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JUNGSTER II

STANDARD DATA: Gross wt. 1,375. Empty wt. 739. Fuel capacity 16. Wingspan 22’4″. Length 16’11”. PERFORMANCE: Top mph 170. Cruise mph 148. Stall mph 5. Climb rate 3,500. Takeoff run…

ODEA Developer
STANDARD DATA: Gross wt. 1,375. Empty wt. 739. Fuel capacity 16. Wingspan 22'4". Length 16'11".
PERFORMANCE: Top mph 170. Cruise mph 148. Stall mph 5. Climb rate 3,500. Takeoff run 200. Landing roll 800.

The Jungster II is a follow-up design that grew out of experience with the Jungster I. The intent was to create a plane with the same open-cockpit concept, but to increase speed and capacity so that it would be an acceptable cross-country airplane. The Jungster II uses the same design and construction concepts, except that it is just a little bit bigger, has a single extended parasol-type wing, and uses a welded steel-tube center section. Engines rated from 85 to 180 hp are used. Plans are no longer available.

ODEA DeveloperWriter
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