190-01150-12 Rev. B RFMS Garmin G500H as installed in Bell 206A
Page 12 of 24 FAA APPROVED
3.1.2 MFD Knobs & MFD Soft Keys
The MFD controls are adjacent to and beneath the MFD display. The rotary
knobs are used to scroll through various pages/page groups of the MFD.
Pressing the knob will activate a cursor and allow for the user to enter data and
manipulate settings.
Soft keys at the bottom of the display allow for the rapid selection of pre-defined
functions to be performed on each page. The soft keys operate by press and
release. More detailed configuration is typically available by pressing the MENU
button, located on the right side of the display.
Pressing and holding down the CLR key will display the main map page on the
MFD. Details of the functions available on the MFD are explained in the Garmin
G500H Cockpit Reference Guide defined in Paragraph 1.1.
3.1.3 Helicopter Synthetic Vision Technology (HSVT)
The HSVT function may be turned on or off, as desired. To access the HSVT
softkey menu, press the PFD softkey on the GDU 620, followed by the SYN VIS
softkey. Synthetic vision terrain, horizon headings, and airport signs can be
toggled on and off from this menu. Press the BACK softkey to return to the root
PFD menu.
3.1.4 HSVT Terrain
When the G500H has SVT enabled aural and visual terrain and obstacle alerting
will be provided by the Terrain HSVT function of the G500H system. Terrain
HSVT modes (normal, RP, and inhibit) can be selected via softkey on the
Terrain page on the G500H MFD.
3.1.5 Altitude Alerter
The Altitude Bug Setting will flash when approaching within 1000 feet of the
selected altitude, and an audio tone is played when approaching or deviating
within 200 feet of the selected altitude.
3.2 EMERGENCY PROCEDURES
These procedures supersede those presented as markings or placards, or
documented in the aircraft’s FAA approved Rotorcraft Flight Manual as a result
of the installation of the G500H system. All other emergency procedures remain
in effect.
3.2.1 Loss of Electrical Power
In the event of a total loss of electrical power, the G500H system will cease to
operate and the pilot must utilize the standby instruments and visual references
to fly the aircraft.Primary Flight Display
3.2.2 Primary Flight Display
If primary flight information (Heading, Altitude or Airspeed) on the PFD is not
available or appears invalid, utilize the standby instruments installed as required.
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