L-3 Skywatch Traffic Advisory System; L-3 Stormscope Weather Information System; Revision 1 - Cirrus SR22 Pilot Operating Handbook

Section 2
Limitations
11. The SYNTHETIC VISION SYSTEM (SVS) cannot be used for
flight guidance, navigation, traffic avoidance, or terrain avoidance.
Maneuvering the airplane in any phase of flight such as taxi,
takeoff, approach, landing, or roll out shall not be predicated on
SVS imagery. The synthetic vision system is not intended to be
used independently
Consequently,
instrumentation is not available. Otherwise, the traditional attitude
instrumentation will always be visible in the foreground with SVS
features in the background.
12. Use of the TRAFFIC ADVISORY SYSTEM (TAS) to maneuver the
airplane to avoid traffic is prohibited. The TAS is intended for
advisory use only. TAS is intended only to help the pilot to visually
located traffic. It is the responsibility of the pilot to see and
maneuver to avoid traffic.
13. Use of use of portable electronic devices during takeoff and
landing is prohibited.

L-3 Skywatch Traffic Advisory System

1. Traffic information shown on the Perspective Integrated Avionics
System displays is provided as an aid in visually acquiring traffic.
Pilots must maneuver the aircraft based only upon ATC guidance
or positive visual acquisition of conflicting traffic.
2. If the pilot is advised by ATC to disable transponder altitude
reporting, Traffic Advisory System must be turned OFF.
3. When option installed, the appropriate revision of the L-3 Avionics
Systems SkyWatch Traffic Advisory System Model SKY497 Pilot's
Guide (p/n 009-10801-001) must be available to the pilot during
flight.

L-3 Stormscope Weather Information System

1. Use of the Stormscope is not intended for hazardous weather
penetration (thunderstorm penetration). Stormscope information,
as displayed on the Perspective Integrated Avionics System, is to
be used only for weather avoidance, not penetration.
2. When option installed, the appropriate revision of the L-3 Avionics
Systems WX500 Stormscope Series II Weather Mapping Sensor
User's Guide, (p/n 009-11501-001) must be available to the pilot
during flight.
2-22
of traditional
SVS is disabled
attitude instrumentation.
when traditional
Cirrus Design
SR22
attitude
P/N 13772-004

Revision 1