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Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter
Step
Procedure 7- -4 Remove Temperature Compensation
1
Select the LANDING prompt from PERF INDEX page to
display the LANDING 1/2 page, shown in Figure 7--19.
2
Select TEMP COMP on the LANDING page.
A28- - 1146- - 181
REV 3 Mar 2009
Honeywell International Inc. Do not copy without express permission of Honeywell.
Figure 7- -19
LANDING 1/2 Page
01874.01
Flight Plan
7-39
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