Piper PA-30 Twin Comanche

Twin Turboprops

ICAO aircraft code PA30

Manufacturer Piper Aircraft

Country United States

New price USD 0.061 million (1965)

The Piper PA-30 Twin Comanche is an American twin-engined cabin monoplane designed and built by Piper Aircraft.

Specifications

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Piper PA-30 Twin Comanche Specifications

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General

ICAO aircraft code

PA30

Manufacturer

Piper Aircraft

Manufactured

1963 - 1972

Country

United States

New purchase price

USD 0.061 million (1965)

Aircraft performance

Engine:

2x Lycoming O- 320
Piston

Power:

160 HP

Max Cruise Speed:

178 Kts
330 Km/h

Approach Speed (Vref):

60 Kts

Travel range:

1,000 Nm
1,852 Kilometers

Service Ceiling:

18,600 feet

Rate of Climb:

1460 feet / minute
7.42meter / second

Take Off Distance:

470 meter - 1,541.98 feet

Landing Distance:

570 meter - 1,870.06 feet

Weight & dimensions

Max Take Off Weight:

1,690 Kg
3,726 lbs

Max Landing Weight:

1,690 Kg
3,726 lbs

Max Payload:

310 Kg
683 lbs

Fuel Tank Capacity:

120 gallon
454 liter

Disclaimer: The information on this page may not be accurate or current. Never use it for flight planning or any other aircraft operation purposes. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacture or official aviation authorities.

About the Piper PA-30 Twin Comanche

The Piper PA-30 Twin Comanche is an American twin-engined cabin monoplane designed and built by Piper Aircraft. It was a twin-engined development of the PA-24 Comanche single-engined aircraft. A variant with counter-rotating propellers was designated the Piper PA-39 Twin Comanche C/R.