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Report 601
Basic Airplane Data for Meyers Model 200
CAUTION
This report was subsequently modified. DO NOT USE IT FOR CONTROL SURFACE
TRAVELS!! Use the official FAA Type Certificate Data Sheets found in the general section of the site.
Specifically, the flap, rudder and elevator trim travels are INCORRECT in this early report.
The wing angles of incidence, airfoils, dihedral, washout and chord lines are correct.
I believe the angle of incidence of the horizontal stabilizer (1.5 deg) is correct.
This is the only reference I can find to that angle. I'll post when I can confirm.
Paul M. Whetstone, President
Email pwhetstone@meyersaircraft.com
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