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VAN'S RV-10

VAN'S RV-10The performance, handling and cost of the RV-10 make it the obvious choice in the limited field of four-seat kit airplanes, and make it a viable alternative to four-seat production airplanes – singles or twins - as well.

The RV-10 is a four-person airplane, not just an airplane with four seats. It will carry four FAA standard people, full fuel and sixty pounds of baggage. The cabin accommodates four full-sized adults. Both front and back seats will hold people 6'4" tall and provide them with truly comfortable leg and headroom. Composite gull-wing doors let occupants board from both sides.

The RV-10 is designed to fly well on various versions of the bulletproof six-cylinder Lycoming O-540 engine, developing between 235 and 260 hp. In our prototype, power is provided by a fuel injected 260 hp Lycoming IO-540.

When many pilots say "performance", they really mean "speed." The RV-10 is quite a fast airplane – it will cruise just under 200 mph – but speed is only part of the story.

The RV-10 derives its high cruise speed from a clean, light airframe, instead of from a big, consumptive engine. This means that cruise at lower speeds can be very economical. Company pilots often choose to cruise at 50-55% power and take advantage of the economy available there. At 175 mph, the RV-10 is getting more miles per gallon than most of the luxury cars, pickup trucks and SUVs it is flying over.

RVs are known for short-field capability and the RV-10 is no exception. Even at gross weight, the RV-10 can operate out of very short runways and climb well at high density altitudes. At the end of a flight, the generous wing area, big slotted flaps and robust steel rod landing gear allow the RV-10 to land at virtually any small airport -- grass, gravel or pavement. If you can land closer to your destination, you can gain a lot of time over "faster" airplanes that must use big paved airports a long way from town.

Occupant protection is an important design criteria. The composite cabin top provides roll-over protection. The cabin interior is designed around Oregon Aero seats and seat cushions, (provided in the kit) which provide the best available impact mitigation — and comfort. Like all other RVs, the RV-10 has impressively low stall and landing speeds. If necessary, it can be safely landed in very small spaces at speeds that give the occupants the best possible chance of escaping injury.

The baggage compartment will accept 100 lbs of "stuff" loaded through the baggage door on the left side. If fewer than four people are traveling, the rear seat backs may be removed in a couple of minutes for extra baggage space.

RVs have always enjoyed a reputation for excellent handling qualities. The RV-10 continues this tradition, in a manner appropriate to a four-place airplane. It is a very responsive airplane, but at the same time stable and easy to fly. It is not an aerobatic airplane, so flick-of-the-wrist sensitivity is not the point. Pilot workload is very low, because the airplane responds quickly and positively to small control inputs from the between-the-knees sticks and rigid pushrods running on ball bearings. It is not the least bit "twitchy" and does not require constant attention to maintain heading or altitude. A long trip in the RV-10 can be positively relaxing.

RV–10 Specifications

Exterior Dimensions
Span 31 ft 9in.
Length 24 ft 5 in.
Height 8 ft 8 in
Wing Area 148 sq ft
Weights
Empty Weight 1520-1630 lbs to correspond with engine choices.
Empty weight and performance measured with Hartzell 2-blade constant speed propeller.
Gross Weight 2700 lbs
Loadings
Wing Loading 18.6 lb/sq ft
Power Loading 13.5 - 10.4 lb/hp
Powerplant/Systems
Engine 235-260 hp
Propeller Hartzell C/S
Fuel Capacity 60 US gal
Other
Baggage 100 lbs

RV–10 Performance

Speed and ranges in statute mph.*235 hp performance estimated.
Speeds and ranges in statute mph (sm)
Light Weight 2200 lbs * 235 hp 260 hp
Speed
Top Speed 204 mph 211 mph
Cruise [75% @ 8000 ft] 194 mph 201 mph
Cruise [55% @ 8000 ft] 174 mph 180 mph
Stall Speed 57 mph 57 mph
Ground Performance
Takeoff Distance 415 ft 360 ft
Landing Distance 500 ft 525 ft
Climb/Ceiling
Rate of Climb 1,669 fpm 1,950 fpm
Ceiling (est) 20,538 ft 24,000 ft
Gross Weight2700 lbs * 235 hp 260 hp
Empty Weight 1,585 lbs 1,600 lbs
Speed
Top Speed 201 mph 208 mph
Cruise [75% @ 8000 ft] 190 mph 197 mph
Cruise [55% @ 8000 ft] 170 mph 176 mph
Stall Speed 63 mph 63 mph
Ground Performance
Takeoff Distance 583 ft 500 ft
Landing Distance 650 ft 650 ft
Climb/Ceiling
Rate of Climb 1,221 fpm 1,450 fpm
Ceiling (est) 16,839 ft 20,000 ft
Range
Range [75% @ 8000 ft] 883 sm 825 sm
Range [55% @ 8000 ft] 1070 sm 1000 sm