PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
4-67
Electronic Flight Instrument System (EFIS)
Monitored Parameter Tolerance
Bank angle Greater than ±65_
Pitch attitude up Greater than 30_
Pitch attitude down Greater than 20_
Excessive Attitude Declutter Parameters
Table 4--20
Thefollowingitemsareremovedfromthedisplaywhenthelogic intable
4--20 has been satisfied:
D 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.
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.Selectingthe varioustestsshows theinvalidflagsfor
the following PFD information shown in figure 4--38:
D Micro Air Data Computer
D Flight Director
D Radio Altitude
D Attitude and Heading
D Navigation.
To Next Page
Loading...
