Arado W 2

{{Infobox aircraft

|name=W 2

|image=Arado W II Le Document aéronautique December,1928.jpg

|caption=

|type=Seaplane Trainer

|manufacturer=Arado

|designer=

|first_flight=1928

|introduction=

|retired=

|status=

|primary_user=Deutsche Verkehrsfliegerschule

|more_users=

|produced=

|number_built=2

|variants=

}}

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.

Specifications

File:Arado_W_II_3-view_Le_Document_aéronautique_December,1928.png

{{Aircraft specs

|ref=Jane's all the World's Aircraft 1928{{cite book |title=Jane's all the World's Aircraft 1928 |editor1-last=Grey |editor1-first=C.G. |year=1928 |publisher=Sampson Low, Marston & company, ltd |location=London |page=129c}}

|prime units?=met

|crew=2=

|length m=12.55

|span m=17.4

|height m=3.2

|wing area sqm=53.8

|aspect ratio=

|airfoil=

|empty weight kg=1600

|gross weight kg=

|gross weight lb=

|gross weight note=

|max takeoff weight kg=2000

|fuel capacity=

|more general=

|eng1 number=2

|eng1 name=Siemens-Halske Sh.12

|eng1 type=9-cylinder air-cooled radial piston engines

|eng1 hp=110

|prop blade number=2

|prop name=fixed pitch propellers

|prop dia m=

|prop dia ft=

|prop dia in=

|prop dia note=

|max speed kmh=145

|cruise speed kmh=

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=

|stall speed kts=

|stall speed note=

|never exceed speed kmh=

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

|minimum control speed kmh=72

|range km=

|range miles=

|range nmi=

|range note=

|combat range km=

|combat range miles=

|combat range nmi=

|combat range note=

|ferry range km=

|ferry range miles=

|ferry range nmi=

|ferry range note=

|endurance=

|ceiling m=2060|g limits=

|roll rate=

|glide ratio=

|climb rate ms=1

|climb rate ftmin=

|climb rate note=

|time to altitude={{cvt|2000|m}} in 35 minutes

|wing loading kg/m2=37

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass={{cvt|0.0494|hp/lb|kW/kg|order=flip}}

|more performance=

}}

References

{{reflist}}

Further reading

  • {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=73 }}
  • World Aircraft Information Files. Brightstar Publishing, London. File 889 Sheet 73