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(slightly higher approach speeds should be used under turbulent air
conditions). After all approach obstacles are cleared, progressively
reduce power to reach idle just before touchdown 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 20 knots has been demonstrated.
June 2007
4-22 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
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 75-80 KIAS 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....................................................................... 75-80 KIAS
After clear of obstacles:
5. Flaps .........................................................................................UP
After Landing
1. Power Lever ...................................................................1000 RPM
2. Fuel Pump................................................................................OFF
3. Flaps ..........................................................................................UP
4. Transponder .......................................................................... STBY
5. Lights ..................................................................... AS REQUIRED
6. Pitot Heat .................................................................................OFF
• Note •
As the airplane slows the rudder becomes less effective and
taxiing is accomplished using differential braking.
June 2007
Information Manual 4-23
Cirrus Design Section 4
SR22 Normal Procedures
Shutdown
1. Fuel Pump (if used) ................................................................OFF
2. Throttle.................................................................................... IDLE
3. Ignition Switch.....................................................................CYCLE
• Caution •
Note that the engine hesitates as the switch cycles through
the "OFF" position. If the engine does not hesitate, one or both
magnetos are not grounded. Prominently mark the propeller
as being "Hot," and contact maintenance personnel
immediately
4. Mixture ..............................................................................CUTOFF
5. All Switches .............................................................................OFF
6. Magnetos .................................................................................OFF
7. ELT........................................................... TRANSMIT LIGHT OUT
• Note •
After a hard landing, the ELT may activate. If this is suspected,
press the RESET button.
8. Chocks, Tie-downs, Pitot Covers ........................... AS REQUIRED
June 2007
4-24 Information Manual
Section 4 Cirrus Design
Normal Procedures SR22
Stalls
SR22 stall characteristics are conventional. Power-off stalls may be
accompanied by a slight nose bobbing if full aft stick is held. Power-on
stalls are marked by a high sink rate at full aft stick. Power-off stall
speeds at maximum weight for both forward and aft C.G. positions are
presented in Section 5 - Performance Data.
When practicing stalls at altitude, as the airspeed is slowly reduced,
you will notice a slight airframe buffet and hear the stall speed warning
horn sound between 5 and 10 knots before the stall. Normally, the stall
is marked by a gentle nose drop and the wings can easily be held level
or in the bank with coordinated use of the ailerons and rudder. Upon
stall warning in flight, recovery is accomplished by immediately by
reducing back pressure to maintain safe airspeed, adding power if
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(32)
