Honeywell FMZ Series Pilot's Manual page 401

Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter
Step Procedure 7- -3 Review and Insert Temperature
2 The --22°C TEMP COMP 1/2 page, shown in Figure 7--15,
is displayed by pushing the TEMP COMP prompt on the
LANDING page.
The proposed altitudes for each of the arrival flight plan
constraints is displayed in reverse video on the TEMP
COMP page.
The temperature compensation is applied only to the
altitude constraints from the navigation database. No
changes are applied to performance computed values or
the pilot--entered constraints.
A28- - 1146- - 181
REV 3 Mar 2009
Honeywell International Inc. Do not copy without express permission of Honeywell.
Compensated Altitude Constraints
Into Flight Plan
Figure 7- -15
TEMP COMP 1/2
Flight Plan
7-35