Van's RV-3

Piston single engine • Low Wing • Fixed gear

Range Map

Origin:

nm at current load

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Payload vs. Range

Configure weights

Default: 190 lbs

Default: 30 lbs

Occupants
lbs lbs / pax

gal

Fuel on board

lbs

Extra weight

nm

Range

Available Range / nm
Mission capable. Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required. You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight. Reduce payload by lbs to safely operate this aircraft.
Extra weight is the additional payload available with your selected passengers.

Mission Profile

170
KTAS
Cruise Speed
517
nm
Max Range
23500
ft
Service Ceiling
1
Occupants
170
lbs
Wet Payload
Used market Only available used
Experimental Amateur-built, no type certificate

Estimated Ownership Costs

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About the Van's RV-3

Overview

The Van’s RV-3 is a single-seat, low-wing Experimental Amateur-Built kit aircraft from Van’s Aircraft of Aurora, Oregon, first flown in 1971 as Richard VanGrunsven’s first kit design and the airplane from which the entire RV line grew. Built with a 100 to 160 hp Lycoming (commonly a 150 hp O-320), it cruises about 170 knots true, climbs around 2,050 fpm, and is an aerobatic taildragger rated to +6/-3 g in its reinforced-spar RV-3B form. Light, fast, and efficient on modest power, roughly 300 were built; it is long out of production, with only the RV-3B wing kit catalogued in later years.

The RV-3 is the genesis of Van’s “Total Performance” philosophy and the direct ancestor of the two-seat RV-4 and RV-8. It is bought used and flown by owners who want a pure single-seat sportplane with historical significance; support is thinner than for current models. Choose the Van’s RV-3 when you want the original RV, a light single-seat aerobatic taildragger, and you accept the thinner parts support and workmanship variance of an early, low-production, out-of-production homebuilt.

Key Features for GA Buyers

  • Van’s founding design. VanGrunsven’s first kit, first flown in 1971, and the direct ancestor of every later RV.
  • Light and fast on little power. Strong cruise and climb on 100 to 160 hp.
  • Aerobatic. The reinforced-spar RV-3B is rated to +6/-3 g.
  • Pure single-seater. A focused, low-weight sport airframe with no passenger compromise.

Trade-offs

  • Out of production and rare. Roughly 300 built, so parts and type support are thinner than for current RVs.
  • Spar history. Early RV-3/RV-3A airframes needed a main-spar reinforcement (the RV-3B fix); confirm the modification status of any example.
  • Single seat. No passenger; builders who want two seats step to the RV-4 or RV-8.
  • Limited published data. Van’s never published a full V-speed set for the RV-3, so some envelope figures are not available from a reproducible source.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 19.92 ft
Height
5.0 ft
Length
19.0 ft
Parking area (ft2)
718.08 ft2
Max Takeoff Weight
1,100 lbs
Useful Load
350 lbs
Fuel Capacity
30 gal

Performance

Cruise Speed
Source: manufacturer figure 170 KTAS
Range
517 NM
Service Ceiling
23,500 ft
Rate of Climb
2050 fpm

Engine

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Sources

Where the figures on this page come from. Van's RV-3 specifications are traced to published references; estimated values are flagged inline next to the figure.

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