A320 G+B HYD LG extension
Hello folks,
apologies if this has been discussed before but couldn't find the specific reference. In the above mentioned failure the procedure is to extend the gear at 200 kias in order to revert to direct law to enhance controllability due to the single elevator remaining. Question here : Why 200 kias ? On the A330 that's the limit speed to get the gear down by gravity, but there's nothing specified for the A320.
Thanks !