Someone knows if this memo is translated into english?
From the available documentation: (AMM FMGEC / EFCS)
AP Operational Conditions:
(2) AP engagement inhibition and disengagement logics
(a) Pitch and roll angle limits
- Roll angle
. AP engagement is inhibited when abs(phi) > 40°
. AP is automatically disengaged when abs(phi) > 45°.
- Pitch angle
. AP engagement is inhibited when theta < -10° or theta > +22°
. AP is automatically disengaged when theta < -13° or theta > 25°.
(b) AP engagement is inhibited in flight when CAS < VLS or CAS > (VMO/MMO or VLE/VFE).
(c) AP engagement is inhibited when the FMGEC receives the "pitch angle protection active" information from the FCPC.