Piper PA-61 Aerostar

Twin Turboprops

ICAO aircraft code PA61

Manufacturer Piper Aircraft

Country United States

New price USD 0.16 million (2020)

The Piper PA-61 Aerostar was designed by Ted R.

Specifications

Full description

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Piper PA-61 Aerostar specifications

General

ICAO aircraft code

PA61

Manufacturer

Piper Aircraft

Manufactured

1967 - 1984

Country

United States

New purchase price

USD 0.16 million (2020)

Aircraft performance

Avionics:

Dual Collins VHF-250 , Dual VIR-350 etc.

Engine:

2x Lycoming IO-540-K
Piston

Power:

290 HP

Max Cruise Speed:

240 Kts
444 Km/h

Approach Speed (Vref):

74 Kts

Travel range:

1,063 Nm
1,969 Kilometers

Service Ceiling:

25,000 feet

Rate of Climb:

1800 feet / minute
9.14meter / second

Take Off Distance:

759 meter - 2,490.13 feet

Landing Distance:

619 meter - 2,030.82 feet

Weight & dimensions

Max Take Off Weight:

2,721 Kg
5,999 lbs

Max Landing Weight:

2,721 Kg
5,999 lbs

Max Payload:

930 Kg
2,050 lbs

Fuel Tank Capacity:

177 gallon
670 liter

Baggage Volume:

0.85 m3 / 30 ft3

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-61 Aerostar

The Piper PA-61 Aerostar was designed by Ted R. Smith as a twin-engined propeller-driven aircraft produced from 1967 to 1984. The light transport aircraft was initially built by Ted Smith Aerostar Company before it became Piper Aircraft Corporation. A total of 1,010 aircraft were produced.