On climb out, what torque will the lead set, and at what KIAS will they climb?

On climb out, what torque will the lead set, and at what KIAS will they climb?

• A. 70% torque and 150 KIAS
• B. 75% torque and 155 KIAS
• C. 80% torque and 160 KIAS
• D. 85% torque and 165 KIAS

Answer: (C)

The correct answer indicates that during the climb-out phase, the lead will set torque at 80% and maintain a climb speed of 160 KIAS. This value is in line with standard operating practices for the aircraft during initial climb, where efficiency and rate of climb are prioritized. The choice of 80% torque effectively balances the need for performance with engine management, allowing the aircraft to gain altitude efficiently while maintaining an optimal airspeed. Achieving a climb speed of 160 KIAS is appropriate in this scenario, as it ensures that the aircraft is in a good performance regime, allowing for a safe and effective ascent. Climbing at this speed offers a good compromise between rate of climb and drag, which is crucial during the early stages of flight when altitude clearance and aircraft handling are critical. The other choices suggest torque and speeds that either exceed typical operating parameters or do not align with the climb-out profiles that are commonly adhered to in flight operations. This helps reinforce the rationale behind selecting 80% torque and 160 KIAS as the best performance setting for the climb-out phase.

The correct answer indicates that during the climb-out phase, the lead will set torque at 80% and maintain a climb speed of 160 KIAS. This value is in line with standard operating practices for the aircraft during initial climb, where efficiency and rate of climb are prioritized. The choice of 80% torque effectively balances the need for performance with engine management, allowing the aircraft to gain altitude efficiently while maintaining an optimal airspeed.

Achieving a climb speed of 160 KIAS is appropriate in this scenario, as it ensures that the aircraft is in a good performance regime, allowing for a safe and effective ascent. Climbing at this speed offers a good compromise between rate of climb and drag, which is crucial during the early stages of flight when altitude clearance and aircraft handling are critical.

The other choices suggest torque and speeds that either exceed typical operating parameters or do not align with the climb-out profiles that are commonly adhered to in flight operations. This helps reinforce the rationale behind selecting 80% torque and 160 KIAS as the best performance setting for the climb-out phase.