Beagle B.206

Airplanes

Length

10.0584 m

Flat Wing Span

13.716 m

Height

3.3528 m

Max Seating

Cruise Speed

350.837 km/h

Max Speed

415.2108 km/h

Max Ceiling

8260.08 m

Number of Engines

Aircraft Engine

First Flight

1961-08-15

Entry Into service

1965-01-01

Number Built

Maximum Take-Off Weight

3.4015 t (paragliders: kg)

Maximum Range

1620 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Beagle B.206	3.4015	1620

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Beechcraft L-23 Seminole	Lycoming O-480	9.4488	13.716	6	Compare
SIPA S.70	Mathis G.8R	10.2	13.8	8	Compare
Fouga CM.170 Magister	Turbomeca Marboré	10.06	12.15		Compare
Fouga CM.175 Zéphyr	Turbomeca Marboré	10.06	12.15		Compare
Cessna 425	Pratt & Whitney Canada PT6	10.668	13.4112		Compare
Saro Cutty Sark	Armstrong Siddeley Genet Major	10.3632	13.716		Compare

All data (27 fields)

Name: Beagle B.206
Manufacturer: Beagle Aircraft
Description: The Beagle B.206 is a 1960s British seven-seat twin-piston engined liaison and communication aircraft built by Beagle Aircraft Limited at Shoreham Airport and Rearsby Aerodrome.
ICAO Code: BASS
First Flight: 1961-08-15
Entry Into service: 1965-01-01
Production End: 1969-01-01
Designer: Beagle Aircraft
Type: Light transport
Length (m): 10.0584
Height (m): 3.3528
Cockpit Crew: 1
Max Seating: 6
Max Speed (km/h): 415.2108
Cruise Speed (km/h): 350.837
Max Ceiling (m): 8260.08
Rate of Climb (m/s): 6.8072
Capacity Description: 6 passengers
National Origin: United Kingdom
Number Built: 79
Powerplant Description: 2 × Rolls-Royce Continental GTSIO-520-C air-cooled flat-six engines, 254 kW (340 hp) each
Primary Users: Royal Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Beagle_B.206
Flat Wing Span (m): 13.716
Wake Category: L
Aircraft Engine: Continental IO-520
Number of Engines: 2