Fms Mode Engagement Procedure; Flight Management System (Fms) Navigation Mode (Option) - Honeywell PRIMUS 1000 Pilot's Manual

PRIMUSr1000 Integrated Avionics System
Step
5 Set the heading bug on the HSI to the intercept heading for
the selected course.
6 Push the APR button on the GC.
VOR Approach Mode Engagement Procedure
FLIGHT MANAGEMENT SYSTEM (FMS) NAVIGATION
MODE (OPTION)
The FMS mode is flown when the pilot selects FMS on the DC. The
FMS mode is flown as described in table 8--3.
Step
1 Couple either the pilot' s or copilot' s flight director to the
autopilot with the CPL switch on the GC.
2 Enter the data required for navigation into the FMS.
3 Select FMS as the navigation source on the coupled side
DC.
4 Push the NAV button on the GC.

FMS Mode Engagement Procedure

Characteristics common to FMS are described below.
Instead of using course error and radio deviation from the SG, a
D
composite lateral steering command is used from the FMS
navigation computer through the IAC symbol generator function.
The IAC supplies the flight control function with required steering
D
commands.
This lateral steering command is lateral gain programmed in the
D
FMS navigation computer, and therefore, is not gain programmed
again in the IAC.
Modes of Operation
8-10
Procedure
Table 8--2
Procedure
Table 8--3
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