Garmin Pilatus PC_6 Guide de l'utilisateur télécharger pdf (Page 83)

Garmin G950 Cockpit Reference Guide for the Pilatus PC-6

190-00851-02 Rev. A

Abnormal Operation

Flight

Instruments EIS

Nav/Com/

XPDR/Audio AFCS GPS Nav

Flight

Planning Procedures

Hazard

Avoidance

Additional

Features

Abnormal

Operation

Annun/

Alerts Appendix Index

ABNORMAL OPERATION

REVERSIONARY MODE

Should a system detected failure occur in either display, the G950 automatically

enters reversionary mode. In reversionary mode, critical ﬂight instrumentation is

combined with engine instrumentation on the remaining display.

Reversionary display mode can be manually activated by pressing the display

backup button installed in the cockpit.

NOTE: The Pilot’s Operating Handbook (POH) and/or Airplane Flight Manual

(AFM) always takes precedence over the information found in this section.

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 failure of both PFDs,

the emergency frequency (121.500 MHz) automatically becomes the active frequency

on both COM radios.

HAZARD DISPLAYS WITH LOSS OF GPS POSITION

If GPS position is lost, or becomes invalid, selected hazards being displayed on the

Navigation Map Page are removed until GPS position is again established.

Loss of Hazard Functions with Loss of GPS

Position

1 2 ... 78 79 80 81 82 83 84 85 86 87 88 ... 127 128

Pas de commentaire

Garmin Pilatus PC_6 Guide de l'utilisateur Page 83