- Design and development
- Variants
- Specifications (Vale)
- References Notes Bibliography
name=Magni Vale | image=Magni PM-3-4 Vale, Museo Nazionale della Scienza e della Tecnologia (Milan).jpg | caption= The only Magni Vale on display at Museo della Scienza e della Tecnologia "Leonardo da Vinci", Milan, Italy }}{{Infobox Aircraft Type | type=Monoplane tourer and aerobatic trainer | national origin=Italy | manufacturer=Piero Magni-Aviazione | designer=Piero Magni | first flight=1930s | introduced= | retired= | status= | primary user= | number built=1 | developed from= | variants with their own articles= }} |
The Magni Vale PM-3-4 was an Italian civil monoplane for use as a tourer or aerobatic trainer designed and built by Piero Magni-Aviazione in Milan. Design and developmentThe Vale was a sleek single-seat parasol wing braced monoplane powered by a {{convert|130|hp|kW|0|abbr=on}} Farina T.58 radial engine. An improved variant, the Supervale PM-4-1 had a {{convert|140|hp|kW|0|abbr=on}} Fiat A.54 engine. The start of the second world war halted design and development by the company. Variants- Vale PM-3-4
Powered by a {{convert|130|hp|kW|0|abbr=on}} Farina T.58 radial engine. - Supervale PM-4-1
Powered by a {{convert|140|hp|kW|0|abbr=on}} Fiat A.54 engine. Specifications (Vale) Performance figures calculated {{Aircraft specs |ref=Les Ailes 7 February 1935 |prime units?=met |genhide= |crew=One |length m=5.50 |length note= |span m=8.90 |span note= |height m=2.02 |height note= |wing area sqm=10.69 |aspect ratio= |airfoil= |empty weight kg=540 |empty weight note= |gross weight kg=765 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |more general=
|eng1 number=1 |eng1 name=Farina T.58 |eng1 type=5-cylinder radial engine |eng1 hp=130 |eng1 note= |power original= |more power= |prop blade number=2 |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop dia note=ground adjustable pitch
|perfhide= |max speed kmh=250 |max speed note= |cruise speed kmh=200 |cruise speed note= |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=90 |minimum control speed note= |range km=1000 |range miles= |range nmi= |range note= |endurance= |ceiling m=7000 |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |fuel consumption kg/km= |fuel consumption lb/mi= |power/mass= |thrust/weight= |more performance= }}{{aircontent |see also= |related= |similar aircraft= |lists= }}
ReferencesNotes }}Bibliography{{refbegin}}- {{cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=|pages=}}
{{refend}} 3 : Italian civil utility aircraft 1930–1939|Single-engined tractor aircraft|Parasol-wing aircraft |