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MFD’s MAP Page, must be set to either STRIKE or CELL.
The Avidyne system software partnumber for this installation
is 530-00112-000 or later.
Refer to Avidyne FlightMax EX5000C Pilot’s Guide, P/N 600-00108-
000 Rev 03 or later for a more complete description of the MFD, its
operating modes, and additional detailed operating procedures.
June 2007
7-88 Information Manual
Section 7 Cirrus Design
Airplane Description SR22
Autopilot
Serials with Avionics Configuration A - 0002 through 1601, 1603
through 1643 and 1645 through 1662 without PFD:
These airplanes are equipped with an S-TEC System Thirty Autopilot
with GPSS. This airplane is equipped with an S-TEC System Thirty
Autopilot. This two-axis autopilot system receives roll axis control
inputs from an integral electric turn coordinator and altitude
information from an altitude transducer plumbed into the pitot-static
system. The programmer, roll computer/amplifier, and annunciators
are contained entirely within the turn coordinator case. The Multifunction
Control Knob at the upper left of the turn coordinator provides
mode selection, disengage, and turn command functions. A button on
each control yoke handle may be used to disengage the autopilot. A
separate pitch computer provides the ALT hold function. The S-Tec
System Thirty Autopilot features:
• Roll Stabilization.
• Turn Command.
• NAV/LOC/GPS tracking; HI and LO sensitivity.
• Altitude Hold.
• GPS Steering (GPSS) for smoother turns onto a course or
during course tracking.
A separate GPSS converter provides GPS roll steering to the
autopilot. A GPSS/HDG button allows the operator to switch between
HDG and Roll Steering modes. In the HDG mode the autopilot
responds to the HDG bug on the HSI. In the GPSS mode, the autopilot
responds to roll steering inputs from the GPS navigator. 28 VDC for
autopilot operation is supplied through the 5-amp AUTOPILOT circuit
breaker on the Essential Bus.
Refer to S-TEC System Thirty Autopilot Pilot's Operating Handbook
(P/N 8777) dated Feb. 1999 or later, S-TEC-Meggit Global Positioning
System Steering (GPSS) Converter Pilot's Operating Handbook (P/N
8799) dated 8 Feb. 2001 or later, and the applicable POH supplement
for a more complete description of the autopilot, its operating modes,
and additional detailed operating procedures.
June 2007
Information Manual 7-89
Cirrus Design Section 7
SR22 Airplane Description
Serials with Avionics Configuration B - 0002 through 1601, 1603
through 1643 and 1645 through 1662 without PFD:
These airplanes are equipped with an S-TEC System 55X Autopilot
with Altitude Selector/Alerter. The System 55X autopilot is a two-axis
autopilot system. The system consists of a flight guidance
programmer/computer, altitude encoder, altitude selector / alerter, turn
coordinator, and HSI. Mode selection and vertical speed selection is
made on the programmer/computer panel. A button on each control
yoke handle may be used to disengage the autopilot. The autopilot
makes roll changes through the aileron trim motor and spring cartridge
and makes pitch changes for altitude hold through the elevator trim
motor.
The SR22 installation of the S-Tec System 55X Autopilot features:
• Heading Hold and Command;
• NAV/LOC/GPS/GS tracking, high and low sensitivity, and
automatic 45° course intercept;
• GPS Steering (GPSS);
• Altitude Pre-select, Hold and Command, Altitude display, and
baro correction;
• Altitude and Decision Height (DH) alert; and
• Vertical Speed Hold and Command.
28 VDC for autopilot and altitude selector/alerter is supplied through
the 5-amp AUTOPILOT circuit breaker on the Essential Bus.
Refer to S-Tec System Fifty-Five X Autopilot Pilot's Operating
Handbook, P/N 87109 dated 8 November 2000 or later, S-Tec Altitude
Selector / Alerter (P/N 0140) Pilot's Operating Handbook, P/N 8716,
original release, or later, and the applicable POH supplement for a
more complete description of the autopilot, its operating modes, and
additional detailed operating procedures.
Avionics Configuration PFD - Serials 0435 and subsequent with
PFD:
These airplanes are equipped with an S-TEC System 55X or 55SR
Autopilot and are fully integrated with the Entegra PFD. Heading,
Altitude and VSI (55X only) reference bugs are provided to aid in
autopilot control and pilot situational awareness. When in an active
June 2007
7-90 Information Manual
Section 7 Cirrus Design
Airplane Description SR22
autopilot mode, full guidance is provided, including smooth transitions
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(81)
