In Normal Law, which protections are provided?

• A. Angle of attack protection; Load factor protection; High-speed protection; Bank angle limits.
• B. Protections identical to Alternate Law.
• C. No protections.
• D. Only stall protection.

Answer: (A)

In Normal Law, the aircraft’s flight control system provides a set of protections that keep you within safe aerodynamic and structural limits. The protections include limiting the angle of attack to prevent entering a stall, limiting the load factor (g) to prevent overstressing the airframe, preventing the aircraft from overspeed by capping speed or guiding the attitude to stay within safe limits, and enforcing a bank angle limit to maintain controllability and margin in turns. Together, these protections form a protective envelope that helps the airplane respond safely to pilot inputs and abnormal conditions.