If the Secondary Flight Control Computers are in command, the airplane is in which Law?

When the Secondary Flight Control Computers are in command, the airplane is operating in Direct Laws. This mode provides the pilots with direct control of the aircraft's flight surfaces without the usual protections and limitations present in the other flight envelope protections designed to enhance safety and structural integrity during flight.

In Direct Laws, commands are directly transferred to the control surfaces with minimal computer intervention, which allows for more responsive handling characteristics. While this can be advantageous for certain maneuvers, it also means that the automatic protections against excessive angles of attack or stalls are not available. This state typically occurs when there are failures in the primary flight control computers or during certain phases of flight where manual control is preferred.

The other options represent different levels of handling and protection. Normal Laws provide the highest degree of automatic protections against stalling and excessive maneuvers. Alternate Laws may offer limited protections but with some level of computer control. Emergency Laws engage when the system detects a critical failure, but they are intended as a last-resort operation mode.