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...