Steep turns show the relationship between the “rate and radius” of a turn (the faster the rate, the smaller the radius); an airplane’s inherent overbanking tendency (which requires some amount of aileron pressure against the bank); variations in the horizontal and vertical components of lift; and how increases in load factor and angle of attack also raise an airplane’s stall speed. A level 60-degree-bank turn, for example, doubles an airplane’s load factor (to 2 Gs) and raises its stall speed to 70 knots from 50 knots at 1 G.
Steep turn success on a checkride requires maintaining the desired bank angle (plus or minus 5 degrees); maintaining the desired airspeed (plus or minus 10 knots), and rolling out on the desired heading (plus or minus 10 degrees).
Be prepared to discuss:
Overbanking tendency: The faster-moving outside wing provides more lift during a steep turn and tends to increase bank angle.
Rate and radius: The faster the rate of turn, the smaller its radius.
Maneuvering speed and the effect of aircraft weight: Maneuvering speed is highest at an airplane’s maximum gross weight. Light weight results in a lower maneuvering speed.
Load factor and accelerated stalls: A constant-altitude turn with 45 degrees of bank imposes 1.4 Gs, and a turn with 60 degrees of bank imposes 2 Gs. Stall speed increases with the square root of the load factor, so an airplane that stalls at 50 knots in unaccelerated, level flight will stall at 70 knots at 2 Gs. The margin between maneuvering speed and stall speed is sharply reduced during steep turns (and may disappear completely).
Helpful hints: