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Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter
MOT GENERAL REQUIREMENTS
Only one active MOT flight plan is permitted.
An active MOT flight plan is canceled by performing one of the following:
Performing a direct--to to a non--MOT flight plan waypoint.
D
Pushing 6L CANCEL on the active flight plan page.
D
The TU mode is engaged by pushing the GA button on the guidance
D
control panel.
MOT is prohibited in the polar regions. MOT is only permitted on
en route waypoints.
NOTE:
Activation of a MOT flight plan is not permitted during
departure and arrival procedures, as well as active missed
approach procedures.
MOT is permitted when actively flying HOLD and ORBIT patterns. With
MOTinitiated when flying a HOLD or ORBIT, the original pattern fix is
retained and the pattern terminated.
NOTE:
After MOT, a subsequent return to the pattern fix results in
re--entering the HOLD/ORBIT using normal FMS entry
methodology.
When, during an active MOT flight plan, the FMS receives notification
of subsequent MOT button pushes, the following occurs:
Pushing the MOT button for the first time results in disengagement
D
of MOT mode while the MOT flight plan continues to be displayed.
Pushing the MOT button for the first time results in engagement of
D
MOT mode with a new MOT flight plan.
When the TU mode is engaged, the MOT mode is canceled and the
FROM waypoint is set to the MOT waypoint.
When the MOT flight plan is active, non--MOT flight plan waypoint
sequencing is suspended.
When the MOT flight plan is activated, LNAV is automatically armed
and engaged when permitted by FMS. Subsequently, pushing NAV on
the guidance controller disconnects LNAV while the MOT flight plan
continues to be displayed.
A28- - 1146- - 181
REV 3 Mar 2009
Honeywell International Inc. Do not copy without express permission of Honeywell.
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