# Summit 2

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American powered parachute

Summit 2 General information Type Powered parachute National origin United States Manufacturer Aircraft Sales and Parts Summit Aerosports Status In production Number built 250 (February 2005)[1] History Introduction date 1999

The **Summit 2**, also called the **Summit II**, is an American [powered parachute](/source/Powered_parachute) that was originally designed and manufactured in 1999 by [Aircraft Sales and Parts](/source/Aircraft_Sales_and_Parts) of [Vernon, British Columbia](/source/Vernon%2C_British_Columbia) and now produced by [Summit Aerosports](/source/Summit_Aerosports) of [Yale, Michigan](/source/Yale%2C_Michigan).[1][2][3][4]

## Design and development

The aircraft was designed to comply with the US [FAR 103 Ultralight Vehicles](/source/FAR_103_Ultralight_Vehicles) rules as a two-seat trainer, or as an [amateur-built aircraft](/source/Homebuilt_aircraft). It features a [parachute](/source/Parachute)-style [high-wing](/source/High-wing), two-seats-in-[tandem](/source/Tandem), [tricycle landing gear](/source/Tricycle_landing_gear) and a single 64 hp (48 kW) [Rotax 582](/source/Rotax_582) engine in [pusher configuration](/source/Pusher_configuration). The 65 hp (48 kW) [Hirth 2706](/source/Hirth_2706), 50 hp (37 kW) [Rotax 503](/source/Rotax_503), 80 hp (60 kW) [Rotax 912](/source/Rotax_912) and the 60 hp (45 kW) [HKS 700E](/source/HKS_700E) engines are factory options.[1][2][4][5][6]

The aircraft is built from a combination of [6061-T6 aluminium](/source/6061-T6_aluminium), [4130 steel](/source/4130_steel) and [stainless steel](/source/Stainless_steel) tubing. The canopy is attached to the carriage at four points, instead of the more conventional two points, to improve stability. In flight steering is accomplished via rail-mounted sliding foot pedals that actuate the canopy brakes, creating roll and yaw. Steering is via a 2:1 ratio system of pulleys that reduce the force required and increase control authority. The lack of pivoting control bars allows [cockpit fairings](/source/Cockpit_fairing) to be fitted. On the ground the aircraft has lever-controlled nosewheel steering. The aircraft is factory supplied in the form of an assembly kit that requires 20–30 hours to complete.[1][2][4][6]

## Specifications (Summit 2)

*Data from* Cliche and Summit[2][5]

**General characteristics**

- **Crew:** one

- **Capacity:** one passenger

- **Length:** 10 ft 4 in (3.15 m)

- **Height:** 6 ft 4 in (1.93 m) to top of propeller guard

- **Wing area:** 550 sq ft (51 m2)

- **Empty weight:** 310 lb (141 kg)

- **Gross weight:** 950 lb (431 kg) when fitted with a Mustang S-550 rectangular canopy

- **Fuel capacity:** 10 U.S. gallons (38 L; 8.3 imp gal)

- **Powerplant:** 1 × [Rotax 582](/source/Rotax_582) twin cylinder, [two-stroke](/source/Two-stroke), liquid-cooled [aircraft engine](/source/Aircraft_engine), 64 hp (48 kW)

**Performance**

- **Cruise speed:** 26 mph (42 km/h, 23 kn) with a square canopy

- **Maximum glide ratio:** 4:1

- **Rate of climb:** 400 ft/min (2.0 m/s)

## References

1. ^ [***a***](#cite_ref-KitplanesFeb2005_1-0) [***b***](#cite_ref-KitplanesFeb2005_1-1) [***c***](#cite_ref-KitplanesFeb2005_1-2) [***d***](#cite_ref-KitplanesFeb2005_1-3) Downey, Julia: *2005 Trikes 'Chutes and Rotorcraft Directory*, Kitplanes, Volume 22, Number 2, February 2005, page 52. Belvoir Publications. ISSN 0891-1851

1. ^ [***a***](#cite_ref-Cliche_2-0) [***b***](#cite_ref-Cliche_2-1) [***c***](#cite_ref-Cliche_2-2) [***d***](#cite_ref-Cliche_2-3) Cliche, Andre: *Ultralight Aircraft Shopper's Guide* 8th Edition, page D-16. Cybair Limited Publishing, 2001. [ISBN](/source/ISBN_(identifier)) [0-9680628-1-4](https://en.wikipedia.org/wiki/Special:BookSources/0-9680628-1-4)

1. **[^](#cite_ref-SummitWhy_3-0)** [Summit Aerosports](/source/Summit_Aerosports) (2012). ["Why a Summit Powered Parachute?"](http://www.summitaerosports.com/why.htm). Retrieved March 22, 2012.

1. ^ [***a***](#cite_ref-WDLA04_4-0) [***b***](#cite_ref-WDLA04_4-1) [***c***](#cite_ref-WDLA04_4-2) Bertrand, Noel; Rene Coulon; et al: *World Directory of Leisure Aviation 2003-04*, page 86. Pagefast Ltd, Lancaster OK, 2003. ISSN 1368-485X

1. ^ [***a***](#cite_ref-Specs_5-0) [***b***](#cite_ref-Specs_5-1) [Summit Aerosports](/source/Summit_Aerosports) (2012). ["Summit 2 Specifications"](http://www.summitaerosports.com/page-s2specs.html). Retrieved March 22, 2012.

1. ^ [***a***](#cite_ref-KitplanesDec2012_6-0) [***b***](#cite_ref-KitplanesDec2012_6-1) Bernard, Mary and Suzanne B. Bopp: *Summit Aerosports: Summit 2, Steel Breeze and Mini Breeze*, Kitplanes, Volume 29, Number 12, December 2012, page 27-28. Belvoir Publications. ISSN 0891-1851

## External links

- [Official website](http://www.summitaerosports.com/)

v t e Aircraft Sales and Parts and Aeroplane Manufactory aircraft Aircraft Beaver RX 550 Plus Beaver SS Chinook Plus 2 Summit 2 Summit SS Summit 103 Mini Breeze Summit Steel Breeze Affiliated Companies Canadian Ultralight Manufacturing GSC Systems ASAP Canopies Steel Breeze Powered Parachutes Summit Aerosports ulparts.com Predecessor Companies Birdman Enterprises Spectrum Aircraft Beaver RX Enterprises Freedom Lite Legend Lite Successor Company Aeroplane Manufactory

v t e Uncertified aircraft developed in Canada ASAP Beaver RX 550 Plus Beaver SS Chinook Plus 2 Summit 2 Summit SS Ameri-Cana Eureka Birdman Chinook Blue Yonder Merlin EZ Flyer EZ Fun Flyer EZ Harvard EZ King Cobra Twin Engine EZ Flyer Bushcaddy/CADI/CLASS L-160 R-80 R-120 Fisher Avenger Celebrity Classic Dakota Hawk FP-202 Koala FP-303 FP-404 FP-505 Skeeter FP-606 Sky Baby Horizon 1 Horizon 2 R-80 Tiger Moth Super Koala Youngster Froebe Brothers Froebe helicopter Murphy Aircraft Moose Rebel Yukon Norman J6 Karatoo Nordic I Nordic II Nordic III Nordic IV Nordic V Nordic VI Nordic VII Nordic 8 Mini Explorer Normand Dube Aerocruiser Aerocruiser Plus Aerocruiser 450 Turbo Spectrum Aircraft/ Freedom Lite/Legend Lite Beaver SS-11 Skywatch UltraFlight Lazair Ultravia Pelican Zenair CH 601 CH 701 CH 801 CH 2000

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Adapted from the Wikipedia article [Summit 2](https://en.wikipedia.org/wiki/Summit_2) by Wikipedia contributors ([contributor history](https://en.wikipedia.org/wiki/Summit_2?action=history)). Available under [Creative Commons Attribution-ShareAlike 4.0 International](https://creativecommons.org/licenses/by-sa/4.0/). Changes may have been made.
