General Electric CJ610
From Wikipedia, the free encyclopedia
The General Electric CJ610 is a non-afterburning turbojet engine derived from the military J85, and is used on a number of civilian business jets. The model has logged over 16.5 million hours of operation. Civilian versions have powered business jets such as the Learjet 23 and the Hamburger Flugzeugbau HFB-320 Hansa Jet.
Another variant, the CF700, adds a rear-mounted "flade" connected directly to the low-pressure turbine blade.
[edit] Aircraft used on
- Aero Commander 1121 Jet Commander
- HFB-320 Hansa Jet
- Learjet 23
- Learjet 24
- Learjet 25
- Learjet 28
- Learjet 29
[edit] Specifications
- Compressor stages: 8t
- Turbine stages: 2
- Maximum diameter: 17.7 inches
- Length: 45.4 to 51.1 inches (depending on accessory equipment installed)
- Dry weight: 396 - 421 pounds (depending on accessory equipment installed)
- Max power specific fuel consumption: 0.96 - 0.97
- Max thrust at sea level: 2850 - 3100 lbf
