Embraer EMB145 - Page 1306

AIRPLANE
OPERATIONS
MANUAL
GROUND SERVICING
TEMPORARY REVISION 41.1
1-12-60
Page
5
Code
01
Copyright © by Embraer. Refer to cover page for details.
AOM-145/1114
ATA
EICAS
MESSAGE
or
CONDITION
LOCATION PROCEDURE
34
Absence of
DME 1
distance
information
on the RMU
and on the
PFD and
MFD
(Transitory
condition of
Integrated
Navigation
Unit 1)
DME
(1) On RMU 1, push the DME
function key.
(2) Move the cursor of RMU 1 to the
DME 1 window.
(3) Do the test of frequency
selection:
(a) Put the cursor on the selected
frequency code.
(b) Turn the dual concentric
knobs.
A frequency code can be set.
(4) Do the self-test:
(a) Set the RMU 1 to the DME 1
window.
(b) Push and hold the RMU TST
function key.
On the RMU, the DME 1
window shows:
 TEST and DME TEST
(amber).
 TEST (amber) and DME
PASS (green), at the end of
the test cycle.
NOTE: A DME ERR (red) is the
indication that the selected DME
is defective.