Piper PA-30 Twin Comanche
The Piper PA-30 and PA-39 Twin Comanche was a twin-engine development of the PA-24 Comanche single-engine aircraft produced by Piper. As with the Comanche, a number of engine options were available, the base 180-hp version typically being used as a twin-engine trainer, with the 260-hp version being used for personal transport. A version with turbocharged engines for higher altitude flight was also developed, and the PA-39 was a version with counter-rotating engines (to ease engine-out operations). As the Twin Comanche was produced on the same production line as its single-engine cousin, production ceased when the production line was wiped out in a flood in the early 1960s, and Piper chose instead to focus on its equally popular 140/180 and Cherokee line, eventually giving birth to the twin-engine, highly popular Seneca.
Specifications (PA-30-160 Twin Comanche)General Characteristics Crew: one, pilot Capacity: 3 passengers Length: 25 ft 2 in (7.67 m) Wingspan: 36 ft 0 in (10.97 m) Height: 8 ft 2 in (2.49 m) Wing area: 178 ft² (16.5 m²) Empty: 2,210 lb (1,002 kg) Loaded: lb ( kg) Maximum takeoff: 3,600 lb (1,633 kg) Powerplant: 2x Lycoming IO-320-B1A, 160 hp (120 kW) each
Performance Maximum speed: 206 mph (330 km/h) Range: 1,122 miles (1,795 km) Service ceiling: 25,000 ft (7,622 m) Rate of climb: 1,460 ft/min (445 m/min) Wing loading: lb/ft² ( kg/m²) Power/Mass: hp/lb ( kW/kg)
Related content
Related development:
Piper PA-24 Comanche Comparable aircraft: Designation sequence: PA-25 - PA-28 - PA-29 - PA-30 - PA-31 - PA-32 - PA-33 PA-35 - PA-36 - PA-38 - PA-39 - PA-40 - PA-42 - PA-44
|
|