Air Copter A3C

{{Short description|French autogyro}}

{{Infobox aircraft begin

| name=A3C

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| type = Autogyro

| national origin = France

| manufacturer = Air Copter

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| status = In production (2011)

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The Air Copter A3C is a French autogyro, designed and produced by Air Copter of Lherm, Haute-Garonne. The aircraft is supplied as a kit for amateur construction.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 174. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

Design and development

The A3C was designed to comply with amateur-built aircraft rules. It features a single main rotor, a two-seat side-by-side configuration enclosed cockpit with a windshield, tricycle landing gear and a four-cylinder, air and liquid-cooled, four-stroke, dual-ignition, turbocharged {{convert|115|hp|kW|0|abbr=on}} Rotax 914 or a normally-aspirated {{convert|100|hp|kW|0|abbr=on}} Rotax 912S engine mounted in pusher configuration.

Air Copter is well known as a designer and manufacturer of gyroplane rotor blades and other dynamic components and they also make their own components for the A3C. The aircraft's {{convert|8.40|m|ft|1|abbr=on}} diameter rotor has a chord of {{convert|20|cm|in|1|abbr=on}} and employs a NACA 8H12 airfoil. The main rotor has a pre-rotator to shorten take-off distance. The aircraft has an empty weight of {{convert|250|kg|lb|abbr=on}} and a gross weight of {{convert|450|kg|lb|abbr=on}}, giving a useful load of {{convert|200|kg|lb|abbr=on}}.{{cite web|url = http://articles.janes.com/articles/Janes-All-the-Worlds-Aircraft/Air-Copter--Air-Copter-Sarl-France.html|title = Air Copter - Air Copter Sarl (France), Aircraft - Manufacturer|access-date = 26 December 2012|last = Jane's Information Group|date = 3 November 2011|archive-date = 26 January 2013|archive-url = https://archive.today/20130126201039/http://articles.janes.com/articles/Janes-All-the-Worlds-Aircraft/Air-Copter--Air-Copter-Sarl-France.html|url-status = dead}}

Specifications (A3C)

{{Aircraft specs

|ref=Bayerl

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|crew=one

|capacity=one passenger

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|airfoil=NACA 8H12

|empty weight kg=250

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|gross weight kg=450

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|fuel capacity={{convert|34|L}}

|more general=

|eng1 number=1

|eng1 name=Rotax 914

|eng1 type=four cylinder, liquid and air-cooled, turbocharged, four stroke aircraft engine

|eng1 kw=

|eng1 hp=115

|prop blade number=3

|prop name=composite

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|rot number=1

|rot dia m=8.40

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|max speed kmh=170

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|cruise speed kmh=140

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|climb rate ms=4

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References