Garmin Software Version 0321.19 Bedienungsanleitung PDF herunterladen (Seite 24)

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

3-2

9. In an in-flight emergency, depressing and holding the COM transfer button

for 2 seconds will tune the emergency frequency of 121.500 MHz. If the

display is available, it will also show it in the "Active" frequency window.

10. If the white ‘TAWS N/A’ status annunciator is displayed on the PFD or

MFD TAWS page, the system will no longer provide TAWS alerting or

display relative terrain elevations. The crew must maintain compliance

with procedures that ensure minimum terrain separation.

11. If the red ‘TAWS FAIL’ status annunciator is displayed on the PFD or

MFD TAWS page, the system will no longer provide TAWS alerting or

display relative terrain elevations. The crew must maintain compliance

with procedures that ensure minimum terrain separation.

12. The following warnings and cautions appear in various locations on the

PFD or MFD.

Annunciation Cause

AHRS Aligning – Keep

Wings Level

Attitude and Heading Reference System is aligning.

Keep wings level using standby attitude indicator.

ATTITUDE FAIL Display system is not receiving attitude reference

information from the AHRS; accompanied by the

removal of sky/ground presentation and a red X over

the attitude area.

AIRSPEED FAIL Display system is not receiving airspeed input from

the air data computer; accompanied by a red X

through the airspeed display.

ALTITUDE FAIL Display system is not receiving altitude input from the

air data computer; accompanied by a red X through

the altimeter display.

VERT SPEED FAIL Display system is not receiving vertical speed input

from the air data computer; accompanied by a red X

through the vertical speed display.

HDG Display system is not receiving valid heading input

from the AHRS; accompanied by a red X through the

digital heading display.

Red X A red X through any display field, such as COM

frequencies, NAV frequencies, or engine data,

indicates that display field is not receiving valid data.

LOI GPS integrity is insufficient for the current phase of

flight.

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