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<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->{{Inline|date=January 2024}}
__NOTOC__
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<!-- 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=F.500 Monitor
|name=F.500 Monitor
|image=Stampe SR.7B Coventry 1956.jpg
|image= File:Stampe SR.7B Coventry 1956.jpg
|caption=Stampe & Renard SR.7B Monitor IV OO-SRZ at Coventry Airport, England in July 1956
|caption=Stampe & Renard SR.7B Monitor IV OO-SRZ at Coventry Airport, England in July 1956
}}{{Infobox Aircraft Type
}}{{Infobox Aircraft Type
Line 26: Line 25:
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 {{convert|140|hp|abbr=on|adj=on}} 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|Stampe et Renard]] under the designation '''SR.7B Monitor IV'''.
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 {{convert|140|hp|abbr=on|adj=on}} 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|Stampe et Renard]] under the designation '''SR.7B Monitor IV'''.
<!-- ==Operational history== -->
<!-- ==Operational history== -->

==Variants==
==Variants==
;F.500 Monitor I
;F.500 Monitor I
:Prototype with a {{convert|140|hp|kW|abbr=on|disp=flip}} [[Renault 4Pei]] or [[Renault 4Po-05]] engine, of wooden construction, one built, first flown on 11 July 1952.
:Prototype with a {{convert|140|hp|kW|abbr=on|order=flip}} [[Renault 4Pei]] or [[Renault 4Po-05]] engine, of wooden construction, one built, first flown on 11 July 1952.
;F.510 Monitor II
;F.510 Monitor II
:French production aircraft with a {{convert|260|hp|kW|abbr=on|disp=flip}} [[Salmson 8As-04]] engine, metal construction, one built, first floen on 5 August 1955.
:French production aircraft with a {{convert|260|hp|kW|abbr=on|order=flip}} [[Salmson 8As-04]] engine, metal construction, one built, first flown on 5 August 1955.
;F.520 Monitor III
;F.520 Monitor III
:Prototype Monitor I re-engined with a {{convert|170|hp|kW|abbr=on|disp=flip}} [[Régnier 4L-02]] engine, first flown on 15 June 1953.
:Prototype Monitor I re-engined with a {{convert|170|hp|kW|abbr=on|order=flip}} [[Régnier 4L]]-02 engine, first flown on 15 June 1953.
;F.521 Monitor III
;F.521 Monitor III
:with a {{convert|170|hp|kW|abbr=on|disp=flip}} [[Régnier 4L-22]] engine, one built.
:with a {{convert|170|hp|kW|abbr=on|order=flip}} [[Régnier 4L]]-22 engine, one built.
;SR.7B Monitor IV
;SR.7B Monitor IV
:Belgian production aircraft.
:Belgian production aircraft.


==Specifications (Monitor II) ==
==Specifications (Monitor II) ==
{{Aircraft specs
{{Aerospecs
|ref=The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1759
|ref=The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1759
|prime units? = met
|met or eng?=<!-- eng for US/UK aircraft, met for all others -->met
|crew=Two
|crew=Two
|capacity=
|length m=7.28
|length m=7.28
|length ft=23
|length ft=23
|length in=10½
|length in=10.5
|span m=9.44
|span m=9.44
|span ft=30
|span ft=30
|span in=11½
|span in=11.5
|swept m=<!-- swing-wings -->
|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=2.20
|height m=2.20
|height ft=7
|height ft=7
|height in=2½
|height in=2.5
|wing area sqm=14
|wing area sqm=14
|wing area sqft=150.70
|wing area sqft=150.70
|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 -->
|empty weight kg=
|empty weight lb=
|gross weight kg=802
|gross weight kg=802
|gross weight lb=1768
|gross weight lb=1768
|lift kg=<!-- lighter-than-air -->
|lift lb=<!-- lighter-than-air -->
|eng1 number=1
|eng1 number=1
|eng1 type=[[Salmson 8AS-04]] 8-cylinder inverted Vee piston engine
|eng1 name=[[Salmson 8As-04]] 8-cylinder inverted Vee piston engine
|eng1 kw=<!-- prop engines -->164
|eng1 kw=<!-- prop engines -->164
|eng1 hp=<!-- prop engines -->220
|eng1 hp=<!-- prop engines -->220
|eng1 kn=<!-- jet/rocket engines -->
|eng1 lbf=<!-- jet/rocket engines -->
|eng1 kn-ab=<!-- afterburners -->
|eng1 lbf-ab=<!-- afterburners -->
|eng2 number=
|eng2 type=
|eng2 kw=<!-- prop engines -->
|eng2 hp=<!-- prop engines -->
|eng2 kn=<!-- jet/rocket engines -->
|eng2 lbf=<!-- jet/rocket engines -->
|eng2 kn-ab=<!-- afterburners -->
|eng2 lbf-ab=<!-- afterburners -->
|max speed kmh=270
|max speed kmh=270
|max speed mph=168
|max speed mph=168
|endurance=3 hours 0 minutes
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=<!-- if max speed unknown -->
|cruise speed mph=<!-- if max speed unknown -->
|range km=
|range miles=
|endurance h=<!-- if range unknown -->3
|endurance min=<!-- if range unknown -->0
|ceiling m=
|ceiling ft=
|glide ratio=<!-- sailplanes -->
|climb rate ms=
|climb rate ftmin=
|sink rate ms=<!-- sailplanes -->
|sink rate ftmin=<!-- sailplanes -->
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}
}}


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|lists=<!-- related lists -->
|lists=<!-- related lists -->
|see also=<!-- other relevant information -->
|see also=<!-- other relevant information -->

}}
}}


== Notes ==
==References==
⚫
{{commons category|Stampe & Renard SR-7B}}
<references />
{{Reflist}}


==References==
==Bibliography==
* The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985), 1985, Orbis Publishing, Page 1759
* The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985), 1985, Orbis Publishing, Page 1759
*{{cite book |title= Les avions Farman |last= Liron |first= J.L. |year= 1984|publisher= Éditions Larivère|location=Paris|isbn=|pages=230–1}}
*{{cite book |last1=Liron |first1=Jean |title=Les avions Farman |year=1984 |publisher=Éditions Larivière |location=Paris |oclc=37146471|series=Collection Docavia|volume=21}}

==External links==
⚫
{{commonscat|Stampe & Renard SR-7B}}


{{Farman aircraft}}
{{Farman aircraft}}
{{Aviation lists}}


[[Category:Farman aircraft|F.0500]]
[[Category:Farman aircraft|F.0500]]
[[Category:French civil trainer aircraft 1950–1959]]
[[Category:1950s French civil trainer aircraft]]
[[Category:Low-wing aircraft]]
[[Category:Single-engined tractor aircraft]]
[[Category:Aircraft first flown in 1952]]

Latest revision as of 15:59, 25 January 2024

F.500 Monitor
Stampe & Renard SR.7B Monitor IV OO-SRZ at Coventry Airport, England in July 1956
Role Two-seat trainer
Manufacturer Societe Anonye des Usines Farman
Stampe et Renard
First flight 11 July 1952

The Farman F.500 Monitor was a 1950s Franco-Belgian two-seat training aircraft.

Development

[edit]

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 140 hp (100 kW) 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

[edit]
F.500 Monitor I
Prototype with a 100 kW (140 hp) Renault 4Pei or Renault 4Po-05 engine, of wooden construction, one built, first flown on 11 July 1952.
F.510 Monitor II
French production aircraft with a 190 kW (260 hp) Salmson 8As-04 engine, metal construction, one built, first flown on 5 August 1955.
F.520 Monitor III
Prototype Monitor I re-engined with a 130 kW (170 hp) Régnier 4L-02 engine, first flown on 15 June 1953.
F.521 Monitor III
with a 130 kW (170 hp) Régnier 4L-22 engine, one built.
SR.7B Monitor IV
Belgian production aircraft.

Specifications (Monitor II)

[edit]

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

General characteristics

  • Crew: Two
  • Length: 7.28 m (23 ft 10.5 in)
  • Wingspan: 9.44 m (30 ft 11.5 in)
  • Height: 2.20 m (7 ft 2.5 in)
  • Wing area: 14 m2 (150.70 sq ft)
  • Gross weight: 802 kg (1,768 lb)
  • Powerplant: 1 × Salmson 8As-04 8-cylinder inverted Vee piston engine , 164 kW (220 hp)

Performance

  • Maximum speed: 270 km/h (168 mph, 146 kn)
  • Endurance: 3 hours 0 minutes

See also

[edit]

Aircraft of comparable role, configuration, and era

References

[edit]
Wikimedia Commons has media related to Stampe & Renard SR-7B.

Bibliography

[edit]
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985), 1985, Orbis Publishing, Page 1759
  • Liron, Jean (1984). Les avions Farman. Collection Docavia. Vol. 21. Paris: Éditions Larivière. OCLC 37146471.
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