Performance Data - Honeywell FMZ Series Pilot's Manual

Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter

PERFORMANCE DATA

The PERF DATA pages are accessed by pushing the CONFIRM INIT
prompt (6R) on the PERFORMANCE INIT 3/3 page. The PERF DATA
has four pages. The performance data pages permit the pilot to monitor
important performance calculations made by the FMS such as the
hover ceiling, velocity hover limit, and velocity flyaway limit. Category
A ceiling altitudes, best range and endurance are also displayed.
PERF DATA 1/4 -- The PERF DATA 1/4 page, shown in Figure 4--20,
D
shows information computed by the FMS. Hover ceiling, velocity
hover limit, and velocity flyaway limit are determined by using
density altitude information computed by the FMS and the tables in
the Agusta ECM. Best range speed and distance are displayed on
line 4 and best endurance speed and distance are displayed on
line 5.
A28- - 1146- - 181
REV 3 Mar 2009
Honeywell International Inc. Do not copy without express permission of Honeywell.
Figure 4- -20
PERF DATA 1/4
Operational Example
4-19