Roland S-STOL

{{Short description|German STOL aircraft}}

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

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

{{Infobox aircraft begin

| name=S-STOL

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}}{{Infobox aircraft type

| type=Ultralight aircraft and Light-sport aircraft

| national origin=Germany

| manufacturer=Roland Aircraft

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| status=In production (2012)

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The Roland S-STOL is a German STOL ultralight and light-sport aircraft, produced by Roland Aircraft. 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 73. WDLA UK, Lancaster UK, 2011. ISSN 1368-485XTacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 77. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

Design and development

The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit accessed via doors, fixed tricycle landing gear and a single engine in tractor configuration.

The aircraft is made from sheet aluminum. Its {{convert|8.20|m|ft|1|abbr=on}} span wing has an area of {{convert|11.4|m2|sqft|abbr=on}} leading edge slots and flaps. The wing is supported by V-struts with jury struts. The standard engine available is the {{convert|80|hp|kW|0|abbr=on}} Rotax 912UL four-stroke powerplant. The S-STOL can be de-rigged for storage and folding wings are a factory option. The aircraft can be fitted with wheels, skis and floats and can be used to tow gliders and hang gliders.

Operational history

Reviewer Marino Boric described the design in a 2015 review saying, "high reliability, robustness and real short-field ability make it a good-natured aircraft with forgiving characteristics both in the air and on the ground, where

its robust undercarriage, high ground clearance and tundra tires help it cope with the roughest strips."

Specifications (S-STOL)

{{Aircraft specs

|ref=Bayerl and Roland Aircraft{{cite web |url=http://www.roland-aircraft.de/index.php/s-stol/stol-technische-daten |title=STOL Technische Daten |publisher=Roland-aircraft.de |date= |accessdate=2012-08-29 |url-status=dead|archiveurl=https://web.archive.org/web/20120611105515/http://www.roland-aircraft.de/index.php/s-stol/stol-technische-daten |archivedate=2012-06-11 }}

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|capacity=one passenger

|length m=6.10

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|span m=8.20

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|wing area sqm=11.4

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|empty weight kg=275

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|gross weight kg=530

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|fuel capacity={{convert|90|L}} in two wing tanks

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|eng1 number=1

|eng1 name=Rotax 912UL

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

|eng1 kw=60

|eng1 hp=

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|max speed kmh=180

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|cruise speed kmh=140

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|stall speed kmh=58

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|ceiling m=

|ceiling ft=15000

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|g limits=+6/-3

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|climb rate ms=6.5

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|wing loading kg/m2=46.5

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See also

References

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