Embraer EMB145 - Page 1921

POWERPLANT
AIRPLANE
O
PERATIONS
MANUAL
2-10-50
Page
20
Code
01 REVISION 41
Copyright © by Embraer. Refer to cover page for details.
AOM
-
145/1114
TYPE
MESSAGE
MEANING
E1 (2) CTL A (B) FAIL
A failure in the Engine control
system has been detected.
E1 (2) CTL FAIL
(if applicable)
A failure in the Engine control
system has been detected.
ENG1 (2) TLA FAIL
Thrust Lever Angle sensor has
failed.
ENG NO TO DATA
Takeoff Data has not been
successfully entered with
engine running and above
53% N2.
FADEC ID NO DISP
(if applicable)
There are different FADEC
applications installed in the
airplane.
ENG 1 (2) OUT
(if applicable)
N2 has dropped below
8500
rpm (underspeed
shutdown limit) uncommanded.
E1(2) NO DISP
(if applicable)
Associated FADEC has
detected a non-dispatch
failure
condition.
E1 (2) EXCEEDANCE
(if applicable)
ITT or N2 exceeded the current
ITT or N2 limit during an
interval of the flight leg.
CAUTION
E1 (2) FPMU NO DISP
(if applicable)
An incompatible FPMU was
installed on a A1E engine.
E1 (2) OIL IMP BYP
The differential pressure
across the oil filter has
exceeded the normal range.
ADVISORY
E1 (2) FUEL IMP BYP
The differential pressure
ac
ross the fuel filter has
exceeded the normal range.