Describe effects on aircraft performance during a turn.

Description should include the following:

Applying aileron pressure is necessary to place the aircraft in the desired angle of bank, while simultaneous application of rudder pressure is necessary to counteract the resultant adverse yaw.
Because more lift is required during a turn than during straight-and-level flight, the AOA must be increased by applying elevator back pressure. The steeper the turn, the more elevator back pressure is needed.

PLT164

Process/Skill Questions: