- Design and development
- Specifications (day version)
- References
- Further reading
| name=Aviméta 132 | image=Aviméta 132 left front photo NACA Aircraft Circular No.63.jpg | caption= }}{{Infobox Aircraft Type | type=Eight-passenger transport monoplane | national origin=France | manufacturer=Aviméta (Société pour la Construction d'Avions Métallique ) | designer= | first flight=1927 | introduced= | retired= | status= | primary user= | number built=1 | developed from= | variants with their own articles=
}} |
The Aviméta 132 was a French three-engined monoplane transport for eight-passengers designed and built by Aviméta (Société pour la Construction d'Avions Métallique ). It was the first French all-metal aircraft but only one aircraft was built. Design and developmentThe Aviméta 132 was a high-wing monoplane with a fixed conventional landing gear, powered by three uncowled {{convert|230|hp|kW|0|abbr=on}} Salmson 9Ab radial air-cooled piston engines. Fuel tanks were built into the wings, fitted with jettison valves to empty the tanks in an emergency. The enclosed cockpit sat two crew with a cabin for eight passengers. It was intended to build both a day and night version but only one aircraft was built and it did not enter production. Specifications (day version){{Aircraft specs
|ref=Flight
|prime units?=met
|crew=2
|capacity=8 pax
|length m=14.3
|span m=21.8
|height m=3.75
|wing area sqm=752
|aspect ratio=
|airfoil=
|empty weight kg=2700
|gross weight kg=10850
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
|eng1 number=3
|eng1 name=Salmson 9Ab
|eng1 type=9-cylinder air-cooled radial piston engines
|eng1 hp=230
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|max speed kmh=180
|cruise speed kmh=170
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=900
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=3750
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude={{cvt|2000|m}} in 19 minutes
|wing loading kg/m2=68.5
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass={{cvt|0.0641|hp/lb|kW/kg|order=flip}}
|more performance=
}}
References{{Commons category}}1. ^{{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 |page=85c}}
2. ^{{cite web |last1=Parmentier |first1=Bruno |title=Aviméta 132 |url=https://www.aviafrance.com/aviafrance1.php?ID=10145&ID_CONSTRUCTEUR=137&ANNEE=0&ID_MISSION=0&MOTCLEF= |website=Aviafrance|accessdate=2 March 2018 |location=Paris |language=French |date=4 December 2001}}
}}Further reading- {{cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=}}
{{DEFAULTSORT:Avimeta 132}} 4 : French airliners 1920–1929|Trimotors|Aviméta aircraft|High-wing aircraft |