What is the procedure for an engine failure at takeoff in the Pilatus PC-12 NG?

The procedure for an engine failure at takeoff in the Pilatus PC-12 NG emphasizes the importance of maintaining control of the aircraft, which is critical during such an emergency. Upon recognizing an engine failure, the pilot must immediately pitch for best glide speed to optimize the aircraft's performance and reduce the likelihood of stall. This action maximizes the aircraft's lift-to-drag ratio, allowing the pilot to maintain control longer and make informed decisions regarding the landing approach.

Landing straight ahead is a prudent strategy because it avoids unnecessary turns that could lead to further loss of altitude or control. In the event of engine failure shortly after takeoff, the options for landing become limited, and a straight-ahead approach is often the safest route.

Continuing to gain altitude or troubleshooting during an engine failure can be dangerous because it may lead to a further loss of control and reduce the chances of landing safely. Similarly, performing a controlled descent or executing a roll maneuver would not address the immediate need for controlled flight and safe landing. Therefore, prioritizing control, pitching for best glide speed, and planning for a landing straight ahead are essential steps in ensuring a successful outcome in the event of an engine failure at takeoff.