- Farman F.500
__NOTOC__ Infobox Aircraft
name=F.500 Monitor
caption=
type=Two-seat trainer
manufacturer=Societe Anonye des Usines Farman
Stampe et Renard
designer=
first flight=1952
introduced=
retired=
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variants with their own articles=The Farman F.500 Monitor was a 1950s Franco-Belgian two-seat training aircraft.
Development
Farman had earlier produced the
Stampe SV.4 under licence, and with the co-operation ofStampe designed a two-seat training monoplane using SV-4 components designated the Farman F.500. The prototype, named the Monitor I, first flew on11 July 1952 , it was a cantilever low-wing monoplane of mixed construction and conventional tail unit. It had a fixed tailwheel landing gear and room for two crew in tandem under a continuous canopy and was powered by a 140hp (104kW) Renault 4Pei engine. The production version designated the Monitor II was placed into production and first flew on5 August 1955 , it had all-metal wings and a Salmson-Argus engine. Production also took place in Belgium with Stampe et Renard under the designation SR.7B Monitor IV.Variants
;F.500 Monitor I:Protoype with a 140hp (104kW) Renault 4Pei engine, one built.;F.500 Monitor II:French production aircraft with a Salmson-Argus engine.;F.500 Monitor III:Prototype Monitor I re-engined with a Regnier 4 engine.;SR.7B Monitor IV:Belgian production aircraft.
pecifications (Monitor II)
aerospecs
ref=The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1759
met or eng?= metcrew=Two
capacity=
length m=7.28
length ft=23
length in=10½
span m=9.44
span ft=30
span in=11½
swept m=
swept ft=
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dia m=
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width m=
width ft=
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height m=2.20
height ft=7
height in=2½
wing area sqm=14
wing area sqft=150.70
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=802
gross weight lb=1768
lift kg=
lift lb=eng1 number=1
eng1 type=Salmson-Argus 8-cylinder inverted Vee piston engine
eng1 kw= 164
eng1 hp= 220
eng1 kn=
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eng2 number=
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eng2 lbf-ab=max speed kmh=270
max speed mph=168
max speed mach=
cruise speed kmh=
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range km=
range miles=
endurance h= 3
endurance min= 0
ceiling m=
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sink rate ftmin=armament1=
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armament6=References
* The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1759
ee also
aircontent
related=
similar aircraft=
*de Havilland Canada DHC-1 Chipmunk
sequence=lists=
see also=
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