AIRPLANE
OPERATIONS
MANUAL
GENERAL
REVISION 41
1-00-30
Page
7
Code
01
Copyright © by Embraer. Refer to cover page for details.
AOM-145/1114
Anti Ice System
PITOT 1-2-3 INOP messages modified in order to avoid spurious
occurrences during APU starting.
Powerplant System
ENG NO TO DATA message modified in order to avoid an unlikely
scenario of a takeoff performed with only one engine running.
New messages :
CHECK A1E PERF (only applicable to EMB-145 XR model),
E1-2 FPMU NO DISP (only applicable to EMB-145 XR
model),
E1-2 EXCEEDANCE.
A1E thrust rating modes included on EICAS/RMU/MFD.
New upper range limit for fuel flow indication due to A1E engine.
ITT and N2 Dynamic Redlines.
Oil Pressure Indication modified in order to avoid spurious
indication of low oil pressure values.
ENG 1-2 REV DISAGREE message change in order to avoid a
failure without indication on EICAS.
Pressurization System
Changes to Cabin Altitude Rate.
New function HIGH ALT on MFD Bezel (only applicable to
EMB-145 XR model).
New message HI ALT LDG-T/O (only applicable to EMB-145 XR
model).
Changes to cabin altitude indication on EICAS display.
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