CLIMBS AND CLIMBING TURNS
Description
A fundamental maneuver whereby the airplane changes attitude
from level to a climb attitude.
Objective
To develop the fundamental techniques required for increasing
altitude.
Elements
·
Clear the area
·
Choose forced landing area (always be aware of options)
·
Select outside references
·
Configure aircraft: pitch 5-10º above horizon then power
as necessary to maintain achieve either a normal or cruise climb (C172RG: 25” Hg, 2500 RPM, 90 KIAS), best angle of climb (VX)
(C172RG: 25” Hg, 2700 RPM, 67 KIAS) or best rate of
climb (VY) (C172RG: 25” Hg, 2500 RPM, 84 KIAS).
o
For turning climbs, bank at approx. 30º for new heading
·
Anticipate left-turning tendencies with sufficient rudder
pressure
·
Use outside references to maintain climb
·
Trim to maintain climb
·
Anticipate altitude (approx. 10% of climb rate), pitch for
level flight, adjust power and trim as necessary
o
For turning climbs, anticipate heading (approx. 50% of bank
angle)
·
Maintain ball centered
·
Look for traffic
Common Errors
·
Attempting to establish climb pitch attitude by referencing the
airspeed indicator, resulting in “chasing” the airspeed
·
Applying elevator pressure too aggressively, resulting in an
excessive climb angle
·
Applying elevator pressure too aggressively during level-off
resulting in negative “G” forces
·
Inadequate or inappropriate rudder pressure during climbing turns
·
Allowing the airplane to yaw in straight climbs, usually due to
inadequate right rudder pressure
·
Fixation on the nose during straight climbs, resulting in
climbing with one wing low
·
Failure to initiate a climbing turn properly with use of rudder
and elevators, resulting in little turn, but rather a climb with one wing low
·
Improper coordination resulting in a slip which counteracts the
effect of the climb, resulting in little or no altitude gain
·
Inability to keep pitch and bank attitude constant during
climbing turns
·
Attempting to exceed the airplane’s climb capability
References
FAA-H-8083-3A Airplane Flying Handbook p. 3-13