Garmin Software Version 0552.00 Guide de l'utilisateur télécharger pdf (Page 86)

190-00645-00 Rev. A

Garmin G1000 Cockpit Reference Guide for the Quest Kodiak 100

SECTION 11 – ABNORMAL

OPERATION

11-2

11.2 ABNORMAL COM OPERATION

When a COM tuning failure is detected by the system,

the emergency frequency (121.500 MHz) is automatically

loaded into the active frequency ﬁeld of the COM radio

for which the tuning failure was detected. In the event of

a dual display failure, the emergency frequency (121.500

MHz) automatically becomes the active frequency to the

pilot through the pilot headset.

11.3 UNUSUAL ATTITUDES

The PFD will ‘declutter’ when the aircraft enters an

unusual attitude. Only the basic primary functions will

be displayed in these situations.

Red extreme pitch warning chevrons pointing toward

the horizon are displayed starting at 50 degrees above and

30 degrees below the horizon line.

Figure 11-2 Extreme Pitch Indication

11.4 STORMSCOPE OPERATION WITH

LOSS OF HEADING INPUT

If heading is lost, strikes and/or cells must be cleared

manually after the execution of each turn. This is to

ensure that the strike and/or cell positions are depicted

accurately in relation to the nose of the aircraft.

11.5 HAZARD DISPLAYS WITH LOSS OF

GPS POSITION

If GPS position is lost, or becomes invalid, selected

hazards being displayed on the Navigation Map Page

will be removed until GPS position is again established.

The icons in the lower right of the screen, indicating the

selected functions for display, will show an ‘X’, as shown

in Figure 11-3.

Figure 11-3 Loss of Hazard Functions

with Loss of GPS Position

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Garmin Software Version 0552.00 Guide de l'utilisateur Page 86