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DC heading error signal that is compatible with the autopilot. The end
result is an autopilot that can be directly coupled to the roll steering
commands produced by the GPS Navigator, eliminating the need for
the pilot to make any further adjustments to the PFD course arrow.
REV (Reverse Course) – When REV is selected, the autopilot will
automatically execute high sensitivity gain for an approach where
tracking the front course outbound or tracking the back course inbound
is required. The APR and REV annunciators will illuminate when REV
is selected.
Revision 2: 07-18-05
P/N 11934-S27 15 of 16
Cirrus Design Section 9
SR20 Supplements
APR (Approach) – When APR is selected, the autopilot provides
increased sensitivity for VOR or GPS approaches. APR may also be
used to provide increased sensitivity for enroute course tracking.
ALT (Altitude Hold), Mode – When ALT is selected, the autopilot will
hold the altitude at the time the mode was selected. Altitude hold will
not engage if an autopilot roll mode is not engaged. Altitude correction
for enroute barometric pressure changes may be made by rotation of
the VS knob on the autopilot programmer/computer. Clockwise
rotation will increase and counterclockwise rotation will decrease
altitude 20 feet for each ‘click.’ The maximum adjustment is ±360 feet.
Adjustments greater than 360 feet can be made by selecting VS mode
and flying the airplane to the new altitude and then re-engaging ALT
mode.
VS (Vertical Speed) Mode – When VS is selected, the autopilot will
synchronize to and hold the vertical speed at the time the mode was
selected. Altitude hold will not engage if an autopilot roll mode is not
engaged. The vertical speed is displayed in 100-foot increments at the
far right of the programmer/computer window next to the VS
annunciation. A plus (+) value indicates climb and a negative or minus
(-) value indicates descent. Vertical speed can be adjusted by rotating
the VS knob on the programmer/computer. Clockwise rotation
increases and counterclockwise rotation decreases rate of climb (or
descent) 100 FPM for each ‘click.’ The maximum adjustment is ±1600
FPM.
Revision 2: 07-18-05
16 of 16 P/N 11934-S27
Section 9 Cirrus Design
Supplements SR20
Revision 2: 07-18-05
Intentionally Left Blank
P/N 11934-S28 1 of 8
Cirrus Design Section 9
SR20 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
Garmin GTX 330 Mode S
Transponder
When a Garmin GTX 330 Transponder is installed in the Cirrus Design
SR20, this 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.
Original: 07-03-04
2 of 8 P/N 11934-S28
Section 9 Cirrus Design
Supplements SR20
Figure - 1
GARMIN GTX 330
STBY
OFF
ON
IDENT
VFR
0 1 2 3 4 5 6 7 8 9
CLR
FUNC
START
STOP
CRSR
ALT
1 2 3 4 5
10 9 8 7 6
1. Identification Key
2. Mode Selector Keys
a. OFF
b. STBY (Standby)
c. ON
d. ALT
3. Display Window
4. FUNC (Function) Key
5. CRSR (Cursor)
6. CLR (Clear) Key
7. START/STOP Key
8. Photocell
9. VFR Key
10. Selector Keys
a. 0-7 - Code Selection
b. 8-9 - Display Brightness/Contrast
ALT 1200 FLIGHT TIME
01:23:20
Garmin GTX 330 Transponder
Original: 07-03-04
P/N 11934-S28 3 of 8
Cirrus Design Section 9
SR20 Supplements
Section 1 - General
The airplane is equipped with a single Garmin GTX 330 ATC Mode S
transponder with IDENT capability. This supplement provides
complete operating instructions for the GTX 330 and does not require
any additional data be carried in the airplane.
Section 2 - Limitations
No Change.
Section 3 - Emergency Procedures
No Change.
Section 4 - Normal Procedures
• Note •
Expected coverage from the GTX 330 is limited to “line of
sight.” Low altitude or aircraft antenna shielding by the
airplane itself may result in reduced range. Range can be
improved by climbing to a higher altitude.
After Engine Start
1. Avionics Power Switch ...............................................................ON
The transponder will turn on in the same mode of operation
　
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