hueyracer wrote:
Whn reaching the ACA-does this not mean that from thisnaltitude on, the approach is no longer asymetrical?
No - that would only be true if the approach was continued at idle power on the remaining engine. Which is highly unlikely.
DA simply
cannot be below ACA. If the aircraft has a published ACA, then it must also have an EOA so that DA will always be above the ACA.