PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
5-21
Engine Instrument and Crew Alerting System (EICAS)
D Engine Instrument Test -- If on the ground, when the No. 1 EFIS
DC test button is pushed, the failure flags are shown. The test
display is shown only as longas theTEST 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
AD--50962@
Engine Instrument Display With Failures
Figure 5--7
NOTES: 1. The CAS display goes to its test format during TEST.
2. If metric units are displayed for certain parameters,
metric labels are shown during TEST.
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