Culver Dart

Design and development

In the early 1930s Al Mooney was working for the Lambert Aircraft Corporation, builders of the Monocoupe series aircraft. He designed a small two-seat monoplane, the Monosport G. When the company ran into financial difficulties Mooney bought the rights to his design and with K.K. Culver formed the Dart Aircraft Company. The aircraft was renamed the Dart Dart or Dart Model G.

The aircraft was a low-wing monoplane designed to be light with clean lines to enable it to use low powered aero-engines. It had a fixed undercarriage and a tailwheel. The initial version was named the Dart G powered by a 90 hp (67 kW) Lambert R-266 radial engine. That engine was in short supply, so the aircraft was fitted with a Ken-Royce engine and designated the Dart GK. The final version was the Dart GW powered by a Warner Scarab Junior radial engine. Two special aircraft were built with larger engines. In 1939 the company was renamed the Culver Aircraft Company and the aircraft was renamed the Culver Dart.

Variants

Dart G

Initial production version powered by a 90 hp (67 kW) Lambert R-266 - ca. 50 built.

Dart GC

125 hp (93 kW) Continental O-200 - 10 built

Dart GK

Variant fitted with a 90 hp (67 kW) Ken-Royce 5G engine - 25 built.

Dart GW

Final production version powered by a 90 hp (67 kW) Warner Scarab Junior - 8 built.

Dart GW Special

Two aircraft fitted with larger Warner engines, one with a 125 hp (93 kW) Warner Scarab engine, and the other with 145 hp (108 kW) Warner Super Scarab SS-50A engine.

X-F 220 Super Dart

An experimental variant modified with a 220 hp (160 kW) Continental R-670, 8 foot wing reduction and a 188 mph (163 kn; 303 km/h) cruise speed. Used by Rodney Jocelyn in national aerobatics.

Specifications (Dart GW)

Data from Simpson, 2001, p.170

General characteristics

Crew: 2

Length: ()

Wingspan: 29 ft 6 in (8.99 m)

Height: 6 ft 1 in (1.85 m)

Wing area: 176 ft² (16.35 m²)

Empty weight: 940 lb (426 kg)

Max. takeoff weight: 1,540 lb (699 kg)

Powerplant: 1 × Warner Scarab Junior 5-cyl. air-cooled radial piston engine, 90 hp (67 kw)

Performance

Maximum speed: 131 mph (211 km/h)

Range: 495 miles (797 km)

Service ceiling: 16,000 ft (4875 m)