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may be difficult to determine if the aircraft has entered a spiral or the
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
Revision A7
P/N 13772-001 3-21
Cirrus Design Section 3
SR22 Emergency Procedures
CAPS Deployment
The Cirrus Airframe Parachute System (CAPS) should be activated in
the event of a life-threatening emergency where CAPS deployment is
determined to be safer than continued flight and landing.
• WARNING •
CAPS deployment is expected to result in loss of the airframe
and, depending upon adverse external factors such as high
deployment speed, low altitude, rough terrain or high wind
conditions, may result in severe injury or death to the
occupants. Because of this, CAPS should only be activated
when any other means of handling the emergency would not
protect the occupants from serious injury.
• Caution •
Expected impact in a fully stabilized deployment is equivalent
to a drop from approximately 13 feet.
• Note •
Several possible scenarios in which the activation of the
CAPS would be appropriate are discussed in Section 10 -
Safety Information, of this Handbook. These include:
• Mid-air collision
• Structural failure
• Loss of control
• Landing in inhospitable terrain
• Pilot incapacitation
All pilots should carefully review the information on CAPS
activation and deployment in Section 10 before operating the
airplane.
Once the decision is made to deploy CAPS, the following actions
should be taken:
1. Airspeed....................................................... MINIMUM POSSIBLE
(Continued on following page)
Revision A7
3-22 P/N 13772-001
Section 3 Cirrus Design
Emergency Procedures SR22
The maximum demonstrated deployment speed is 133 KIAS.
Reducing airspeed allows minimum parachute loads and prevents
structural overload and possible parachute failure.
2. Mixture (If time and altitude permit) ................................. CUTOFF
Generally, a distressed airplane will be safer for its occupants if
the engine is not running.
3. Activation Handle Cover.................................................. REMOVE
The cover has a handle located at the forward edge. Pull cover
down to expose activation T-handle.
4. Activation Handle (Both Hands) ............. PULL STRAIGHT DOWN
Pull the activation T-handle from its holder. Clasp both hands
around the handle and pull straight down in a strong, steady, and
continuous motion. Maintain maximum pull force until the rocket
activates. Pull forces up to, or exceeding, 45 pounds may be
required. Bending of the handle-housing mount is to be expected.
• WARNING •
Jerking or rapidly pulling the activation T-handle will greatly
increase the pull forces required to activate the rocket. Use a
firm and steady pulling motion – a “chin-up” type pull
enhances successful activation.
After Deployment:
5. Mixture ...............................................................CHECK, CUTOFF
6. Fuel Selector ............................................................................OFF
Shutting off fuel supply to engine will reduce the chances of fire
resulting from impact at touchdown.
7. Bat-Alt Master Switches...........................................................OFF
8. Ignition Switch ..........................................................................OFF
9. Fuel Pump................................................................................OFF
10.ELT............................................................................................ ON
11.Seat Belts and Harnesses .............................................. TIGHTEN
(Continued on following page)
Revision A7
P/N 13772-001 3-23
Cirrus Design Section 3
SR22 Emergency Procedures
All occupants must have seat belts and shoulder harness securely
fastened.
12.Loose Items .....................................................................SECURE
If time permits, all loose items should be secured to prevent injury
　
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