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Embraer EMB145 - Page 82

Embraer EMB145
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AIRPLANE
OPERATIONS
MANUAL
GENERAL
REVISION 41
1-00-30
Page
1
Code
01
Copyright © by Embraer. Refer to cover page for details.
AOM-145/1114
EICAS VERSIONS
VERSIONS 14A AND 15A
Fix the Pitch Trim Runaway Monitoring logic (airplanes equipped
with EICAS 14 or 15 are not allowed to use the Autopilot below
1500 ft).
VERSION 14
CAT II capability.
VERSION 15
Oil pressure green indication increased to 95 psi and red above it
(on EICAS 14 it was green up to 90 psi and amber above it).
Higher brake temperature limits for LR brakes.
ICE/SPS ADVANCED renamed SPS/ICE SPEEDS.
Flaps 18 capability.
Autopilot “wing rocking” improvements.
VERSION 15B
Fixes the nuisance “Check PFD” message.
VERSION 16
ENG1 (2) REV DISAGREE message logic improved in order to
avoid spurious alarms.
RUD HDOV PROT FAIL message logic improved in order to avoid
spurious alarms.
Enhanced engine Time Limited Dispatch (TLD) incorporated:
E1 (2) CTL A (B) DEGRAD removed;
E1 (2) CTL A (B) FAIL revised (indicates loss of CVG/MMV
control);
E1 (2) NO DISP incorporated;
E1 (2) SHORT DISP incorporated.

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