2-20 P/N 11934-004
Section 2 Cirrus Design
Limitations SR20
10. 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 of traditional attitude instrumentation.
Consequently, SVS is disabled when traditional attitude
instrumentation is not available. Otherwise, the traditional attitude
instrumentation will always be visible in the foreground with SVS
features in the background.
11. 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. The L-3 Avionics Systems SkyWatch Traffic Advisory System
Model SKY497 Pilot’s Guide P/N 009-10801-001 Rev B (6/6/00) or
later must be available to the pilot during flight.
Enhanced Vision System
1. The Enhanced Vision System (EVS) 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
EVS imagery. The EVS shall only be used as an aide to assist the
flight crew to visually acquire objects normally viewed through the
cockpit windows.
2. The Max Viz Enhanced Vision System Information Manual, P/N
309100024 Revision 1 or later must be available to the pilot during
flight.
Revision 1
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