What is the maximum allowable takeoff weight stated for the aircraft in pounds?

The correct choice reflects the specific operational limitations outlined for the aircraft, which is crucial for ensuring the safety and performance during flight operations. The maximum allowable takeoff weight is a critical parameter that ensures the aircraft can safely ascend, maintain control, and land effectively. In this case, the stated maximum allowable takeoff weight of 10,450 lbs ensures that the aircraft remains within its structural and aerodynamic limits.

This weight considers the design specifications of the aircraft, including factors such as engine performance, wing loading, and other aerodynamic characteristics. Operating within this limit helps prevent issues like reduced climb performance or potential structural failure during flight. Knowing and adhering to the maximum allowable takeoff weight is essential for compliance with regulations, such as those outlined in Part 135 operations, which govern commercial flying and require strict adherence to operational limitations.

Maintaining awareness of these limits is vital for flight crews to ensure both safety and regulatory compliance, making the choice of 10,450 lbs the appropriate answer based on the aircraft's approved specifications.