Garmin G1000 NXi, Руководство пилота

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190-02177-02 Rev. A
Garmin G1000 NXi Pilot’s Guide for the Cessna NAV III
55
FLIGHT INSTRUMENTS
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 2-19 Heading and Course Indications (True)
Changing the navigation angle true/magnetic setting:
1) Use the FMS Knob to select the ‘Aux - System Setup 1’ Page on the MFD.
2) Push the
FMS
Knob to activate the cursor.
3) Turn the large
FMS
Knob to highlight the NAV Angle setting in the ‘Display Units’ Box.
4)
Turn the small FMS Knob to highlight the desired setting and press the ENT Key.
• ‘Magnetic(º)’ - Angles corrected to the computed magnetic deviation
• ‘True(ºT)’ - References angles to true north
TURN RATE INDICATOR
The Turn Rate Indicator is located directly above the rotating compass card. Tick marks to the left and right
of the lubber line denote half-standard and standard turn rates. A magenta Turn Rate Trend Vector shows the
current turn rate. The end of the trend vector gives the heading predicted in six seconds, based on the present
turn rate. A standard-rate turn is shown on the indicator by the trend vector stopping at the standard turn
rate tick mark, corresponding to a predicted heading of 18˚ from the current heading. At rates greater than 4
deg/sec, an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid.
Figure 2-20 Turn Rate Indicator and Trend Vector
Arrow Shown
for Turn Rate
>4 Degrees per
Second
Standard
Turn Rate
Half Standard
Turn Rate
BEARING POINTERS AND INFORMATION WINDOWS
Two bearing pointers and associated information can be displayed on the HSI for NAV and GPS sources by
pressing the PFD Opt Softkey then either the Bearing 1 or Bearing 2 Softkey. The bearing pointers are cyan
and are single-line (BRG1) or double-line (BRG2). A pointer symbol is shown in the information window to
indicate the navigation source. The bearing pointers never override the CDI and are visually separated from
the CDI by a white ring. The white ring is not shown when the HSI Map is enabled. Bearing pointers may
be selected but not necessarily visible due to data unavailability.