Six Chuter SR7
American powered parachute
From Wikipedia, the free encyclopedia
The Six Chuter SR7 is an American powered parachute that was designed and produced by Six Chuter of Yakima, Washington, introduced in 1997.[1][2][3]
| SR7 | |
|---|---|
| General information | |
| Type | Powered parachute |
| National origin | United States |
| Manufacturer | Six Chuter |
| Status | Production completed |
| History | |
| Introduction date | 1997 |
Design and development
The SR7's design goals included that it be capable of carrying large-sized pilots and passengers.[1][2]
The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules as a two-seat ultralight trainer or as an amateur built. It features a parachute-style high-wing, two-seats-in-tandem, tricycle landing gear and a single 64 hp (48 kW) Rotax 582 engine in pusher configuration.[1][2][3]
The SR7 is built from a combination of aluminium and 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 SR7 model was factory supplied in the form of an assembly kit that requires 40 hours to complete.[1]
Variants
Specifications (XR7XL)
Data from KitPlanes[2]
General characteristics
- Crew: one
- Capacity: one passenger
- Length: 8 ft 6 in (2.59 m)
- Wingspan: 39 ft 6 in (12.04 m)
- Height: 7 ft 0 in (2.13 m)
- Wing area: 500 sq ft (46 m2)
- Empty weight: 299 lb (136 kg)
- Gross weight: 700 lb (318 kg)
- Fuel capacity: 10 U.S. gallons (38 L; 8.3 imp gal)
- Powerplant: 1 × Rotax 582 twin cylinder, two-stroke, liquid-cooled aircraft engine, 64 hp (48 kW)
Performance
- Cruise speed: 26 mph (42 km/h, 23 kn)
- Range: 50 mi (80 km, 43 nmi)
- Service ceiling: 10,000 ft (3,000 m)
- Rate of climb: 500 ft/min (2.5 m/s)