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Supplement
for
SR22 Airplanes Registered in the European
Union
1. This supplement is required for operation of Cirrus Design SR22
airplane serial numbers 0002 and subsequent when registered in
the European Union. This supplement must be attached to the
applicable SR22 EASA/FAA-approved Airplane Flight Manual.
2. The information contained within this supplement is to be used in
conjunction with the basic AFM and supplements. The information
contained herein supplements or supersedes that in the basic
manual and approved supplements only in those areas indicated.
3. Compliance with the limitations contained in the basic manual and
approved supplements is mandatory.
4. Foreign operating rules and any references to such rules in the
basic manual and approved supplements are not applicable in the
European Union. The aircraft must be equipped and operated in
accordance with applicable operating requirements.
• Note •
A Kinds of Operating Equipment List (KOEL) may not
necessarily apply in the European Union.
Original: 04-12-06
2 of 2 13772-122
Section 9 Cirrus Design
Supplements SR22
Section 1 - General
No Change.
Section 2 - Limitations
No Change.
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 - Systems Description
No Change.
Section 8 - Handling, Servicing & Maintenance
No Change.
Section 9 - Supplements
No Change.
Section 10 - Safety Information
No Change.
Original: 04-12-06
P/N 13772-123 1 of 4
Cirrus Design Section 9
SR22 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
Avidyne Flight Director
When the Avidyne Flight Director is installed in the Cirrus Design
SR22, this POH Supplement is applicable and must be inserted in the
Supplements Section (Section 9) of the Cirrus Design SR22 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 SR22 Pilot’s Operating Handbook.
• Note •
This POH Supplement Revision dated Revision 01: 12-15-07
supersedes and replaces the original release of this
supplement dated Original: 10-12-05.
Revision 01: 12-15-07
2 of 4 P/N 13772-123
Section 9 Cirrus Design
Supplements SR22
Avidyne Primary Flight Display with Flight Director
Section 1 - General
The Flight Director system enhances situational awareness by
reducing cockpit workload through providing a visual cue for the pilot
to follow as indicated by the PFD’s Flight Director Steering Command
Bar. Through turning or pitching the airplane as “directed” by the
Steering Command Bar, the pilot will follow the necessary course to
arrive at a programmed destination.
Figure - 1
Revision 01: 12-15-07
P/N 13772-123 3 of 4
Cirrus Design Section 9
SR22 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 SR22 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
　
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