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 | | I should point out that because with a canard aircraft both surfaces are lifting wings (the canard actually has a much greater wing loading than the main wing) their size, position, interference with each other, high lift devices, etc., have a very important effect on the cg range, the flying qualities, and low speed performance. |
 | | Part one (fuselage, canard, inboard wing, vertical stabs, control system, and landing gear) should be ready by March or April and will include drawing changes to use the larger AN 220-2 control system pulleys which are much easier to obtain than those shown in the plans. |
 | | The rudders are supposed to be attached to the elevators - not the wings. |
| cozybuilders.org /ref_info/Canard_Pusher/CPs_1_to_82_Sections.txt (20146 words) |
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