Embraer EMB145 - Page 1304

AIRPLANE
OPERATIONS
MANUAL
GROUND SERVICING
TEMPORARY REVISION 41.1
1-12-60
Page
3
Code
01
Copyright © by Embraer. Refer to cover page for details.
AOM-145/1114
ATA
EICAS
MESSAGE
or
CONDITION
LOCATION PROCEDURE
34
Absence of
ADF 1
bearing
information
on the
RMU and
on the PFD
and MFD
(Transitory
condition of
Integrated
Navigation
Unit 1)
ADF
(1) Set the cursor of RMU 1 to the
ADF 1 window.
(2) Do the test of the frequency
selection:
(a) Put the cursor on the selected
frequency code.
(b) Turn the dual concentric
knobs.
A frequency code can be set.
(3) Do the self-test:
(a) Set the RMU 1 to the ADF 1
window.
(b) Push and hold the RMU TST
function key.
On the RMU, the ADF 1
window shows:
 TEST and ADF TEST
(amber).
 TEST (amber) and ADF
PASS (green), at the end of
the test cycle.
NOTE: An ADF ERR (red) is the
indication that the selected ADF
is defective.