Van's Aircraft RV-6

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RV-6
VansRV-6withfirepaint.jpg
An RV-6 with an elaborate paint scheme at Sun 'n Fun 2006.
Role kit aircraft
Manufacturer Van's Aircraft
Designer Richard VanGrunsven
First flight June 1986[1]
Number built 2520 (Jan 2014)[2]
Unit cost
USD$41,000-$97,000
Developed from Van's Aircraft RV-4
Variants Aviation Industries of Iran AVA-202
A RV-6 taxiing at the Brockville Ontario fly-in June 2005. This aircraft has the earlier design forward-hinged canopy
A RV-6A landing at Tauranga_Airport Runway 07R
A RV-6A – the nose wheel equipped version of the RV-6. This aircraft has the later sliding canopy.
A RV-6 instrument panel showing typical instruments and avionics found in these aircraft
Cockpit of a Van’s RV-6 at an English rally in 2006.
Van's RV-6A landing

The Van's RV-6 and RV-6A are two-seat, single-engine, low-wing homebuilt airplanes sold in kit form by Van's Aircraft. The RV-6 is the tail-wheel equipped version while the RV-6A features a nose-wheel. The RV-6 was the first aircraft in the popular Van’s RV series to feature side-by-side seating and the first to offer a nosewheel option. It was first flown in 1985. Over 2500 kits have been completed and flown.[2]

The RV-6 kit has been superseded by the similar, but improved, RV-7. Kit components are still available to allow builders to complete RV-6s under construction, but no new complete kits are available.

Development[edit]

Van’s Aircraft designer, Richard VanGrunsven, designed the RV-6 series as a two seat side-by-side development of the RV-4, which was itself a development of the single seat RV-3.

Market demand motivated VanGrunsven to design the RV-6 and offer it as an optional nosewheel design. The original two seater RV-4 has been a remarkable success, but the tandem seating configuration was not considered ideal by many potential owners as it leaves the passenger isolated in the back seat. Many female spouses of builders especially favoured the side-by-side configuration over the tandem arrangement.

VanGrunsven worked diligently to create a side-by-side design with a generous 43-inch-wide (1,100 mm) cockpit that did not sacrifice the RV-4’s handling, STOL performance and especially its high cruise speed. In the end the RV-6 prototype produced cruise speeds that are only 3 mph (5 km/h) slower than the RV-4 with the same engine.

The first RV-6s had a forward hinged canopy design. This was a simple one-piece arrangement, but it made taxiing the aircraft with the canopy open more difficult. Later kits had the option of a rearward sliding canopy that could more easily provide ventilation on the ground.

The RV-6A version features steel rod landing gear with the nosewheel strut attached to the engine mount. The nosewheel is friction castering and the aircraft is steered with differential braking. The brakes are mounted conventionally on the rudder pedal toes.

Nigerian Air Force RV-6A Air Beetle[edit]

The RV-6 has a rare distinction in the world of kit built aircraft - it is used as a military training aircraft. Searching for a suitable trainer that could be assembled in Nigeria using local labour, the government of that country settled on the RV-6A. Van's produced 60 kits to fulfill the order and these were assembled and test flown in Nigeria, entering service with the Nigerian Air Force in 1989 as elementary training aircraft under the name "Air Beetle". The air training school is based at Kaduna, Nigeria. The only other amateur aircraft to have this distinction is the Pazmany PL-1, which was built as a trainer for Taiwan's Air Force in the 1970s.

AVA-202[edit]

A modified version of the RV-6A is manufactured in Iran by Aviation Industries of Iran as the AVA-202. First flown in 1997, the main change from the RV-6A is a greater wingspan of 28.67 ft (8.74 m).[3]

Operators[edit]

 Nigeria

Specifications (RV-6 180 hp)[edit]

Data from Van's website[4][5]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 20 ft 2 in (6.15 m)
  • Wingspan: 23 ft 0 in (7.01 m)
  • Height: 5 ft 3 in (1.60 m)
  • Empty weight: 965 lb (438 kg)
  • Gross weight: 1,600 lb (726 kg)
  • Fuel capacity: 38 U.S. gallons (140 L; 32 imp gal)
  • Powerplant: 1 × Lycoming O-360 four cylinder, four-stroke, air-cooled, horizontally-opposed aircraft engine, 180 hp (130 kW)

Performance

  • Maximum speed: 210 mph (338 km/h; 182 kn)
  • Cruise speed: 199 mph (173 kn; 320 km/h)
  • Stall speed: 49 mph (43 kn; 79 km/h)
  • Range: 720 mi (626 nmi; 1,159 km) at 75% and 8000 feet
  • Service ceiling: 25,700 ft (7,833 m)
  • Rate of climb: 2,275 ft/min (11.56 m/s)
  • Wing loading: 14.5 lb/sq ft (71 kg/m2)

See also[edit]

Related development
Aircraft of comparable role, configuration and era

References[edit]

  1. ^ Lambert 1993, pp. 580–581.
  2. ^ a b Vans Aircraft (16 Jan 2014). "First Flights". Retrieved 16 Jan 2014. 
  3. ^ Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 156. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  4. ^ Van's Aircraft (2008). "Specifications". Retrieved 10 March 2012. 
  5. ^ Van's Aircraft (2008). "Performance". Retrieved 10 March 2012. 

External links[edit]