Farman F.500

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=
status=
primary user=
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produced=
number built=
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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 of Stampe designed a two-seat training monoplane using SV-4 components designated the Farman F.500. The prototype, named the Monitor I, first flew on 11 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 on 5 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?= met

crew=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=
swept in=
rot number=
rot dia m=
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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=
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rot area sqft=
volume m3=
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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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max speed kmh=270
max speed mph=168
max speed mach=
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range km=
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endurance h= 3
endurance min= 0
ceiling m=
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armament1=
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References

* The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1759

ee also

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* de Havilland Canada DHC-1 Chipmunk
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