Garmin Software Version 0369.13 Guía de usuario descargar pdf (Pagina 154)

Garmin G1000 Cockpit Reference Guide for the DA40/40F

190-00324-07 Rev. A

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 primary functions will be

displayed in these situations.

The following information is removed from the PFD

(and corresponding softkeys are disabled) when the air-

craft experiences unusual attitudes:

• Trafﬁc Annunciations

• AFCS Annunciations

• Flight director Com

mand Bars

• Inset Map

• Temperatures

• DME Information

Window

• Wind Data

• Selected Heading Box

• Selected Course Box

• Transponder Status

Box

• System Time

• PFD Setup Menu

• Windows displayed in

the lower right corner

of the PFD:

– Timer/References

– Nearest Airports

– Flight Plan

– Messages

– Procedures

– DME Tuning

• Barometric Minimum

Descent Altitude Box

• Glideslope, Glidepath,

and Vertical Deviation

Indicators

• Altimeter Barometric

Setting

• Selected Altitude

• VNV Target Altitude

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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