Which flight control protection is available in alternate law?

In alternate law, certain flight control protections are indeed retained, and load factor protection is one of them. This protection serves to prevent the aircraft from exceeding its structural limits during maneuvers. Essentially, if a pilot exceeds a predefined load factor, the flight control laws will intervene to help prevent any potential structural damage to the aircraft.

Load factor protection in alternate law is important for ensuring the safety of the aircraft during critical flight phases, allowing the aircraft to limit its load and maintain control without reaching dangerous conditions. On the other hand, high angle of attack protection and roll protection are typically disabled or not available in alternate law. This is significant, as it emphasizes the limitations that come into play when the aircraft reverts to this mode due to certain failures or abnormal conditions.

In summary, load factor protection is a feature retained even when operating under alternate law, contributing to the overall safety and performance of the aircraft during certain flight conditions.