AIRBUS Dual RA fault & Flight control laws
Hi - Wondering if any Airbus experts can help me with the following:
When both RAD ALTS fail on the bus, I understand the flight control laws revert to direct law (flare law?) for landing.
My question is; on approach, when the gear is selected down and the AP turned off, and the 330 flight controls revert to FLARE LAW, will there be a "direct law" ECAM triggered ? (and subsequent approach/landing distance procedures).
I ask as I imagine it could pop up at a very inconvenient time during approach and would be much easier delt with prior to comencing an approach.
Any thoughts ?
Cheers.