HB-Flugtechnik Dandy

{{Short description|Austrian ultralight aircraft}}

{{Use dmy dates|date=December 2022}}

{{Use British English|date=December 2022}}

{{Infobox Aircraft Begin

| name=Dandy

| image=

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}}{{Infobox Aircraft Type

| type=Ultralight aircraft

| national origin=Austria

| manufacturer=HB-Flugtechnik

| designer=Heino Brditschka

| first flight=

| introduced=

| retired=

| status=In production (2015)

| primary user=

| more users=

| produced=

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| developed from=

| variants with their own articles=

}}

The HB-Flugtechnik Dandy is an Austrian ultralight aircraft that was designed by Heino Brditschka and produced by HB-Flugtechnik. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 58. WDLA UK, Lancaster UK, 2011. ISSN 1368-485XTacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 60. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

Design and development

The Dandy was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed conventional landing gear and a single engine in tractor configuration.

The aircraft fuselage is made from welded steel tubing, with the wings constructed from aluminum tubing and all surfaces covered in doped aircraft fabric. Its {{convert|9.6|m|ft|1|abbr=on}} span wing has an area of {{convert|12.6|m2|sqft|abbr=on}}. The standard engine available is the {{convert|80|hp|kW|0|abbr=on}} Rotax 912UL four-stroke powerplant.

Variants

;Dandy

:Model with side-by-side seating. In production, 2015.

;Cubby

:Model with tandem seating, resembling a Piper J-3 Cub. In production, 2015.

Specifications (Dandy)

{{Aircraft specs

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|crew=one

|capacity=one passenger

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|empty weight kg=260

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|gross weight kg=450

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|fuel capacity={{convert|60|L}}

|more general=

|eng1 number=1

|eng1 name=Rotax 912UL

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

|eng1 kw=60

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|max speed kmh=170

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|cruise speed kmh=150

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|stall speed kmh=50

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|wing loading kg/m2=35.7

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References

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