# FALCON 7X

No 214

AUGUST 30, 2011


# MANDATORY

ATA 27

FLIGHT CONTROLS MODULAR ELECTRONIC FLIGHT CONTROL SYSTEM

FCS STANDARD 2.1.7.3 

# FALCON SERVICE BULLETIN

Copyright © 2011 by Dassault Aviation All rights reserved. No part of this work may be reproduced or copied in any form or by any means without written permission

of Dassault Aviation.

785FLIGHT CONTROLS MODULAR ELECTRONIC FLIGHT CONTROL SYSTEM

FCS STANDARD 2.1.7.3

Initial issuance August 30, 2011
List of effective pages : 1 to 9 

## FALCON 7X 7X-214

ATA 27FLIGHT CONTROLS MODULAR ELECTRONIC FLIGHT CONTROL SYSTEM

FCS STANDARD 2.1.7.3

1. PLANNING INFORMATION

A. EFFECTIVITY This Service Bulletin is applicable to FALCON 7X aircraft with serial numbers 1 and subsequent which have not previously implemented DASSAULT AVIATION modification 7X M1245.

NOTE 1: Dassault Aviation Service Bulletin 7X-215 “ GENERAL - AIRPLANE FLIGHT MANUAL

REVISION 13 - ELECTRONIC CHECKLIST V0008 DATABASE” must be performed simultaneously.

NOTE 2: The implementation of the following Service Bulletin is a prerequisite:

• Service Bulletin FALCON 7X-211 ( or modifications FALCON 7X M1235 and M1236) “ADDITION OF A REVERSION LOGIC AND MANUAL OVERRIDE”.

B. REASON The purpose of this Service Bulletin is to modify the digital flight control system to lift the limitations set by Service Bulletin 7X-211 (M1235 and M1236).

C. DESCRIPTION The operation consists in: • replacing the following modules: • HSTC 3 module ( 403CZ ), • HSTC 4 module ( 1304CZ ), • uploading the following modules:

CAUTION: UPLOADING MUST BE PERFORMED BY AN OPERATOR AUTHORIZED BY THE

COMPONENT MANUFACTURER DASSAULT EQUIPMENTS AFTER A SPECIFIC TRAINING. • MAIC xA modules ( 1402CZ )/( 1202CZ )/( 601CZ )/( 401CZ ), • MFCC xA modules ( 901CZ )/( 1101CZ )/( 1301CZ ), • MFCC xB modules ( 801CZ )/( 1001CZ )/( 1201CZ ). • replacing the speed limitation placards on the instrument panel.

D. COMPLIANCE Mandatory:

• It is anticipated that this Service Bulletin will be rendered mandatory by an EASA Airworthiness Directive. • As prescribed by the Airworthiness Authorities of the country of registration of the aircraft. 

## FALCON 7X 7X-214

August 30, 2011 ATA 27

Initial issuance Page 1 / 9DASSAULT AVIATION Proprietary DataE. APPROVAL

This Service Bulletin covers DASSAULT AVIATION modification FALCON 7X M1245 which has been approved by EASA. The technical content of this document is approved under the authority of DOA nr. EASA.21J.051.

F. LABOR

Estimated labor-hours: • 6 hours for access. • 1 hour for the replacement of the modules. • 3 hours for the uploading of the modules. • 1 hour for the tests.

NOTE: These labor-hours only concern the work described in this Service Bulletin and do not include other maintenance work which may be performed on this occasion.

G. MATERIAL - PRICE AND AVAILABILITY The modification kit may be obtained from either address listed below:
Western hemisphere: DASSAULT FALCON JET CORP.
SPARES DISTRIBUTION CENTER
200 RISER ROAD LITTLE FERRY, NJ 07643 U.S.A. Telephone: • CANADA and U.S.A.: 1-800-800-4036 • MEXICO: 001-800-800-4036 • Other countries: 1-201-541-4809
Fax: • CANADA and U.S.A.: 1-800-800-4817 • MEXICO: 001-800-800-4817 • Other countries: 1-201-440-7021
Other continents: DASSAULT AVIATION Falcon Spares
BOITE POSTALE N°101
AEROPORT DU BOURGET 93350 - LE BOURGET Cedex (FRANCE) Please contact your Dassault Aviation Account Representative Telephone: 33 (0)1.48.35.56.78 Fax: 33 (0)1.48.35.56.00
Price and availability on request.

H. TOOLING - PRICE AND AVAILABILITY • Normal maintenance tooling. 

## FALCON 7X 7X-214

August 30, 2011 ATA 27

Initial issuance Page 2 / 9DASSAULT AVIATION Proprietary Data• maintenance computer ( TO-45-100 ) including software application media installed with MEM40507-01 installation media. • Standard USB cable. • Refer to paragraph 3. “MATERIAL INFORMATION”

I. WEIGHT AND BALANCE Change in weight: None. Change in balance with respect to 25% MAC: None.

J. REFERENCES

Standard Practices: • GENERAL MAINTENANCE AND SAFETY PRECAUTIONS (Refer to TASK 20-00-00-910-801 ).
Aircraft Maintenance Manual:

• ENERGIZATION / DE-ENERGIZATION OF THE AIRCRAFT WITH THE ELECTRICAL GROUND POWER UNIT (GPU) (Refer to TASK 24-00-00-860-803 ). • GROUND TEST OF THE FCS (Refer to TASK 27-00-00-700-802 ).

• FUNCTIONAL TEST OF THE FLIGHT CONTROL SYSTEM WITH HYDRAULIC POWER (Refer to TASK 27-00-00-720-801 ).

• FUNCTIONAL TEST OF THE FLIGHT CONTROL SYSTEM WITHOUT HYDRAULIC POWER (Refer to TASK 27-00-00-720-802 ).

• REMOVAL / INSTALLATION OF THE LH REAR FCS MODULES ( Refer to TASK 27-90-01-900-802 ). • REMOVAL / INSTALLATION OF THE RH REAR MODULES (Refer to TASK 27-90-01-900-804 ).

• PRESSURIZATION / DE-PRESSURIZATION OF THE HYDRAULIC SYSTEMS WITH THE HYDRAULIC GROUND POWER UNIT (GPU) (Refer to TASK 29-00-00-860-803 )

• USE OF THE CENTRAL MAINTENANCE COMPUTER (CMC) - QUICK REFERENCE HANDBOOK (Refer to TASK 45-10-00-910-801 ).
Fault Isolation Manual: • AIRCRAFT SERIAL LINKS (Refer to SDS 27-90-01 ). • TROUBLESHOOTING PROCEDURE FOR THE FCS (Refer to TASK 27-00-00-910-801 )

K. OTHER PUBLICATIONS AFFECTED The following publication is revised to account for the changes introduced by this Service Bulletin: • Airplane Flight Manual CP58. • Chapter 5-40 CP010 (revision 2) The following publications will be revised at a later date to account for the changes introduced by this Service Bulletin: • Illustrated Parts Catalog. • Aircraft Maintenance Manual. • CODDE 1 revision 7. 

## FALCON 7X 7X-214

August 30, 2011 ATA 27

Initial issuance Page 3 / 9DASSAULT AVIATION Proprietary Data2. ACCOMPLISHMENT INSTRUCTIONS

A. PRELIMINARY STEPS (1) The aircraft must be in the maintenance configuration (Refer to TASK 20-00-00-910-801 ): • aircraft on wheels, • no other work performed on electrical sytems and landing gears.
CAUTION: UPLOADING OF THE MODULES CAN ONLY BE DONE WHEN THE FCS SYSTEM

IS COMPLETELY OPERATIONAL. (2) Perform the ground test of the FCS (Refer to TASK 27-00-00-700-802 , paragraphs 3 and 4. ):

• If the ground test is completed with the amber " FCS: TEST FAIL " or " CHECK STATUS " CAS messages displayed on the primary display unit, perform the troubleshooting procedure for the FCS (Refer to TASK 27-00-00-910-801 , paragraph 4. B. to 4. D. ). • If no FCS related CAS and/or Fault messages are displayed, then perform the “CLOSE-UP” paragraph of the ground test of the FCS (Refer to TASK 27-00-00-700-802 , paragraph 5 ).

B. PROCEDURE

CAUTION: STRICTLY RESPECT THE FOLLOWING SEQUENCE.

NOTE: The removed modules must be sent to one of the addresses listed in paragraph 1. G. of this Service Bulletin. (1) In the LH rear FCS rack ( 2003CZ ) , replace the HSTC 3 module ( 403CZ ) ( Refer to TASK 27-90-01-900-802 ). (2) In the RH rear FCS rack ( 2004CZ ) , replace the HSTC 4 module ( 1304CZ ) ( Refer to TASK 27-90-01-900-804 ). (3) Upload the following modules (refer to DASSAULT AVIATION FCS data loading procedure DT EQUIP 43913 issue D):
CAUTION: UPLOADING MUST BE PERFORMED BY AN OPERATOR AUTHORIZED BY THE

COMPONENT MANUFACTURER DASSAULT EQUIPMENTS AFTER A SPECIFIC TRAINING.
NOTE: The MAIC and MFCC modules to be uploaded are installed in LH front FCS rack ( 2001CZ ) and RH front FCS rack ( 2002CZ ). • MAIC 1A module ( 1402CZ ), • MAIC 3A module ( 1202CZ ), • MAIC 2A module ( 601CZ ), • MAIC 4A module ( 401CZ ), • MFCC 1A module ( 901CZ ), • MFCC 1B module ( 801CZ ), • MFCC 2A module ( 1101CZ ), • MFCC 2B module ( 1001CZ ), • MFCC 3A module ( 1301CZ ), • MFCC 3B module ( 1201CZ ). 

## FALCON 7X 7X-214

August 30, 2011 ATA 27

Initial issuance Page 4 / 9DASSAULT AVIATION Proprietary Data(4) Remove all the speed limitation placards installed on the instrument panel ( A-fig. 1) and replace each of them with a new one (B-fig. 1) using araldite AV138M + hardener HV998

. NOTE: Depending on the aircraft configuration, two or three placards are needed.

C. FINAL STEPS

CAUTION: STRICTLY RESPECT THE FOLLOWING SEQUENCE. (1) Partially perform “MODULE TEST” ( Refer to TASK 27-00-00-720-801 , only paragraph 5. A. “Job set-up” ). (2) Check the identification of the modules ( Refer to TASK 27-00-00-720-802 , only paragraph 5 “MODULE IDENTIFICATIONS” ).

MODULES NEW P/N
MFCC 1A module ( 901CZ ) ENS7X101-13
MFCC 1B module ( 801CZ ) ENS7X102-13
MFCC 2A module ( 1101CZ ) ENS7X101-13
MFCC 2B module ( 1001CZ ) ENS7X102-13
MFCC 3A module ( 1301CZ ) ENS7X101-13
MFCC 3B module ( 1201CZ ) ENS7X102-13
MAIC 1A module ( 1402CZ ) ENS7X501-23
MAIC 2A module ( 601CZ ) ENS7X501-23
MAIC 3A module ( 1202CZ ) ENS7X501-23
MAIC 4A module ( 401CZ ) ENS7X501-23
HSTC 3 module ( 403CZ ) 0877X403-13
HSTC 4 module ( 1304CZ ) 0877X404-14
(3) Go to the 27-90 " AIRCRAFT SERIAL LINKS " maintenance screens ( Refer to TASK 45-10-00-910-801 ) and verify that no failure exists between MAICx and MAUx modules ( Refer to SDS 27-90-01 ). (4) Remove the four multi-function probe covers ( KPC3-780-45 ). (5) On the overhead panel ( 5000PM ) , set the " PROBE 1+2" pushbutton ( R9810PM ) , the " PROBE 3" pushbutton ( R9820PM ) and the "PROBE 4" pushbutton ( R9830PM ) to the ON position. (6) Perform the ground test of the FCS (Refer to TASK 27-00-00-700-802 , paragraph 4. ):

• If the ground test is completed with the amber " FCS: TEST FAIL " or " CHECK STATUS " CAS messages displayed on the primary display unit, perform the troubleshooting procedure for the FCS (Refer to TASK 27-00-00-910-801 , paragraph 4. B. to 4. D ). • If no FCS related CAS and/or Fault messages are displayed, then perform the “CLOSE-UP” paragraph of the ground test of the FCS (Refer to TASK 27-00-00-700-802 , paragraph 5 ).

D. DOCUMENTATION 

## FALCON 7X 7X-214

August 30, 2011 ATA 27

Initial issuance Page 5 / 9DASSAULT AVIATION Proprietary Data(1) Record the results of this Service Bulletin in the “NEW STANDARD INSTALLATION CHECKLIST” sheet attached. (2) Have the “NEW STANDARD INSTALLATION CHECKLIST” sheet signed by an aircraft inspector. (3) Send back the “NEW STANDARD INSTALLATION CHECKLIST” sheet and the “FIELD UPLOAD RECORD” to DASSAULT AVIATION at technicalcenter@dassault-aviation.com. (4) Update the Airplane Flight Manual with CP58 pages. (5) Incorporate Chapter 5-40 CP010 (revision 2).

E. RECORDING Record compliance with this Service Bulletin in the appropriate aircraft documents. Fill out the electronic Service Bulletin reply form located in the ”Service Bulletin" page on the Falcon portal. 

## FALCON 7X 7X-214

August 30, 2011 ATA 27

Initial issuance Page 6 / 9DASSAULT AVIATION Proprietary Data3. MATERIAL INFORMATION

A. MODIFICATION OF MODULE PART NUMBERS (1) Module Part Numbers to be uploaded

NEW P/N QTY DESIGNATION OLD P/N
ENS7X101-13 1 MFCC 1A module ( 901CZ ) ENS7X101-12

ENS7X102-13 1 MFCC 1B module ( 801CZ ) ENS7X102-12

ENS7X101-13 1 MFCC 2A module ( 1101CZ ) ENS7X101-12

ENS7X102-13 1 MFCC 2B module ( 1001CZ ) ENS7X102-12

ENS7X101-13 1 MFCC 3A module ( 1301CZ ) ENS7X101-12

ENS7X102-13 1 MFCC 3B module ( 1201CZ ) ENS7X102-12

ENS7X501-23 1 MAIC 1A module ( 1402CZ ) ENS7X501-22

ENS7X501-23 1 MAIC 2A module ( 601CZ ) ENS7X501-22

ENS7X501-23 1 MAIC 3A module ( 1202CZ ) ENS7X501-22

ENS7X501-23 1 MAIC 4A module ( 401CZ ) ENS7X501-22
(2) Module Part Numbers to be removed and replaced

NEW P/N QTY DESIGNATION OLD P/N
0877X403-13 1 HSTC 3 module ( 403CZ ) 0877X403-12

0877X404-14 1 HSTC 4 module ( 1304CZ ) 0877X404-13

B. MODIFICATION KIT

KIT P/N SBF7X0214A

NOTE: • Depending on the aircraft configuration, two or three placards are needed: • 2 kits for aircraft without the Electronic Flight Bag (EFB) installation, • 3 kits for aircraft with the EFB installation.

NEW P/N QTY KEY WORD OLD P/N
F7XC531811115 1 Speed limitation placard F7XC531811115A1

C. RENTAL TOOLS

NEW P/N QTY DESIGNATION 

## FALCON 7X 7X-214

August 30, 2011 ATA 27

Initial issuance Page 7 / 9DASSAULT AVIATION Proprietary DataMEM405-01 including: • MGB660-01 • MEM40501-01 • MEM40505-01 • MEM40506-01 • MEM40504-01 • MEM40508-01 1 • 1 • 1 • 1 • 1 • 1 • 1 FCS UPLOADER including:

• Extraction tool • Electronic unit • LHF interface module • RHF interface module • Hand-held scanner • Installation plug DDM001-04 including: • DDM00101-04 • DDM00102-04 1 • 1 • 1 FCS 2.1.7.3 UPLOAD SUPPORT including:

• FCS software media (std 2.1.7.3) • FCS label paperbook
MEM40507-01 1 CD installation media

D. LOCAL PROCUREMENT

• araldite AV138M

• hardener HV998 

## FALCON 7X 7X-214

August 30, 2011 ATA 27

Initial issuance Page 8 / 9DASSAULT AVIATION Proprietary DataFigure 1: SPEED LIMITATION PLACARDS

END OF DOCUMENT 

## FALCON 7X 7X-214

August 30, 2011 ATA 27

Initial issuance Page 9 / 9DASSAULT AVIATION Proprietary DataNOT CLASSIFIED



## Procedure

FCS DATA LOADING PROCEDURE

SCOPE

Falcon 7X



## Approved

Division Dassault Equipements - Direction Technique

page : 1 / 6 6

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. REFERENCE ISSUE DATE DT EQUIP 43913 D 28/05/2010REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

TABLE OF CONTENTS 2 Approved

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIAT ION Proprietary Data. 

## TABLE OF CONTENTS

1

. INTRODUCTIO N

.................................................................................................................. . .... . 3 1 .1 Purpose of the procedu r e

................................................................................................. . 3 1 .2 Reference documents

...................................................................................................... . 3 1 .2.1 AMM documents

................................................................................................. . 3 1 .2.2 Authorities Documents

........................................................................................ . 3 1 .3 Tooling con f iguratio n

........................................................................................................ . 4 1 .4 Energ y

........................................................................................................................ . ..... . 4 1 .5 Acces s

........................................................................................................................ . ..... . 4 1 .6 List of acro n y ms

.............................................................................................................. . . 4 1 .7 Operators skills..............................................................................................................

. .. . 5 1 .8 Uploading e s timated time s

............................................................................................... . 5 1 .8.1 LH Front m o dule s

................................................................................................ . 5 1 .8.2 RH Front modules

............................................................................................... . 5

2

. PROCEDUR E

..................................................................................................................... . ...... . 6 2 .1 Software LH FRONT R a ck uploadi n g

.............................................................................. . 6 2 .1.1 Initialization (fig 1)

........................................................................................... .. .. . 8 2 .1.2 Uploading

.......................................................................................................... . 1 1 2 .1.2.1 Uploading MAIC 2A / MAIC 4A modules

........................................ . 1 1 2 .1.2.2 Uploading MFCC 1 A/B - MFCC 2 A/B - MFCC 3 A/B modul e s

........ . 1 7 2 .1.2.3 Uploading MAIC 2A - MAIC 4A - MFCC 1 A/B - MFCC 2 A/B - MFCC 3A/B modu l es

....................................................................... . 2 4 2 .1.3 Sticking of labels

............................................................................................... . 3 1 2 .1.4 Printing of r eport (fig 3 )

...................................................................................... . 3 2 2 .1.5 Close-up LH FRONT R a c k

................................................................................ . 3 5 2 .2 Software RH FRONT Rack uploa d in g

............................................................................ . 3 6 2 .2.1 Initialization (fig 2)

............................................................................................. . 38 2 .2.2 Uploading

.......................................................................................................... . 4 1 2 .2.2.1 Uploading SFCC 1 - S F CC 2 - SFCC 3 modules

........................... . 4 1 2 .2.2.2 Uploading MAIC 1A - MAIC 3A module s

........................................ . 48 2 .2.2.3 Uploading SFCC 1 - S F CC 2 - SFCC 3 - MA I C 1A - MAIC 3 A modules

.......................................................................................... . 5 5 2 .2.3 Sticking of labels

............................................................................................... . 6 1 2 .2.4 Printing of r eport (fig 4 )

...................................................................................... . 6 2 2 .2.5 Close-up RH FRONT Rack

............................................................................... . 6 5 2 .3 Supplement

.................................................................................................................... . 6 5 2 .3.1 Checks asked in the SB .....................................................................................6 5REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 3. INTRODUCTION 3

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. 

## 1 . INTRODUCTION

1 .1 Purpose of the procedure

This task gives the data loading procedure for th e field loadable modules of the FCS of the F7X.:

• MFCC

• SFCC

• MAIC This procedure is to perform on a FCS installed on aircraft : Repair center or production line The associated Service Bulletin (SB) will give specific information as specific items to follow for FCS standard to upload It references aircraft level instructions, which must be provided by the aircraft Service Bulletin CAUTION : To perform this FCS data loading procedur e, the A/C shall be without FCS failures It is forbidden to use "FCS ENGAGE" push button during the FCS Data loading procedure



### 1 .2 Reference documents

1 .2.1 AMM doc u ments
This Data Modules are consultable in Fa lcon Portal (AMM documentation - Field F7X)

20-30-00-910-803 Electrostatic discharge (E SD) standard practices 24-00-00-860-801 Energization / de-energi zation of the aircraft 24-00-00-860-806 Opening / Closing of the SSPC 24-00-00-860-807 Opening / Closing of the circuit breakers 24-34-13-960-801 Replacement of the PMA converter fuses 25-13-13-900-801 Removal / Installation of the cockpit linings 27-90-01-900-801 Removal / Installation of the LH Front FCS modules 27-90-01-900-803 Removal / Installation of the RH Front FCS modules

1 .2.2 Authorities Documents
DO178B – Software considerations in Air borne systems and Equipment Certification

This document is not useful for the procedure performing.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 3. INTRODUCTION 4

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. 

### 1 .3 Tooling configu r ation

TO-20-008 TOOL BOX MEM 405-01 FCS UPLOADER TOOL including:

• MEM 40501-01 ELECTRONIC UNIT

• MEM 40504-01 HAND HELD SCANNER

• MEM 40505-01 LHF INTERFACE MODULE

• MEM 40506-01 RHF INTERFACE MODULE

• MGB 660-01 EXTRACTION TOOL

DDM001-xx FCS UPLOAD SUPPORT including:

• DDM00101-xx FCS SOFTWARE MEDIA

• DDM00102-xx FCS LABELS PAPERBOOK Where xx is dedicated to the FCS standard to be uploaded (given in the SB) STANDARD USB CABLE LAPTOP PC equipped with software application installed with the MEM40507-01 INSTALLATION MEDIA (Tool version 1.0.46.0)



### 1 .4 Ener g y

ELECTRICAL



### 1 .5 Access
This access procedures are consultable in Falcon Portal (AMM documentation - Field 7X)

221XZ Cockpit lateral lining n°5 221YZ Cockpit lateral lining n°6 222XZ Cockpit lateral lining n°5 222YZ Cockpit lateral lining n°6



### 1 .6 List of acron y ms

A/C : Aircraft AMM : Aircraft Maintenance Manual FBW : Fly By Wire CMC : Centralized Maintenance Computer FCS : Flight Control System LHF : Left Hand Front MAIC : Maintenance and Avionic Interface Computer MDU : Multifunction Display UnitREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 3. INTRODUCTION 5

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. MFCC : Main Flight Control Computer RHF : Right Hand Front SB : Service Bulletin SFCC : Secondary Flight Control Computer SPDB : Secondary Power Distribution Box



### 1 .7 Operators skills

This procedure shall always be performed by an operator authorized by the component manufacturer DASSAULT EQUIPEMENTS af ter a training performed by DASSAULT EQUIPEMENTS teams. This operator will sign the field upload report.

An inspector will sign the SB report when the inst allation of the new FCS standard has been fully completed.



### 1 .8 Uploading estimated times

1 .8.1 LH Front m odules

• MAIC 2A / MAIC 4A : up to 8' per module (about 16')

• MFCC 1 (AB) / MFCC 2 (AB) / MFCC 3 (AB) : up to 6' per module (about 36')

1 .8.2 RH Front m odules

• MAIC 1A / MAIC 3A : up to 8' per module (about 16')

• SFCC 1 / 2 / 3 : up to 5' per module (about 15')REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 6

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. 

## 2 . PROCEDURE

2 .1 Software LH FRONT Rack uploading

NOTE : see hereafter the LHF Rack layout.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 7

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 8

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. 2 .1.1 Initializati o n (fig 1)

• No electrical energy (refer to 24-00-00-860-801 )

• Get the labels paperbook (DDM00102-xx) (fig 1-G) with the related modules identification labels.

• Connect the "uploading" laptop PC to the local means (electri cal connection AC 110V/220V) if its own battery is not charged enough to en sure full time uploading (roughly 1H20mn). NOTE : interruption during uploading will cause depot level return for the related modules

• Remove the linings 221XZ - 221YZ (refer to 25-13-13-900-801 )

• Open the LH FRONT Rack (refer to 27-90-01-900-801 para 3)

• Start the uploading laptop PC (be sure that screen and hard dr ive stand-by mode are disabled) and insert the FCS software media (DDM00101-xx) (fig 1-F),

• Extract the plug from slot 17 with the extraction tool ( MGB 660-01 )

• Insert and screw in slot 17 the LHF module interface ( MEM 40505-01 ) (fig 1-A)

• Plug the 128 contact movable connector from the LHF module interface ( MEM 40505-01 ) on the fixed 128 contact connect or of the Electronic Unit ( MEM 40501-01 ) (fig 1-B)

• Plug the hand-held scanner ( MEM 40504-01 ) on the A type USB port of the Electronic Unit ( MEM 40501-01 ) (fig 1-C)

• Connect the cable between B type USB port plug of Electronic Unit ( MEM 40501-01 ) to the A type USB port plug of uploading laptop PC (fig 1-D / fig 1-E)

• Open J7 breaker (LF E3 - 113CZ ) on the LH front SPDB ( L1000PM ) (refer to 24-00-00-860- 807 )

• Open K8 breaker (LF E4 - 314CZ ) on the RH front SPDB ( R1000PM ) (refer to 24-00-00-860- 807 )

• Set the TEST E1 switch ( R511CZ ) and TEST E2 switch ( L511CZ ) to the OFF position (DOWN)

• Start the "FCS UPLOADER" application on the laptop (icon on the desktop) A dedicated welcome screen reminds the operator to check the different re quired connections to upload. A message drawing attention on the laptop running on its own battery can be displayed

NOTE : the aircraft is de-energized.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 9

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next"

• Clic on "Add" and enter the uploading operator's nameREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 10

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Select your name in the list

• Clic on "Next"

• Enter the aircraft serial number

• Select the LH FRONT RACK

• If the aircraft power supplies are st ill "ON", this red message occurs

NOTE : This screen stays in this state until th e application detects automatically power supplies switched off; then the following screen appearsREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 11

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next"

2 .1.2 Uploading

Depending of the upload requested for the new sta ndard as detailed in the SB, the operator could have to upload:

 MFCC and MAIC, go to chapter 4.1.2.3

 MFCC only, go to chapter 4.1.2.2

 MAIC only, go to chapter 4.1.2.1

2 .1.2.1 Uploading M A IC 2 A / M A IC 4 A m odules

• Notch the case MAICREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 12

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next"

• Perform the following steps in chronological order :

o Energize the aircraft (refer to 24-00-00-860-801 )

o On the maintenance panel ( 1010TP ) set the TEST E1 switch ( R511CZ ) and TEST E2 switch ( L511CZ ) to the ON position (UP position)

• Close J7 breaker (LF E3 - 113CZ ) on the LH front SPDB ( L1000PM ) (refer to 24-00-00-860- 807 )

• Close K8 breaker (LF E4 - 314CZ ) on the RH front SPDB ( R1000PM ) (refer to 24-00-00-860- 807 )

• Notch the case when done

• After electrical power supplie s detection, the link between LH FRONT RACK and Electronic Unit ( MEM40501-01 ) is automatically doneREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 13

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. NOTE : During the link setting up, a bell-ringing like "DING/DON G" can be heard from the laptop

• Clic on "Next" when the "Next" button is enable

• SCAN 1 : scan the modules MAIC2A (slot 6) and MAIC 4A (slot 4) bar codes ( to facilitate the scan, lift the left locking lever)

• Clic on "Next"

NOTE : if the operator make an error as : wrong slot scanned, scanning or der not respected, slot already scanned, wrong module P/N with respect of the scanned slot, FCS software update media not detected,..., following messages would be displayedREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 14

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. In this case, clic on OK and start again the opera tion starting from the module which caused the
error message

• "Next" command is available as soon as the two modules are correctly recognized

• Clic on "Next"

• Clic on "Next". The screen below could be displayed during th e CD ROM activity

• SCAN 2 : scan the labels MAIC2A and MAIC4A on the related FCS labels paperbook (DDM00102-xx)REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 15

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next"

Column "NEW P/N" is automatically fed with scanned MAIC2A and MAIC4A label informations from related FCS standard labels paperbook

NOTE : If the scanned P/N on the new label doesn't match with the one expected in the column "NEW P/N", the following message is displayed. In this case c lic "OK" and start again the operation starting from the module which caused the error message

Bar code reading is finished. A message warns that an upl oading operation is to begin.

NOTE : if you click on "NO", uploading is aborte d and the application goes back to screen SCAN 2

• Clic on "YES" Uploading begins and is announced by . It is mandatory not to disconnect the laptop and not de-energize the aircraft during uploading. Up loading runs module after module and is stated by a bargraph located bottom of the uploadi ng window. A correctly uploaded module is announced byREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 16

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • A failed uploading sequence is notched . A warning message asks to check the connections and electrical powers but the next module uploading sequence goes on

• When one or several slots are notched clic on "Retry" to re-start the related modules failed uploading sequences. CAUTION : The operator can apply a "Retry". If a failu re persists, quit the application and shut down the A/C, then perform the procedure again at the beginning (refer to chapter "Initialization"). In case of persistent failure, the relate d uploaded module is however new FCS standard upgraded but considered as faulty and must be replaced.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 17

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • The uploading procedure is successfully complete d when the whole displayed slots are notched

• Clic on "Quit", the applica tion "FCS UPLOADER" closes

IMPORTANT :

• Inside the LH FRONT RACK slot 6 and slot 4,unstick the MAIC2A and MAIC4A modules labels scanned at step SCAN1 Then go to chapter 4.1.3.

2 .1.2.2 Uploading M F

CC 1 A /B - M FCC 2 A

/B - M F

CC 3A/B modules

• Notch the case MFCCREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 18

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next"

• Perform the following steps in chronological order :

o Energize the aircraft (refer to 24-00-00-860-801 )

o On the maintenance panel ( 1010TP ) set the TEST E1 switch ( R511CZ ) and TEST E2 switch ( L511CZ ) to the ON position (UP position)

• Close J7 breaker (LF E3 - 113CZ ) on the LH front SPDB ( L1000PM ) (refer to 24-00-00-860- 807 )

• Close K8 breaker (LF E4 - 314CZ ) on the RH front SPDB ( R1000PM ) (refer to 24-00-00-860- 807 )

• Notch the case when done

• After electrical power supplie s detection, the link between LH FRONT RACK and Electronic Unit ( MEM40501-01 ) is automatically doneREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 19

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. NOTE : During the link setting up, a bell-ringing like "DING/DONG" can be heard from laptop

• Clic on "Next" when the "Next" button is enable

• SCAN 1 : scan the modules MFCC3A (slot 13), MFCC3B (slot12), MFCC2A (slot 11), MFCC2B (slot 10), MFCC1A (slot 9) and MFCC1B (s lot 8) bar codes. To facilitate the scan, lift the left locking lever.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 20

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next"

NOTE : if the operator make an error as : wrong slot scanned, scanning or der not respected, slot already scanned, wrong module P/N with respect of the scanned slot, FCS software update media not detected,..., following messages would be displayed

In this case, clic on OK and start again the opera tion starting from the module which caused the
error message

• "Next" command is available as soon as the six modules are correctly recognized

• Clic on "Next"REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 21

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next". The screen below could be displayed during th e CD ROM activity

• SCAN 2 : Scan the labels MFCC3A, MFCC3B, MFCC2A, MFCC2B, MFCC1A and MFCC1B on the related FCS labels paperbook (DDM00102-xx)

• Clic on "Next"

Column "NEW P/N" is automatically fe d with scanned MFCC3A, MFCC3B, MFCC2A, MFCC2B, MFCC1A and MFCC1B label informati ons from related FCS standard labels paperbook

• NOTE : If the scanned P/N on the new label doesn't match with the one expected in the column "NEW P/N", the following message is displayed. In this case c lic "OK" and start again the operation starting from the module which caused the error messageREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 22

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. Bar code reading is finished. A message warns that an upl oading operation is to begin.

NOTE : if you click on "NO", uploading is aborte d and the application goes back to screen SCAN 2

• Clic on "YES" Uploading begins and is announced by . It is mandatory not to disconnect the laptop and not de-energize the aircraft during uploading. Uploading runs module after module and is stated by a bargraph located bottom of the uploading wind ow. A correctly uploaded module is notched

• A failed uploading sequence is notched . A warning message asks to check the connections and electrical powers but the next module uploading sequence goes onREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 23

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • When one or several slots are notched clic on "Retry" to re-start the related modules failed uploading sequences.

CAUTION : The operator can apply a "Retry". If a failu re persists, quit the application and shut down the A/C, then perform the procedure again at the beginning (refer to chapter "Initialization"). In case of persistent failure, the relate d uploaded module is however new FCS standard upgraded but considered as faulty and must be replaced.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 24

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • The uploading procedure is successfully comp leted when the whole displayed slots are notched

• Clic on "Quit", the applica tion "FCS UPLOADER" closes

IMPORTANT :

• Inside the LH FRONT RACK slot 13, 12, 11, 10, 09 and 08, unstick the MFCC3A, MFCC3B, MFCC2A, MFCC2B, MFCC1A and MFCC1B m odules labels scanned at step SCAN1 Then go to chapter 4.1.3.

2 .1.2.3 Uploading M A IC 2 A - M A IC 4 A - M F

CC 1 A /B - M FCC 2 A

/B - M FCC 3A/B modules

• Notch the cases MFCC and MAICREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 25

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next"

• Perform the following steps in chronological order

o Energize the aircraft (refer to 24-00-00-860-801 )

o On the maintenance panel ( 1010TP ) set the TEST E1 switch ( R511CZ ) and TEST E2 switch ( L511CZ ) to the ON position (UP position)

• Close J7 breaker (LF E3 - 113CZ ) on the LH front SPDB ( L1000PM ) (refer to 24-00-00-860- 807 )

• Close K8 breaker (LF E4 - 314CZ ) on the RH front SPDB ( R1000PM ) (refer to 24-00-00-860- 807 )

• Notch the case when done

• After electrical power supplie s detection, the link between LH FRONT RACK and Electronic Unit ( MEM40501-01 ) is automatically doneREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 26

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. NOTE : During the link setting up, a bell-ringing like "DING/DONG" can be heard from laptop

• Clic on "Next" when the "Next" button is enable

• SCAN 1 : scan the modules MFCC3A (slot 13), MFCC3B (slot12), MFCC2A (slot 11), MFCC2B (slot 10), MFCC1A (slot 9), MFCC1B (slo t 8), MAIC2A (slot 6), MAIC4A (slot 4) bar codes. To facilitate the sca n, lift the left locking lever.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 27

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next"

NOTE : if the operator make an error as wrong sl ot scanned, scanning orde r not respected, slot already scanned, wrong module P/N with respect of the scanned slot, FCS software update media not detected,..., following messages would be displayed

• In this case, clic on OK and start again the opera tion starting from the module which caused the
error message

• "Next" command is available as soon as the eight modules are correctly recognized

• Clic on "Next"REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 28

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next". The screen below could be displayed during th e CD ROM activity

• SCAN 2 : Scan the labels MFCC3A, MFCC3B, MFCC2A, MFCC2B, MFCC1A, MFCC1B, MAIC2A, MAIC4A on the re lated FCS labels paperbook (DDM00102-xx)

• Clic on "Next"

Column "NEW P/N" is automatically fe d with scanned MFCC3A, MFCC3B, MFCC2A, MFCC2B, MFCC1A, MFCC1B, MAIC2A and MAIC4A label informations from the related FCS standard paperbook

• NOTE : If the scanned P/N on the new label doe sn't match with the one expected in the column"NEW P/N", the following message is displa yed. In this case clic"OK" and start again the operation starting from the module which caused the error messageREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 29

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. Bar code reading is finished. A message warns that an upl oading operation is to begin.

NOTE : if you click on "NO", uploading is aborte d and the application goes back to screen SCAN 2

• Clic on "YES" Uploading begins and is announced by . It is mandatory not to disconnect the laptop and not de-energize the aircraft during uploading. Uploading runs module after module and is stated by a bargraph located bottom of the uploading wind ow. A correctly uploaded module is notchedREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 30

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • A failed uploading sequence is notched . A warning message asks to check the connections and electrical powers but the next module uploading sequence goes on

• When one or several slots are notched clic on "Retry" to re-start the related modules failed uploading sequences.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 31

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. CAUTION : The operator can apply a "Retry". If a failu re persists, quit the application and shut down the A/C, then perform the procedure again at the beginning (refer to chapter "Initialization"). In case of persistent failure, the relate d uploaded module is however new FCS standard upgraded but considered as faulty and must be replaced.

• The uploading procedure is successfully complete d when the whole displayed slots are notched

• Clic on "Quit", the applica tion "FCS UPLOADER" closes

IMPORTANT :

• Inside the LH FRONT RACK, unstick th e MFCC3A, MFCC3B, MFCC2A, MFCC2B, MFCC1A; MFCC1B, MAIC2A and MAIC4A modules labels scanned at step SCAN1 Then go to chapter 4.1.3.

2 .1.3 Sticking of labelsREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 32

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Stick the new labels related FCS standard labels paperbook (DDM00102-xx) scanned at step SCAN2 and pay attention to the slot, the P/N and the S/N.

• Stick pre-identified stamp on the label

• This operation will be carried out by the operator.

CAUTION : The modules whose operation of remo te loading has failed must mandatory be identified by the new label of the uploaded standa rd. They will be considered broken down and the procedure of installation/remove modules will have being appl ied in this case (refer to 27-90-01- 900-801 ).

2 .1.4 Printing of report (fig 3)

When the label sticking procedure is fulfilled, the operator has to print the uploading report created by the application "FCS UPLOADER". This report contains:

• Informations given by the operator :

o Aircraft type,

o Aircraft Serial Number,

o Repair station,

o Operator,

o Rack

• Information given by FCS software media :

o Upload standard

• Informations given by the tool (MEM40501-01) :

o Date, MFCCs slot 13 to 08

MAIC2A slot 6

MAIC4A Slot 4REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 33

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. o Tool name,

o Tool version,

o Module Part Number,

o Module Serial Number,

o Upload status.

Laptop directory : "My Docume nts\Dassault-Aviation\FCS Uploader\Logs\Falcon 7X\n°A/C (A/C serial number entered by the operat or at the beginning of the procedure)

If more than one report is record ed in the directory, the last on e in time shall be considered. This report is to be : - Printed - Commented (if necessary) - Signed and stamped by the operator - Scanned and sent to DSC Support by e-mail (address will be confirmed in the SB)

Moreover the operator shall send to DSC Support by e-mail (address will be confirmed in the SB) ALL the “Module by Module” uploading report s available in the Laptop directory: “My Documents \ Dassault-Aviation \ FCS Uploader \ Modules”.

NOTE :If no RH FRONT rack module to upload or if RH FRONT modules are already uploaded, go to § 4.1.5 else go to § 4.2.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 34

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. Fig 3

Uploading LH FRONT Rack report

************************************************************ *** FIELD UPLOAD RECORD *** ************************************************************

AIRCRAFT : Falcon 7X SERIAL NUMBER : 1 UPLOAD STANDARD: 2.1.7.1 RACK : LH FRONT RACK DATE : 2010-01-05 REPAIR STATION : DASSAULT AVIATION OPERATOR : Jérôme CAPPELLE TOOL : FCS Uploader TOOL VERSION : 1.0.46.0

+------+-------------+-------+-------------+---------------+ | SLOT | MODULE P/N | S/N | NEW P/N | UPLOAD STATUS |

+------+-------------+-------+-------------+---------------+ | 13 | ENS7X101-11 | 9999 | ENS7X101-12 | PASSED | | 12 | ENS7X102-11 | 9999 | ENS7X102-12 | PASSED | | 11 | ENS7X101-11 | 8888 | ENS7X101-12 | PASSED | | 10 | ENS7X102-11 | 8888 | ENS7X102-12 | PASSED | | 09 | ENS7X101-11 | 7777 | ENS7X101-12 | PASSED | | 08 | ENS7X102-11 | 7777 | ENS7X102-12 | PASSED | | 06 | ENS7X501-18 | 9999 | ENS7X501-20 | PASSED | | 04 | ENS7X501-18 | 8888 | ENS7X501-20 | PASSED |

+------+-------------+-------+-------------+---------------+

+----------------------------------------------------------+ | Results of the aircraft tests specified in the Service | | Bulletin: | | | | PASSED FAILED | | |

+----------------------------------------------------------+ +------------------------| COMMENT |-----------------------+ | | | | | |
| | | |
| | | |

+----------------------------------------------------------+

SIGNATURE : STAMP :REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 35

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. 2 .1.5 Close-up LH FRONT Rack

• On the maintenance panel ( 1010TP ) set the TEST E1 switch ( R511CZ ) and TEST E2 switch ( L511CZ ) to the OFF position (DOWN position)

• De-energize the aircraft (refer to 24-00-00-860-801 )

• Set out the laptop the FCS software media (DDM00101-xx) and keep it

• Switch off the laptop

• Disconnect the USB cable between th e laptop and the Electronic Unit ( MEM 40501-01 )

• Disconnect the hand-held scanner ( MEM 40504-01 ) from Electronic Unit ( MEM 40501-01 )

• Disconnect the movable connector 128 contact between LHF interface module ( MEM 40505- 01 ) and Electronic Unit ( MEM 40501-01 )

• Set out the LHF interface module ( MEM 40505-01 ) from slot 17 of LH FRONT rack

• Insert plug in slot 17 of LH FRONT rack with the extraction tool (MGB 660-01)

• Close the LH FRONT rack and install the linings (refer to 27-90-01-900-801 para 8)

• Take care of the FCS standards labels paperbook as well as CD ROM.

Go to chapter 4.3REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 36

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. 

### 2 .2 Software RH FRONT Rack uploading

NOTE : see hereafter the RHF Rack layout.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 37

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 38

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. 2 .2.1 Initializati o n (fig 2)

• No electrical energy (refer to 24-00-00-860-801 )

• Get the labels paperbook (DDM00102-xx) (fig 1-G) with the related modules identification labels.

• Connect the "uploading" laptop PC to the local means (electri cal connection 110V/220V AC) if its own battery is not charged enough to en sure full time uploading (roughly 1H20mn). NOTE : interruption during uploading will cause depot level return for the related modules

• Remove the linings 222XZ - 222YZ (refer to 25-13-13-900-801 )

• Open the RHF Rack (refer to 27-90-01-900-803 para 3)

• Start the uploading laptop PC (be sure that screen and hard dr ive stand-by mode are disabled) and insert the FCS software media (DDM00101-xx) (fig 2-F) .

• Extract the plug from slot 1 with the extraction tool ( MGB 660-01 )

• Insert and screw in slot 1 the RHF module interface ( MEM 40506-01 ) (fig 2-A)

• Plug the 128 contact movable connector from the RHF module interface ( MEM 40506-01 ) on the fixed 128 contact connect or of the Electronic Unit ( MEM 40501-01 ) (fig 2-B)

• Plug the hand-held scanner ( MEM 40504-01 ) on the A type USB port of the Electronic Unit ( MEM 40501-01 ) (fig 2-C)

• Connect the cable between B type USB port plug of Electronic Unit ( MEM 40501-01 ) to the A type USB port plug of uploading laptop PC (fig 2-D / fig 2-E)

• Remove F1 fuse ( R9500CZ ) out of PMAC 1 ( R107CZ ) and remove F1 fuse ( L9500CZ ) out of PMAC 2 ( L107CZ ) (refer to 24-34-13-960-801 para 4 )

• Open B4 breaker (FBW RR E4 - 614CZ ) on the RH Rear SPDB ( R2000PM ) (refer to 24-00-00- 860-807 )

• Open H5 breaker (FBW RF E4 - 214CZ ) on the RH Front SPDB ( R1000PM ) (refer to 24-00- 00-860-807 )

• Open H3 breaker (FBW RF E3 - 613CZ ) on the LH Front SPDB ( L1000PM ) (refer to 24-00-00- 860-807 )

• Energize the aircraft (refer to 24-00-00-860-801 )

• On the MDU "ELEC" functional diagram located inside the FCS C/B status page, set OUT the 1S01 SSPC (FBW LR E3 - 413CZ ) (refer to 24-00-00-860-806 )

• De-energize the aircraft (refer to 24-00-00-860-801 )

• Set the TEST E1 switch ( R511CZ ) and TEST E2 switch ( L511CZ ) to the OFF position (DOWN)

• Start the "FCS UPLOADER" application on the laptop (icon on the desktop) A dedicated welcome screen reminds the operator to check the different re quired connections to upload. A message drawing attention on the laptop running on its own battery can be displayed NOTE : the aircraft is de-energized.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 39

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next"

• Clic on "Add" and enter the uploading operator's nameREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 40

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Select your name in the list

• Clic on "Next"

• Enter the aircraft serial number

• Select the RH FRONT RACK

• If the aircraft power supplies are st ill "ON", this red message occursREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 41

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. NOTE : this screen stays in this state until the application detects auto matically power supplies switched off; then the following screen appears

• Clic on "Next"

2 .2.2 Uploading

Depending of the upload requested for the new sta ndard as detailed in the SB, the operator could have to upload:

 SFCC and MAIC, go to chapter 4.2.2.3

 SFCC only, go to chapter 4.2.2.1

 MAIC only, go to chapter 4.2.2.2

2 .2.2.1 Uploading SFCC 1 - SFCC 2 - S F CC 3 modules

• Notch the case SFCCREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 42

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next"

• Perform the following steps in chronological order :

o Energize the aircraft (refer to 24-00-00-860-801 )

o On the maintenance panel ( 1010TP ) set the TEST E1 switch ( R511CZ ) and TEST E2 switch ( L511CZ ) to the ON position (UP position)

o Close H5 breaker (FBW RF E4 - 214CZ ) on the RH Front SPDB ( R1000PM ) (refer to 24-00-00-860-807 )

o Close H3 breaker (FBW RF E3 - 613CZ ) on the LH Front SPDB ( L1000PM ) (refer to 24-00-00-860-807 )

• Notch the case when done

• After electrical power supplie s detection, the link between RH FRONT RACK and Electronic Unit ( MEM40501-01 ) is automatically done NOTE : During the link setting up, a bell-ringing like "DING/DONG" can be heard from laptopREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 43

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next" when the "Next" button is enable

• SCAN 1 :scan the modules SFCC1 (slot 8), SFCC2 (s lot 9) and SFCC3 (slot 10). To facilitate the scan, lift the right locking lever.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 44

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next"

NOTE : if the operator make an error as wrong sl ot scanned, scanning orde r not respected, slot already scanned, wrong module P/N with respect of the scanned slot, FCS software update media not detected,..., following messages would be displayed

• In this case, clic on OK and start again the opera tion starting from the module which caused the
error message

• "Next" command is available as soon as the three modules are correctly recognized

• Clic on "Next"REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 45

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next". The screen below could be displayed during th e CD ROM activity

• SCAN 2 : scan the labels SFCC1, SFCC2 and SFCC3 on the related FCS labels paperbook (DDM00102-xx)

• Clic on "Next"

Column "NEW P/N" is automatically fed with scanned SFCC1, SFCC2 and SFCC3 label informations from related FCS standard labels paperbook.

NOTE : If the scanned P/N on the new label doe sn't match with the one expected in the column"NEW P/N", the following message is displa yed. In this case clic"OK" and start again the operation starting from the module which caused the error messageREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 46

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. Bar code reading is finished. A message warns that an upl oading operation is to begin.

NOTE: if you click on "NO", uploa ding is aborted and the applic ation goes back to screen SCAN 2

Uploading begins and is announced by . It is mandatory not to disconnect the laptop and not de-energize the aircraft during uploading. Uploading runs module after module and is stated by a bargraph located bottom of the uploading wind ow. A correctly uploaded module is notched

• A failed uploading sequence is notched . A warning message asks to check the connections and electrical powers but the next module uploading sequence goes onREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 47

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • When one or several slots are notched clic on "Retry" to re-start the related modules failed uploading sequences.

CAUTION : The operator can apply a "Retry". If a failu re persists, quit the application and shut down the A/C, then perform the procedure again at the beginning (refer to chapter "Initialization"). In case of persistent failure, the relate d uploaded module is however new FCS standard upgraded but considered as faulty and must be replaced.

• The uploading procedure is successfully complete d when the whole displayed slots are notchedREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 48

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Quit", the applica tion "FCS UPLOADER" closes

IMPORTANT :

• Inside the RH FRONT RACK slot 8, 9 and 10,unstick the SFCC1, SFCC2 and SFCC3 modules labels scanned at step SCAN1 Then go to chapter 4.2.3.

2 .2.2.2 Uploading M A IC 1 A - M A IC 3 A m odules

• Notch the case MAIC

• Clic on "Next"

• Perform the following steps in chronological order

o Energize the aircraft (refer to 24-00-00-860-801 )

o On the maintenance panel ( 1010TP ) set the TEST E1 switch ( R511CZ ) and TEST E2 switch( L511CZ ) to the ON position (UP position)REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 49

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. o Close H5 breaker (FBW RF E4 - 214CZ ) on the RH Front SPDB ( R1000PM ) (refer to 24-00-00-860-807 )

o Close H3 breaker (FBW RF E3 - 613CZ ) on the LH Front SPDB ( L1000PM ) (refer to 24-00-00-860-807 )

• Notch the case when done

• After electrical power supplie s detection, the link between RH FRONT RACK and Electronic Unit ( MEM40501-01 ) is automatically done

NOTE : During the link setting up, a bell-ringing like "DING/DONG" can be heard from laptopREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 50

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next" when the "Next" button is enable

• SCAN 1 scan the modules MAIC3A (slo t 12) and MAIC1A (slot 14) bar code (to facilitate the scan, lift the right locking lever)

• Clic on "Next"REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 51

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. NOTE : if the operator make an error as wrong sl ot scanned, scanning orde r not respected, slot already scanned, wrong module P/N with respect of the scanned slot, FCS software update media not detected,..., following messages would be displayed

• In this case, clic on OK and start again the opera tion starting from the module which caused the
error message

• Next" command is available as soon as th e two modules are co rrectly recognized

• Clic on "Next"

• Clic on "Next". The screen below could be displayed during th e CD ROM activity

• SCAN 2 : Scan the labels MAIC3A and MAIC1A on the related FCS labels paperbook (DDM00102-xx)REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 52

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "Next"

Column "NEW P/N" is automatically fed with scanned MAIC3A and MAIC1A label informations from related FCS standard labels paperbook

NOTE : If the scanned P/N on the new label doe sn't match with the one expected in the column"NEW P/N", the following message is displa yed. In this case clic"OK" and start again the operation starting from the module which caused the error message

Bar code reading is finished. A message warns that an upl oading operation is to begin.

NOTE : if you click on "NO", uploading is aborte d and the application goes back to screen SCAN 2REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 53

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Clic on "YES" Uploading begins and is announced by . It is mandatory not to disconnect the laptop and not de-energize the aircraft during uploading. Up loading runs module after module and is stated by a bargraph located bottom of the uploading wi ndow. A correctly upload ed module is notched

• A failed uploading sequence is notched . A warning message asks to check the connections and electrical powers but the next module uploading sequence goes onREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 54

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • When one or several slots are notched clic on "Retry" to re-start the related modules failed uploading sequences.

CAUTION : The operator can apply a "Retry". If a failu re persists, quit the application and shut down the A/C, then perform the procedure again at the beginning (refer to chapter "Initialization"). In case of persistent failure, the relate d uploaded module is however new FCS standard upgraded but considered as faulty and must be replaced.

• The uploading procedure is successfully complete d when the whole displayed slots are notched

• Clic on "Quit",the applica tion "FCS UPLOADER" closesREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 55

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. IMPORTANT :

• Inside the RH FRONT RACK slot 12 and slot 14, unstick the MAIC3A and MAIC1A modules labels scanned at step SCAN1 Then go to chapter 4.2.3.

2 .2.2.3 Uploading SFCC 1 - SFCC 2 - S F CC 3 - M A I C 1A - M A I C 3A modules

• Notch the cases SFCC et MAIC

• Clic on "Next"

• Perform the following steps in chronological order :

o Energize the aircraft (refer to 24-00-00-860-801 )

o On the maintenance panel ( 1010TP ) set the TEST E1 switch ( R511CZ ) and TEST E2 switch( L511CZ ) to the ON position (UP position)

o Close H5 breaker (FBW RF E4 - 214CZ ) on the RH Front SPDB ( R1000PM ) (refer to 24-00-00-860-807 )

o Close H3 breaker (FBW RF E3 - 613CZ ) on the LH Front SPDB ( L1000PM ) (refer to 24-00-00-860-807 )

• Notch the case when doneREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 56

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • After electrical power supplie s detection, the link between LH FRONT RACK and Electronic Unit ( MEM40501-xx ) is automatically done

NOTE : During the link setting up, a bell-ringing like "DING/DON G" can be heard from the laptop

• Clic on "Next" when the "Next" button is enableREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 57

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • SCAN 1 : scan the modules SFCC1 (slot 8), SFCC2 (slot 9), SFCC3 (slot 10), MAIC3A (slot 12) and MAIC1A (slot 14) bar codes (to facilit ate the scan, lift the right locking lever)

• Clic on "Next"

NOTE : if the operator make an error as wrong sl ot scanned, scanning orde r not respected, slot already scanned, wrong module P/N with respect of the scanned slot, FCS software update media not detected,..., following messages would be displayedREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 58

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • In this case, clic on OK and start again the opera tion starting from the module which caused the
error message

• "Next" command is available as soon as the five modules are correctly recognized

• Clic on "Next"

• Clic on "Next". The screen below could be displayed during th e CD ROM activity

• SCAN 2 : Scan the labels SFCC1, SFCC2, SFCC3, MAIC3A, and MAIC1A on the related FCS labels paperbook (DDM00102-xx)

• Clic on "Next"REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 59

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. Column "NEW P/N" is automatically fed with scanned SFCC1, SFCC2, SFCC3, MAIC3A, MAIC1A label information from the re lated FCS standard labels paperbook

NOTE : If the scanned P/N on the new label doe sn't match with the one expected in the column"NEW P/N", the following message is displa yed. In this case clic"OK" and start again the operation starting from the module which caused the error message

Bar code reading is finished. A message warns that an upl oading operation is to begin.

NOTE : if you click on "NO", uploading is aborte d and the application goes back to screen SCAN 2

• Clic on "YES" Uploading begins and is announced by . It is mandatory not to disconnect the laptop and not de-energize the aircraft during uploading. Uploading runs module after module and is stated by a bargraph located bottom of the uploading wind ow. A correctly uploaded module is notchedREFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 60

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • A failed uploading sequence is notched . A warning message asks to check the connections and electrical powers but the next module uploading sequence goes on

• When one or several slots are notched clic on "Retry" to re-start the related modules failed uploading sequences.

CAUTION : The operator can apply a "Retry". If a failu re persists, quit the application and shut down the A/C, then perform the procedure again at the beginning (refer to chapter "Initialization"). In case of persistent failure, the relate d uploaded module is however new FCS standard upgraded but considered as faulty and must be replaced.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 61

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • The uploading procedure is successfully complete d when the whole displayed slots are notched

• Clic on "Quit", the applica tion "FCS UPLOADER" closes

IMPORTANT :

• Inside the RH FRONT RACK, unstick the SFCC1 (s lot 8) - SFCC2 (slot 9) - SFCC3 (slot 10) - MAIC3A (slot 12) - MAIC1A (slot 14 ) modules labels scanned at step SCAN1 Then go to 4.2.3.

2 .2.3 Sticking of labels

• Stick the new labels related FCS standard labels paperbook (DDM00102-xx) scanned at step SCAN2 and pay attention to the slot, the P/N and the S/N.

• Stick pre-identified stamp on the label

• This operation will be carried out by the operator.

CAUTION : The modules whose operation of remote loading failed must mandatory be identified by the new label of the downloaded standard. They will be considered broken down and the procedure of installation/remove modules will have being appl ied in this case (refer to 27-90-01- 900-803 ).REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 62

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. 2 .2.4 Printing of report (fig 4)

When the label sticking procedure is fulfilled, the operator has to print the uploading report created by the application "FCS UPLOADER".

This report contains :

• Informations given by the operator :

o Aircraft type,

o Aircraft Serial Number,

o Repair station,

o Operator,

o Rack

• Information given by FCS software media :

o Upload standard

• Informations given by the tool (MEM40501-01) :

o Date,

o Tool name,

o Tool version,

o Module Part Number,

o Module Serial Number,

o Upload status.

Laptop directory : "My Docume nts\Dassault-Aviation\FCS Uploader\Logs\Falcon 7X\n°A/C (A/C serial number entered by the operat or at the beginning of the procedure)

See examples on LH FRONT rack in chapter 4.1.4

If more than one report is record ed in the directory, the last on e in time shall be considered. This report is to be : MAIC3A slot 12

MAIC1A Slot 14 SFCC1 SFCC2 SFCC3 Slot 8 to 10REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 63

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. - Printed - Commented (if necessary) - Signed and stamped by the operator - Scanned and sent to DSC Support by e-mail (address will be confirmed in the SB)

Moreover the operator shall send to DSC Support by e-mail (address will be confirmed in the SB) ALL the “Module by Module” uploading report s available in the Laptop directory: “My Documents \ Dassault-Aviation \ FCS Uploader \ Modules”.

See examples on LH FRONT rack in chapter 4.1.4

NOTE :If no LH FRONT rack modul e to upload or if LH FRONT rack modules are already uploaded, go to item § 4.2.5 else go to § 4.1.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 64

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. Fig 4

Uploading RH FRONT Rack report

************************************************************ *** FIELD UPLOAD RECORD *** ************************************************************

AIRCRAFT : Falcon 7X SERIAL NUMBER : 1 UPLOAD STANDARD: 2.1.7.1 RACK : RH FRONT RACK DATE : 2010-01-05 REPAIR STATION : DASSAULT EQUIPEMENTS OPERATOR : Jérôme CAPPELLE TOOL : FCS Uploader TOOL VERSION : 1.0.46.0

+------+-------------+-------+-------------+---------------+ | SLOT | MODULE P/N | S/N | NEW P/N | UPLOAD STATUS |

+------+-------------+-------+-------------+---------------+ | 08 | ENS7X201-14 | 9999 | ENS7X201-14 | PASSED | | 09 | ENS7X201-14 | 8888 | ENS7X201-14 | PASSED | | 10 | ENS7X201-14 | 7777 | ENS7X201-14 | PASSED | | 12 | ENS7X501-18 | 8888 | ENS7X501-20 | PASSED | | 14 | ENS7X501-18 | 7777 | ENS7X501-20 | PASSED | | | | | | | | | | | | |

+------+-------------+-------+-------------+---------------+
+----------------------------------------------------------+ | Results of the aircraft tests specified in the Service | | Bulletin: | | | | PASSED FAILED | | |

+----------------------------------------------------------+ +------------------------| COMMENT |-----------------------+ | |
| | | |
| | | |
| | | |

+----------------------------------------------------------+

SIGNATURE : STAMP :REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 65

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. 2 .2.5 Close-up RH FRONT Rack

• On the maintenance panel ( 1010TP ) set the TEST E1 switch ( R511CZ ) and TEST E2 switch ( L511CZ ) to the OFF position (DOWN)

• On the MDU "ELEC" functional diagram, in the C/B status page related to "FLIGHT CONTROLS", set the 1S01 SSPC (FBW LR E3 - 413CZ ) on IN (refer to 24-00-00-860-806 )

• De-energize the aircraft (refer to 24-00-00-860-801 )

• Set out the laptop the FCS software media (DDM00101-xx) and keep it

• Switch off the laptop

• Disconnect the USB cable between th e laptop and the Electronic Unit ( MEM 40501-01 )

• Disconnect the hand - held scanner ( MEM 40504-01 ) from Electronic Unit ( MEM 40501-01 )

• Disconnect the movable conector 128 c ontacts between RHF interface module ( MEM 40505- 01 ) and Electronic Unit ( MEM 40501-01 )

• Set out the RHF interface module ( MEM 40506-01 ) from slot 1 of RH FRONT rack

• Insert plug in slot 1 of RH FR ONT rack with extraction tool ( MGB660-01 )

• Close the RH FRONT rack and install the linings (refer to 27-90-01-900-803 para 8)

• Install fuse F1 ( R9500CZ ) of PMAC 1 ( R107CZ ) and install fuse F1 ( L9500CZ ) of PMAC 2 ( L107CZ ) (refer to 24-34-13-960-801 para 6 )

• Close B4 breaker (FBW RR E4 - 614CZ ) on the RH Rear SPDB ( R2000PM ) (refer to 24-00-00- 860-807 )

• Take care of the FCS standards labels paperbook (DDM00102-xx) as well as CD ROM (DDM00101-xx)

.



### 2 .3 Supplement

2 .3.1 Checks asked in the SB The uploading of some modules is a part of the FCS standard upgrade covered by a dedicated Service Bulletin.

The Service Bulletin details the impacted modules, the job to do and the checks to perform for the validation of the new standard installation.

Part of these tests is used to validate the uploaded modules.

There will be:

• Execution of the “MODULE TEST” triggered te st on the CMC screen “FCS ELECTRONIC FAILURES (1/4)” A part of this automatic test checks the cons istency of all the modul es versions (Hardware and Software) with a compatibility table embedded in the MAIC4 module.REFERENCE INDICE DATE DT EQUIP 43913 D 28/05 / 2010 NOT CLASSIFIED

Approved 4. PROCEDURE 66

This document is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data. • Check on CMC screen “MODULE IDENTIFICATION” of the new P/N of all the modules impacted by the standard upgrade The operator will have check the compliance between the BS and the displayed references and report them on the Falcon Portal

A test failed causes the display of a dedicated maintenance message (2790EFCS307 “SYSTEM COMPATIBILITY CHECK”) associat ed with the internal failure upon each failed module.

• A ground test, similar of the pilot test in maintenance conditions

The test closes the maintenance operation and will check the serviceability of the FCS for a flight.

The operator has to fill in the LH FRONT rack and/or RH FRONT rack uploading report the result of the tests performed on the aircraft (PASSED or FAILED).	
	

			
			

	 	
	
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