Originally Posted by AZR
I was unable to find any credible document indicating that the stick free longitudinal behavior is different in Alternate law versus Normal law.
FCOM 1.27.30 Reconfiguration control laws:
Alt 1/2; Pitch control,
Flight mode:
Flight law is a load factor demand law, similar to normal law, with limited pitch rate feedback and gains, ...
Flare mode:
Flare law is identical to normal flare law
As I read this, alternate law pitch control is not identical to normal law.