Crosswind Limitations for Take-off
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Crosswind Limitations for Take-off
Hi hoping someone can help.
In my 737 800W Performance Manual (preamble) it mentions - Do not use corrected Stab Trim values (i.e., Flaps and Thrust adjustment table on Loadsheet) to determine if CofG ≤ 25%.
Why is this necessary?
Thanks
In my 737 800W Performance Manual (preamble) it mentions - Do not use corrected Stab Trim values (i.e., Flaps and Thrust adjustment table on Loadsheet) to determine if CofG ≤ 25%.
Why is this necessary?
Thanks
