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词条 Boeing Model 204
释义

  1. Variants

  2. Specifications (204)

  3. References

name=Model 204 image=Boeing model 204 Aero Digest February,1930.jpg caption=

}}{{Infobox Aircraft Type

type=passenger flying-boat national origin=United States manufacturer=Boeing designer= first flight= introduced=1929 retired= status= primary user= number built=7 developed from=Boeing Model 6E variants with their own articles=
}}

The Boeing Model 204 was an American biplane, pusher configuration flying-boat aircraft built by Boeing in 1929. Externally the 204 looked identical to the Boeing Model 6E, but a number of internal changes, including increasing the passenger capacity to four, gave it a new Type Certificate and model number.[1]

Construction was started on five aircraft, but only two were completed.[1] The first, designated 204 and the second 204A. A third aircraft was built by a private owner who had bought the three incomplete machines. The 204A was a dual-control version which was later owned by Peter Barnes, who flew it on his private Seattle-Victoria, British Columbia main run.[2]

The C-204 Thunderbird, a modified 204, was the first type produced by Boeing Aircraft of Canada. These had altered wing and tailplane incidence and a reduction in upper wing area. The prototype was first flown on 30 March 1930, the first of a batch of four. They failed to sell readily, though they were sometimes leased for work. Eventually three were sold. All worked in British Columbia, remaining active until 1939.[3]

Variants

204

Four-seat variant of the Model 6E, one built.

204A

As the Model 204 with dual-control, one built.

C-204 Thunderbird

4 204s built by Boeing-Canada.[3][4]

Specifications (204)

{{aerospecs
|ref=Bowers, 1966, pg. 138
|met or eng?=eng
|crew=one pilot
|capacity=four passengers
|length m=9.93
|length ft=32
|length in=7
|span m=12.10
|span ft=39
|span in=8.25
|height m=3.66
|height ft=12
|height in=
|wing area sqm=43.66
|wing area sqft=470
|empty weight kg=1,496
|empty weight lb=3,298
|gross weight kg=2,240
|gross weight lb=4,940
|eng1 number=1
|eng1 type=Pratt & Whitney R-1340 Wasp
|eng1 kw=305
|eng1 hp=410
|eng2 number=
|eng2 type=
|eng2 kw=
|eng2 hp=
|max speed kmh=185
|max speed mph=115
|cruise speed kmh=153
|cruise speed mph=95
|stall speed kmh=
|stall speed mph=
|range km=563
|range miles=350
|endurance h=
|endurance min=
|ceiling m=2,743
|ceiling ft=9,000
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=5.1
|climb rate ftmin=1,000
|sink rate ms=
|sink rate ftmin=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

{{commons category|Boeing aircraft}}
Notes
1. ^Bowers, 1966, pg. 137
2. ^Bowers, 1966, pg. 138
3. ^Molson and Taylor pp.113-4
4. ^Bowers, 1966, pg. 139
Bibliography
{{refbegin}}
  • Bowers, Peter M. Boeing aircraft since 1916. London: Putnam Aeronautical Books, 1966.
  • {{cite book |title= Canadian Aircraft since 1909|last=Molson|first=K.M.|last2= Taylor|first2=H.A. |year=1982 |publisher=Putnam Publishing|location=London |isbn= 0-370-30095-5}}
{{refend}}{{Boeing model numbers}}

6 : United States aircraft 1920–1929|Boeing aircraft|Flying boats|Single-engined pusher aircraft|Biplanes|Aircraft first flown in 1929

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