Honeywell FMZ Series Pilot's Manual page 60

Flight management system fms for the agusta aw139/ab139 helicopter software version nz 7.1
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Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter
This message is displayed when a flight plan is attempted to be
loaded from the selected external storage device and the control
D file is already in the process of being saved to any external
storage device.
— DB TRANSFER ABORTED -- This is an advisory system
message indicating the transfer of the database has been
aborted.
— DB TRANSFER COMPLETE -- This is an advisory system
message indicating the transfer of the database has been
completed.
— DB TRANSFER IN PROGRESS -- This is an advisory system
message indicating the transfer of the database is in progress.
— DME X FAILED -- This is an alerting system message indicating
the FMS senses a DME failure and X represents the radio
number.
— DUPLICATE FLT PLAN NAME -- This is an advisory operator
message indicating the flight plan name entered to save the
active flight plan already exists in the custom database.
— END OF FLIGHT PLAN -- This is an alerting system message
indicating the last defined waypoint has been passed. This
message does not apply to the destination waypoint.
— ENDING WPT NOT FOUND -- This is an advisory operator
message indicating the ending waypoint of a flight plan cannot
be found.
— ENTERING POLAR REGION -- This is an alerting system
message indicating the FMS position has just crossed above
89 degrees north/south latitude and special polar rules apply.
— EXCEEDS CERT CEILING -- This is an advisory operator
message indicating the entered altitude is above the certified
ceiling for the aircraft.
— EXCEEDS CG LIMIT -- This is an advisory operator message
indicating the gross CG calculated to a value outside the
minimum or maximum envelope.
— EXCEEDS MAX GROSS WT -- This is an advisory operator
message indicating the gross weight exceeds the maximum
ramp weight in the ACDB or when the gross weight value minus
the HOOK weight exceeds the ACDB value for maximum takeoff
weight.
A28- - 1146- - 181
REV 3 Mar 2009
Honeywell International Inc. Do not copy without express permission of Honeywell.
System Components
3-19

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