Embraer EMB145 Operation Manual page 1922

TYPE
E1 (2) ADC DATA FAIL Loss of either ADC data or
E1 (2) FADEC FAULT
(if applicable)
E1 (2) CTL A (B)
DEGRAD
ADVISORY
(if applicable)
E1 (2) SHORT DISP
(if applicable)
CHECK XXX PERF
(XXX=A, A1, A1/1, A1P, A3,
A1/3, A1E)
REVISION 41
AIRPLANE
OPERATIONS
MANUAL
MESSAGE
(if applicable)
Copyright © by Embraer. Refer to cover page for details.
MEANING
synthesized T2
temperature source.
A dispatchable MMEL FADEC
fault was detected.
A dispatchable MMEL FADEC
fault was detected.
A dispatchable MMEL FADEC
fault was detected.
Inform t he FADEC application
installed in
Displayed only on ground with
flaps 0° and parking brakes
applied.
2-10-50
POWERPLANT
used as
the airplane.
Page Code
21 01