Embraer EMB145 - Page 1345

GROUND SERVICING
AIRPLANE
O
PERATIONS
MANUAL
1-12-60
Page
12
Code
01
REVISION 41
Copyright © by Embraer. Refer to cover page for details.
AOM
-
145/1114
ATA
EICAS
MESSAGE
or
CONDITION
LOCATION PROCEDURE
28
FCU X
ARINC 429
message
appears on
the repeater
indicator
panel
FCU
Do the electrical fuel quantity
indication check.
Transitory condition of the wing fuel
conditioning unit.
On the repeater indicator panel, set
the toggle switch to the TEST
position and clear the fault message.
28
FCU X FAIL
message on
the repeater
indicator
panel
FCU
Do the electrical fuel quantity
indication check.
Transitory condition of the wing fuel
conditioning unit.
On the repeater indicator panel, set
the toggle switch to the TEST
position and clear the fault message.
34
HDG 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.