Suvarna Garge (Editor)

Rans S 21 Outbound

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Manufacturer
  
Rans S-21 Outbound wwwflyingmagcomsitesflyingmagcomfilesstyles

The Rans S-21 Outbound is an American STOL homebuilt aircraft that was designed by Randy Schlitter and is under development by Rans Designs of Hays, Kansas, introduced at AirVenture in 2016. The aircraft is intended to be supplied as a quick-build kit for amateur construction.

Contents

Rans S-21 Outbound RANS introduces OUTBOUND General Aviation News

Design and development

Rans S-21 Outbound Rans offers new Titanpowered aircraft AOPA

The S-21 Outbound features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cabin accessed via doors, fixed tricycle landing gear or optionally conventional landing gear and a single engine in tractor configuration.

Rans S-21 Outbound Rans S21 to debut at Oshkosh Backcountry Pilot

The aircraft is made from aluminum sheet, with both leading edge and trailing edge extruded spars. The sheet metal parts employ final-size matched holes to reduce builder errors and speed construction. Its 28 ft (8.5 m) span wing mounts flaps and has a wing area of 141 sq ft (13.1 m2). The standard engine used is the 180 hp (134 kW) Continental Titan X-340 powerplant. Tundra tires up to 26 in (66 cm) may be fitted.

Rans S-21 Outbound Rans announces fastest and biggest aircraft S21 Outbound FLYER

The aircraft has a typical empty weight of 985 lb (447 kg) and a gross weight of 1,800 lb (820 kg), giving a useful load of 815 lb (370 kg). With full fuel of 31.75 U.S. gallons (120.2 L; 26.44 imp gal) the payload for the crew/pilot, passengers and baggage is 625 lb (283 kg).

The S-21 will compete with the CubCrafters Carbon Cub EX and the American Legend Super Legend HP in the kit aircraft market.

Specifications (S-21 Outbound)

Data from Manufacturer and AVweb

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Wingspan: 28 ft (8.5 m)
  • Wing area: 141 sq ft (13.1 m2)
  • Aspect ratio: 5.53:1
  • Empty weight: 985 lb (447 kg)
  • Gross weight: 1,800 lb (816 kg)
  • Fuel capacity: 31.75 U.S. gallons (120.2 L; 26.44 imp gal)
  • Powerplant: 1 × Continental X-340 Titan four cylinder, air-cooled, four stroke aircraft engine, 180 hp (130 kW)
  • Performance

  • Maximum speed: 150 mph (241 km/h; 130 kn)
  • Stall speed: 38 mph (33 kn; 61 km/h)
  • Never exceed speed: 215 mph (187 kn; 346 km/h)
  • Range: 527 mi (458 nmi; 848 km)
  • Endurance: 3.9 hours
  • Service ceiling: 14,500 ft (4,420 m)
  • G limits: +6/-4
  • Maximum glide ratio: 11.1
  • Wing loading: 12.76 lb/sq ft (62.3 kg/m2)
  • Power/mass: 10 lb/hp
  • References

    Rans S-21 Outbound Wikipedia


    Similar Topics