Piper PA-61 Aerostar

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

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Piper PA-61 Aerostar Specifications

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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.

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