Arado Ar 66

Airplanes

Length

8.3 m

Flat Wing Span

10 m

Height

2.93 m

Flat Wing Area

29.63 m²

Flat Wing Aspect Ratio

6.2

Cruise Speed

175 km/h

Max Speed

210 km/h

Max Ceiling

4500 m

Number of Engines

First Flight

1932-01-01

Entry Into service

1933-01-01

Number Built

1456

Maximum Take-Off Weight

1.33 t (paragliders: kg)

Total Fuel Capacity

172

Maximum Range

7 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Arado Ar 66	1.33	172	7

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Boeing F3B		7.57	10.06		Compare
Armstrong Whitworth Siskin		7.62	10.0584		Compare
Ambrosini S.7		8.17	8.79		Compare
Aubert Cigale	Lycoming O-320	7.5	10	3	Compare
Avro 636		8.2296	10.0584		Compare
Beechcraft Bonanza		8.2296	10.0584		Compare

All data (23 fields)

Name: Arado Ar 66
Manufacturer: Arado Flugzeugwerke
Description: The Arado Ar 66 was a single-engined twin-seat training biplane designed and produced by the German aircraft manufacturer Arado.
First Flight: 1932-01-01
Entry Into service: 1933-01-01
Designer: Walter Rethel
Type: Trainer
Length (m): 8.3
Height (m): 2.93
Max Speed (km/h): 210
Cruise Speed (km/h): 175
Max Ceiling (m): 4500
Rate of Climb (m/s): 4.33
Armament: 2 kg and 4 kg anti-personnel bombs
Endurance (h): 4.1
Number Built: 1456
Powerplant Description: 1 × Argus As 10C inverted V-8 air-cooled piston engine, 179 kW (240 hp) each
Primary Users: Luftwaffe
Wikipedia Article (URL): en.wikipedia.org/wiki/Arado_Ar_66
Flat Wing Span (m): 10
Flat Wing Area (m²): 29.63
Flat Wing Aspect Ratio: 6.2
Number of Engines: 1