Honeywell FMZ Series Pilot's Manual page 117

Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter
LANDING 2/2 -- The following values are displayed on the
D
LANDING 2/2 page, shown in Figure 4--49, when a runway is
selected. When a runway is not selected, DENSITY ALT only is
displayed on the LANDING 2/2 page.
— Surface slope (1L)
— Surface width (1L)
— Surface threshold (1R)
— Headwind/tailwind and crosswind (2R)
— Density altitude (3L).
Operational Example
4-48
Honeywell International Inc. Do not copy without express permission of Honeywell.
Figure 4- -49
LANDING 2/2
A28- - 1146- - 181
REV 3 Mar 2009