Excessive Attitude Declutter Parameters; Pfd Test Mode - Honeywell PRIMUS 1000 Pilot's Manual

Monitored Parameter
Bank angle
Pitch attitude up
Pitch attitude down

Excessive Attitude Declutter Parameters

The following items are removed from the display when the logic in table
4--20 has been satisfied:
FD mode annunciations and command bars and couple arrow
D
Marker beacons
D
Vertical deviation scale, pointer, and annunciator
D
ADI localizer scale
D
Speed bugs and readout
D
Radio altitude display
D
Altitude select, airspeed display and vertical speed bug data
D
All flags and comparators except ATT and ADC (IAS/ALT)
D
Low bank annunciator
D
RA set digits.
D
NOTE: Declutter mode is inhibited when windshear flight director
mode is engaged.

PFD TEST MODE

This test can be initiated with the DC when airspeed is valid and less
than 60 knots, and the weight--on--wheels (WOW) switch is in the
on--ground mode. Selecting the various tests shows the invalid flags for
the following PFD information shown in figure 4--38:
Micro Air Data Computer
D
Flight Director
D
Radio Altitude
D
Attitude and Heading
D
Navigation.
D
A28--1146--112--00
PRIMUSr1000 Integrated Avionics System
Greater than ±65_
Greater than 30_
Greater than 20_
Table 4--20
Electronic Flight Instrument System (EFIS)
Tolerance
4-67