Arado W 2
The Arado W 2 was a two-seat twin-engine seaplane trainer developed for the DVS in 1928. It was a cantilever monoplane with a fabric-covered steel tube fuselage that accommodated the pilot and instructor in tandem open cockpits. The undercarriage consisted of two pontoons carried on steel struts.
| W 2 | |
|---|---|
![]()  | |
| Role | Seaplane Trainer | 
| Manufacturer | Arado | 
| First flight | 1928 | 
| Primary user | Deutsche Verkehrsfliegerschule | 
| Number built | 2 | 
Specifications
    

Arado W II 3-view drawing from Le Document aéronautique December,1928
Data from Jane's all the World's Aircraft 1928[1]
General characteristics
- Crew: 2=
 - Length: 12.55 m (41 ft 2 in)
 - Wingspan: 17.4 m (57 ft 1 in)
 - Height: 3.2 m (10 ft 6 in)
 - Wing area: 53.8 m2 (579 sq ft)
 - Empty weight: 1,600 kg (3,527 lb)
 - Max takeoff weight: 2,000 kg (4,409 lb)
 - Powerplant: 2 × Siemens-Halske Sh.12 9-cylinder air-cooled radial piston engines, 82 kW (110 hp) each
 - Propellers: 2-bladed fixed pitch propellers
 
Performance
- Maximum speed: 145 km/h (90 mph, 78 kn)
 - Minimum control speed: 72 km/h (45 mph, 39 kn)
 - Service ceiling: 2,060 m (6,760 ft)
 - Rate of climb: 1 m/s (200 ft/min)
 - Time to altitude: 2,000 m (6,600 ft) in 35 minutes
 - Wing loading: 37 kg/m2 (7.6 lb/sq ft)
 - Power/mass: 0.0812 kW/kg (0.0494 hp/lb)
 
References
    
| Wikimedia Commons has media related to Arado W II. | 
- Grey, C.G., ed. (1928). Jane's all the World's Aircraft 1928. London: Sampson Low, Marston & company, ltd. p. 129c.
 
Further reading
    
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 73.
 - World Aircraft Information Files. Brightstar Publishing, London. File 889 Sheet 73
 
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