Honeywell FMZ Series Pilot's Manual page 64

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
— NO CROSSING POINT FOUND -- This is an advisory operator
message indicating no crossing point with the flight plan was
found.
— NO CRS TO ARC INTERCEPT -- This is an advisory operator
message indicating the course entered does not intercept the
arc.
— NO FLIGHT PLAN -- This is an advisory operator message
indicating the entered origin or origin/destination does not match
a stored flight plan with the same origin or origin/destination.
— NO INPUT ALLOWED -- This is an advisory operator message
indicating the attempted input is not permitted.
— NO POSITION SENSORS -- This is an alerting system message
indicating no position sensors are available for navigation.
— NO PRESENT POSITION -- This is an advisory system
message indicating an action was requested requiring the
present position. In addition, this message is displayed when an
FMS mode key is selected and there is no present position.
— NOT A NAVAID -- This is an advisory operator message
displayed when an entry is required to be a navaid, and
something other than a navaid is entered.
— NOT A HELIPORT -- This is an advisory operator message
displayed when an entry is required to be a heliport, and
something other than a heliport name is entered.
— NOT AN AIRPORT -- This is an advisory operator message
displayed when an entry is required to be an airport, and
something other than airport name is entered.
— NOT IN DATA BASE -- This is an advisory operator message
indicating the pilot requested some data that was not in the
database and can not be pilot--defined.
— OFFSET CANCEL -- This is an alerting system message
indicating the offset has been canceled.
— OFFSET CANCEL NEXT WPT -- This is an alerting system
message indicating the offset is canceled at the next waypoint
in the flight plan.
— PERF VNAV UNAVAILABLE -- This is an alerting system
message indicating the pilot requested a performance/VNAV
function before sufficient data was entered.
A28- - 1146- - 181
REV 3 Mar 2009
Honeywell International Inc. Do not copy without express permission of Honeywell.
System Components
3-23

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