GENERAL AIRCRAFT MONOSPAR ST-25 Civil Aircraft Model Details

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General Information of GENERAL AIRCRAFT MONOSPAR ST-25

Developed From : General Aircraft Monospar ST-10

First Flight : 12954

Manufacturer : General Aircraft Ltd, Hanworth

National Origin : United Kingdom

Number Built : 60

Produced : 1935-1939

General characteristics of GENERAL AIRCRAFT MONOSPAR ST-25

Crew : 1

Empty Weight : 1,680 lb (762 kg)

Gross Weight : 2,875 lb (1,304 kg)

Height : 7 ft 10 in (2.39 m)

Length : 26 ft 4 in (8.03 m)

Powerplant : 2 × Pobjoy Niagara II 7-cyl. air-cooled radial piston engine, 90 hp (67 kW) each

Wing Area : 217 sq ft (20.2 m2)

Wingspan : 40 ft 2 in (12.24 m)

Performance of GENERAL AIRCRAFT MONOSPAR ST-25

Maximum Speed : 142mph (229km/h; 123kn)

Range : 585mi (508nmi; 941km)

Rate Of Climb : 800ft/min (4.1m/s)

Service Ceiling : 16,000ft (4,877m)

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