Will AGCAS activate with the landing gear down?

Will AGCAS activate with the landing gear down?

• A. Yes, it will activate
• B. No, it will not activate
• C. It activates intermittently
• D. Activation depends on altitude

Answer: (B)

The correct response, indicating that AGCAS (Automatic Ground Collision Avoidance System) will not activate with the landing gear down, aligns with how AGCAS is designed to function. The primary purpose of AGCAS is to prevent potential ground collisions during flight. Typically, AGCAS is programmed to engage under certain operational conditions associated with airborne scenarios, often prioritizing safety during flight maneuvers that could lead to an unintentional descent towards the ground. When the landing gear is deployed, the aircraft is likely already in preparation for landing, which somewhat negates the risk factors AGCAS is intended to mitigate. In a landing configuration, such as having the landing gear down, the aircraft is transitioning to a safe and controlled descent and is unlikely to experience a scenario where AGCAS would need to intervene. Therefore, the system is deactivated to avoid unnecessary alerts or interventions during this phase of flight. The other options suggest varying scenarios in which AGCAS might activate, but these do not accurately reflect the aircraft's operational design and the specific functionality of the AGCAS system during landing phases.

The correct response, indicating that AGCAS (Automatic Ground Collision Avoidance System) will not activate with the landing gear down, aligns with how AGCAS is designed to function. The primary purpose of AGCAS is to prevent potential ground collisions during flight.

Typically, AGCAS is programmed to engage under certain operational conditions associated with airborne scenarios, often prioritizing safety during flight maneuvers that could lead to an unintentional descent towards the ground. When the landing gear is deployed, the aircraft is likely already in preparation for landing, which somewhat negates the risk factors AGCAS is intended to mitigate.

In a landing configuration, such as having the landing gear down, the aircraft is transitioning to a safe and controlled descent and is unlikely to experience a scenario where AGCAS would need to intervene. Therefore, the system is deactivated to avoid unnecessary alerts or interventions during this phase of flight.

The other options suggest varying scenarios in which AGCAS might activate, but these do not accurately reflect the aircraft's operational design and the specific functionality of the AGCAS system during landing phases.