Comparison Monitor Parameters - Honeywell PRIMUS 1000 Pilot's Manual

PRIMUSr1000 Integrated Avionics System
Parameter Monitored
Pitch (PIT) Attitude
Roll (ROL) Attitude
Attitude (ATT)
Heading (HDG)
Altitude (ALT)
Airspeed (IAS)
Localizer (LOC) deviation
Glideslope (GS) deviation
Instrument Landing System
(ILS)
Radio Altimeter (RA)
CAS MSG
NOTE: The comparison is made when the pilot and copilot have the
same type but different sources selected for display. If, for
example, the pilot and copilot both have ILS1 selected
(amber annunciation of the source), no comparison monitor
is active on that data (LOC, GS).
Electronic Flight Instrument System (EFIS)
4-60
±5_
±6_
Active only when both pitch and roll
comparators are already tripped.
±6_ (level flight)
±200 feet
±5 knots
±40 µA (» 1/2 dot below 1200 feet
AGL)
±50 µA (» 1/2 dot below 1200 feet
AGL)
Active when both LOC and GS
comparators are already tripped
1/8 x (RA1+RA2) + 10 feet
Annunciated when there is a
miscompare between the symbol
generators and the processing of
the EICAS CAS messages.

Comparison Monitor Parameters

Table 4--17
Tolerances
2
A28--1146--112--00