Embraer EMB145, Operation Manual

Page: 87 / 2662

GENERAL AIRPLANE
OPERATIONS
MANUAL
1-00-30
Page
6
Code
01 REVISION 41
Copyright © by Embraer. Refer to cover page for details.
A
O
M-145/1
114
VERSION 19
The EICAS 19 features implemented in the software are described
below:
Air conditioning system

The Bleed Temperature Pointers were modified to remain amber at
all the times that the messages BLD 1(2) LOW TEMP are
displayed.
Brake System

New digital brake temperature indication on MFD (if IM-600 Digital
BRK TEMP parameter is enabled).
EICAS Internal Logic

New message DAU AC ID MISCMP.
Electrical System

GPU Voltage Indication modified in order to avoid dashes when the
indication should be 0 V.
Flap System

Flap 22 indication in red on EICAS display and NO TAKEOFF
CONFIG message when the aircraft is not certified to take off with
flaps 22º.
Fuel System

New Message FUEL EQ XFEED OPN to inform that the imbalance
was correct and the crossfeed valve is still open.

Fuel Test Page units label modified in order to show the correct
English/Metric configuration.
General Changes

Synchronization of the Speed Target Bug with the previous
selected Speed Target instead of synchronizing with the current
aircraft’s speed shown on the Speed Tape when VS Vertical Flight
Director Mode is de-selected.

Windshear indication on PFD always in red when RA test button is
pressed.

Due to mandatory installation of IM-600 on this EICAS version and
on, the CAT II Operation is available and indicated.