Embraer EMB145, Operation Manual

Page: 83 / 2662

GENERAL AIRPLANE
OPERATIONS
MANUAL
1-00-30
Page
2
Code
01 REVISION 41
Copyright © by Embraer. Refer to cover page for details.
A
O
M-145/1
114

Improvements in other engine messages not TLD related:

E1 (2) LOW N1 revised (available only for takeoff below V1-15);

ENG1 (2) OUT incorporated;

ENG 1-2 OUT incorporated;

ENG1 (2) TLA FAIL revised;

FADEC ID NO DISP incorporated;

CHECK xxx PERF incorporated;

E1 (2) ADC DATA FAIL removed.

New FD control laws with different gain programming for FD modes
in order to improve the Flight Director capture speed.

Incorporation of the VERTICAL and LATERAL MODE OFF
messages.

IC CONFIG FAIL cyan message (dispatchable) created to indicate
a IM-600 failure and use by the IC-600 of the latest IM-600 valid
data.

CONFIG MISMATCH cyan message (no takeoff) created to
indicate that there is a discrepancy in the configuration module (IM-
600) of each IC-600. The configuration module stores several
aircraft configuration parameters.
VERSION 16.5

Anti-Icing system improvements (new messages and logic):

A/I LOW CAPACITY incorporated;

WG1 (2) A/ICE FAIL and WG ASYMETRY removed;

WG A/ICE FAIL incorporated;

ENG A/ICE OVERPRES incorporated;

ENG1 (2) A/ICE FAIL renamed to E1 (2) A/ICE FAIL.

TAT 1-2 HEAT INOP logic changed to improve TAT and SAT
indications and to increase the probes life.

Brake messages logic changed to avoid failure messages due to
power drop during APU start on ground.

A1P and A1/3 thrust labels renamed from ALT T/O and T/O, to T/O
and T/O RSV respectively.

ATTCS NO MRGN improvements for the A3 engine.

Support to the 8.33 kHz tune function in the FMZ 2000 FMS.

APU FUEL LO PRESS logic changed to avoid spurious messages
during APU pressure transients.

Support to Inertial System (IRS) as an AHRS replacement.

Improvement in the Cabin Pressure Control System (CPCS)
indication in order to avoid unnecessary amber indication on the
EICAS.