Cirrus SR20 Flight Operations Manual page 47

Cirrus SR20 and SR22
Section 3
the control yoke sufficient to rotate the aircraft. Pitch the aircraft for
approximately 7º to intercept V
coordination with proper rudder input during the climb out.
1. Brakes..................................................Release (steer with rudder)
Initially, a slight amount of differential braking may be required for
directional control. As airspeed increases, both feet should be
removed from toe brakes and directional control maintained with
rudder inputs.
2. Power Lever ........................................................ FULL FORWARD
Smoothly increase power lever full forward for maximum takeoff
power. Do not confuse any detents for a full power setting. Engine
speed should be approximately 2700 RPM. Discontinue takeoff if
any rough or sluggish acceleration is noted.
3. Engine Parameters ............................................................ CHECK
Monitor engine parameters during the takeoff roll. If any abnormal
or questionable indications arise, abort the takeoff early in the
takeoff roll.
4. Elevator Control ....................................... ROTATE Smoothly at V
As airspeed approaches V
pressure to the control yoke to increase the angle of attack
sufficient to rotate the aircraft.
V (SR20) 65 KIAS
R
V (SR22) 70-73 KIAS
R
5. Flaps .......................................................................................... UP
Retract the flaps after the following conditions have been met.
Slight back pressure may be required after flap retraction
• SR20 - 85 KIAS,
• SR22 - 80 KIAS,
• Positive rate of climb,
• Clear of terrain and obstacles.
P/N 23020-002
June 2008
Standard Operating Procedures
or V as appropriate. Maintain
X Y
, smoothly and gradually apply back
R
Flight Operations Manual
R
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