CHANDELLE
Description
A maximum performance 180º climbing turn.
Objective
To teach planning, orientation, division of attention and
control feel for maximum performance flight.
Elements
·
Clear the area
·
Choose forced landing area
·
Configure aircraft for maneuvering: ≤ VA with
propeller to full (C172RG: 18” Hg, 2500 RPM, 106 KIAS at MGW), gear up,
flaps up, cowl flaps open, altitude ≥1500’ AGL
·
Select outside references (off wingtip for 90º point)
·
Establish a coordinated 30° bank turn
·
Throttle to full (C172RG: 25” Hg, 2500 RPM)
·
Apply pitch to arrive at 90° reference point with max
desired pitch
·
Anticipate need for rudder pressure
·
Maintain pitch attitude once at 90º with increasing back
elevator pressure while reducing bank to 180º point
o
As aircraft slows, greater back elevator is required to maintain
pitch
·
At 180° point, roll wings level, (90º point is now off
opposite wing from the start), slightly above stall speed
o
Rolling out of a left chandelle requires more right rudder
pressure
o
Rolling out of a right chandelle requires little rudder pressure,
but will require right rudder pressure to maintain heading upon completion of
rollout
·
Gently reduce pitch to straight-and-level but maintain
altitude and build airspeed
·
Adjust throttle to maintain altitude
·
Maintain ball centered
·
Look for traffic
Easy way to remember the maneuver’s basics: “Bank and Yank”.
Can do this maneuver at cruise (C172RG: 18” Hg, 2300 RPM)
for constant-speed propellers, but should use maximum RPM for fixed-pitch
propellers (watch to not go into red line on tachometer).
Common Errors
·
Failure to adequately clear the area
·
Too shallow an initial bank, resulting in a stall
·
Too steep an initial bank, resulting in failure to gain maximum
performance
·
Allowing the actual bank to increase after establishing initial bank
angle
·
Failure to start the recovery at the 90° point in the turn
·
Allowing the pitch attitude to increase as the bank is rolled out
during the second 90° of turn
·
Removing all of the bank before the 180° point is reached
·
Nose low on recovery, resulting in too much airspeed
·
Control roughness
·
Poor coordination (slipping or skidding)
·
Stalling at any point during the maneuver
·
Execution of a steep turn instead of a climbing maneuver
·
Failure to scan for other aircraft
·
Attempting to perform the maneuver by instrument reference rather
than visual reference
References
FAA-H-8083-3A Airplane Flying Handbook p. 9-4