Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter
A28--1146--181
REV 3 Mar 2009
Operational Example
4-38
Honeywell International Inc. Do not copy without express permission of Honeywell.
CLIMB
As the climb continues, intermediate altitude clearances are entered
using the altitude selector. The FMS gives advisory information on the
flight plan page to climb to the selected altitude or the next altitude
constraint, whichever is lowest. Altitude restrictions associated with a
waypoint are entered on the multifunction control display unit (MCDU)
adjacent to the appropriate waypoint. The 7000 feet at constraint on
ARDIA was entered at 2R, as shown in Figure 4--39.
Figure 4--39
Constraint Information on ACTIVE FLT PLAN 1/5
The PERF DATA prompt at 6R is displayed after takeoff until the aircraft
is within 200 NM of the destination. The PERF DATA prompt permits
access to the PERF DATA pages described in Section 5, Performance.
When the aircraft is within 200 NM, the PERF DATA prompt changes
to ARRIVAL. The ARRIVAL prompt permits access to the ARRIVAL
page described in Section 6, Navigation.
Summary of Contents for FMZ Series
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