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Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter
— 5L -- When the temperature compensation mode is OFF, this line
is blank and is nonoperational.
When the temperature compensation mode is not OFF, an
approach exists in the displayed flight plan, and a valid landing
temperature exists for the temperature compensation mode and
<TEMP COMP is displayed in the data field.
The TEMP COMP page is displayed when the TEMP COMP
prompt is pushed.
— 5R -- Selection of this line accesses the ARRIVAL page.
— 6L -- Access to DESCENT is on this line when the performance
mode is FULL PERF.
— 6R -- Selection of this line gives access to the ACTIVE FLT PLAN
page.
The calculated data from the information on the LANDING 1/2 page
D
is displayed on the LANDING 2/2 page, shown in Figure 5--19. The
LANDING 2/2 page is displayed by pushing the NEXT function key
when the LANDING 1/2 page is displayed.
— 1L -- The slope of the surface is displayed. When no surface has
been selected, entry prompts are displayed. The width of the
surface is displayed when a surface has been selected. No entry
is permitted.
A28- - 1146- - 181
REV 3 Mar 2009
Honeywell International Inc. Do not copy without express permission of Honeywell.
Figure 5- -19
LANDING 2/2 Page
01850.01
Performance
5-35
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