Cirrus Design Section 2
SR22 Limitations
P/N 13772-004 2-23P/N 13772-004 2-23
Max Viz Enhanced Vision System (Optional)
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 01 or later must be available to the pilot
during flight.
MD302 Standby Attitude Module (Optional)
1. Selection of the option menu of the MD302 is limited to ground or
visual meteorological conditions.
2. The display has an operational lower temperature limit of -22°F
(-30°C). Visibility of the display may be reduced between -4°F
(-20°C) and -22°F (-30°C).
3. The appropriate revision of the Mid-Continent Instruments and
Avionics MD302 Standby Attitude Module Pilot’s Guide (p/n
9017846) must be available to the pilot whenever the system is in
use.
Air Conditioning System (Optional)
The use of Recirculation Mode during flight is prohibited.
Inflatable Restraint System
Use of a child safety seat with the inflatable restraint system is
prohibited.
Flap Limitations
Approved Takeoff Settings .......................................... UP (0%) or 50%
Approved Landing Settings ..................................... 0%, 50%, or 100%
Paint
To ensure that the temperature of the composite structure does not
exceed 150°F (66°C), the outer surface of the airplane must be
painted in accordance with the paint colors and schemes as specified
Revision 1
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