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Calculate pivotal altitude prior to flight, (PA=Ground speed squared divided by 11.3)
1. Clearing turns
2. Increase to 90 KIAS
3. Select suitable reference points(“pylons”) and position the aircraft so the
maneuver can be entered on a heading 45 degrees to downwind.
4. When the pylon passes below the wing, smoothly roll into a turn using
coordinated aileron and rudder so that the pylon maintains a constant
position relative to the wingtip.
5. As the turn around the pylon progresses, make pitch changes to compensate for
variations in ground speed and maintain the pylons position relative to the wingtip.
a. Pylon forward- control forward- reduce bank
b. Pylon rearward- control rearward- increase bank.
Accelerated Stall Maneuver
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