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arrive at a programmed destination.
The Avidyne system software version for this installation is 530-00159-
XXX, where X can be any digit from 0 to 9.
Figure - 1
Revision 02: 12-15-07
P/N 11934-S34 3 of 4
Cirrus Design Section 9
SR20 Supplements
Section 2 - Limitations
1. The Flight Director System integrates with the Primary Flight
Display (PFD) System. Adherence to the PFD imitations in the
basic SR20 Pilot’s Operating Handbook is mandatory.
2. The Avidyne FlightMax Entegra-Series PFD Pilot’s Guide, P/N
600-00142-000, Revision 03, or latest revision, must be available
to the pilot during all flight operations.
Section 3 - Emergency Procedures
No Change.
Section 4 - Normal Procedures
No Change.
Section 5 - Performance
No Change.
Section 6 - Weight & Balance
No Change.
Section 7 - System Description
Fully integrated with the S-Tec System 55X Autopilot, the Flight
Director system replaces the “flying W” aircraft reference symbol on
the PFD with the Flight Director Steering Command Bars and Wedge.
The system consists of two lighted push-buttons installed on the
upper, LH side of the instrument panel and associated relays and
wiring between the PFD and autopilot. The remaining portion of the
Flight Director system is entirely software dependant.
When a vertical mode of the autopilot is being used, a set of flight
director command bars will indicate the required steering of the aircraft
to achieve the commanded tracking from the autopilot. In autopilot
mode, “AP” will be in the autopilot annunciation field, the command
bars will be visible and magenta and the aircraft should track the bars.
In flight director only mode, “FD” will be displayed in the autopilot
annunciation field, the command bars will be visible and green, and
Revision 02: 12-15-07
4 of 4 P/N 11934-S34
Section 9 Cirrus Design
Supplements SR20
the pilot is expected to actuate the flight controls as required to track
the bars.
The following describes push-button annunciation and related
Autopilot and Flight Director status:
The Flight Director system is powered by 28 VDC through the 5-amp
AUTOPILOT circuit breaker on the Essential Bus.
Refer to Avidyne FlightMax Entegra-Series PFD Pilot’s Guide, for a
more complete description of the Flight Director, its operating modes,
and additional detailed operating procedures.
No
Annunciation
• Autopilot off.
or
• Autopilot not active in either roll or pitch control.
Green
AP ON
Annunciation
• Autopilot active in roll and/or pitch control.
• If Autopilot active in roll and pitch control, “AP”
annunciation appears on top edge of PFD, and
Flight Director Steering Command Bars
MAGENTA.
Amber
AP OFF
FD ON
Annunciation
• Autopilot uncoupled.
• If Autopilot active in roll and pitch control, Flight
Director ON, “FD” annunciation appears on top
edge of PFD, and Flight Director Steering
Command Bars GREEN.
Revision 02: 12-15-07:
11934-S37 1 of 56
Cirrus Design Section 9
SR20 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
SR20 Airplanes Equipped with the
“G3 Wing”
When the G3 Wing is installed on the Cirrus Design SR20 Serials
1878, 1886 and subsequent, this POH Supplement is applicable and
must be inserted in the Supplements Section (Section 9) of the Cirrus
Design SR20 Pilot’s Operating Handbook. This document must be
carried in the airplane at all times. Information in this supplement adds
to, supersedes, or deletes information in the basic SR20 Pilot’s
Operating Handbook.
• Note •
This POH Supplement Change, dated Revision 01: 08-26-09,
supersedes and replaces the Original issue of this POH
Supplement dated 11-11-07.
Revision 01: 08-26-09
2 of 56 11934-S37
Section 9 Cirrus Design
Supplements SR20
Revision 01: 08-26-09
Intentionally Left Blank
11934-S37 3 of 56
Cirrus Design Section 9
SR20 Supplements
Section 1 - General
The G3 Wing is constructed in a conventional spar, rib, and shear
section arrangement. The upper and lower skins are bonded to the
spar, ribs, and aft shear web forming a torsion box that carries all of
the wing bending and torsion loads. The rear shear webs are similar in
construction but do not carry through the fuselage. The main spar is
laminated epoxy/carbon fiber in a C-section, and is continuous from
　
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