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March 2010
Intentionally Left Blank
Information Manual 10-3
Cirrus Design Section 10
SR20 Safety Information
Introduction
The Cirrus Design SR20 is a modern, advanced technology airplane
designed to operate safely and efficiently in a flight environment.
However, like any other aircraft, pilots must maintain proficiency to
achieve maximum safety, utility, and economy.
As the pilot you must be thoroughly familiar with the contents of this
Handbook, the Handbook Supplements, the SR20 Flight Checklist,
and operational guides and data provided by manufacturers of
equipment installed in this airplane. You must operate the airplane in
accordance with the applicable FAA operating rules and within the
Limitations specified in Section 2 of this Handbook.
The Normal Procedures section of this handbook was designed to
provide guidance for day-to-day operation of this airplane. The
procedures given are the result of flight testing, FAA certification
requirements, and input from pilots with a variety of operational
experience. Become fully familiar with the procedures, perform all the
required checks, and operate the airplane within the limitations and as
outlined in the procedures.
March 2010
10-4 Information Manual
Section 10 Cirrus Design
Safety Information SR20
Cirrus Airframe Parachute System (CAPS)
Deployment
The Cirrus Airframe Parachute System (CAPS) is designed to lower
the aircraft and its passengers to the ground in the event of a lifethreatening
emergency. However, because CAPS deployment is
expected to result in damage to 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 aircraft occupants, its use should not be taken lightly.
Instead, possible CAPS activation scenarios should be well thought
out and mentally practiced by every SR20 pilot.
The following discussion is meant to guide your thinking about CAPS
activation. It is intended to be informative, not directive. It is the
responsibility of you, the pilot, to determine when and how the CAPS
will be used.
Deployment Scenarios
This section describes possible scenarios in which the activation of the
CAPS might be appropriate. This list is not intended to be exclusive,
but merely illustrative of the type of circumstances when CAPS
deployment could be the only means of saving the occupants of the
aircraft.
Mid-air Collision
A mid-air collision may render the airplane unflyable by damaging the
control system or primary structure. If a mid-air collision occurs,
immediately determine if the airplane is controllable and structurally
capable of continued safe flight and landing. If it is not, CAPS
activation should be considered.
Structural Failure
Structural failure may result from many situations, such as:
encountering severe gusts at speeds above the airplane’s structural
cruising speed, inadvertent full control movements above the
airplane’s maneuvering speed, or exceeding the design load factor
while maneuvering. If a structural failure occurs, immediately
determine if the airplane is controllable and structurally capable of
March 2010
Information Manual 10-5
Cirrus Design Section 10
SR20 Safety Information
continued safe flight and landing. If it is not, CAPS activation should be
considered.
Loss of Control
Loss of control may result from many situations, such as: a control
system failure (disconnected or jammed controls); severe wake
turbulence, severe turbulence causing upset, severe airframe icing, or
sustained pilot disorientation caused by vertigo or panic; or a spiral/
spin. If loss of control occurs, determine if the airplane can be
recovered. If control cannot be regained, the CAPS should be
activated. This decision should be made prior to your pre-determined
decision altitude (2,000’ AGL, as discussed below).
Landing Required in Terrain not Permitting a Safe Landing
If a forced landing is required because of engine failure, fuel
exhaustion, excessive structural icing, or any other condition CAPS
activation is only warranted if a landing cannot be made that ensures
little or no risk to the aircraft occupants. However, if the condition
occurs over terrain thought not to permit such a landing, such as: over
extremely rough or mountainous terrain, over water out of gliding
distance to land, over widespread ground fog or at night, CAPS
activation should be considered.
Pilot Incapacitation
Pilot incapacitation may be the result of anything from a pilot’s medical
 
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本文鏈接地址:西銳20飛機信息手冊 SR22 AIRPLANE INFORMATION MANUAL 1148-126(121)
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