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Under some conditions, engine roughness may occur while operating
at best economy. If this occurs, enrich mixture as required to smooth
engine operation. Any change in altitude or Power Lever position will
require a recheck of EGT indication.
Mixture Description Exhaust Gas Temperature
Best Power 75° F Rich Of Peak EGT
Best Economy 50° F Lean Of Peak EGT
March 2010
Information Manual 4-21
Cirrus Design Section 4
SR20 Normal Procedures
Descent
1. Altimeter................................................................................... SET
2. Cabin Heat/Defrost ................................................ AS REQUIRED
3. Landing Light .............................................................................ON
4. Fuel System....................................................................... CHECK
5. Mixture ................................................................... AS REQUIRED
6. Brake Pressure .................................................................. CHECK
Before Landing
1. Seat Belt and Shoulder Harness .....................................SECURE
2. Fuel Pump ......................................................................... BOOST
3. Mixture ......................................................................... FULL RICH
4. Flaps ...................................................................... AS REQUIRED
5. Autopilot ................................................................. AS REQUIRED
Landing
• Caution •
Landings should be made with full flaps. Landings with less
than full flaps are recommended only if the flaps fail to deploy
or to extend the aircraft’s glide distance due to engine
malfunction. Landings with flaps at 50% or 0%; power should
be used to achieve a normal glidepath and low descent rate.
Flare should be minimized.
Normal Landing
Normal landings are made with full flaps with power on or off. Surface
winds and air turbulence are usually the primary factors in determining
the most comfortable approach speeds.
Actual touchdown should be made with power off and on the main
wheels first to reduce the landing speed and subsequent need for
braking. Gently lower the nose wheel to the runway after airplane
speed has diminished. This is especially important for rough or soft
field landings.
March 2010
4-22 Information Manual
Section 4 Cirrus Design
Normal Procedures SR20
Short Field Landing
For a short field landing in smooth air conditions, make an approach at
75 KIAS with full flaps using enough power to control the glide path
(slightly higher approach speeds should be used under turbulent air
conditions). After all approach obstacles are cleared, progressively
reduce power and maintain the approach speed by lowering the nose
of the airplane. Touchdown should be made power-off and on the main
wheels first. Immediately after touchdown, lower the nose wheel and
apply braking as required. For maximum brake effectiveness, retract
the flaps, hold the control yoke full back, and apply maximum brake
pressure without skidding.
Crosswind Landing
Normal crosswind landings are made with full flaps. Avoid prolonged
slips. After touchdown, hold a straight course with rudder and brakes
as required.
The maximum allowable crosswind velocity is dependent upon pilot
capability as well as aircraft limitations. Operation in direct crosswinds
of 21 knots has been demonstrated.
Balked Landing/Go-Around
In a balked landing (go-around) climb, disengage autopilot, apply full
power, then reduce the flap setting to 50%. If obstacles must be
cleared during the go-around, climb at the best angle of climb with
50% flaps. After clearing any obstacles, retract the flaps and
accelerate to the normal flaps-up climb speed.
1. Autopilot .....................................................................DISENGAGE
2. Power Lever ........................................................FULL FORWARD
3. Flaps ........................................................................................50%
4. Airspeed.........................BEST ANGLE OF CLIMB (81 – 83 KIAS)
After clear of obstacles:
5. Flaps .........................................................................................UP
March 2010
Information Manual 4-23
Cirrus Design Section 4
SR20 Normal Procedures
After Landing
1. Power Lever ................................................................... 1000 RPM
2. Fuel Pump ...............................................................................OFF
3. Flaps ..........................................................................................UP
　
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