Huntwing

{{Short description|British ultralight trike}}

{{Use dmy dates|date=May 2017}}

{{Use British English|date=May 2017}}

{{Infobox aircraft begin

| name=Huntwing

| image=

| caption=

}}{{Infobox aircraft type

| type=Homebuilt ultralight trike

| national origin=United Kingdom

| manufacturer=

| designer=John Hunt

| first flight=1982

| introduced=

| retired=

| status=Plans available (2015)

| primary user=

| more users=

| produced=

| number built=20

| developed from=

| variants with their own articles=

}}

The Huntwing is a British ultralight trike that was designed by John Hunt of Clydach, Monmouthshire. The aircraft is supplied in the form of plans for amateur construction.Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 362. BAI Communications, 15 July 1998. {{ISBN|0-9636409-4-1}}

Design and development

The Huntwing was designed to comply with the British BCAR Section S microlight category. It was first flown in 1982 and introduced commercially in 1992. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit with a cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.{{cite web|url=http://www.huntwing.co.uk/|title=Huntwing|work=huntwing.co.uk|accessdate=12 May 2015}}

The aircraft is made from bolted-together aluminium tubing, with its 75% double surface wing covered in Dacron sailcloth. The {{convert|33.4|ft|m|1|abbr=on}} span wing is supported by a single tube-type kingpost, uses an "A" frame weight-shift control bar, has a nose angle of 121°, 24 top and six bottom battens and has a wing area of {{convert|161|sqft|m2|abbr=on}}. The acceptable power range is {{convert|50|to|64|hp|kW|0|abbr=on}} and the standard powerplants used include the twin cylinder, liquid-cooled, two-stroke {{convert|52|hp|kW|0|abbr=on}} Rotax 462 snowmobile engine, the twin cylinder, air-cooled, two-stroke {{convert|50|hp|kW|0|abbr=on}} Rotax 503 aircraft engine and the twin cylinder, liquid-cooled, two-stroke, dual-ignition {{convert|64|hp|kW|0|abbr=on}} Rotax 582 powerplant. The BMW R100RS four-stroke motorcycle engine can also be fitted.{{cite web|url=http://www.huntwing.co.uk/specs.html|title=Specifications|work=huntwing.co.uk|accessdate=12 May 2015}}{{cite web|url=http://www.huntwing.co.uk/faq.html|title=Frequently asked questions|work=huntwing.co.uk|accessdate=12 May 2015}}{{cite web|url=http://www.huntwing.co.uk/bmw%20photos/Bmw%20story%20for%20Internet.htm|title=The Huntwing BMW Trike|work=huntwing.co.uk|accessdate=12 May 2015}}

The plans wing is built by the amateur-builder and fitted with a Top Flight Sails sail. Alternatively a Mainair Blade wing can be used.

The manufacturer estimates the construction time from the supplied plans as 500 hours.

Operational history

The designers says that 10 sets of plans have been shipped and about 20 aircraft completed and flown.

In May 2015 eleven examples were registered in the United Kingdom with the Civil Aviation Authority.{{cite web|url = http://www.caa.co.uk/application.aspx?catid=60&pagetype=65&appid=1&mode=summary&aircrafttype=hunt&pageIndex=1|title = Make / Model Inquiry Results|accessdate = 12 May 2015|last = Civil Aviation Authority|date = 12 May 2015|archive-date = 18 May 2015|archive-url = https://web.archive.org/web/20150518073419/http://www.caa.co.uk/application.aspx?catid=60&pagetype=65&appid=1&mode=summary&aircrafttype=hunt&pageIndex=1|url-status = dead}}

Specifications (Huntwing 462LC)

{{Aircraft specs

|ref=Designer

|prime units?=imp

|genhide=

|crew=one

|capacity=one passenger

|length m=

|length ft=

|length in=

|length note=

|span m=

|span ft=33.4

|span in=

|span note=

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=

|wing area sqft=161

|wing area note=

|aspect ratio=7.25:1

|airfoil=

|empty weight kg=

|empty weight lb=

|empty weight note=

|gross weight kg=372

|gross weight lb=

|gross weight note=

|fuel capacity={{convert|50|L}}

|more general=

|eng1 number=1

|eng1 name=Rotax 462

|eng1 type=twin cylinder, liquid-cooled, two stroke aircraft engine, with a 2.58:1 reduction drive

|eng1 kw=

|eng1 hp=52

|prop blade number=3

|prop name=Ivoprop

|prop dia m=

|prop dia ft=5

|prop dia in=4

|prop note=

|perfhide=

|max speed kmh=

|max speed mph=70

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=60

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=

|stall speed kts=

|stall speed note=

|never exceed speed kmh=

|never exceed speed mph=74

|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=+4/-2

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=700

|climb rate note=

|time to altitude=

|sink rate ms=

|sink rate ftmin=

|sink rate note=

|lift to drag=

|wing loading kg/m2=24.8

|wing loading lb/sqft=

|wing loading note=

|power/mass=

|thrust/weight=

|more performance=

|avionics=

}}

References

{{reflist}}