Van's Aircraft RV-10

The Van's Aircraft RV-10 is a four-seat, single-engine, low-wing homebuilt airplane sold in kit form by Van's Aircraft. It is the first four-seat airplane in the popular RV series.[4] The RV-10 first flew on 29 May 2003, and the first kit parts were delivered to a customer in September 2003.

RV-10
Role Homebuilt aircraft
National origin United States
Manufacturer Van's Aircraft
Designer Richard VanGrunsven
First flight 29 May 2003[1]
Introduction 2003
Number built 933 (October 2019)[2]
Unit cost
US$114,230–$127,485[3]
Developed from Van's Aircraft RV-7
Variants Van's Aircraft RV-14
Construction of an RV-10 wing in a garage
An RV-10 at the Van's Aircraft display at Sun n Fun 2006 in Lakeland Florida
RV10 at EAA Airventure 2014
RV-10 landing

As of October 2019, 933 RV-10s have been completed and flown.[2]

Design and development

The architect of the line of Van's aircraft, Richard VanGrunsven, designed the RV-10 to satisfy a market demand for a four-seat version of the popular RV series aircraft.[1] The RV-10 was designed from the start as a touring aircraft and as such it forgoes the aerobatic capabilities and the lighter handling common to the aircraft in the RV line from the RV-3 to RV-8. Instead the RV-10 design focuses on greater stability and payload.[5]

The design power is 210 to 260 hp (157 to 194 kW) and the prototype was flown with a Lycoming IO-540 powerplant of 260 hp (194 kW), which is the maximum that the airframe was designed to accept.[6] When Van's introduced the RV-10 they planned three engine configurations. One configuration using a smaller lighter 210 HP Continental IO-360ES, and two others using the larger 235 and 260HP Lycoming I/O-540. The #1 factory demonstrator used the IO-540, while the #2 RV-10 used the Continental IO-360. Vans decided to discontinue the support for the Continental engine after a poll which indicated that most builders would install the Lycoming engine,[7] although this poses problems for builders in certain countries with engine displacement limitations, in which the Continental's 360 cubic inch displacement would be acceptable.[8]

This is the first aircraft in the RV line that does not have a hinged or sliding canopy. VanGrunsven instead opted for two gull-winged doors to provide access to the four seats.

This design has benefited from many of the production changes that were pioneered with the RV-7, RV-8 and the RV-9. Like those aircraft, the RV-10 uses computer assisted design to produce a kit with pre-drilled rivet holes, thus greatly reducing assembly time for the builder. The RV-10 is available only as a tricycle landing gear version and no tailwheel or retractable landing gear versions are planned.

The aircraft is constructed of aluminum with the cabin structure and gull-winged doors made from composite materials. The landing gear is tubular steel with the nosewheel mounting tube welded to the engine mount. As in all nose-wheel equipped RV aircraft, the nosewheel is free castering and the aircraft is steered with differential braking. The brakes are mounted conventionally on the rudder pedal toes.

The amount of time and effort required to build the airplane can vary greatly, but Vans claims that the average first-time builder can complete it in 2,000 hours.[6]

The total price of the standard-build kit as of December 2016, was US$46,090, which did not include an engine or avionics. A "quick-build" option was $59,530.[3]

In February 2019 BRS Aerospace released a kit to installed a ballistic parachute on the RV-10. The kit can be installed on a completed RV-10 or one under construction. The parachute takes up one third of the aircraft's baggage bay and weighs 82 lb (37 kg).[9]

Variants
Aircraft Turbine Solution Group PBS TP-100 RV-10
The RV-10 was selected as the testbed aircraft for the Diemech TP 100 241 hp (180 kW) turboprop engine, which first flew on 8 June 2014.[10] The testbed aircraft was outfitted with 120 gallon fuel tanks and was to be tested at altitudes of up to 20,000 ft (6,096 m).[11][12]

Specifications (RV-10)
The RV-10 from the front, showing the gull-winged doors for cabin entry

Data from Manufacturer[13]

General characteristics

  • Crew: one
  • Capacity: three passengers
  • Length: 24 ft 5 in (7.44 m)
  • Wingspan: 31 ft 9 in (9.68 m)
  • Height: 8 ft 8 in (2.64 m)
  • Wing area: 148 sq ft (13.7 m2)
  • Empty weight: 1,630 lb (739 kg)
  • Gross weight: 2,700 lb (1,225 kg)
  • Fuel capacity: 60 U.S. gallons (230 L; 50 imp gal)
  • Powerplant: 1 × Lycoming O-540 six-cylinder, air-cooled aircraft engine, 260 hp (190 kW)
  • Propellers: 2-bladed constant speed Hartzell Propeller

Performance

  • Maximum speed: 208 mph (335 km/h, 181 kn)
  • Cruise speed: 197 mph (317 km/h, 171 kn) 75% power at 8,000 ft (2,438 m)
  • Stall speed: 63 mph (101 km/h, 55 kn)
  • Range: 825 mi (1,328 km, 717 nmi) 75% power at 8,000 ft (2,438 m)
  • Service ceiling: 20,000 ft (6,100 m)
  • Rate of climb: 1,450 ft/min (7.4 m/s)
  • Wing loading: 18.6 lb/sq ft (91 kg/m2)
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See also

Related development

Aircraft of comparable role, configuration and era

References
  1. Vans Aircraft (April 2019). "Van's RV-10". Retrieved 13 April 2019.
  2. Vans Aircraft (October 2019). "First Flights". Retrieved 18 October 2019.
  3. Vans Aircraft Website Cost Estimator December 2016 https://www.vansaircraft.com/public/cost-estimator.htm
  4. Vandermeullen, Richard: 2011 Kit Aircraft Buyer's Guide, Kitplanes, Volume 28, Number 12, December 2011, page 74. Belvoir Publications. ISSN 0891-1851
  5. Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011–12, page 124. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  6. Kitplanes Staff: 2008 Kit Aircraft Directory, page 78, Kitplanes Magazine December 2007 Volume 24, Number 12, Belvoir Publications, Aviation Publishing Group LLC.
  7. 2005 #1 Issue of the RVator
  8. http://www.fomento.gob.es/NR/rdonlyres/1AC8F7F7-4133-4A0D-B4D2-9E2DFF400334/111570/3161982.pdf
  9. Cook, Marc (19 February 2019). "BRS Releases Parachute For Van's RV-10". AVweb. Retrieved 20 February 2019.
  10. "The RV-10 aircraft completed its first flight" (Press release). PBS Velká Bíteš. June 2014. Retrieved 26 August 2016.
  11. Bertorelli, Paul (26 March 2012). "Is There Room For A 240-HP Turbine?". AVweb. Retrieved 27 March 2012.
  12. "Turboprop solution". AOPA Pilot: 38. June 2014.
  13. Van's Aircraft. "RV-12". vansaircraft.com. Archived from the original on 2 April 2020. Retrieved 8 May 2020.
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