Garmin Software Version 0321.19 Manual de usuario descargar pdf (Pagina 37)

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

DIAMOND MODEL DA 40

DIAMOND MODEL DA 40 F

190-00492-10 Rev 5 Diamond DA 40 / DA 40F

Page 37 of 65

For cases in which the battery capacity is not sufficient to reach a suitable

airport, an emergency battery is installed to power the standby attitude gyro and

floodlight. This battery is switched on with the HORIZON EMERGENCY

Switch. It provides power for 1 hour and 30 minutes when the floodlight is

switched on.

3.8 AVIONICS EMERGENCIES

3.8.1 PFD OR MFD DISPLAY FAILURE

a) DISPLAY BACKUP button on audio panel…PUSH (button shall be OUT)

3.8.1.1 AUTOMATIC ENTRY OF DISPLAY REVERSIONARY MODE

If the PFD and MFD have automatically entered reversionary mode, use the

following procedure:

a) DISPLAY BACKUP button on audio panel…PUSH (button shall be OUT)

NOTE

After automatic entry of reversionary mode, it is required to press the DISPLAY

BACKUP button on the audio panel. With the DISPLAY BACKUP button

pushed, if the problem causing the automatic entry of reversionary mode is

resolved the system will remain in reversionary mode. A maximum of one

attempt to return to normal mode may be made using the following procedure.

b) DISPLAY BACKUP button on audio panel……PUSH (button shall be IN)

• If the system returns to normal mode, leave the DISPLAY BACKUP

button in and continue.

• If the system remains in reversionary mode, or abnormal display

behavior such as display flashing occurs, then return the DISPLAY

BACKUP button the OUT position.

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Garmin Software Version 0321.19 Manual de usuario Pagina 37