# Van's Aircraft RV-14

The Van's Aircraft RV-14 is an American aerobatic kit aircraft designed by Richard VanGrunsven and produced by Van's Aircraft. It was introduced at AirVenture in July 2012. The aircraft is supplied as a kit for amateur construction.
As of November 2022, 207 RV-14s have been completed and flown.

## Design and development

Derived from the four-seat RV-10, RV-14 design work was commenced several years before its 2012 debut. It is an aerobatic two-seater designed to accommodate large pilots and offer greater baggage space, to comply with the US experimental amateur-built aircraft rules. The design goals included improved visibility, a wider cabin, a low landing speed achieved by larger and more effective flaps, good rate-of-climb and glide ratio, landing gear that meets FAR Part 23 certification standards and an airframe designed to accommodate the Lycoming IO-390 powerplant. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear and a single engine in tractor configuration.
The RV-14 is built from aluminum sheet. The prototype was fitted with a 210 hp (157 kW) Lycoming IO-390 four-stroke powerplant. The kit is intended to be easier to assemble than earlier Van's designs through the use of pre-punched and pre-formed fuselage longerons, pre-installed wiring, plug-in avionics, a pre-trimmed and ready-to-install bubble canopy, pre-welded canopy frame, pre-fitted engine baffles as well as matched pre-punched holes. The RV-14 offers several instrument panel choices, including one designed to take modern electronic flight instrument systems (EFIS), like the Dynon SkyView, without any additional cutting, as well as a blank panel that can be customized by the builder.
In July 2020 Van's introduced a new version of the Lycoming IO-390, designated as the IO-390-EXP119 and optimized for the RV-14. The engine has new exhaust and induction systems and puts out 215 hp (160 kW). It has a revised oil sump, aluminum induction pipes, oil pump and accessory case that saves 10 lb (5 kg) of weight. With this powerplant the RV-14 is 11 mph (18 km/h) faster in cruise speed and climbs 250 ft/min (1.27 m/s) faster.
The manufacturer offers aircraft type transition training and has built an RV-14 for this purpose.

## Variants
### RV-14

    Two-seat conventional landing gear variant with tailwheel.

### RV-14A

    Two-seat tricycle landing gear variant.

## Specifications (RV-14A)

Data from AVweb, KitPlanes and manufacturer
General characteristics
* Crew: one
* Capacity: one passenger
* Length: 21 ft 1 in (6.43 m)
* Wingspan: 27 ft 0 in (8.23 m)
* Height: 8 ft 2 in (2.49 m)
* Wing area: 126.1 sq ft (11.72 m$^2$)
* Empty weight: 1,240 lb (562 kg)
* Gross weight: 2,050 lb (930 kg)
* Fuel capacity: 50 U.S. gallons (190 L; 42 imp gal)
* Powerplant: 1 × Lycoming IO-390 four cylinder, air-cooled, four stroke aircraft engine, 210 hp (160 kW)
* Propellers: 2-bladed Hartzel C2YR-1BFP/F7497-2 or C2YR-1BFP/F7497
Performance
* Maximum speed: 207 mph (333 km/h, 180 kn)
* Cruise speed: 190 mph (310 km/h, 170 kn)
* Stall speed: 54 mph (87 km/h, 47 kn)
* Range: 938 mi (1,510 km, 815 nmi)
* Service ceiling: 18,000 ft (5,500 m)
* g limits: +6/-3g at the aerobatic gross weight of 1,900 lb (862 kg)
* Wing loading: 16.26 lb/sq ft (79.4 kg/m$^2$)