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Flight Management System (FMS) for the Agusta AW139/AB139 Helicopter
GPS(X) STATUS 2/2 -- The following information is displayed on the
GPS(X) STATUS 2/2 page, shown in Figure 6--62:
Receiver Autonomous Integrity Monitoring (RAIM)
D
Horizontal Figure of Merit (HFOM)
D
Vertical Integrity Limit (VINT)
D
Vertical Figure of Merit (VFOM)
D
Time (UTC) and date
D
Operating mode
D
Satellites tracked.
D
RAIM and FOM indicate current uncertainty of position expressed in
NM.
Navigation
6-76
Honeywell International Inc. Do not copy without express permission of Honeywell.
Figure 6- -62
GPS 1 STATUS 2/2
A28- - 1146- - 181
REV 3 Mar 2009
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