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beginning of a spin.
• WARNING •
In all cases, if the aircraft enters an unusual attitude from
which recovery is not expected before ground impact,
immediate deployment of the CAPS is required.
The minimum demonstrated altitude loss for a CAPS
deployment from a one-turn spin is 920 feet. Activation at
higher altitudes provides enhanced safety margins for
parachute recoveries. Do not waste time and altitude trying to
recover from a spiral/spin before activating CAPS.
Inadvertent Spin Entry
1. CAPS............................................................................. ACTIVATE
March 2010
3-30 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR22
Inadvertent Spiral Dive During IMC Flight
In all cases, if the aircraft enters an unusual attitude from which
recovery is not assured, immediately deploy CAPS. Refer to Section
10, Safety Information, for CAPS deployment information.
1. Power Lever ............................................................................IDLE
2. Stop the spiral dive by using coordinated aileron and rudder
control while referring to the attitude indicator and turn coordinator
to level the wings.
3. Cautiously apply elevator back pressure to bring airplane to level
flight attitude.
4. Trim for level flight.
5. Set power as required.
6. Use autopilot if functional otherwise keep hands off control yoke,
use rudder to hold constant heading.
7. Exit IMC conditions as soon as possible.
March 2010
Cirrus Design Section 3
SR22 Emergency Procedures
Information Manual 3-31
Other Emergencies
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.
Emergency Engine Shutdown On Ground
1. Power Lever ............................................................................ IDLE
2. Fuel Pump (if used) .................................................................OFF
3. Mixture ..............................................................................CUTOFF
4. Fuel Selector............................................................................OFF
5. Ignition Switch..........................................................................OFF
6. Bat-Alt Master Switches...........................................................OFF
March 2010
3-32 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR22
Left/Right Brake Over-Temperature Annunciation
BRAKE TEMP Warning
Brake temperature is greater than 293°F. Refer to Section 10 - Safety
Information: Taxiing, Steering, and Braking Practices for additional
information
1. Stop aircraft and allow the brakes to cool.
Starter Engaged Annunciation
STARTER ENGAGED Warning
Starter stuck engaged. MCU detects 24 VDC to Starter 30 seconds
after initial engagement.
On-Ground
1. Ignition Switch ..........................................................................OFF
2. Battery Switches ......................................................................OFF
In-Flight
1. STARTER Circuit Breaker ......................................................PULL
2. Land as soon as practical.
BRAKE TEMP
START ENGAGE
March 2010
Cirrus Design Section 3
SR22 Emergency Procedures
Information Manual 3-33
CAPS Deployment
The Cirrus Airframe Parachute System (CAPS) should be activated in
the event of a life-threatening emergency where CAPS deployment is
　
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