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If the power lever is stuck at or near the idle position and straight and
level flight cannot be maintained, establish glide and perform the
Forced Landing checklist.
1. Power Lever Movement......................................................VERIFY
2. Power ............................................................................ SET if able
3. Flaps ........................................................................SET if needed
4. Mixture ..................................... AS REQUIRED (full rich to cut-off)
5. Land as soon as possible.
Original Issue: 01-20-09
P/N 13772-142 9 of 14
Cirrus Design Section 9
SR22 Supplements
Section 3A - Abnormal Procedures
Inadvertent Icing Encounter
Flight into known icing conditions is prohibited. However, if icing is
inadvertently encountered:
1. Pitot Heat ...................................................................................ON
2. Exit icing conditions. Turn back or change altitude.
3. Cabin Heat .....................................................................MAXIMUM
4. Windshield Defrost...................................................... FULL OPEN
5. Alternate Induction Air ...............................................................ON
6. Landing Configuration................................................. FLAPS 50%
7. Airspeed......................................................................90 - 95 KIAS
Landing without Aileron Control
1. Control Yoke................................................... ATTEMPT TO FREE
Clasp both hands around the control yoke and twist right and left
in a strong, steady, and continuous motion.
2. If no aileron control:
a. Maintain roll control using smooth rudder pedal inputs.
b. Maximum Bank Angle ..........................DO NOT EXCEED 20°
c. Maximum Landing Crosswind .................................10 KNOTS
d. Landing Configuration .......................................... FLAPS 50%
e. Airspeed ...............................................................90 - 95 KIAS
Original Issue: 01-20-09
10 of 14 P/N 13772-142
Section 9 Cirrus Design
Supplements SR22
Landing without Rudder Control
1. Rudder Pedals ...............................................ATTEMPT TO FREE
Place feet on rudder pedals and push right and left pedals in a
strong, steady, and continuous motion.
2. If no rudder control:
a. Maintain directional control using smooth aileron inputs.
b. Maximum Bank Angle...........................DO NOT EXCEED 20°
c. Maximum Landing Crosswind..................................10 KNOTS
d. Landing Configuration .......................................... FLAPS 50%
e. Airspeed .............................................................. 90 - 95 KIAS
Original Issue: 01-20-09
P/N 13772-142 11 of 14
Cirrus Design Section 9
SR22 Supplements
Section 4 - Normal Procedures
Before Starting Engine
1. Preflight Inspection ...................................................COMPLETED
• WARNING •
Ensure that the airplane is properly loaded and within the
AFM’s weight and balance limitations prior to takeoff.
2. Weight and Balance............................................Verify within limits
3. Emergency Equipment ................................................ON BOARD
4. Passengers ..................................................................... BRIEFED
• Note •
Ensure all the passengers have been fully briefed on smoking,
the use of the seat belts, doors, emergency exits, egress
hammer, and CAPS.
Additionally, ensure all passengers have been briefed not to
touch and/or obstruct the control yokes or rudder pedals. The
pilot will demonstrate the full-extension of the controls so that
the passenger will understand needed clearances.
Verify CAPS handle safety pin is removed.
5. Passenger Door ..............................................................LATCHED
• Note •
From outside of aircraft verify both top and bottom latch of
door is securely latched. Press firmly at each door latch
position to ensure the security of door.
6. Seats, Seat Belts, and Harnesses ................ADJUST & SECURE
• Caution •
Crew seats must be locked in position and control handles
fully down before flight. Ensure seat belt harnesses are not
twisted.
Original Issue: 01-20-09
12 of 14 P/N 13772-142
Section 9 Cirrus Design
Supplements SR22
Section 5 - Performance Data
Length Conversion
Meters Feet
200 656
400 1312
600 1969
800 2625
1000 3281
1200 3937
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