曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

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
The maximum demonstrated deployment speed is 133 KIAS.
Reducing airspeed allows minimum parachute loads and prevents
structural overload and possible parachute failure.
(Continued on following page)
March 2010
3-34 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR22
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
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
from flying objects in the cabin at touchdown.
March 2010
Cirrus Design Section 3
SR22 Emergency Procedures
Information Manual 3-35
13. Assume emergency landing body position.
The emergency landing body position is assumed by placing both
hands on the lap, clasping one wrist with the opposite hand, and
holding the upper torso erect and against the seat backs.
14. After the airplane comes to a complete stop, evacuate quickly and
move upwind.
As occupants exit the airplane, the reduced weight may allow
winds to drag the airplane further. As a result of landing impact,
the doors may jam. If the doors cannot be opened, break out the
windows with the egress hammer, located in the console between
the front seats, and crawl through the opening.
March 2010
3-36 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR22
March 2010
Intentionally Left Blank
Information Manual 3A-1
Cirrus Design Section 3A
SR22 Abnormal Procedures
Section 3A
Abnormal Procedures
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：西銳20飛機信息手冊 SR22 AIRPLANE INFORMATION MANUAL 2979(23)