Samiksha Jaiswal (Editor)

Comp Air 12

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Length
  
13 m

Manufacturer
  
Comp Air

Comp Air 12 aviaprositesdefaultfilesstylesnewsphotopub

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.

Specifications (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 (345 mph; 556 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

    References

    Comp Air 12 Wikipedia
    (Text) CC BY-SA