GROUND SERVICING
AIRPLANE
OPERATIONS
MANUAL
1-12-60
Page
8
Code
01
TEMPORARY REVISION 41.1
Copyright © by Embraer. Refer to cover page for details.
AOM-145/1114
ATA
EICAS
MESSAGE
or
CONDITION
LOCATION PROCEDURE
27
Aileron – No
roll control
through the
switch
(Transitory
condition of
the roll trim
electrical
circuit)
AILERON
Make sure that the ROLL TRIM
circuit breaker is closed.
Energize the airplane with hydraulic
pressure.
Do a roll trim test through the roll trim
switch:
(1) Push the roll trim switch to the
LWD position for approximately
3 seconds. The roll trim system is
automatically deactivated in
3 seconds.
(2) Push the roll trim switch to the
RWD position for approximately
3 seconds. The roll trim system is
automatically deactivated in
3 seconds.
34
LT Flag on
the ISIS
(SMITHS
and
THALES)
ISIS
(1) On the circuit breaker panel, open
and close the INTEG STBY circuit
breaker.
NOTE: Before turning on the
ISIS, make sure that there is no
dynamic pressure applied to
Pitot/Static 3. It must be
equivalent to an airspeed equal to
or greater than 60 knots.
The airplane must be maintained
stationary during the ISIS
initialization.
(2) The display shows an initialization
page for 70 seconds (ISIS
SMITHS) or for 90 seconds (ISIS
THALES).
(3) Wait until the ISIS completes its
initialization.
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