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__NOTOC__
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{|{{Infobox Aircraft Begin
{|{{Infobox Aircraft Begin
|name=C.VII-W
|name=C.VII-W
|image=Fokker C.VII.jpg
|image=File:Fokker C.VIIW bij De Mok 2161 027198.jpg
|caption=
|caption=Fokker C.VII-W
}}{{Infobox Aircraft Type
}}{{Infobox Aircraft Type
|type=Reconnaissance aircraft
|type=Reconnaissance aircraft
|manufacturer=[[Fokker]]
|manufacturer=[[Fokker]]
|designer=
|designer=
|first flight={{avyear|1928}}
|first flight=1928
|introduced=
|introduced=
|retired=
|retired=
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|}
|}


The '''Fokker C.VII-W''' was a reconnaissance seaplane built in the Netherlands in the late 1920s. Sharing elements of the highly successful [[Fokker C.V|C.V]] design, the C.VII-W was a conventional, single-bay biplane with wings of unequal span braced with N-struts. The undercarriage consisted of a standard twin-pontoon arrangement, and the fin and rudder continued through to the ventral side of the fuselage, creating a cruciform tail. The pilot and observer sat in tandem, open cockpits. The wing structure was wooden with fabric and plywood covering, and the fuselage was of steel tube construction with fabric covering.
The '''Fokker C.VII-W''' was a reconnaissance seaplane built in the Netherlands in the late 1920s. Sharing elements of the highly successful [[Fokker C.V|C.V]] design, the C.VII-W was a conventional, [[single-bay]] biplane with wings of unequal span braced with N-struts. The undercarriage consisted of a standard twin-pontoon arrangement, and the fin and rudder continued through to the ventral side of the fuselage, creating a cruciform tail. The pilot and observer sat in tandem, open cockpits. The wing structure was wooden with fabric and plywood covering, and the fuselage was of steel tube construction with fabric covering.


The first twelve of the thirty examples produced were sent to the Dutch East Indies, with the rest remaining in the Netherlands. The type was withdrawn from front-line service in 1940, but some machines remained active in the East Indies as trainers until the Japanese invasion in 1942.
The first twelve of the thirty examples produced were sent to the Dutch East Indies, with the rest remaining in the Netherlands. The type was withdrawn from front-line service in 1940, but some machines remained active in the East Indies as trainers until the Japanese invasion in 1942.
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*[[Royal Netherlands Navy]]
*[[Royal Netherlands Navy]]
<!-- ==Units using this aircraft/Operators (choose)== -->
<!-- ==Units using this aircraft/Operators (choose)== -->

==Specifications==
==Specifications (C.VII-W)==
{{aerospecs
[[File:Fokker_C_VII_W_3-View_L'Air_April_15,1929.png|thumb|Fokker C VII W 3-View drawing from L'Air April 15,1929]]
|ref=
{{Aircraft specs
|met or eng?=<!-- eng for US/UK aircraft, met for all others. You MUST include one or the other here, or no specifications will show -->met
|ref=Jane's all the World's Aircraft 1928<ref name=JAWA1928>{{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 |pages=151c}}</ref>
|crew=Two, pilot and observer
|prime units?=met
|capacity=
<!--
|length m=9.50
General characteristics
|length ft=31
-->
|length in=2
|crew=2
|span m=12.90
|length m=9.98
|span ft=42
|span in=4
|span m=12.9
|height m=4
|swept m=<!-- swing-wings -->
|wing area sqm=37
|swept ft=<!-- swing-wings -->
|swept in=<!-- swing-wings -->
|rot number=<!-- helicopters -->
|rot dia m=<!-- helicopters -->
|rot dia ft=<!-- helicopters -->
|rot dia in=<!-- helicopters -->
|dia m=<!-- airships etc -->
|dia ft=<!-- airships etc -->
|dia in=<!-- airships etc -->
|width m=<!-- if applicable -->
|width ft=<!-- if applicable -->
|width in=<!-- if applicable -->
|height m=4.00
|height ft=13
|height in=2
|wing area sqm=37.0
|wing area sqft=398.3
|swept area sqm=<!-- swing-wings -->
|swept area sqft=<!-- swing-wings -->
|rot area sqm=<!-- helicopters -->
|rot area sqft=<!-- helicopters -->
|volume m3=<!-- lighter-than-air -->
|volume ft3=<!-- lighter-than-air -->
|aspect ratio=<!-- sailplanes -->
|aspect ratio=<!-- sailplanes -->
|airfoil=
|empty weight kg=1,200
|empty weight lb=2,650
|empty weight kg=1102
|empty weight note=training mission; {{cvt|1120|kg}} reconnaissance mission
|gross weight kg=1,700
|gross weight lb=3,750
|gross weight kg=1415
|gross weight note=training mission; {{cvt|1620|kg}} reconnaissance mission
|lift kg=<!-- lighter-than-air -->
|max takeoff weight kg=
|lift lb=<!-- lighter-than-air -->
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{cvt|330|L|USgal impgal}} fuel; {{cvt|30|L|USgal impgal}} oil
|more general=
<!--
Powerplant
-->
|eng1 number=1
|eng1 number=1
|eng1 type=[[Armstrong Siddeley Lynx]]
|eng1 name=[[Armstrong Siddeley Lynx]]
|eng1 kw=<!-- prop engines -->168
|eng1 type=7-cylinder air-cooled radial piston engine
|eng1 hp=<!-- prop engines -->225
|eng1 hp=225

|eng1 kn=<!-- jet/rocket engines -->
|prop blade number=2
|eng1 lbf=<!-- jet/rocket engines -->
|prop name=fixed pitch propeller
|eng1 kn-ab=<!-- afterburners -->
|eng1 lbf-ab=<!-- afterburners -->
|prop dia m=<!-- propeller aircraft -->
|prop dia ft=<!-- propeller aircraft -->
|eng2 number=
|prop dia in=<!-- propeller aircraft -->
|eng2 type=
|eng2 kw=<!-- prop engines -->
|prop dia note=
<!--
|eng2 hp=<!-- prop engines -->
Performance
|eng2 kn=<!-- jet/rocket engines -->
-->
|eng2 lbf=<!-- jet/rocket engines -->
|eng2 kn-ab=<!-- afterburners -->
|eng2 lbf-ab=<!-- afterburners -->
|max speed kmh=160
|max speed kmh=160
|max speed mph=100
|cruise speed kmh=130
|max speed mach=<!-- supersonic aircraft -->
|cruise speed note=<br>
*'''Landing speed:''' {{cvt|70|km/h|mph kn}}
|cruise speed kmh=<!-- if max speed unknown -->
|stall speed kmh=
|cruise speed mph=<!-- if max speed unknown -->
|stall speed mph=
|range km=1,000
|stall speed kts=
|range miles=621
|stall speed note=
|endurance h=<!-- if range unknown -->
|never exceed speed kmh=
|endurance min=<!-- if range unknown -->
|never exceed speed mph=
|ceiling m=2,400
|never exceed speed kts=
|ceiling ft=7,880
|never exceed speed note=
|glide ratio=<!-- sailplanes -->
|range km=
|climb rate ms=1.2
|range miles=
|climb rate ftmin=240
|range nmi=
|sink rate ms=<!-- sailplanes -->
|range note=
|sink rate ftmin=<!-- sailplanes -->
|combat range km=
|armament1=
|combat range miles=
|armament2=
|combat range nmi=
|armament3=
|combat range note=
|armament4=
|ferry range km=
|armament5=
|ferry range miles=
|armament6=
|ferry range nmi=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling m=3600
|ceiling note=training mission; {{cvt|3200|m}} reconnaissance mission
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude={{cvt|1000|m}} in 6.8 minutes (training) / 9 minutes (reconnaissance); {{cvt|2000|m}} in 15.8 minutes (training) / 21 minutes (reconnaissance);
|wing loading kg/m2=38.2
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|more performance=
<!--
Armament
-->
|guns= reconnaissance mission - provision for a machine gun on a [[Scarff ring]] in the rear cockpit
|bombs= reconnaissance mission - provision for light bomb racks under the observers cockpit
}}
}}


<!-- ==See also== -->
{{aircontent
<!-- include as many lines are appropriate. additional lines/entries with carriage return. -->
|see also=
|related=<!-- related developments -->
|similar aircraft=<!-- similar or comparable aircraft -->
|lists=<!-- related lists -->
}}
==References==
==References==
{{commonscat|Fokker C.VII}}
{{commons category|Fokker C.VII}}
{{reflist}}

==Bibliography==
*{{cite journal |last1=Ledet|first1=Michel|title=Le Fokker C-VII W (première partie)|journal=Avions: Toute l'aéronautique et son histoire |date=January 1997 |issue=46 |pages=15–17 |trans-title=|language=French |issn=1243-8650}}
*{{cite journal |last1=Ledet|first1=Michel|title=Le Fokker C-VII W (deuxième et dernière partie)|journal=Avions: Toute l'aéronautique et son histoire |date=February 1997 |issue=47 |pages=34–42 |trans-title=|language=French |issn=1243-8650}}
* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=404 }}
* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=404 }}
* {{cite book |title=World Aircraft Information Files |publisher=Bright Star Publishing|location=London |pages=File 894 Sheet 34 }}
* {{cite book |title=World Aircraft Information Files |publisher=Bright Star Publishing|location=London |pages=File 894 Sheet 34 }}
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{{Fokker aircraft}}
{{Fokker aircraft}}
{{aviation lists}}


[[Category:Dutch military reconnaissance aircraft 1920–1929]]
[[Category:1920s Dutch military reconnaissance aircraft]]
[[Category:Floatplanes]]
[[Category:Floatplanes]]
[[Category:Fokker aircraft|C 07]]
[[Category:Fokker aircraft|C 07]]
[[Category:Single-engined tractor aircraft]]
[[Category:Single-engined tractor aircraft]]
[[Category:Biplanes]]
[[Category:Biplanes]]
[[Category:Aircraft first flown in 1928]]

Latest revision as of 00:54, 16 April 2023

C.VII-W
Fokker C.VII-W
Role Reconnaissance aircraft
Manufacturer Fokker
First flight 1928
Primary user Royal Netherlands Navy
Number built 30

The Fokker C.VII-W was a reconnaissance seaplane built in the Netherlands in the late 1920s. Sharing elements of the highly successful C.V design, the C.VII-W was a conventional, single-bay biplane with wings of unequal span braced with N-struts. The undercarriage consisted of a standard twin-pontoon arrangement, and the fin and rudder continued through to the ventral side of the fuselage, creating a cruciform tail. The pilot and observer sat in tandem, open cockpits. The wing structure was wooden with fabric and plywood covering, and the fuselage was of steel tube construction with fabric covering.

The first twelve of the thirty examples produced were sent to the Dutch East Indies, with the rest remaining in the Netherlands. The type was withdrawn from front-line service in 1940, but some machines remained active in the East Indies as trainers until the Japanese invasion in 1942.

Operators

[edit]
 Netherlands

Specifications (C.VII-W)

[edit]
Fokker C VII W 3-View drawing from L'Air April 15,1929

Data from Jane's all the World's Aircraft 1928[1]

General characteristics

  • Crew: 2
  • Length: 9.98 m (32 ft 9 in)
  • Wingspan: 12.9 m (42 ft 4 in)
  • Height: 4 m (13 ft 1 in)
  • Wing area: 37 m2 (400 sq ft)
  • Empty weight: 1,102 kg (2,429 lb) training mission; 1,120 kg (2,470 lb) reconnaissance mission
  • Gross weight: 1,415 kg (3,120 lb) training mission; 1,620 kg (3,570 lb) reconnaissance mission
  • Fuel capacity: 330 L (87 US gal; 73 imp gal) fuel; 30 L (7.9 US gal; 6.6 imp gal) oil
  • Powerplant: 1 × Armstrong Siddeley Lynx 7-cylinder air-cooled radial piston engine, 168 kW (225 hp)
  • Propellers: 2-bladed fixed pitch propeller

Performance

  • Maximum speed: 160 km/h (99 mph, 86 kn)
  • Cruise speed: 130 km/h (81 mph, 70 kn)
  • Landing speed: 70 km/h (43 mph; 38 kn)
  • Service ceiling: 3,600 m (11,800 ft) training mission; 3,200 m (10,500 ft) reconnaissance mission
  • Time to altitude: 1,000 m (3,300 ft) in 6.8 minutes (training) / 9 minutes (reconnaissance); 2,000 m (6,600 ft) in 15.8 minutes (training) / 21 minutes (reconnaissance);
  • Wing loading: 38.2 kg/m2 (7.8 lb/sq ft)

Armament

  • Guns: reconnaissance mission - provision for a machine gun on a Scarff ring in the rear cockpit
  • Bombs: reconnaissance mission - provision for light bomb racks under the observers cockpit

References

[edit]
Wikimedia Commons has media related to Fokker C.VII.
  1. ^ Grey, C.G., ed. (1928). Jane's all the World's Aircraft 1928. London: Sampson Low, Marston & company, ltd. pp. 151c.

Bibliography

[edit]
  • Ledet, Michel (January 1997). "Le Fokker C-VII W (première partie)". Avions: Toute l'aéronautique et son histoire (in French) (46): 15–17. ISSN 1243-8650.
  • Ledet, Michel (February 1997). "Le Fokker C-VII W (deuxième et dernière partie)". Avions: Toute l'aéronautique et son histoire (in French) (47): 34–42. ISSN 1243-8650.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 404.
  • World Aircraft Information Files. London: Bright Star Publishing. pp. File 894 Sheet 34.
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