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Piper PA-30 Twin Comanche

 

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



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