Aerocomp Comp Air Jet
From Wikipedia, the free encyclopedia
The Aerocomp Comp Air Jet is a turbofan-powered civil utility aircraft that first flew in 2004 and is being marketed for homebuilding. It is configured as a conventional, low-wing monoplane with tricycle undercarriage. The single jet engine in the tail is fed by air intakes on the sides of the rear fuselage.
[edit] Specifications (Comp Air Jet)
[edit] General characteristics
- Crew: one pilot
- Capacity: 7 passengers
- Length: ft in ( m)
- Wingspan: ft in ( m)
- Height: ft in ( m)
- Wing area: ft² ( m²)
- Empty: 4,500 lb (2,045 kg)
- Loaded: lb ( kg)
- Maximum takeoff: 8,900 lb (4,045 kg)
- Powerplant: 1× Ivchenko AI-25 turbofan, 3,400 lbf (15.2 kN) thrust
- Powerplant: 1× Honeywell TFE731 turbofan, 3,500 lbf (15.3 kN) thrust (planned to replace the AI-25 in production aircraft)
[edit] Performance
- Maximum speed: 370 mph (592 km/h)
- Range: 1,446 miles (2,315 km)
- Service ceiling: 29,900 ft (9,116 m)
- Rate of climb: ft/min ( m/min)
- Wing loading: lb/ft² ( kg/m²)
- Thrust-to-weight:
[edit] External link
[edit] Related content
Related development: Aerocomp Comp Air 12
Comparable aircraft:
Designation sequence:
Lists relating to