: FIRE LOOP. DIRTY. FALSE FIRE WARNING DURING FLIGHT. AFTER A/C LANDED, PILOT REPORTED INDICATION WAS INTERMITTENT. COWL WAS REMOVED, ENGINE INSPECTED, NO INDICATION OF FIRE/OVERHE
- [SDR DRU2004F00000](https://openairdocs.org/sdr/DRU2004F00000), Jan 13, 2004: FIRE DETECTOR. FALSE INDICATION. FALSE FIRE WARNING DURING FLIGHT. AFTER THE AIRCRAFT LANDED, THE PILOT REPORTED THAT THE INDICATION WAS INTERMITTENT. THE RT ENGINE COWLING WAS REMOVED, AND THE
- [SDR 2003006](https://openairdocs.org/sdr/2003006), Dec 17, 2003: ENGINE. MALFUNCTIONED. DURING FLT AT APPROXIMATELY 2:00 AM, AIRCRAFT WAS ENROUTE WHEN THE PILOT NOTICED THAT THE LT ENGINE OIL PRESSURE WAS DECREASING. THE PILOT ALSO NOTICED THAT THE
- [SDR CJP2003F00002](https://openairdocs.org/sdr/CJP2003F00002), Feb 17, 2003: CONTROL BOX. INTERMITTENT. FLIGHT CREW EXPERIENCED INTERMITTENT RIGHT ENGINE FIRE WARNING. AIRCRAFT LANDED AT INTENDED DESTINATION. MAINTENANCE TROUBLESHOT ENGINE PYLON WIRING WHICH IS TH
- [SDR DRU2003F00000](https://openairdocs.org/sdr/DRU2003F00000), Feb 10, 2003: BLANKET. BURNED. DURING INSP BY MECH, A BLACK STREAK (FORE TO AFT) WAS NOTICED ON LT HORIZ STAB, THAT BOOT LOOKED BURNT ON L.E. EXAMINATION REVEALED THAT BOOT MUST HAVE SHORTED 
- [SDR ESUA116360](https://openairdocs.org/sdr/ESUA116360), Sep 13, 2002: LINE. LOOSE. PILOT DECLARED AN EMERGENCY ON APPROACH, IT WAS DISCOVERED THAT THE HYDRAULIC PRESSURE INDICATED (0). THE GEAR WAS ABLE TO BE PLACED IN THE DOWN AND LOCKED POSI
- [SDR ESY2002F00000](https://openairdocs.org/sdr/ESY2002F00000), Aug 15, 2002: ENGINE. FAILED. FIFTEEN MINUTES AFTER TAKE-OFF, EXPERIENCED FAILURE OF RT ENGINE, WHILE CLIMBING, LEAVING, EVERYTHING WAS NORMAL. NO PREVIOUS ENG ABNORMALITY HAD BEEN NOTED. AT
- [SDR IKM2002F00001](https://openairdocs.org/sdr/IKM2002F00001), Apr 5, 2002: WHEEL. CRACKED. WHEEL, CRACKED, BEAD SEAL AREA.
- [SDR IY22002F00000](https://openairdocs.org/sdr/IY22002F00000), Dec 13, 2001: STRUCTURE. CORRODED. DURING PREPARATION OF AIRCRAFT FOR PAINT, CORROSION WAS FOUND ON THE TOP OF THE LEFT WING BETWEEN WING STATIONS 125.00 TO 181.10 AND SPAR NR 5 TO 8 UNDER A RAIS
- [SDR JDMA648B](https://openairdocs.org/sdr/JDMA648B), Feb 14, 2001: LINE. CRACKED. HYDRAULIC TRANSFER LINE IN AUXILARY SYSTEM, LINE WAS FOUND BROKEN AT FLAIR CAUSING LOSS OF HYDRAULIC FLUID AND HYDRAULIC SYSTEM FAILURE. AIRCRAFT WAS REPAIRED A
- [SDR 20010205CW013](https://openairdocs.org/sdr/20010205CW013), Jan 9, 2001: HYDRAULIC LINE. CHAFED. PILOT LOST HYDRAULIC PRESSURE IN FLIGHT. INSPECTION REVEALED HYDRAULIC PRESSURE LINE FROM LEFT ENGINE TO AUXILLARY HYDRALUIC PUMP MANIFOLD LINE, CHAFFED AT CLAM
- [SDR CA001019018](https://openairdocs.org/sdr/CA001019018), Sep 21, 2000: ACCUMULATOR. SEPARATED. (CAN) AFTER FLAPS SELECTED TO 10 DEGREES HYDRAULIC PRESSURE DROPPED TO 0 PSI ALTERNATE GEAR EXTENSION USED. FOUND THRUST REVERSER ACCUMULATOR SPLIT IN TWO. WHIC
- [SDR 20010117AP001](https://openairdocs.org/sdr/20010117AP001), Sep 20, 2000: ENGINE. FLAMED OUT. ENGINE FLAMED OUT DURING CRUISE-FOUND EXCESSIVE CORROSION OF COMPRESSOR CASING
- [SDR 20001016SH006](https://openairdocs.org/sdr/20001016SH006), Aug 3, 2000: CONTROL UNIT. MALFUNCTIONED. CMH - LOST CABIN PRESSURIZATION AFTER DEPARTURE OUT OF COLUMBUS. RETURNED TO CMH. INSPECTED BLEED AIR LINES IN HEX HOSE AND IN CABIN, RAN BOTH ENGINES, NO LEAKS
- [SDR 20000329SH050](https://openairdocs.org/sdr/20000329SH050), Jan 10, 2000: STARTER GEN. FAILED. DURING FLIGHT ON 1-10-2000, PILOT NOTICED VIBRATION IN AIRCRAFT, SHORTLY THEREAFTER, GENERATOR OFF-LINE. PILOT LANDED AIRCRAFT AT GJT. STARTER/GENERATOR WAS REP
- [SDR CA991209027](https://openairdocs.org/sdr/CA991209027), Nov 2, 1999: TRANSCEIVER. MALFUNCTIONED. (CAN) AFTER FLYING THROUGH RAIN ON APPROACH, COMMUNICATION RADIOS BECAME GARBLED/UNREADABLE. BENCH CHECK OF UNITS REVEALED TRANSCEIVER UNITS TO BE INTERNALLY CO
- [SDR 95ZZZX6579](https://openairdocs.org/sdr/95ZZZX6579), Nov 17, 1995: HOSE. FAILED. PILOT STATED LT NACELLE ANTI-ICE INOP AND TRIPPING CIRCUIT BREAKER ON LANDING. AFTER REMOVAL OF TOP COWLING, FOUND HOSE CONNECTING ANTI-ICE TUBE AND ANTI-ICE TE

## STCs that may be installed (OpenAirDocs) (4)

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

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