Piper PA-30 Twin Comanche

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.

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