BendixKing KSN 770 - Pilots Guide - Manual (Page 314)

KSN 765/770 Integrated Communication Navigation Display
D200802000009
REV 2 Jun 2014 15-41
Flight Management System (FMS)
Honeywell International Inc. Do not copy without express permission of Honeywell.
For the example flight plan, VECTORS is selected and the approach
and transition are inserted into the flight plan. The resulting display is
shown in Figure 15--36.
NOTE: Altitude constraints for the approach and associated missed
approach are entered into the flight plan.
Figure 15--36
Approach Inserted Into the Flight Plan
FLYING AN APPROACH
Before starting an approach transition that is flown by the FMS, it is
important to verify that the transition is cleared by ATC.
NOTE: To avoid autopilot mode confusion, do not select Approach
Mode on autopilot until the KSN has transitioned from
Terminal to Approach mode.
When using the GPS as the
primary source of navigation, the
APPROACH annunciator will
display prior to the final approach
fix and remain displayed for the
remainder of the approach. This is a positive cue to the flight crew that
the sensor configuration is correct and sensor integrity is within limits
for the approach. The loss of integrity ( LOI ) annunciator must be off
throughout the approach. If the LOI annunciator is displayed, the FMS
should not be used for the remainder of the approach. The flight crew
can continue the approach using raw data (when available on the
approach procedure) or perform the missed approach procedure.