# Embraer Service Bulletin 190-31-0068

Copy: Revision IR ("SB190-31-0068_RevIR"), 16 pages: PDF https://openairdocs.org/files/sha256/38/01/3801d68cc90bdd4c504e125380c0525a9667154949bd4683a75494c1a0d69223; text https://openairdocs.org/service-documents/embraer/sb-190-31-0068/file/3801d68cc90b.md. Rights: © Embraer S.A. Filed by the FAA in regulations.gov docket FAA-2019-0976, the docket of AD 2020-05-21. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Embraer](https://openairdocs.org/service-documents/embraer.md)
- Type: Service bulletin (Service Bulletin)
- Number: 190-31-0068
- Latest revision known: 190-31-0068, Revision IR (OpenAirDocs)
- Page: https://openairdocs.org/service-documents/embraer/sb-190-31-0068

## Text (16 pages)

Rights: © Embraer S.A. Filed by the FAA in regulations.gov docket FAA-2019-0976, the docket of AD 2020-05-21. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

INDICATING/RECORDING SYSTEMS - LOAD 25.8 VERSION FOR PRIMUS EPIC FIELD-LOADABLE
SOFTWARE SYSTEM
In connection with the use of this document, Embraer does not provide any express or implied warranties and expressly disclaims any
warranty of merchantability or fitness for a particular purpose.
This document contains trade secrets, confidential, proprietary information of Embraer and technical data subject to U.S. Export
Administration Regulation ("EAR") and other countries export control laws and regulations. Diversion contrary to the EAR and other laws
and regulations is strictly forbidden. The above restrictions may apply to data on all pages of this document.
1. PLANNING INFORMATION 
A. SB EFFECTIVITY 
Aircraft affected:
MODEL SN
Embraer 190( ) and 195( )
19000002, 19000004, 19000006 thru 19000108, 19000110 thru
19000139, 19000141 thru 19000158, 19000160 thru 19000176,
19000178 thru 19000202, 19000204 thru 19000213, 19000215
thru 19000223, 19000226 thru 19000234, 19000237 thru
19000242, 19000244 thru 19000249, 19000251 thru 19000260,
19000262 thru 19000276, 19000280 thru 19000287, 19000289
thru 19000295, 19000297 thru 19000303, 19000305, 19000306,
19000308 thru 19000314, 19000316, 19000318, 19000320,
19000321, 19000323 thru 19000325, 19000327 thru 19000333,
19000335 thru 19000337, 19000339 thru 19000341, 19000343,
19000344, 19000346, 19000348 thru 19000361, 19000363 thru
19000374, 19000376 thru 19000379, 19000381 thru 19000437,
19000439 thru 19000452, 19000454 thru 19000466, 19000468
thru 19000518, 19000520, 19000521, 19000523 thru 19000525,
19000527, 19000529 thru 19000532, 19000535 thru 19000544,
19000546 thru 19000558, 19000560 thru 19000570, 19000572
thru 19000610, 19000612 thru 19000631, 19000633 thru
19000640, 19000642 thru 19000648, 19000650 thru 19000653,
19000657, 19000660, 19000662 thru 19000682, 19000684 thru
19000686, 19000688, 19000689, 19000692 thru 19000694,
19000696 thru 19000704, 19000706 thru 19000708, 19000710
thru 19000731, 19000733 thru 19000745, 19000747 thru
19000749, 19000752, 19000753, 19000757, and 19000761 thru
19000764.
Affected component:
Network Interface Controller (NIC) / Processor (PROC), Actuator Input-Output Processor (AIOP) and
Central Maintenance Computer (CMC) modules with Pentium II or Pentium M processors.
In-production effectivity:
This bulletin does not affect any in-production aircraft.
B. CONCURRENT REQUIREMENTS 
(1) For aircraft equipped with Head-up Guidance System (HGS), the Head-up Display (HUD)
Software version 811, PN 9801-6270-004 or higher is required.
SERVICE BULLETIN
Date:  Jan 07, 2019
Revision No.: 
SB190-31-0068
Page 1 of 13
Copyright © by Embraer S.A. All rights reserved - See title page for details.

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(2) For all aircraft, installation of Full-Authority Digital Electronic-Control (FADEC) software Version
5.40 or higher is required.
(3) For aircraft equipped with Digital Voice-Data Recorder (DVDR) Universal PN 1605-01-00 or PN
1605-00-00, the accomplishment of SB190-31-0062 is required at the same time of Load 25.8
installation.
C. REASON 
(1) HISTORY
Primus Epic LOAD 25.8 modifications consist of systems improvements and corrections to field
issues found during aircraft operation. The main improvements addressed on LOAD 25.8 are:
– Engine indication logic improvement;
– Change on the Brake Temperature Monitoring System (BTMS) logic to mitigate LG NO
DISPATCH Engine Indication and Crew Alerting System (EICAS) message;
– Altitude split for ground maintenance troubleshooting;
– Improvement on Runway Awareness and Advisory System (RAAS) Inhibit parameter
showed on the Config Page;
– Servo response monitor adjustment to mitigate uncommanded Autopilot (AP) pitch up
event;
– APM Options parameters.
(2) OBJECTIVE
This Service Bulletin introduces PRIMUS EPIC software LOAD 25.8 PN PS7027709-00312.
(3) EXPECTED BENEFITS
LOAD 25.8 presents improvements in the aircraft operation through changes implemented in the
Automatic-Flight Control System (AFCS), Electronic Display System (EDS), Fly-by-wire (FBW)
Maintenance Function, and Aircraft Personality Module (APM) Options:
– EDS system improvement to prevent erroneous indications of both engines (N1/N2 and
ITT);
– EDS system improvement by modifying the break temperature delta from 25 °C to 3 °C for
the LG NO DISPATCH Crew Alerting System (CAS) message and Central Maintenance
Computer (CMC) Fault messages;
– Improvement on APM Options parameters "cmfMeteoReportEnable" to enable the
Meteorological Reports and in the "aircraftTypeATC" to comply with the International Civil
Aviation Organization (ICAO) designation;
– Sys Config Page display improvement in order to show the Runway Awareness and
Advisory System (RAAS) Inhibit information properly on the screen;
– The Servo Response Monitor had an improvement in the monitor's response time in order
to get faster response and Autopilot disengagement when an uncommanded pitch control
input from the autopilot servo occurs. Wheel and Pedal commands follow a similar control
path;
– Improvements of Altitude Split Detection Logic.
SERVICE BULLETIN
SB190-31-0068
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Date:  Jan 07, 2019
Revision No.: 
Copyright © by Embraer S.A. All rights reserved - See title page for details.

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As featured in LOAD 25.5.0.1, 25.6, and 25.7, LOAD 25.8 also has common software load
capability, which will allow its installation in aircraft equipped with NIC/PROC, AIOP and CMC
Pentium II or Pentium M modules. Also, as previously introduced in LOAD 25.7, PRIMUS EPIC
LOAD 25.8 will also permit transmitting AHEAD data when the aircraft is on ground (preflight
phase).
NOTE: Pentium II NIC/PROC modules are not intermixable with Pentium M NIC/PROC
modules, and Pentium II AIOP modules are not intermixable with Pentium M AIOP
modules.
The modification of Modular Avionics Unit (MAU) modules from Pentium II to Pentium M
is performed through the accomplishment of SB190-31-0039 - INSTALLATION OF
PENTIUM M CARDS ON MAU (MODULAR AVIONICS UNIT);
As featured in LOAD 25.5.0.1, 25.6, and 25.7, the CMC modules Pentium II and Pentium M are
interchangeable in LOAD 25.8. Refer to AIPC 45-45-01  - CENTRAL MAINTENANCE
COMPUTER MODULE for modules Part Numbers information.
(4) REVISION HISTORY
None.
D. DESCRIPTION 
The modification presented in this bulletin consists of uploading PRIMUS EPIC LOAD 25.8 version and
doing the flight control system return-to-service test, to do the check of its functionality.
It is necessary to load the current and applicable databases as follows:
– APM Settings version applicable to LOAD 25.8
– APM Options version applicable to LOAD 25.8
– Operational software on Custom I/O modules
– CMC LDI database V14.2
– EGPWS Envelope Modulation database
– EGPWS Terrain Threat database
– FMS Aircraft Performance Database PN 60000692-003 or higher version
– FMS Company Route Database, applicable only for operators that have the subscription to this
database
– FMS Navigation Database
– Only on aircraft equipped with EPIC Communications Management Function (CMF), it is required
to upload the AMI Database PN 69002212-504 (for aircraft equipped with Pentium II) or PN
69002855-506 (for aircraft equipped with Pentium M) or a customized version applicable to
LOAD 25.8
– Only for aircraft equipped with Electronic Checklist (ECL), it is required to upload the applicable
Electronic Checklist (ECL) Database:
 
ECL Designer Tool version 7.4
Subdatabase: Erj024.sdb
SERVICE BULLETIN
Date:  Jan 07, 2019
Revision No.: 
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Copyright © by Embraer S.A. All rights reserved - See title page for details.

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– Only for aircraft equipped with Aeronautical Telecommunications Network (ATN)-Controller Pilot
Datalink Communication (CPDLC), it is required to upload the Air Traffic Control (ATC) Database
PN 69000767-506 or higher version. The new ATC Database PN 69000767-506 is in accordance
with ICAO Doc EUR NSAP Address Registry (EUR Doc 028) Version 8.0 from April 27th, 2018.
 The previous ATC Database PN 69000767-505 was in accordance with Version 2.0 from April
26th, 2012.
 The installation of the latest ATC Database is recommended because it includes 56 new ATC 's
NSAPs (Network Service Access Point).
To reload the applicable databases, it is necessary to connect a notebook Personal Computer (PC)
with Remote Terminal (RT) version 23.2 + Data Loading System (DLS) version 8.1.1 to the Local Area
Network (LAN) port.
Before you do the upload of PRIMUS EPIC LOAD 25.8, only for aircraft equipped with CMC Module
Pentium II, it is required to upload a blank Aircraft Condition-Monitoring Function (ACMF) User
Application. To do this, it is necessary to connect a notebook Personal Computer (PC) with Remote
Terminal (RT) + Data Loading System (DLS) applicable to the currently installed version of PRIMUS
EPIC LOAD. Refer to ITEM GSE 270 for the required version of RT and DLS applicable to the currently
installed version of PRIMUS EPIC LOAD.
Load 25.8 will implement a security code for the APM Options. It is an 8-character password necessary
to install the APM Options. This password will be available on Honeywell website after the Purchase
Order is received.
NOTE: The modification presented in this bulletin does not affect Fatigue Critical Structure (FCS).
E. COMPLIANCE 
This bulletin can be accomplished at the operator’s discretion.
F. APPROVAL 
The changes to the type design specified in this Service Bulletin have been approved by Agência
Nacional de Aviação Civil (ANAC).
NOTE: If any aircraft listed in the SB effectivity has an incorporated modification or repair that is not
from EMBRAER and which affects the content of this Service Bulletin, the operator will take
full responsibility for obtaining approval by a regulatory agency for any adaptation necessary
before the incorporation of this Service Bulletin.
G. ESTIMATED MANPOWER 
This is an estimate of the manpower necessary to accomplish this Service Bulletin on a single aircraft.
It is intended for direct labor only, performed by experienced personnel and does not include the time
to plan, prepare or inspect the work. Sealant, paint or adhesive curing times are not included either.
It is assumed that all the tools, parts and other means are readily available when necessary.
An adjustment to these values may be necessary to meet particular circumstances.
– Access opening: 0.3 man-hours.
– Inspection: None.
– Modification: 7.0 man-hours.
– Access closure: 0.3 man-hours.
– Test: 0.5 man-hours.
SERVICE BULLETIN
SB190-31-0068
Page 4 of 13
Date:  Jan 07, 2019
Revision No.: 
Copyright © by Embraer S.A. All rights reserved - See title page for details.

### Page 5

H. WEIGHT AND BALANCE 
None.
I. SOFTWARE ACCOMPLISHMENT SUMMARY 
None.
J. REFERENCES 
AIPC 190/( ) Aircraft Illustrated Parts Catalog - 45-45-01 - CENTRAL MAINTENANCESYSTEM.
AMM 190/( ) Aircraft Maintenance Manual PART II - 20-00-00 - STANDARDPRACTICES-AIRFRAME.
AMM 190/( ) Aircraft Maintenance Manual PART II - 27-00-00 - FLIGHT CONTROLS.
AMM 190/( ) Aircraft Maintenance Manual PART II - 31-41-00 and 31-41-03 -INDICATING/RECORDING SYSTEMS.
AMM 190/( ) Aircraft Maintenance Manual PART II - 34-61-00 - NAVIGATION.
AMM 190/( ) Aircraft Maintenance Manual PART II - 45-45-00 - CENTRALMAINTENANCE SYSTEM.
ITEM 190/( ) Illustrated Tool and Equipment Manual.
SB190-31-0039 INDICATING/RECORDING SYSTEMS - INSTALLATION OF PENTIUM MCARDS ON MAU (MODULAR AVIONICS UNIT).
SB190-31-0062 INDICATING/RECORDING SYSTEMS - DVDR HARNESS MODIFICATION- FDR BUS 512.
HONEYWELL Honeywell Document SIL D201805000044.
K. OTHER PUBLICATIONS AFFECTED 
AIPC 190/( ) Aircraft Illustrated Parts Catalog - 31-41-00 - INDICATING/RECORDINGSYSTEMS.
AIPC 190/( ) Aircraft Illustrated Parts Catalog - 45-45-01 - CENTRAL MAINTENANCESYSTEM.
AMM 190/( ) Aircraft Maintenance Manual PART I - 31-41-00 - INDICATING/RECORDING SYSTEMS.
AMM 190/( ) Aircraft Maintenance Manual PART II - 31-41-03 - INDICATING/RECORDING SYSTEMS.
ITEM 190/( ) Illustrated Tool and Equipment Manual.
WM 190/( ) Wiring Manual - 31-41-53 and 31-41-54 - INDICATING/RECORDINGSYSTEMS.
SERVICE BULLETIN
Date:  Jan 07, 2019
Revision No.: 
SB190-31-0068
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Copyright © by Embraer S.A. All rights reserved - See title page for details.

### Page 6

ACFOG Airplane Changes Flight Operations Guide.
AOM Airplane Operations Manual.
SOPM Standard Operations Procedures Manual.
IB 190-31-0001 INDICATING/RECORDING SYSTEMS - APM OPTIONS AND SETTINGSGUIDE.
SERVICE BULLETIN
SB190-31-0068
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Date:  Jan 07, 2019
Revision No.: 
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2. MATERIAL INFORMATION 
A. MATERIAL - PRICE AND AVAILABILITY 
(1) MATERIAL AVAILABLE FROM EMBRAER
(a) Download the CMC LDI Database directly from the Flyembraer website
(www.Flyembraer.com):
CMC LDI Part Number Applicability Applicability
190LDI25.8V23.2P2-V14.2
For aircraft equipped with
NIC/PROC Modules
Pentium II For aircraft equipped withFADEC version V5.40,
V5.41, V5.42, V5.50,
V5.61 or higher190LDI25.8V23.2PM-V14.2 For aircraft equipped withNIC/PROC Modules
Pentium M
NOTE: 1) It will be necessary to login to the FlyEmbraer website with a username and
password to download the CMC LDI Database. For details on how to
download and install the CMC LDI software from Flyembraer, refer to Step
3.I. of 3. ACCOMPLISHMENT INSTRUCTIONS this bulletin.
2) LOAD 25.8 requires Full-Authority Digital Electronic-Control (FADEC) version
V5.40 or higher.
(b) Only for aircraft equipped with CMC Pentium II, download a blank ACMF User Application
compatible with LOAD 25.8 directly from the Flyembraer website (www.Flyembraer.com).
NOTE: When you download the ACMF User Application from the Flyembraer website,
make sure that you are logged in (a login name and a password are required). For
details on how to download and install the ACMF User Application from
Flyembraer refer to Step 3.C. of 3. ACCOMPLISHMENT INSTRUCTIONS  of this
bulletin.
(2) MATERIAL AVAILABLE FROM OTHER VENDORS
(a) The compact disk listed in the table below should be procured from the operator’s
inventories or ordered from Honeywell.
Honeywell CD-ROM
Part Number Description Quantity
MM7027704-313 LOAD 25.8 OPS PN PS7027709-00312 01
(b) Check the APM Options PN applicable for each aircraft in the Information Bulletin
IB190-31-0001 - APM OPTIONS AND SETTINGS GUIDE and upload this PN during this
SB accomplishment. For details on how to check the installed the APM Options PN refer to
AMM TASK 31-41-00-970-801-A/200 - Configuration Monitor System (CMS) - System
Configuration Check. The applicable APM Options PN should be procured from the
operator’s inventories or ordered from Honeywell.
NOTE:
1) Once ordered from Honeywell, the APM Options file will be available for
download on Honeywell My Aerospace website (http://
SERVICE BULLETIN
Date:  Jan 07, 2019
Revision No.: 
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Copyright © by Embraer S.A. All rights reserved - See title page for details.

### Page 8

myaerospace.honeywell.com) at the "Aircraft Personality Module (APM)" in
the "SOFTWARE&DATA" menu.
2) Load 25.8 will implement a security code for the APM Options. It is an 8-
character password necessary to install the APM Options. This password will
be available at Honeywell website after the Purchase Order is received
Information Bulletin 190-31-0001 - APM OPTIONS AND SETTINGS GUIDE is located at
Flyembraer website (www.Flyembraer.com) in the path described below:
1 Login to Flyembraer website and access eTechPubs portal.
2 Select "Information Bulletin" under "Service Bulletins".
3 Select IB190-31-0001 - APM OPTIONS AND SETTINGS GUIDE.
(c) APM Settings definition file must be created for the accomplishment of Step 3.F.  of 3.
ACCOMPLISHMENT INSTRUCTIONS.
To create APM Settings definition file, refer to AMM TASK 31-41-03-470-802-A/200  -
Aircraft Personality Module (APM) Settings - Editing and to APM Settings reference files
given in Information Bulletin IB190-31-0001 - APM OPTIONS AND SETTINGS GUIDE.
Refer to Item 2.A.(1)(b)  for IB190-31-0001 - APM OPTIONS AND SETTINGS GUIDE
location at Flyembraer website.
In LOAD 25.8, the CMC Downlink Reports can be configured through APM Settings
parameters. IB190-31-0001 APM Settings Reference Files presents the three existing CMC
Downlink Reports options as provided in Loadable Diagnostic Information (LDI) Files of
previous LOAD versions (from letter A to C). Since these parameters can be changed
according to operators needs, other configurations of CMC Downlink Reports can be
defined following AMM TASK 31-41-03-470-802-A/200 - Aircraft Personality Module (APM)
Settings - Editing instructions.
(d) Make sure that the compact disks with the currently applicable databases listed below are
available before the accomplishment of this bulletin:
– EGPWM Envelope Modulation database;
– EGPWM Terrain Threat database;
– FMS Navigation Database; and
– FMS Company Route Database, applicable only for operators that have the
subscription to this database.
(e) FMS Aircraft Performance Database must be ordered from Honeywell. Make sure that
Performance Database software PN 60000692-003 or higher version is available before the
accomplishment of this Service Bulletin.
(f) Only for aircraft equipped with EPIC Communications Management Function (CMF), make
sure that the compact disk with the applicable AMI Database is available before the
accomplishment of this bulletin, as follows:
AMI Database Software PN NIC/PROC, AIOP Modules
69002212-504 or a customized version
applicable to LOAD 25.8 Pentium II
69002855-506 or a customized version
applicable to LOAD 25.8 Pentium M
SERVICE BULLETIN
SB190-31-0068
Page 8 of 13
Date:  Jan 07, 2019
Revision No.: 
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### Page 9

(g) Only for aircraft equipped with Electronic Checklist (ECL), make sure that the compact disk
with the applicable ECL Database is available before the accomplishment of this bulletin.
(h) Only on aircraft equipped with Controller Pilot Datalink Communication (CPDLC), make
sure that the compact disk with Air Traffic Control (ATC) Database PN 69000767-506 or
higher version is available before the accomplishment of this bulletin.
NOTE: For the ATC Database, refer to 1.D. DESCRIPTION for more details.
B. INDUSTRY SUPPORT INFORMATION 
Contact Honeywell for the necessary documentation or current material prices, availability and
leadtimes.
For the APM Options Part Numbers, operators must contact apmorderentry@honeywell.com. Also for
other databases, refer to Honeywell Service Information Letter (SIL) D201805000044 for details on
ordering the Honeywell Part Numbers mentioned in this Service Bulletin.
For general information on spares orders, contact:
Honeywell Customer Care Center
US & Canada(Toll Free): 1-800-601-3099
International: 1-602-365-3099
www.myaerospace.com
C. MATERIAL NECESSARY FOR EACH AIRCRAFT 
None.
D. MATERIAL NECESSARY FOR EACH SPARE 
None.
E. REIDENTIFIED PARTS 
None.
F. TOOLING - PRICE AND AVAILABILITY 
Whenever required, the necessary tooling presented in the AMM Tasks mentioned in this bulletin
should be procured from the operator’s inventories or ordered as spares.
SERVICE BULLETIN
Date:  Jan 07, 2019
Revision No.: 
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### Page 10

3. ACCOMPLISHMENT INSTRUCTIONS 
NOTE:
1) Obey all of the WARNINGS and CAUTIONS included in the referenced manuals and
procedures.
2) The Manuals and other documents are referred to by acronyms or using a simplified form.
Refer to section 1.J. REFERENCES for more complete definition.
The steps below outline the general accomplishment instructions.
The detailed sequence is included in the respective figure, when necessary.
A. Make sure that the compact disks with the current applicable databases are available before the
accomplishment of the steps below:
(1) EGPWM Envelope Modulation database
(2) EGPWM Terrain Threat database
(3) FMS Aircraft Performance Database PN 60000692-003 (CD PN DM60000692-003) or higher
version
(4) FMS Company Route Database, applicable only for operators that have the subscription to this
database
(5) FMS Navigation Database
(6) EPIC CMF AMI Database PN 69002212-504 (for aircraft equipped with Pentium II) or PN
69002855-506 (for aircraft equipped with Pentium M) or a customized version applicable to
LOAD 25.8, applicable only for aircraft equipped with EPIC CMF
(7) ECL Database, applicable only for aircraft equipped with ECL:
ECL Designer Tool version 7.4
Subdatabase: Erj024.sdb
(8) ATC Database PN 69000767-506 or higher version, applicable only for aircraft equipped with
ATN-CPDLC.
NOTE: For the ATC Database, refer to 1.D. DESCRIPTION for more details.
B. Make sure that the aircraft is safe for maintenance. Refer to the applicable AMM TASK
20-00-00-910-801-A/200 - Aircraft Maintenance Safety Procedures - Standard Procedures.
C. For aircraft equipped with CMC Pentium II, do the full upload of a blank ACMF User Application as
follows:
(1) Do the steps below to download and install the applicable ACMF User Application directly from
the Flyembraer website:
(a) Login to the Flyembraer website using your username and password.
(b) Under the ”Support Center” option, select the “Download Center" menu item.
(c) Select the applicable aircraft model (Commercial Jets).
(d) Select the items in this sequence: Maintenance/Technical Support/E-JETS/Aircraft
Softwares and Reports/ACMF - Aircraft Condition-Monitoring Function/ACMF for Load 25.
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SB190-31-0068
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(e) Click on BLANK file to download.
(f) Unzip the contents of the downloaded file on your Personal Computer (PC) local drive.
Keep the directory structure of the zip file.
(g) Burn the zip file contents on a recordable CD. Keep the original directory structure and use
any CD-Recording application. Use the ISO 9660 file system standard and a volume label
with no more than 16 characters.
NOTE: If the directory structure on the CD is different from the original structure of the zip
file, the Data Loading System (DLS) will not recognize the media and the ACMF
will not be loaded.
(h) After the CD burning, do the full load of the ACMF user application. Refer to AMM TASK
45-45-00-470-801-A/200 - Aircraft Field-Loadable Software Uploading.
NOTE: Make sure that the version of the Remote Terminal (RT) and Data Loading System
(DLS) installed into Personal Computer (PC) is applicable to the currently installed
version of operational software PRIMUS EPIC LOAD.
D. Make sure that the versions of the Remote Terminal (RT) and Data Loading System (DLS) installed
into Personal Computer (PC) are RT 23.2 + DLS 8.1.1 ( Software Tool PN TM7035299-111).
CAUTION: DO NOT POWER CYCLE THE AIRCRAFT BEFORE THE PRIMUS EPIC LOAD 25.8 AND APM
OPTIONS HAVE BEEN FULLY LOADED.
E. Do the full upload of the operational software (PRIMUS EPIC system - LOAD 25.8 - PN
PS7027709-00312). Refer to the applicable AMM TASK 45-45-00-470-801-A/200  - Aircraft Field-
Loadable Software Uploading.
NOTE: The compact disk PN MM7027704-313 is required for the accomplishment of Step 3.E.. Refer
to 2.A. MATERIAL - PRICE AND AVAILABILITY of this bulletin.
F. Create the APM Settings file and do the procedure to full upload the APM settings, according to AMM
TASK 31-41-03-470-802-A/200 - Aircraft Personality Module (APM) Settings - Editing and AMM TASK
45-45-00-470-801-A/200 - Aircraft Field-Loadable Software Uploading. Refer to IB190-31-0001 - APM
OPTIONS AND SETTINGS GUIDE for the APM Settings Reference Files.
NOTE: In LOAD 25.8, the CMC Downlink Reports can be configured through APM Settings
parameters. IB190-31-0001 APM Settings Reference Files presents the three existing CMC
Downlink Reports options as provided in Loadable Diagnostic Information (LDI) Files of
previous LOAD versions (from letter A to C).
Since these parameters can be changed according to operators needs, other configurations of
the CMC Downlink Reports can be defined according to AMM TASK 31-41-03-470-802-A/200
- Aircraft Personality Module (APM) Settings - Editing instructions.
G. Do the full upload of the applicable APM Options according to AMM TASK 45-45-00-470-801-A/200  -
Aircraft Field-Loadable Software Uploading. Refer to the Item 2.A.(2)(b) at 2.A. MATERIAL - PRICE
AND AVAILABILITY for APM Options selection information.
NOTE: Load 25.8 will implement a security code for the APM Options. It is an 8-character password
necessary to install the APM Options. This password will be available on Honeywell website
after the Purchase Order is received.
H. Do the target upload of the operational software to the Custom I/O 1 and Custom I/O 2 modules. Refer
to AMM TASK 45-45-00-470-801-A/200 - Aircraft Field-Loadable Software Uploading.
I. Do the full upload of the CMC LDI Database V14.2, as applicable, as follows:
SERVICE BULLETIN
Date:  Jan 07, 2019
Revision No.: 
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(1) Do the steps below to download and install the CMC LDI database directly from the Flyembraer
website:
(a) Login to the Flyembraer website, using your user name and password.
(b) Under the "Support Center" option, select the "Download Center" menu item.
(c) Select the applicable aircraft model (Commercial Jets).
(d) Select the items using the sequence: Maintenance/Technical Support/E-JETS/Aircraft
Softwares and Reports/ LDI - Loadable Diagnostic Information - Repository/Aircraft LDIs.
(e) Select the applicable program (Embraer 190/195) and then the version LDI V14.2, as
applicable.
(f) Click on the applicable part number to download the file. Refer to Item 2.A.(1)(a) at 2.A.
MATERIAL - PRICE AND AVAILABILITY.
(g) Unzip the contents of the downloaded file on your Personal Computer (PC) local drive.
Keep the directory structure of the zip file.
(h) Burn the zip file contents on a recordable CD. Keep the original directory structure and use
any CD-Recording application. Use the ISO 9660 file system standard and a volume label
with no more than 16 characters.
NOTE: If the directory structure on the CD is different from the original structure of the zip
file, the Data Loading System (DLS) will not recognize the media and the LDI will
not be loaded.
(i) After the CD burning, do the full load of the CMC LDI Database. Refer to AMM TASK
45-45-00-470-801-A/200 - Aircraft Field-Loadable Software Uploading.
J. Do the full upload of EGPWS Envelope Modulation Database. Refer to AMM TASK 45-45-00-470-801-
A/200 - Aircraft Field-Loadable Software Uploading.
K. Do the full upload of EGPWS Terrain Threat Database to the EGPWM module. Refer to AMM TASK
45-45-00-470-801-A/200 - Aircraft Field-Loadable Software Uploading.
L. Do the full upload of the currently applicable FMS Aircraft Performance Database PN 60000692-003 or
higher version. Refer to AMM TASK 45-45-00-470-801-A/200 - Aircraft Field-Loadable Software
Uploading.
M. Do the full upload of the currently applicable FMS Company Route Database, applicable only for
operators that have the subscription to this database. Refer to AMM TASK 45-45-00-470-801-A/200 -
Aircraft Field-Loadable Software Uploading.
N. Do the full upload of latest applicable FMS Navigation Database. Refer to AMM TASK
34-61-00-470-801-A/200 - Navigation Database - Loading.
O. For aircraft equipped with EPIC Communications Management Function (CMF), do the full upload of
the applicable EPIC CMF AMI Database. Refer to AMM TASK 45-45-00-470-801-A/200 - Aircraft Field-
Loadable Software Uploading.
AMI Database Software PN NIC/PROC, AIOPModules
69002212-504 or a customized version applicable to LOAD 25.8 Pentium II
69002855-506 or a customized version applicable to LOAD 25.8 Pentium M
SERVICE BULLETIN
SB190-31-0068
Page 12 of 13
Date:  Jan 07, 2019
Revision No.: 
Copyright © by Embraer S.A. All rights reserved - See title page for details.

### Page 13

P. For aircraft equipped with Electronic Checklist (ECL), do the full upload of the applicable ECL
Database as given below. Refer to AMM TASK 45-45-00-470-801-A/200  - Aircraft Field-Loadable
Software Uploading.
ECL Designer Tool version 7.4
Subdatabase: Erj024.sdb
Q. For aircraft equipped with Controller Pilot Datalink Communication (CPDLC), do the full upload of the
Air Traffic Control (ATC) Database PN 69000767-506 or higher version. Refer to AMM TASK
45-45-00-470-801-A/200 - Aircraft Field-Loadable Software Uploading.
NOTE: For the ATC Database, refer to 1.D. DESCRIPTION for more details.
R. Do the flight controls system return-to-service test. Refer to AMM TASK 27-00-00-070-801-A/200 -
Flight Controls System (Return-to-Service) - Test.
S. Put the aircraft back to a serviceable condition.
T. Write the accomplishment of this bulletin in the applicable documents.
NOTE: 1) Please inform us by e-mail fleet.reliability@embraer.com.br of the aircraft manufacturer
serial number and the SB incorporation date, specifying the SB Part(s) incorporated or
whether the whole SB has been incorporated. This will enable Embraer to consider your
aircraft configuration when providing future modifications.
2) To formally inform that the SB has been incorporated fleet-wide or that the SB will not be
incorporated, so that Embraer can update the affected technical publications, use the
“Service Bulletin Full-Fleet Incorporation Report” form, which is available on the
Flyembraer portal (http://www.flyembraer.com).
3) Use the attached “Service Bulletin Evaluation” form to send us your comments regarding
this SB. Your feedback will be much appreciated as an aid for us to improve the quality
of the SBs.
SERVICE BULLETIN
Date:  Jan 07, 2019
Revision No.: 
SB190-31-0068
Page 13 of 13
Copyright © by Embraer S.A. All rights reserved - See title page for details.

### Page 14

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### Page 15

The purpose of this form is to collect data that will be used to improve the quality of our Service Bulletins and
Reliability Program.
EMBRAER S.A.
FLEET PERFORMANCE & RELIABILITY
Av. Brig. Faria Lima, 2170
São José dos Campos - SP
CEP: 12227-901
Brasil
e-mail: fleet.reliability@embraer.com.br
S.B.: (Number / Rev.) S.B. Title:
  
SB Implementation Report
Aircraft Serial Number or Registration Number:
 
Incorporation Date:
 
Aircraft Flight Hours:
 
Aircraft Landings:
 
SB Evaluation  (Check applicable boxes below and use the space as required to provide any additional information)
Estimated Manpower: [ ] OK [ ] NOT OK
Material & Kits: [ ] OK [ ] NOT OK
Accomplishment Instructions: [ ] OK [ ] NOT OK
Figures: [ ] OK [ ] NOT OK
SB General Evaluation: [ ] OK [ ] NOT OK
Comments:  (Bulletin quality, difficulties found at the time of incorporation, suggested improvements, other)
Company/ Service Center:
 
E-mail:
 
Phone:
 
Address:
 
Form filled by:
 
Work Order:
 
SERVICE BULLETIN EVALUATION
Copyright © by Embraer S.A. All rights reserved - See title page for details.

### Page 16

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