C100-S Chase-Sisley   

General Details
Manufacturer: Chase-Sisley
Plane Name:


Classified as: Unclassified
Country Of Origin: U S A
Designer: Robert Chase
No. of Seats 1
No. Built 1
L/DMax: 38 88 kph/ 46 kt/ 55 mph
MinSink: 0.61 m/s / 2.0 fps / 1.18 kt


Span Area Empty Weight Payload Gross Weight Wing Load Water Ballast
m ft sq.m sq.ft kg lb. kg lb. kg lb. kg
kg lb.
16.76 55 12.82 138 240 530 91 200 331 730 25.82 5.3 0 0
Aspect ratio: 22
Airfoil: NACA 4(3)-165
Structure: aluminum, fiberglass, wood

The C100-S made its first flight in 1968. It uses a 3-piece wing with an airfoil 15% thick and no aerodynamic twist. Wood and Styrofoam are used in the construction of the wing ( as well as the tail), but the entire surface and the stress- bearing material is fiberglass. The fuselage is of all-metal stress-skin construction, with a skid and fixed wheel.


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