Comp Air 12
The Comp Air CA12 is a turboprop-powered civil utility aircraft, currently under development. Comp Air is seeking certification. It is configured as a conventional, low-wing monoplane with tricycle undercarriage. The first flight was on April 14, 2007.
01Specifications (as designed)
General characteristics
- Crew: 1
- Capacity: 8 to 10
- Length: 41 ft 5 in (12.62 m)
- Wingspan: 48 ft (15 m)
- Wing area: 300 sq ft (28 m2)
- Empty weight: 5,880 lb (2,667 kg)
- Max takeoff weight: 10,800 lb (4,899 kg)
- Powerplant: 1 × Honeywell TPE331-14GR turboprop, 1,650 hp (1,230 kW)
Performance
- Cruise speed: 300 kn (350 mph, 560 km/h)
- Stall speed: 73 kn (84 mph, 135 km/h)
- Range: 2,535 nmi (2,917 mi, 4,695 km)
- Rate of climb: 2,800 ft/min (14 m/s) at gross weight
- Wing loading: 35 lb/sq ft (170 kg/m2)
Avionics
Sebastian Communication / OP Technologies
Sources and credits
This article is adapted from the Wikipedia article “Comp Air 12”, written by its contributors and licensed under CC BY-SA 4.0. Fathomly has changed the layout, removed citation markers, navigation and maintenance notices, and adjusted punctuation. This adapted version is shared under the same license. For references, see the original article.
Images, from Wikimedia Commons:
- Comp Air 12.jpg by Autoblindajes, CC BY-SA 4.0
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