Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter
A28--1146--181
REV 3 Mar 2009
4-39
Operational Example
Honeywell International Inc. Do not copy without express permission of Honeywell.
EN ROUTE
Once at cruise altitude, the information on PROGRESS 2/3 page
reflects the commanded speed and altitude information for the cruise
segment, as shown in Figure 4--40. In this example, 140 CAS
represents the recommended cruise speed.
Figure 4--40
En Route Information on PROGRESS 2/3
As the flight progresses, clearance revisions are completed using one
of the two following methods:
1. When the revision is after the TO waypoint, the flight plan is modified
by adding or deleting waypoints.
2. When the revision effects the TO waypoint (such as clearance direct
from present position to another point), that is done by pushing the
DIR
key.
The ACTIVE FLT PLAN page 1, is displayed by pushing the
DIR
function key regardless of what page is currently being displayed.
When the direct--to waypoint is already in the flight plan, pushing the line
select key to the left of the waypoint makes the direct--to the TO
waypoint.
When the direct--to waypoint is not in the flight plan, enter the IDENT
for the direct--to waypoint in the upper left corner of the page where the
dashes are located. The entered IDENT becomes the TO waypoint.
Either of these actions results in the FMS to immediately alter course.
Summary of Contents for FMZ Series
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