Garmin G950 Pilot’s Guide for the Pilatus PC-6
190-00870-02 Rev. A
304
HAZARD AVOIDANCE
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL FEA
TURES
APPENDICES
INDEX
Figure 6-16 Selecting Sector Scan Position
3)
Turn the small
FMS
Knob to place the Bearing Line in the desired position. The location of the Bearing Line
becomes the center point of the Sector Scan.
4)
Turn the large
FMS
Knob to place the cursor in the SECTOR SCAN field.
5)
Turn the small
FMS
Knob to select FULL, 60˚, 40˚, or 20˚ scan.
6)
If desired, readjust the Bearing Line as discussed previously to change the center of the Sector Scan.
7)
Press the
BRG
Softkey again to remove the Bearing Line and cursor. The bearing reference resets to 0º.
Figure 6-17 40˚ Sector Scan
a
ntenna
s
taBilization
When radar stabilization is active, the radar tilt is corrected for pitch and roll, and therefore is kept steady
with respect to an earth fixed reference. The commanded tilt angle is kept constant with respect to the
earth. When the stabilization is disabled, corrections are no longer made for pitch and roll, and the radar
tilt angle is kept constant with respect to the aircraft reference system.