Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter
A28--1146--181
REV 3 Mar 2009
Flight Plan
7-36
Honeywell International Inc. Do not copy without express permission of Honeywell.
Step Procedure 7--3 Review and Insert Temperature
Compensated Altitude Constraints
Into Flight Plan
3
Select the ACTIVATE prompt to insert the temperature
compensated values into the flight plan.
The temperature compensated values are displayed in
reverse video, as shown in Figure 7--16.
Figure 7--16
Activate Changes
The pilot is able to calculate a temperature compensated approach
MDA on the last page in the string of the TEMP COMP pages. The last
page of the TEMP COMP page is accessed by pushing the
NEXT
function key when viewing the TEMP COMP page, shown in
Figure 7--15, until the last page is displayed. The default page of the
MDA TEMP COMP page is shown in Figure 7--17.
Summary of Contents for FMZ Series
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