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loss of attitude data occurs, refer to the mechanical standby
instruments (attitude, heading) and perform the following procedure:
1. Standby Instruments (attitude, heading) ........................MONITOR
If failure occurs while flying in IMC:
2. Autopilot GPSS Mode .................................................... ACTIVATE
3. Autopilot Altitude Hold.................................................... ACTIVATE
4. Exit IMC.
• WARNING •
Aircraft equipped with Software Version 530-00123-000 Rev
00 or higher; Any power interruption to the PFD will result in
June 2007
Information Manual 3-27
Cirrus Design Section 3
SR22 Emergency Procedures
loss of attitude information until the PFD can be restarted on
the ground.
Aircraft equipped with Software Version 530-00159-000 Rev
00 or higher; When subjected to a power loss of less than 20
seconds, the PFD is capable of performing a warm start. In
this event, a “PLEASE STANDBY” message will be displayed
for 2 seconds followed by a “ATTEMPTING QUICK RESTART”
message. In the event of a power loss greater than 20
seconds, a warm start is unlikely, and the power interruption
will result in loss of attitude information until the PFD can be
restarted on the ground.
Power Lever Linkage Failure
If the Power Lever linkage fails in flight, the engine will not respond to
power lever control movements. Use power available and flaps as
required to safely land the airplane.
If the power lever is stuck at or near the full power position, proceed to
a suitable airfield. Fly a forced landing pattern. With landing assured,
shut down engine by moving mixture control full aft to CUTOFF. If
power is needed again, return mixture control to full RICH and regain
safe pattern parameters or go-around. If airspeed cannot be
controlled, shut engine down and perform the Forced Landing
checklist. After landing, bring the airplane to a stop and complete the
Emergency Engine Shutdown on Ground checklist.
If the power lever is stuck at or near the idle position and straight and
level flight cannot be maintained, establish glide to a suitable landing
surface. Fly a forced landing pattern.
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.
June 2007
3-28 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR22
June 2007
Intentionally Left Blank
Information Manual 3A-1
Cirrus Design Section 3A
SR22 Abnormal Procedures
Section 3A
Abnormal Procedures
Table of Contents
Introduction .................................................................................. 3A-3
Abnormal Procedures Guidance.................................................. 3A-4
Ground Procedures...................................................................... 3A-5
Brake Failure During Taxi ......................................................... 3A-5
Aborted Takeoff ........................................................................ 3A-5
In-Flight Procedures..................................................................... 3A-6
Inadvertent Icing Encounter ...................................................... 3A-6
Inadvertent IMC Encounter....................................................... 3A-6
Door Open In Flight .................................................................. 3A-6
Landing Procedures..................................................................... 3A-7
Landing With Failed Brakes...................................................... 3A-7
Landing With Flat Tire............................................................... 3A-7
System Malfunctions.................................................................... 3A-9
Alternator Failure ...................................................................... 3A-9
Engine Indicating System Failure ........................................... 3A-11
LOW VOLTS Warning Light Illuminated ................................. 3A-11
Communications Failure ......................................................... 3A-12
Pitot Static Malfunction ........................................................... 3A-13
Electric Trim/Autopilot Failure................................................. 3A-14
June 2007
3A-2 Information Manual
Section 3A Cirrus Design
Abnormal Procedures SR22
　
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