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Aviation History
1950
1950 - 0206.PDF
FLIGHT 2O JANUARY I950 Flight Stability Unimpaired hj This * SINGLE E1VGIME PERFOBMAIVCE Service Ceiling, Max. Continuous Pmver, Weight 33.500 lbs. . 11,150 ft (R/c-=0.02 'Vgo2 ft/min) Rate of Climb, Max. Continuous Power, Weight 33,500 lbs Sea Level 360 ft/m n 5,000 ft Altitude 300 ft/min Min. Runway Length, required by CAR Take-off, Sea Level, Weight 35.00U lbs 3,986 ft Landing, Sea Level. Weigb! .it,40o lj>s 3,180 ft Even if one engine becomes inoperative, the Scandia's stability and nianunivra- bility remain unimpaired. In fact the plane's single engine performance -.:" puts it in a class by itself. All pilots who have flown the Scandia are unanimous in praise of its remarkable flight characteristics. SVENSKA AEROPLAN AKTIEBOLAGET • SAAB AIRCRAFT COMPANY • SWEDEN
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