10 of 10
P/N 11934-S22
Section 9
Cirrus Design
Supplements
SR20
side of the GNS 430 front panel. Frequency tuning is accomplished by
rotating the large and small concentric knobs to select a standby
frequency and then transferring the frequency to the active window.
The COM frequency display window is at the upper left corner of the
GNS 430 display. Auto-tuning can be accomplished by entering a
frequency from a menu. The COM 1 antenna is located above the
cabin on the airplane centerline. 28 VDC for transceiver operating is
controlled through the Avionics Master Switch and supplied through
the 7.5-amp COM1 circuit breaker on the Avionics Essential Bus.
TERRAIN Interface*
• Note •
*TERRAIN
functionality is a standard feature found in GNS
430 units with main software version 5.01 or above and valid
terrain and obstacle databases installed.
Garmin TERRAIN is a terrain awareness system incorporated into
GNS 430 units to increase situational awareness and aid in reducing
controlled flight into terrain. The TERRAIN function displays altitudes
of terrain and obstructions relative to the aircraft’s altitude and are
advisory in nature only. Individual obstructions may be shown if
available in the database, however, not all obstructions may be
available in the database and data may be inaccurate. TERRAIN
information should be used as an aid to visual acquisition and not use
to navigate or maneuver to avoid terrain.
For for a more detailed description of the TERRAIN function,
refer to
the
Garmin GNS 430 Pilot's Guide and Reference, P/N 190-00140-00,
Revision H dated May 2006 or later revision
.
Revision 2: 08-15-07
