General Aircraft ST-25 Aircraft

Production Details

Design Company:

General Aircraft Ltd, Hanworth

First Flight:

19 June 1935

ST-25 Jubilee:

30 - General Aircraft Ltd, Hanworth

ST-25 De Luxe:

1 - General Aircraft Ltd, Hanworth (converted from Jubilee)

ST-25 Universal:

29 - General Aircraft Ltd, Hanworth (1 converted from De Luxe)

Type Specification

Applies to:

General Aircraft ST-25 Jubilee

Type:

Five seat cabin monoplane

Wing:

Low wing cantilever monoplane. Metal structure with single spar with fabric covering

Fuselage:

Metal structure with fabric covering

Tail Unit:

Fixed tailplane at base of fin. Universal has twin fins

Landing Gear:

Fixed divided type. Main gear below engines with axle to fuselage. Tail wheel

Power Plant:

Two 90 hp Pobjoy Niagara II engines mounted on the wing

Accommodation:

Five seats in enclosed cabin

Span:

40 ft 2 in

Length:

26 ft 4 in

Height:

7 ft 10 in

Wing Area:

217 sq ft

Tare:

1,680 lb

All-up:

2,875 lb

Max Speed:

142 mph

Initial Climb:

800 ft/min

Ceiling:

16,000 ft

Range:

585 miles

Preserved in British Museums

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