Embraer EMB145 Operation Manual page 1921

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