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algorithm. Because it is derived from GPS, Geometric Altitude may
differ from corrected barometric altitude. Therefore, Geometric Altitude
may be in error by as much as 100 ft and should not be used for
navigation. MSL-G is presented solely to provide the pilot additional
situational awareness regarding the true MSL height upon which the
TAWS Terrain Display and Alerting is based.
Original: 07-03-04
12 of 12 P/N 13772-121
Section 9 Cirrus Design
Supplements SR22
Self Test
Proper operation of the TAWS can be verified when the aircraft is on
the ground as follows:
1. Select the TAWS page on the MFD
2. Clear all caution messages in the lower right corner
3. Ensure that the TERR INHIBIT switch is not engaged, and
momentarily push the SELF TEST switch:
a. The amber TERR INOP light should be illuminated.
b. The amber TERR INOP light should extinguish.
c. The red TERR WARN light should be illuminated.
d. An aural “EGPWS SYSTEM OK” is enunciated over cockpit
speaker.
e. The red TERR WARN light should extinguish.
f. The amber TERR CAUT light should be illuminated.
g. The amber TERR CAUT light should extinguish.
h. A terrain self-test pattern should appear on the MFD.
i. The terrain self-test should disappear after several sweeps of
the terrain display.
j. A TAWS Sensor Self Test Caution message should appear in
the lower right comer of the MFD.
4. Acknowledge and clear this caution.
Original: 07-03-04
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
Software Version 530-00159-000
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.
Original: 10-12-05
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.
The Avidyne system software version for this installation is 530-00159-
XXX, where X can be any digit from 0 to 9.
Figure - 1
Original: 10-12-05
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
600-00081-000, 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
Original: 10-12-05
4 of 4 P/N 13772-123
Section 9 Cirrus Design
Supplements SR22
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(131)
