Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter
A28--1146--181
REV 3 Mar 2009
Progress
8-4
Honeywell International Inc. Do not copy without express permission of Honeywell.
01574.02
Figure 8--3
PROGRESS 3/3 Page
The following line select keys correspond to the associated definitions
on the PROGRESS 3/3 page.
D
1L
-- The current cross track (XTK) error relative to the active leg of
the flight plan is displayed on this line. A 0.01 NM resolution is used
when the cross track error is less than 1 NM. Larger cross track
errors are displayed using a 0.1 NM resolution. No entry is
permitted.
D
1R
-- This line permits pilot entry of offset. Procedure 8--1 describes
how to enter and remove an offset.
D
2L and 2R
-- Aircraft track, drift, and heading is displayed on this line.
D
3L and 3R
-- The FMS computed winds and ground speed are
displayed on this line.
D
6L
-- This prompt gives access to the AIR DATA page.
D
6R
-- This prompt gives access to the FLIGHT SUMMARY page.
Summary of Contents for FMZ Series
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