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{{Underlinked|date=February 2019}}
{{Underlinked|date=February 2019}}

__NOTOC__
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{|{{Infobox aircraft begin
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}}{{Infobox aircraft type
}}{{Infobox aircraft type
| type=Trainer
| type=Trainer
| national origin=France
| national origin=[[France]]
| manufacturer=[[Morane-Saulnier]]
| manufacturer=[[Morane-Saulnier]]
| designer=
| designer=
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The '''Morane-Saulnier AS''' was a trainer aircraft built in France after the First World War. It was a high-wing monoplane.
The '''Morane-Saulnier AS''' was a high-wing monoplane single-seat [[touring aircraft]] built in [[France]] after [[WWI]].
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==Specifications==
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{{aerospecs
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|ref=<ref>{{cite web|url=https://www.aviafrance.com/morane-saulnier-as-aviation-france-10154.htm |title=Morane-Saulnier AS - avion de tourisme - Un siècle d'aviation française |publisher=Aviafrance.com |date=2007-11-25 |accessdate=2019-02-06}}</ref>
<!-- ==Units using this aircraft/Operators (choose)== -->
|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
==Specifications (variant specified) ==

{{Aircraft specs
|crew=One
|ref=<ref name=avfrmsas>{{cite web|url=https://www.aviafrance.com/morane-saulnier-as-aviation-france-10154.htm |title=Morane-Saulnier AS - avion de tourisme - Un siècle d'aviation française |publisher=Aviafrance.com |date=2007-11-25 |accessdate=2019-02-06}}</ref>
|capacity=
|prime units?=met
<!--
General characteristics
-->
|crew=
|length m=5.64
|length m=5.64
|length ft=
|span m=8.8
|length in=
|span m=8.80
|span ft=
|span in=
|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=3.15
|height m=3.15
|wing area sqm=13
|height ft=
|height in=
|wing area sqm=13.00
|wing area sqft=
|swept area sqm=<!-- swing-wings -->
|swept area sqft=<!-- swing-wings -->
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|rot area sqft=<!-- helicopters -->
|volume m3=<!-- lighter-than-air -->
|volume ft3=<!-- lighter-than-air -->
|aspect ratio=<!-- sailplanes -->
|aspect ratio=<!-- sailplanes -->
|airfoil=
|wing profile=<!-- sailplanes -->
|empty weight kg=
|empty weight kg=
|empty weight lb=
|gross weight kg=350
|gross weight kg=350
|gross weight lb=500
|max takeoff weight kg=
|fuel capacity=
|lift kg=<!-- lighter-than-air -->
|more general=
|lift lb=<!-- lighter-than-air -->
<!--

Powerplant
-->
|eng1 number=1
|eng1 number=1
|eng1 type=[[Le Rhône]]
|eng1 name=[[Le Rhône Type 9C]]
|eng1 kw=<!-- prop engines -->60
|eng1 type=9-cylinder air-cooled rotary piston engine
|eng1 hp=<!-- prop engines -->80
|eng1 hp=80
|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 -->


|prop blade number=<!-- propeller aircraft -->
|prop name=
|prop dia m=<!-- propeller aircraft -->
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop dia note=
<!--
Performance
-->
|max speed kmh=165
|max speed kmh=165
|max speed mph=
|cruise speed kmh=
|stall speed kmh=
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=<!-- if max speed unknown -->
|never exceed speed kmh=
|cruise speed mph=<!-- if max speed unknown -->
|stall speed kmh=<!-- aerobatic and STOL aircraft -->
|stall speed mph=<!-- aerobatic and STOL aircraft -->
|range km=
|range km=
|range miles=
|endurance h=<!-- if range unknown -->
|endurance min=<!-- if range unknown -->
|ceiling m=
|ceiling m=
|g limits=<!-- aerobatic -->
|ceiling ft=
|g limits=<!-- aerobatic aircraft -->
|roll rate=<!-- aerobatic -->
|roll rate=<!-- aerobatic aircraft -->
|glide ratio=<!-- sailplanes -->
|climb rate ms=
|climb rate ms=
|time to altitude=
|climb rate ftmin=
|wing loading kg/m2=
|sink rate ms=<!-- sailplanes -->
|fuel consumption kg/km=
|sink rate ftmin=<!-- sailplanes -->
|power/mass=


|more performance=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}
<!-- ==See also== -->
{{aircontent
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|see also=
|related=<!-- related developments -->
|similar aircraft=<!-- similar or comparable aircraft -->
|lists=<!-- related lists -->
}}
}}


==References==
==References==
{{reflist}}
{{reflist}}
<!-- ==Further reading== -->

<!-- ==External links== -->
{{commons category|Morane-Saulnier AS}}

{{Morane-Saulnier aircraft}}
{{Morane-Saulnier aircraft}}


Revision as of 14:17, 6 February 2019

Type AS
Role Trainer
National origin France
Manufacturer Morane-Saulnier
First flight 1920

The Morane-Saulnier AS was a high-wing monoplane single-seat touring aircraft built in France after WWI.

Specifications (variant specified)

Data from [1]

General characteristics

  • Length: 5.64 m (18 ft 6 in)
  • Wingspan: 8.8 m (28 ft 10 in)
  • Height: 3.15 m (10 ft 4 in)
  • Wing area: 13 m2 (140 sq ft)
  • Gross weight: 350 kg (772 lb)
  • Powerplant: 1 × Le Rhône Type 9C 9-cylinder air-cooled rotary piston engine, 60 kW (80 hp)

Performance

  • Maximum speed: 165 km/h (103 mph, 89 kn)

References

  1. ^ "Morane-Saulnier AS - avion de tourisme - Un siècle d'aviation française". Aviafrance.com. 2007-11-25. Retrieved 2019-02-06.
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