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Embraer EMB145 - Page 1562

Embraer EMB145
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AIRPLANE
OPERATIONS
MANUAL
CREW
AWARENESS
JUNE 28, 2002
2-04-05
Page
35
Code
01
The EICAS test is commanded only from the pilot's panel, and its
indications are as follows:
− Indications removed: reversion, ignition, FADEC in control, all
engine and trim bugs.
− Indications forced: the crew awareness field will be filled with a
"X".
− Indications presented as invalid: landing gear status, N1, N2,
ITT, fuel flow and quantity, oil pressure, temperature and
quantity, vibration for LP and HP, flaps, spoilers, all cabin and
APU parameters, all trim values.
During IC-600 # 1 first level pilot initiated BIT, RMU 1 will display
the first page of standby engine indication. The RMU 2 is not
included in the IC-600 # 2 first level pilot initiated BIT.