SIPA S.90 Civil Aircraft Model Details

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General Information of SIPA S.90

First Flight : 17302

Introduction : 1948

Manufacturer : SIPA

National Origin : France

Number Built : 113

Primary Users : private owners; French aero clubs

Produced : 1948 - early 1950s

Role : Personal and trainer aircraft

General characteristics of SIPA S.90

Capacity : one passenger

Crew : one

Empty Weight : 807 lb (366 kg)

Height : 5 ft 9 in (1.75 m)

Length : 18 ft 10 in (5.74 m)

Max Takeoff Weight : 1,323 lb (600 kg)

Powerplant : 1 × Continental C85-12F, 85 hp (64 kW)

Propellers : 1 prop, 1 per engine

Useful Load : 516 lb (234 kg)

Wingspan : 28 ft 8 in (8.74 m)

Performance of SIPA S.90

Cruise Speed : 120 mph (104 kt) 194

Maximum Speed : 134 mph (117 kt) 217 km/h

Power/Mass : 15.6 lb/hp (0.11 kW/kg)

Range : 315 miles (273 nm)510 km

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