During hover and transition flight below 80 KIAS, the torque limitation is set at __% torque.

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Multiple Choice

During hover and transition flight below 80 KIAS, the torque limitation is set at __% torque.

Explanation:
In hover and slow flight (below 80 KIAS) the helicopter requires near-maximum power to stay aloft, so the torque limit is set with a safety buffer. Limiting torque to 95% keeps a five-percent margin before the 100% cap, providing room to absorb gusts, transient control inputs, and governor lag without hitting the hard torque limit. This protects the engine, drivetrain, and rotor system from over-torque during these high-demand, low-speed conditions. The other numbers would either be too restrictive for a stable hover or not provide the necessary headroom for unpredictable gusts and maneuvers.

In hover and slow flight (below 80 KIAS) the helicopter requires near-maximum power to stay aloft, so the torque limit is set with a safety buffer. Limiting torque to 95% keeps a five-percent margin before the 100% cap, providing room to absorb gusts, transient control inputs, and governor lag without hitting the hard torque limit. This protects the engine, drivetrain, and rotor system from over-torque during these high-demand, low-speed conditions. The other numbers would either be too restrictive for a stable hover or not provide the necessary headroom for unpredictable gusts and maneuvers.

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