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wind at 360 @26 G30 with a runway heading of 300 gives considerably more than 13kt crosswind component, closer to 24kts by my calculation. granted the demonstrated capability is not a limit, if the pilot believes he can demonstrate it better than the original test pilots Chester

i have stumbled across this forum whilst googling various things, i am tempted to do an add on commercial seaplane to my existing commercial rotorcraft but after reading this topic i felt i needed to post something in the spirit of helping anyone who needs advice or questions answered regarding...