I am learning for an avionics exam and I cannot find any differences between the direct law and the mechanical backup.
I will describe the laws that I learned such that it is easier to see if I have some misconceptions.
- Normal law: Standard mode of operation
- Alternate law: (at least two failures detected):
- Loss of pitch and bank protection
- $\alpha$-protection and high-speed protection replaced by stabilities
- Load factor limitation is still active
- Direct law: (at least two failures second not self-detected)
- All protections lost
- Manual pitch trim
- Mechanical back-up: (all electric supply for control computers lost)
- All protections lost
- Manual pitch trim
Is the only difference between the direct law and the mechanical back-up that we do not have operating computers for control?