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Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter
NAVIGATION IDENTIFICATION
Information regarding the software of the FMS and the navigation
database is displayed on the NAV IDENT page, shown in Figure 6--129.
The NAV IDENT page is accessed by pushing the IDENT prompt on the
NAV INDEX page 1.
The date, time, software version, and active navigation database cycle
are displayed on the NAV IDENT page. The version, size, and region
of the navigation database are also displayed on the NAV IDENT page.
NOTE:
To ensure proper information is used for the Helicopter FMS,
the pilot is to validate the aircraft database before use.
The date and time displayed on this page is synchronized with the GPS
date and time. Changing the date and time is permitted when the GPS
fails or does not have a valid date/time. The new date or time is changed
by entering the new date or time into the scratchpad, as shown in
Figure 6--130, and pushing the line select key adjacent to the item being
changed.
A28- - 1146- - 181
REV 3 Mar 2009
Honeywell International Inc. Do not copy without express permission of Honeywell.
Figure 6- -129
NAV IDENT Page Display
Navigation
6-175
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