Flight Controls

Question 0

High level functions for yaw

Answer 0

Gain on airspeed
Asymmetrical thrust compensation
Yaw dampener
Turn co-ordination

Question 1

High level functions for pitch

Answer 1

Gain on airspeed
Elevator thrust compensation
AOA limiting

Question 2

What happens to the flight controls when the RAT is the only AC power source?

Answer 2

Pitch trim is 1/2 speed
Flaps are 1/2 speed
Flaps are limited to flaps 3

Hyd system 3 accumulater is the power source from rat deployment till AC ESS bus powers ACMP 3a