# Six Chuter SR1

> Mediated Wiki article. Canonical URL: https://mediated.wiki/source/Six_Chuter_SR1
> Markdown URL: https://mediated.wiki/source/Six_Chuter_SR1.md
> Source: https://en.wikipedia.org/wiki/Six_Chuter_SR1
> Source revision: 1321150853
> License: Creative Commons Attribution-ShareAlike 4.0 International (https://creativecommons.org/licenses/by-sa/4.0/)

American powered parachute

SR1 General information Type Powered parachute National origin United States Manufacturer Six Chuter Status Production completed

The **Six Chuter SR1** is an American [powered parachute](/source/Powered_parachute) that was designed and produced by [Six Chuter](/source/Six_Chuter) of [Yakima, Washington](/source/Yakima%2C_Washington).[1]

## Design and development

The aircraft was designed to comply with the US [FAR 103 Ultralight Vehicles](/source/FAR_103_Ultralight_Vehicles) rules, including the category's maximum empty weight of 254 lb (115 kg). It features a [parachute](/source/Parachute)-style [high-wing](/source/High-wing), single-place accommodation, [tricycle landing gear](/source/Tricycle_landing_gear) and a single 52 hp (39 kW) [Rotax 503](/source/Rotax_503) engine in [pusher configuration](/source/Pusher_configuration). The 64 hp (48 kW) [Rotax 582](/source/Rotax_582) engine was a factory option.[1]

The aircraft is built from a combination of [aluminium](/source/Aluminium) and [4130 steel](/source/4130_steel) tubing. In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has lever-controlled nosewheel steering. The aircraft was factory supplied in the form of an assembly kit that requires 40 hours to complete.[1]

## Specifications (SR1)

*Data from* Cliche[1]

**General characteristics**

- **Crew:** one

- **Wing area:** 450 sq ft (42 m2)

- **Fuel capacity:** 5 U.S. gallons (19 L; 4.2 imp gal)

- **Powerplant:** 1 × [Rotax 503](/source/Rotax_503) twin cylinder, [two-stroke](/source/Two-stroke), air-cooled [aircraft engine](/source/Aircraft_engine), 50 hp (37 kW)

**Performance**

- **Rate of climb:** 500 ft/min (2.5 m/s)

## References

1. ^ [***a***](#cite_ref-Cliche_1-0) [***b***](#cite_ref-Cliche_1-1) [***c***](#cite_ref-Cliche_1-2) [***d***](#cite_ref-Cliche_1-3) Cliche, Andre: *Ultralight Aircraft Shopper's Guide* 8th Edition, page D-14. Cybair Limited Publishing, 2001. [ISBN](/source/ISBN_(identifier)) [0-9680628-1-4](https://en.wikipedia.org/wiki/Special:BookSources/0-9680628-1-4)

v t e Six Chuter aircraft Powered parachutes SR1 SR2 SR5 SR7 Power Hawk Discovery Legend P103UL Legend SE Legend XL Legend XL Paragon 912 Skye Ryder Aerochute

This article on an aircraft of the 1990s is a stub. You can help Wikipedia by adding missing information.

- [v](https://en.wikipedia.org/wiki/Template:Aero-1990s-stub)
- [t](/source/Template_talk%3AAero-1990s-stub)
- [e](https://en.wikipedia.org/wiki/Special:EditPage/Template:Aero-1990s-stub)

---
Adapted from the Wikipedia article [Six Chuter SR1](https://en.wikipedia.org/wiki/Six_Chuter_SR1) by Wikipedia contributors ([contributor history](https://en.wikipedia.org/wiki/Six_Chuter_SR1?action=history)). Available under [Creative Commons Attribution-ShareAlike 4.0 International](https://creativecommons.org/licenses/by-sa/4.0/). Changes may have been made.
