Engine Instrument Test; Engine Instrument Display With Failures - Honeywell PRIMUS 1000 Pilot's Manual

Engine Instrument Test -- If on the ground, when the No. 1 EFIS
D
DC test button is pushed, the failure flags are shown. The test
display is shown only as long as the TEST button is pushed. Figure
5--7 shows the gear/flaps/spoiler display, cabin pressurization and
APU status display, and pitch/roll/yaw trim displays. The following
green messages are shown (master caution is not activated when
the messages are caused by the TEST sequence).
- REV
- IGN AB
- ATTCS

Engine Instrument Display With Failures

NOTES: 1. The CAS display goes to its test format during TEST.
2. If metric units are displayed for certain parameters,
A28--1146--112--00
Figure 5--7
metric labels are shown during TEST.
Engine Instrument and Crew Alerting System (EICAS)
PRIMUSr1000 Integrated Avionics System
AD--50962@
5-21