Vmbe again
As I understand it Vmbe is used as a factor to calculate the RTOM, but is it used as a factor for the Max landing mass? Is there a way of working out what the actual brake temperature would be on lets say an A320 at XX,000 kgs, XX kts GS, XX OAT, W/V XX/XX? If the details are put into the landing module of the FOVE and brake energy IS an issue, would there be a message for such a case? Any ideas?