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action may be required.
In combination with the CAS Window, the system issues an audio alert
when specific system conditions are meet and an expanded
description of the condition is displayed in the Alerts Window located
in the lower RH corner of the PFD.
• Note •
For specific pilot actions in response to AFCS alerts, refer to
Section 3A - Abnormal Procedures.
AFCS Status Box and Mode Annunciation
Flight director mode annunciations are displayed on the PFD when the
flight director is active. Flight director selection and autopilot and yaw
damper statuses are shown in the center of the AFCS Status Box.
Lateral flight director modes are displayed on the left and vertical on
the right. Armed modes are displayed in white and active in green.
AFCS status annunciations are displayed on the PFD above the
Airspeed and Attitude indicators. Only one annunciation may occur at
a time. Messages are prioritized by criticality.
Revision 01: 08-26-09
16 of 16 P/N 13772-135
Section 9 Cirrus Design
Supplements SR22
Section 8 – Handling, Service, & Maintenance
No Change.
Section 10 – Safety Information
No Change.
Revision 01: 08-26-09
P/N 13772-136 1 of 6
Cirrus Design Section 9
SR22 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual Supplement
for the
Garmin Terrain Awareness/Warning
System
When the Garmin Terrain Awareness/Warning System is installed on
the aircraft, this POH Supplement is applicable and must be inserted
in the Supplements Section (Section 9) of the Cirrus Design SR22
Pilot’s Operating Handbook. This document must be carried in the
airplane at all times. Information in this supplement adds to,
supersedes, or deletes information in the basic Pilot’s Operating
Handbook.
Original Issue: 05-13-08
2 of 6 P/N 13772-136
Section 9 Cirrus Design
Supplements SR22
Section 1 - General
The airplane is equipped with the Garmin Terrain Awareness/Warning
System that performs the functions of a Class C Terrain Awareness
and Warning System (TAWS) in accordance with TSO C151b.
Refer to the Cirrus Perspective Integrated Flight Deck Pilot’s Guide for
a additional information on the system and its operating modes.
Section 2 - Limitations
1. The Cirrus Perspective by Garmin Integrated Avionics System
Pilot’s Guide for the SR22, P/N 190-00820-00, Revision A or later
must be immediately available to the pilot during flight. The
software status stated in the pilot's guide must match that
displayed on the equipment.
2. Do not use Terrain Awareness and Warning System for navigation
of the aircraft. The TAWS is intended to serve as a situational
awareness tool only and may not provide the accuracy fidelity on
which to solely base terrain or obstacle avoidance maneuvering
decisions.
3. To avoid getting unwanted alerts, TAWS must be inhibited when
landing at an airport that is not included in the airport database.
• Note •
Only vertical maneuvers are recommended responses to
warnings and cautions unless operating in VMC or the pilot
determines, using all available information and instruments,
that a turn, in addition to the vertical escape maneuver, is the
safest course of action. During certain operations, warning
thresholds may be exceeded due to specific terrain or
operating procedures. During day VFR flight, these warnings
may be considered as cautionary.
Pilots are authorized to deviate from their current air traffic
control (ATC) clearance to the extent necessary to comply
with a TAWS warning.
Original Issue: 05-13-08
P/N 13772-136 3 of 6
Cirrus Design Section 9
SR22 Supplements
Section 3 - Emergency Procedures
To prevent unwanted aural alerting during ditching or other off-airport
landings, inhibit the Terrain Awareness System functions by selecting
the INHIBIT Softkey on the TAWS Page.
Response To TAWS Warnings
Red PULL UP Warning
Aural “PULL UP” Warning
Aural “TERRAIN AHEAD” Warning
Aural “OBSTACLE AHEAD” Warning
1. Level the wings, simultaneously adding full power.
2. Increase pitch attitude to 15 degrees nose up.
3. Adjust pitch attitude to ensure terrain clearance while respecting
stall warning. If flaps are extended, retract flaps to the UP position.
4. Continue climb at best angle of climb speed (Vx) until terrain
clearance is assured.
Section 3A - Abnormal Procedures
Response To TAWS Cautions
Amber TERRAIN Caution
Aural “TERRAIN AHEAD” Caution
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西锐20飞机信息手册 SR22 AIRPLANE INFORMATION MANUAL 2979(118)
