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P/N 13772-135
Section 9
Cirrus Design
Supplements
SR22 / SR22T
Section 1 - General
The aircraft is equipped with a Garmin GFC 700 Automatic Flight
Control System (AFCS) which is fully integrated within the Cirrus
Perspective Integrated Avionics System architecture. Refer to Section
7 - System Description and the Cirrus Perspective Pilot’s Guide for
additional description of the AFCS and operating procedures..
Determining status of Autopilot Underspeed Protection (USP)
and Hypoxia Detection and Automatic Descent
If Perspective System software load 0764-09 or later is installed, the
aircraft has these functions installed. Software load is displayed in the
upper RH corner of the first MFD screen presented after power-up.
Determining status of Electronic Stability and Protection (ESP)
If the aircraft is equipped with ESP (software load 0764-09 or later), it
is identified and displayed on the second MFD splash screen
presented after power-up. This page will state “This aircraft is
equipped with Electronic Stability & Protection” if installed.
Section 2 - Limitations
1. The appropriate revision of the Cirrus Perspective Cockpit
Reference Guide (p/n 190-00821-XX, where X can be any digit
from 0 to 9) must be immediately available to the pilot during flight.
The system software version stated in the reference guide must be
appropriate for the system software version displayed on the
equipment.
2. Minimum Autopilot Speed ..................................................80 KIAS
3. Maximum Autopilot Speed ...............................................185 KIAS
4. Autopilot Minimum-Use-Height:
a. Takeoff and Climb................................................400 feet AGL
b. Enroute and Descent.........................................1000 feet AGL
c. Approach (GP or GS Mode) ............ Higher of 200 feet AGL or
Approach MDA, DA, DH.
d. Approach (IAS, VS, PIT or ALT Mode)...Higher of 400 feet
AGL or Approach MDA.
5. Yaw Damper must be turned off for takeoff and landing
Revision 03: 12-14-10
