Garmin Software Version 0321.19 Uživatelský manuál stáhnout pdf (Strana 30)

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

DIAMOND MODEL DA 40

DIAMOND MODEL DA 40 F

190-00492-11 Rev 8 Diamond DA 40 / DA 40F

3-8

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 to the OUT position.

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Garmin Software Version 0321.19 Uživatelský manuál Strana 30