View source for Pro.Mecc Freccia Anemo

{{Short description|Italian ultralight aircraft}}
{{Use dmy dates|date=January 2022}}
{{Use British English|date=January 2022}}
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{|{{Infobox aircraft begin
 | name=Freccia Anemo
 | image=Z-Pro.Mecc Freccia (47695538181).jpg
 | caption=
}}{{Infobox aircraft type
 | type=[[Ultralight aircraft]]
 | national origin=[[Italy]]
 | manufacturer=[[Pro.Mecc]]
 | designer=
 | first flight=
 | introduced=2011
 | retired=
 | status=In production (2012)
 | primary user=
 | more users= <!--Limited to three in total; separate using <br /> -->
 | produced= <!--years in production-->
 | number built=
 | developed from= [[Pro.Mecc Sparviero]]
 | variants with their own articles=
}}
|}
The '''Pro.Mecc Freccia Anemo''' ({{lang-en|Fast Arrow}}) is an Italian [[ultralight aircraft]], designed and produced by [[Pro.Mecc]] of [[Corigliano d'Otranto]]. The aircraft was introduced at the [[AERO Friedrichshafen]] show in 2011. The Freccia is supplied as a complete ready-to-fly-aircraft.<ref name="WDLA11">Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 71. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X</ref><ref name="WDLA15">Tacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015-16'', page 74. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}</ref>

==Design and development==
The Freccia was derived from the earlier [[Pro.Mecc Sparviero]], with additional streamlining and a new elliptical wing planform. It was designed to conform to the [[Fédération Aéronautique Internationale]] microlight rules. It features a cantilever [[low-wing]], a two-seats-in-[[side-by-side configuration]] enclosed cockpit under a [[bubble canopy]], fixed or, optionally, retractable [[tricycle landing gear]] and a single engine in [[tractor configuration]].<ref name="WDLA11" /><ref name="WDLA15"/>

The aircraft is made from [[carbon fibre]]. Its {{convert|8.78|m|ft|1|abbr=on}} span wing has an area of {{convert|10.18|m2|sqft|abbr=on}} and [[Flap (aircraft)|double slotted flaps]] to allow a low [[stall speed]]. Engines available are the {{convert|100|hp|kW|0|abbr=on}} [[Rotax 912ULS]], the [[turbocharged]] {{convert|115|hp|kW|0|abbr=on}} [[Rotax 914]] and the {{convert|130|hp|kW|0|abbr=on}} [[ULPower UL350iS]] [[four-stroke]] powerplant.<ref name="WDLA11" /><ref name="WDLA15"/>
<!-- ==Operational history== -->

==Variants==
;Freccia
:Fixed landing gear model, introduced in 2011<ref name="WDLA11" /><ref name="WDLA15"/>
;Freccia-RG
:Retractable landing gear model, introduced in 2012<ref name="WDLA11" /><ref name="WDLA15"/>
<!-- ==Aircraft on display== -->

==Specifications (Freccia Anemo) ==
{{Aircraft specs
|ref=Bayerl<ref name="WDLA11" />
|prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->
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        General characteristics
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|genhide=

|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=8.78
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=10.18
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=285
|empty weight lb=
|empty weight note=
|gross weight kg=472.5
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|110|L}}
|more general=
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[[Rotax 912ULS]]
|eng1 type=four cylinder, liquid and air-cooled, [[four stroke]] [[aircraft engine]]
|eng1 kw=75<!-- prop engines -->
|eng1 hp=<!-- prop engines -->

|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=

<!--
        Performance
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|perfhide=

|max speed kmh=280
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=260
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=65
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=300
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=8
|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=46.4
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

==References==
{{reflist}}

==External links==
*{{Official website|http://www.promecc.com/}}

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[[Category:2010s Italian ultralight aircraft]]
[[Category:Single-engined tractor aircraft]]