Piper PA-61 Aerostar [+]Compare [E]dit [H]istory

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Object «Piper PA-61 Aerostar» has attributes

Attribute Value
General
Manufacturer Piper Aircraft
Model Piper PA-61 Aerostar
Country United States
Manufactured from 1967 year
Manufactured to 1984 year
Type Twin Turboprops
Icao PA61
Performance
Engine 2x Lycoming IO-540-K
Power, hp 290 hp
Power, lbf Add
Avionics Dual Collins VHF-250 , Dual VIR-350 etc.
Max cruise speed 444 km/h
Approach speed 137 km/h
Travel range 1,969 km
Fuel economy Add
Service ceiling 7,620 m
Rate of climb 9.14 m/sec
Take off distance 759 m
Landing distance 619 m
Weights
Max take off weight 2,721 kg
Max landing weight 2,721 kg
Max payload 930 kg
Fuel tank capacity 670 l
Baggage volume 0.85 m³
Dimensions
Seats 6
Seats - business class Add
Seats - first class Add
Cabin height 1.22 m
Cabin width 1.25 m
Cabin length 3.8 m
Exterior length 10.61 m
Tail height 3.7 m
Fuselage diameter 1.35 m
Wing span 11.18 m
Wing tips No Winglets

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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 26, 2021 (46 fields were changed)
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