Beechcraft Baron

Length
8.5344 m
Flat Wing Span
11.2776 m
Height
2.7432 m
Flat Wing Area
18.5063 m²
Max Seating
6
Cruise Speed
333.3597 km/h
Max Speed
379.6597 km/h
Max Ceiling
6004.56 m
Number of Engines
2
Aircraft Engine
First Flight
1960-02-29
Number Built
7011
Maximum Take-Off Weight
2.3133 t (paragliders: kg)
Total Fuel Capacity
378.5412
Maximum Range
1744.584 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Total Fuel Capacity Maximum Range (km)
Beechcraft Baron 2.3133 378.5412 1744.584

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Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
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Piper PA-34 Seneca 8.72 11.86 Compare
Gulfstream American GA-7 Cougar Lycoming O-320 8.5344 10.9728 Compare
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All data (28 fields)
Name
Beechcraft Baron
Manufacturer
Beechcraft
Description
The Beechcraft Baron is a light twin-engined piston aircraft designed and produced by Beechcraft.
ICAO Code
BE58
First Flight
1960-02-29
Designer
Beechcraft
Type
Civil utility aircraft
Length (m)
8.5344
Height (m)
2.7432
Cockpit Crew
1
Max Seating
6
Max Speed (km/h)
379.6597
Cruise Speed (km/h)
333.3597
Min Speed (km/h)
135.1959
Max Ceiling (m)
6004.56
Rate of Climb (m/s)
8.4836
Capacity Description
6 passengers
National Origin
United States of America
Number Built
7011
Powerplant Description
2 × Continental IO-470-L air-cooled six-cylinder horizontally opposed engines, 194 kW (260 hp) each
Primary Users
United States Army (historical)
Status
In production
Wikipedia Article (URL)
en.wikipedia.org/wiki/Beechcraft_Baron
Flat Wing Span (m)
11.2776
Flat Wing Area (m²)
18.5063
Wake Category
L
Aircraft Engine
Continental O-470
Number of Engines
2