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Section IV page 19 of the "Alon Aircoupe Flight Manual
Model A2" states"
The maximum crosswind component in which the aeroplane has
been demonstrated to be safe for take-off and landing is 20 knots at a height of
10 meters.
Cheers:
Paul
NC2273H
For the BFR in my A2A, one of the questions is: "What is the maximum demonstrated crosswind component for the acft?" The POH makes no reference to the x-wind component.
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