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Cessna 150

Vso………………49 mph               Total Fuel …………..26 gal

Vs………………..56 mph               Usable Fuel………….22.5 gal

Vx……………….52 mph                Min. Oil……………..4 qts

Vy……………….72 mph                Max. Oil……………..6 qts

Va……………….109 mph             Engine………………. CONT 0-200A

Vfe………………100 mph             Horse Pwr……………100 hp

Vno………………120 mph            Gross Wt……………..1600 lbs

Vne………………162 mph             Empty Wt…………….970 lbs

 Best Glide…………….65 mph 

N7734F

 BASIC EMPTY WEIGHT    1080.5 LBS

MOMENT                     35604.1 IN LBS

USEFUL LOAD                     519.5 LBS

GROSS WEIGHT                1600   LBS

N8317J

BASIC EMPTY WEIGHT     1072.5 LBS

MOMENT                     35867.05 IN LBS

USEFUL LOAD                      527.5 LBS

GROSS WEIGHT                 1600   LBS

MAX DEMONSTRATED CROSSWIND – 15mph

SHORT FIELD T.O. w/obstacle – NO FLAPS climb at Vx. The use of 10 degrees of flaps will reduce the takeoff roll but hinder the performance over the obstacle because of the minimum amount of excess thrust available for best angle of climb performance in the C150.