The maximum fuel imbalance permitted for landing is:

The maximum fuel imbalance permitted for landing is:

• A. 100 pounds
• B. 300 pounds
• C. 200 pounds
• D. 500 pounds

Answer: (B)

Fuel balance between the left and right wing tanks directly affects lateral stability and controllability during landing. A heavier wing on one side creates a roll moment that the pilot must counter with aileron input, and it can also influence yaw and handling sensitivity when the aircraft is in the slow, high-drag landing configuration. For the Beechjet 400A, the maximum fuel imbalance allowed for landing is 300 pounds. This limit helps ensure the aircraft remains controllable and that the center of gravity stays within safe limits during the critical flare and touchdown phase. If the imbalance is greater than this, fuel should be transferred between wing tanks using the crossfeed to bring it within the allowable range prior to landing. Smaller imbalances are acceptable, but 300 pounds is the upper boundary for a safe landing.

Fuel balance between the left and right wing tanks directly affects lateral stability and controllability during landing. A heavier wing on one side creates a roll moment that the pilot must counter with aileron input, and it can also influence yaw and handling sensitivity when the aircraft is in the slow, high-drag landing configuration.

For the Beechjet 400A, the maximum fuel imbalance allowed for landing is 300 pounds. This limit helps ensure the aircraft remains controllable and that the center of gravity stays within safe limits during the critical flare and touchdown phase. If the imbalance is greater than this, fuel should be transferred between wing tanks using the crossfeed to bring it within the allowable range prior to landing. Smaller imbalances are acceptable, but 300 pounds is the upper boundary for a safe landing.