Rollason Turbulent Aircraft

Turbulent, RV Smith from British Built Aircraft

Production Details

Design Company:

Rollason Aircraft and Engines Ltd under licence from Druine

First Flight:

1 January 1958

D.31 Turbulent:

26 - Rollason Aircraft and Engines Ltd

D.31A Turbulent:

3 - Rollason Aircraft and Engines Ltd

Type Specification

Applies to:

Rollason D.31 Turbulent

Type:

Single seat ultra light

Wing:

Low wing cantilever monoplane

Fuselage:

Flat sided fuselage with faired top skin

Tail Unit:

Cantilever tailplane with single fin and rudder

Landing Gear:

Divided type fixed undercarriage. Tailskid

Power Plant:

One 31 hp Rollason 4 CO2 4-cylinder air cooled piston engine in the nose driving a two bladed propeller

Accommodation:

Single seat for pilot in cockpit above the wing

Span:

21 ft 5 in

Length:

17 ft 4.5 in

Height:

Unknown

Wing Area:

Unknown

Tare:

349 lb

All-up:

620 lb

Max Speed:

93 mph

Preserved in British Museums

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