Garmin Software Version 0648.02 Uživatelská příručka stáhnout pdf (Strana 116)

Garmin G1000 Cockpit Reference Guide for the Piper PA32

SECTION 11 – ABNORMAL

OPERATION

11-2

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 pitch ex-

ceeds +30˚/-20˚ or bank exceeds 65˚:

• Trafﬁc Annunciations

• Flight director

Command 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

• 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

11.6 DEAD RECKONING

While in Enroute or Oceanic phase of ﬂight, if the

G1000 detects an invalid GPS solution or is unable to

calculate a GPS position, the system will automatically

revert to Dead Reckoning (DR) Mode. In DR Mode,

the G1000 uses its last-known position combined with

continuously updated airspeed and heading data (when

available) to calculate and display the aircraft’s current

estimated position.

NOTE: Dead Reckoning Mode will only function in

Enroute (ENR) or Oceanic (OCN) phase of ﬂight.

In all other phases, an invalid GPS solution will

produce a “NO GPS POSITION” annunciation on

the map and the G1000 will stop navigating in

GPS Mode.

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