# Dassault Mandatory Service Bulletin 7X-214: No revision named

- Rights: © Dassault Aviation. Filed by the FAA in regulations.gov docket FAA-2013-0464; AD 2014-16-23 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- Document: [Dassault Mandatory Service Bulletin 7X-214](https://openairdocs.org/service-documents/dassault/7x-214.md)
- Title as filed: U.S. DOT/FAA - 7X-214-R0
- Pages: 78
- PDF: https://openairdocs.org/files/sha256/8d/40/8d40c8e88ee96e10b4a9e90f5c3af1811b434a72b1c255c3e6e4ca286f2b4545
- Page: https://openairdocs.org/service-documents/dassault/7x-214/file/8d40c8e88ee9

## Text

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### Page 1

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.
785

### Page 2

FLIGHT 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 27

### Page 3

FLIGHT 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 / 9
DASSAULT AVIATION Proprietary Data

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E. 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
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DASSAULT AVIATION Proprietary Data

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• 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
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DASSAULT AVIATION Proprietary Data

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2. 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
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DASSAULT AVIATION Proprietary Data

### Page 7

(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 / 9
DASSAULT AVIATION Proprietary Data

### Page 8

(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 / 9
DASSAULT AVIATION Proprietary Data

### Page 9

3. 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 / 9
DASSAULT AVIATION Proprietary Data

### Page 10

MEM405-01 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 / 9
DASSAULT AVIATION Proprietary Data

### Page 11 (OCR)

DASSAULT  SERVICE BULLETIN
AVIATION
FALCON 7X  7X-214
SPEED LIMITATIONS
SF1  200KIAS
SF2  190KIAS
SF 3  180KIAS
VLO  200KIAS
VLE  245KIAS
VA  218KIA$
MMO  VMO  320KIAS  085  DASSAULT AVIATION Proprietary Data
DETAIL A
SPEED LIMITATIONS
SF1  200KIAS
SF2  190KIAS
SF3  180KIAS
VLO  200KIAS
VLE  245KIAS
VA  218KIAS
DETAIL B
Figure 1: SPEED LIMITATION PLACARDS
August 30, 2011  ATA 27
Initial issuance  Page 9 / 9
END OF DOCUMENT

### Page 12

NOT CLASSIFIED
Procedure 
FCS DATA LOADING PROCEDURE 
SCOPE 
Falcon 7X 
  
Approved 
Division Dassault Equipements - Direction Technique 
      
 
      
   
  
page : 1 / 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. 
 
 
REFERENCE ISSUE DATE 
DT EQUIP 43913 D 28/05/2010

### Page 13

REFERENCE 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 AVIATION Proprietary Data. 
 
TABLE OF CONTENTS 
1. INTRODUCTION........................................................................................................................3  
1.1 Purpose of the procedure..................................................................................................3  
1.2 Reference documents .......................................................................................................3 
1.2.1 AMM documents ..................................................................................................3 
1.2.2 Authorities Documents .........................................................................................3 
1.3 Tooling configuration.........................................................................................................4
1 .4 Energy......................................................................................................................... ......4 
1.5 Access......................................................................................................................... ......4 
1.6 List of acronyms ................................................................................................................4 
1.7 Operators skills..................................................................................................................5 
1.8 Uploading estimated times................................................................................................5  
1.8.1 LH Front modules.................................................................................................5
1 .8.2 RH Front modules ................................................................................................5 
2. PROCEDURE.............................................................................................................................6 
2.1 Software LH FRONT Rack uploading ...............................................................................6 
2.1.1 Initialization (fig 1) ................................................................................................8 
2.1.2 Uploading ...........................................................................................................11 
2.1.2.1 Uploading MAIC 2A / MAIC 4A modules .........................................11 
2.1.2.2 Uploading MFCC 1A/B - MFCC 2A/B - MFCC 3A/B modules.........17  
2.1.2.3 Uploading MAIC 2A - MAIC 4A - MFCC 1A/B - MFCC 2A/B -  
MFCC3A/B modules ........................................................................24
2 .1.3 Sticking of labels ................................................................................................31
2 .1.4 Printing of report (fig 3).......................................................................................32 
2.1.5 Close-up LH FRONT Rack.................................................................................35  
2.2 Software RH FRONT Rack uploading.............................................................................36
2 .2.1 Initialization (fig 2) ..............................................................................................38 
2.2.2 Uploading ...........................................................................................................41 
2.2.2.1 Uploading SFCC 1 - SFCC 2 - SFCC 3 modules ............................41
2 .2.2.2 Uploading MAIC 1A - MAIC 3A modules.........................................48  
2.2.2.3 Uploading SFCC 1 - SFCC 2 - SFCC 3 - MAIC 1A - MAIC 3A 
modules ...........................................................................................55
2 .2.3 Sticking of labels ................................................................................................61
2 .2.4 Printing of report (fig 4).......................................................................................62 
2.2.5 Close-up RH FRONT Rack ................................................................................65 
2.3 Supplement .....................................................................................................................65 
2.3.1 Checks asked in the SB .....................................................................................65

### Page 14

REFERENCE 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 the 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 procedure, 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 documents 
This Data Modules are consultable in Falcon Portal (AMM documentation - Field F7X) 
 
20-30-00-910-803 Electrostatic discharge (ESD) standard practices 
24-00-00-860-801 Energization / de-energization 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 Airborne systems and Equipment Certification 
 
This document is not useful for the procedure performing.

### Page 15

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 configuration 
 
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 Energy 
 
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 acronyms 
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 Unit

### Page 16

REFERENCE 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 after 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 modules 
• 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 modules 
• MAIC 1A / MAIC 3A : up to 8' per module (about 16') 
• SFCC 1 / 2 / 3 : up to 5' per module (about 15')

### Page 17 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913 _ _D  28/05/2010
2.  PROCEDURE
2.1  Software LH FRONT Rack uploading
NOTE : see hereafter the LHF Rack layout.
LHF
Power Supplies
E2 E3  E4
PIN  CFI
Slot #  TOP  ATA #
17  Spare  27-01-1700
16  Spare  27-01-1600
15  LHF PWR3  27-01-1500  00A050-xx (1501 CZ)
14  FDC4-B  27-01-1400  0877X302-xx (1401 CZ)
13  MFCC3_A  27-01-1300  ENS7X101-xx (1301CZ)
12  MFCC3_B  27-01-1200  ENS7X102-xx (1201CZ)
11  MFCC2_A  27-01-1100  ENS7X101-xx (1101CZ)
10  MFCC2_B  27-01-1000  ENS7X102-xx (1001CZ)
9  MFCC1_A  27-01-0900  ENS7X101-xx (901CZ)
8  MFCC1_B  27-01-0800  ENS7X102-xx (801CZ)
7  FDC2-B  27-01-0700  0877XS02-xx (701C2)
6  MAIC2 A  27-01-0600  ENS7X501-xx (601CL)
5  MAI 2  27-01-0500  0877X502-xx (501CL)
4  MAICA_A  27-01-0400  ENS7X501-xx (401CL)
3  MAI_4  27-01-0300  0877X502-xx (301CZ)
2  LHF_PWR2  27-01-0200  00A050-xx (201 CZ)
LHF_PWR4  27-01-0100  00A050-xx (101 CZ)
BOTTOM
Approved  4. PROCEDURE  6
Inis docum  t is the intellectual property of DASSAULT AVIATION. It may not be used, reproduced, modified or disclosed without its authorization. DASSAULT AVIATION Proprietary Data.

### Page 18 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
FCS UPLOADER
MEM405-01  LH FRONT
LHF RACK INSTALLATION  RACK
Slot 17
FIG 1
MEM 40505-01
LHF INTERFACE
Module
MEM 40501-01
ELECTRONIC UNIT
Movable connector  B type USB port [
128 contacts  MEM 40501-01 - PC
between LHF  Portable J
interface module
MEM40505-01 and
Electronic Unit
MEM40501-01  A type USB port
to plug the hand-held
MEM 40504-01
DDM00102-XX  FCS Labels  paperbook  Hand-held scanner  MEM 40504-01
A type USB port [ PC
Portable - MEM
40501-011
FCS software
DDM00101-xx
Approved  4. PROCEDURE
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.

### Page 19

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 Initialization (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 (electrical connection AC 110V/220V) if 
its own battery is not charged enough to ensure 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 drive 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 connector 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 required connections to 
upload. A message drawing attention on the laptop running on its own battery can be displayed 
 
NOTE : the aircraft is de-energized.

### Page 20 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913 D  28/05/2010
4 FCS Uploader
DASSAULT Aviation FCS Uploader
1.0.46.0
Welcome to DASSAULT AVIATION FCS Uploader.
Please ensure that this laptop is properly connected to the Flight Control System
rack.
The aircraft power supplies shall be switched off.
IS DASSAULT  Next›
• Clic on "Next"
4 FCS Uploader
Please select your name in the list
Add  Remove
S DASSAULT
• Clic on "Add" and enter the uploading operator's name
Add user  Add user
Name:  Name: Jérôme CAPPELLE
OK  Cancel  OK  Cancel
4 FCS Uploader
Please select your name in the list
dérôme CAPPELLE
Add  Remove
PASSAU  Next>  Quit
Approved  4. PROCEDURE
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.

### Page 21

REFERENCE 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 still "ON", this red message occurs 
 
 
 
NOTE : This screen stays in this state until the application detects automatically power supplies 
switched off; then the following screen appears

### Page 22

REFERENCE 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: 
ƒ MFCC and MAIC, go to chapter 4.1.2.3 
ƒ MFCC only, go to chapter 4.1.2.2 
ƒ MAIC only, go to chapter 4.1.2.1 
2.1.2.1  Uploading MAIC 2A / MAIC 4A modules 
 
• Notch the case MAIC

### Page 23

REFERENCE 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 supplies detection, the link between LH FRONT RACK and Electronic 
Unit (MEM40501-01) is automatically done

### Page 24 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913 D 28/05/2010
NOTE: During the link setting up, a bell-ringing like "DING/DONG" can be heard from the
laptop
• Clic on "Next" when the "Next" button is enable
4 FCS Uploader
Please scan the labels of the modules in the following order:
Slot  Designation  P/N  S/N
06  MAICZA
04  MAICAA
& DASSAULT  ‹Previous  Quit
SCAN 1 : scan the modules MAICA (slot 6) and MAIC4A (slot 4) bar codes ( to facilitate the
scan, lift the left locking lever)
FCS Uploader
Please scan the labels of the modules in the following order:
Slot  Designation  P/N  S/N
06  MAIC2A  ENS7X501-18  8888
04  MAIC4A  ENS7X501-18  9999
5 DASSAULT  ‹Previous  Next  Quit
Clic on "Next"
NOTE : if the operator make an error as : wrong slot scanned, scanning order 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
FCS Uploader  FCS Uploader
This bar code was already scanned. Please check the
Please insert the FCS software update media.  list.
Ok  Ok  Cancel
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.

### Page 25 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
FCS Uploader
The bar code does not match the expected part
number.
Cancel
In this case, clic on OK and start again the operation 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"
4 FCS Uploader
Please scan the NEW labels in the following order:
Slot  Current P/N  S/N  New P/N
06  ENS7X501-18  9999
04  ENS7X501-18  8888
(4) DASSAULT  ‹Previous
• Clic on "Next". The screen below could be displayed during the CD ROM activity
Opening database..
SCAN 2 : scan the labels MAICZA and MAIC4A on the related FCS labels paperbook
(DDM00102-xx)
4 FCS Uploader
Please scan the NEW labels in the following order:
Slat  Current P/N  S/N  New P/N
06  ENS7X501-18  9999  ENS7X501-20
04  ENS7X501-18  8888  ENS7X501-20
Sy DASSAULT  ‹Previous  Next>
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.

### Page 26

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 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 uploading operation is to begin. 
 
NOTE : if you click on "NO", uploading is aborted 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 window. A correctly uploaded module is 
announced by

### Page 27 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913 D 28/05/2010
4 FCS Uploader
Do not disconnect the laptop.
Do not switch off the aircraft power supplies.
Slot  Current P/N  S/N  New P/N
→ 06  ENS7X501-18  9999  ENS7X501-20
04  ENS7X501-18  8888  ENS7X501-20
The upload is in progress...
( PASSAULT •
• 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
CS Uploader
Upload errors have occurred !
Please check the connections and the aircraft power
supplies
4 FCS Uploader
Do not disconnect the laptop.
Do not switch off the aircraft power supplies.
Slot  Current P/N  S/N  New P/N
× 06  ENS7X501-18  9999  ENS7X501-20
04  ENS7X501-18  8888  ENS7X501-20
The upload is in progress...
(8) DASSAULT
• When one or several slots are notched X clic on "Retry" to re-start the related modules failed
uploading sequences.
CAUTION : The operator can apply a "Retry". If a failure 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 related uploaded module is however new FCS
standard upgraded but considered as faulty and must be replaced.
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.

### Page 28 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
4 FCS Uploader
Slot  Current P/N  S/N  New P/N
Ж 06  ENS7X501-18  9999  ENS7X501-20
≤ 04  ENS7X501-18  8888  ENS7X501-20
(8) DASSAULT  Retry  Quit
• The uploading procedure is successfully completed when the whole displayed slots are notched
4 FCS Uploader
Slot  Current P/N  S/N  New P/N
V 06  ENS7X501-18  9999  ENS7X501-20
V 04  ENS7X501-18  8888  ENS7X501-20
FCS Uploader
The upload operation is successful.
Please disconnect the laptop and switch off the power
supplies.
(S DASSAULT  Cancel
• Clic on "Quit", the application "FCS UPLOADER" closes
IMPORTANT :
Inside the LH FRONT RACK slot 6 and slot 4,unstick the MAICZA and MAICAA modules
labels scanned at step SCANI
Then go to chapter 4.1.3.
2.1.2.2 Uploading MFCC 1A/B - MFCC 2A/B - MFCC ЗА/B modules
• Notch the case MFCC
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.

### Page 29

REFERENCE 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 supplies detection, the link between LH FRONT RACK and Electronic 
Unit (MEM40501-01) is automatically done

### Page 30

REFERENCE 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 (slot 8) bar codes. To facilitate the scan, 
lift the left locking lever.

### Page 31

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 order 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 operation 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"

### Page 32

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 the 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 fed with scanned MFCC3A, MFCC3B, MFCC2A, 
MFCC2B, MFCC1A and MFCC1B 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 clic "OK" and start again the 
operation starting from the module which caused the error message

### Page 33 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
FCS Uploader  FCS Uploader
The bar code does not match the expected part  number.  The serial numbers do not match.
Cancel  Ok  Cancel
FCS Uploader
The new P/N does not belong to this FCS standard.
Please check either the label or the FCS standard
media
Bar code reading is finished.
A message warns that an uploading operation is to begin.
NOTE: if you click on "NO", uploading is aborted and the application goes back to screen
SCAN
You are about to perform an upload operation. Do you
confirm the operation?
• 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 window. A correctly uploaded module is notched
4 FCS Uploader
Do not disconnect the laptop.
Do not switch off the aircraft power supplies.
Slot  Current P/N  S/N  New P/N
→ 13  ENS7X101-11  9999  ENS7X101-12
12  ENS7X102-11  9999  ENS7X102-12
11  ENS7X101-11  8888  ENS7X101-12
10  ENS7X102-11  8888  ENS7X102-12
09  ENS7X101-11  7777  ENS7X101-12
08  ENS7X102-11  7777  ENS7X102-12
The upload is in progress..
DASSAULT
• A failed uploading sequence is notched X. A warning message asks to check the connections
and electrical powers but the next module uploading sequence goes on
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.

### Page 34 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
• FCS Uploader
Do not disconnect the laptop.
Do not switch off the aircraft power supplies.
Slot  Current P/N  S/N  New P/N
/ 13  ENS7X101-11  9999  ENS7X101-12
~ 12  ENS7X102-11  9999  ENS7X102-12
≤ 11  ENS7X101-11  8888  ENS7X101-12
→ 10  ENS7X102-11  8888  ENS7X102-12
09  ENS7X101-11  7777  ENS7X101-12
08  ENS7X102-11  7777  ENS7X102-12
The upload is in progress...
AVIATION
When one or several slots are notched X clic on "Retry" to re-start the related modules failed
uploading sequences.
FCS Uploader
Upload errors have occurred!
Please check the connections and the aircraft power
supplies
FCS Uploader
Do not disconnect the laptop.
Do not switch off the aircraft power supplies.
Slot  Current P/N  S/N  New P/N
/ 13  ENS7X101-11  9999  ENS7X101-12
× 12  ENS7X102-11  9999  ENS7X102-12
≤ 11  ENS7X101-11  8888  ENS7X101-12
→ 10  ENS7X102-11  8888  ENS7X102-12
09  ENS7X101-11  7777  ENS7X101-12
08  ENS7X102-11  7777  ENS7X102-12
The upload is in progress...
A DASSAULT
CAUTION : The operator can apply a "Retry". If a failure 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 related uploaded module is however new FCS
standard upgraded but considered as faulty and must be replaced.
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.

### Page 35 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
4 FCS Uploader
Slot  Current P/N  S/N  New P/N
· 13  ENS7X101-11  9999  ENS7X101-12
× 12  ENS7X102-11  9999  ENS7X102-12
/ 11  ENS7X101-11  8888  ENS7X101-12
/ 10  ENS7X102-11  8888  ENS7X102-12
/ 09  ENS7X101-11  7777  ENS7X101-12
· 08  ENS7X102-11  7777  ENS7X102-12
(S) DASSAULT  Retry
• The uploading procedure is successfully completed when the whole displayed slots are
notched v
4 FCS Uploader
Slot  Current P/N  S/N  New P/N
/ 13  ENS7X101-11  9999  ENS7X101-12
V 12  ENS7X102-11  9999  ENS7X102-12
≤ 11  ENS7X101-11  8888  ENS7X101-12
/ 10  ENS7X102-11  8888  ENS7X102-12
/09  ENS7X101-11  7777  ENS7X101-12
/ 08  ENS7X102-11  7777  ENS7X102-12
FCS Uploader
The upload operation is successful.
Please disconnect the laptop and switch off the power
supplies.
(Ey DASSAULT  Retry  Quit  Ok  Cancel
• Clic on "Quit", the application "FCS UPLOADER" closes
IMPORTANT :
• Inside the LH FRONT RACK slot 13, 12, 11, 10, 09 and 08, unstick the MFC, MFC,
MFCCZA, MFCC2B, MECCIA and MFCC1B modules labels scanned at step SCANI
Then go to chapter 4.1.3.
2.1.2.3 Uploading MAIC 2A - MAIC 4A - MFCC 1A/B - MFCC 2A/B - MFCC ЗA/B modules
• Notch the cases MFCC and MAIC
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.

### Page 36

REFERENCE 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 supplies detection, the link between LH FRONT RACK and Electronic 
Unit (MEM40501-01) is automatically done

### Page 37

REFERENCE 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 (slot 8), MAIC2A (slot 6), MAIC4A (slot 4) 
bar codes. To facilitate the scan, lift the left locking lever.

### Page 38

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 slot scanned, scanning order 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 operation 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"

### Page 39

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 the CD ROM activity  
 
 
 
• SCAN 2 : Scan the labels MFCC3A, MFCC3B, MFCC2A, MFCC2B, MFCC1A, MFCC1B, 
MAIC2A, MAIC4A on the related FCS labels paperbook (DDM00102-xx) 
 
 
 
• Clic on "Next" 
 
Column "NEW P/N" is automatically fed 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 doesn't match with the one expected in the 
column"NEW P/N", the following message is displayed. In this case clic"OK" and start again 
the operation starting from the module which caused the error message

### Page 40 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
FCS Uploader  FCS Uploader
The bar code does not match the expected part  number.  The serial numbers do not match.
Cancel  Ok  Cancel
FCS Uploader
The new P/N does not belong to this FCS standard.
Please check either the label or the FCS standard
media
Cancel
Bar code reading is finished.
A message warns that an uploading operation is to begin.
NOTE: if you click on "NO", uploading is aborted and the application goes back to screen
SCAN 2
You are about to perform an upload operation. Do you
contirm the operation?
Yes  No
• 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 window. A correctly uploaded module is notched
4 FCS Uploader
Do not disconnect the laptop.
Do not switch off the aircraft power supplies.
Slot  Current P/N  S/N  New P/N
→ 13  ENS7X101-11  9999  ENS7X101-12
12  ENS7X102-11  9999  ENS7X102-12
11  ENS7X101-11  8888  ENS7X101-12
10  ENS7X102-11  8888  ENS7X102-12
09  ENS7X101-11  7777  ENS7X101-12
08  ENS7X102-11  7777  ENS7X102-12
06  ENS7X501-18  9999  ENS7X501-20
04  ENS7X501-18  8888  ENS7X501-20
The upload is in progress..
DASSAULT
Approved  4. PROCEDURE  29
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### Page 41 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913 D 28/05/2010
• A failed uploading sequence is notched X. A warning message asks to check the connections
and electrical powers but the next module uploading sequence goes on
4 FCS Uploader
Do not disconnect the laptop.
Do not switch off the aircraft power supplies.
Slot  Current P/N  S/N  New P/N
/ 13  ENS7X101-11  9999  ENS7X101-12
≤ 12  ENS7X102-11  9999  ENS7X102-12
< 11  ENS7X101-11  8888  ENS7X101-12
→ 10  ENS7X102-11  8888  ENS7X102-12
09  ENS7101-11  7777  ENS7X101-12
08  ENS7X102-11  7777  ENS7X102-12
06  ENS7X501-18  9999  ENS7X501-20
04  ENS7X501-18  8888  ENS7X501-20
The upload is in progress.
DASSAULT
• When one or several slots are notched X clic on "Retry" to re-start the related modules failed
uploading sequences.
FCS Uploader
Upload errors have occurred !
Please check the connections and the aircraft power
supplies
4 FCS Uploader
Do not disconnect the laptop.
Do not switch off the aircraft power supplies.
Slot  Current P/N  S/N  New P/N
/ 13  ENS7X101-11  9999  ENS7X101-12
V 12  ENS7X102-11  9999  ENS7X102-12
X 11  ENS7X101-11  8888  ENS7X101-12
→ 10  ENS7X102-11  8888  ENS7X102-12
09  ENS7X101-11  7777  ENS7X101-12
08  ENS7X102-11  7777  ENS7X102-12
ENS7X501-18  9999  ENS7X501-20
04  ENS7X501-18  8888  ENS7X501-20
The upload is in progress...
& PASSAULT
Approved  4. PROCEDURE
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.

### Page 42 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
4 FCS Uploader
Slat  Current P/N  S/N  New P/N
· 13  ENS7X101-11  9999  ENS7X101-12
N 12  ENS7X102-11  9999  ENS7X102-12
× 11  ENS7X101-11  8888  ENS7X101-12
≤ 10  ENS7X102-11  8888  ENS7X102-12
· 09  ENS7X101-11  7777  ENS7X101-12
/ 08  ENS7X102-11  7777  ENS7X102-12
V 06  ENS7X501-18  9999  ENS7X501-20
V04  ENS7X501-18  8888  ENS7X501-20
8) DASSAULT  Retry  Quit
CAUTION : The operator can apply a "Retry". If a failure 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 related uploaded module is however new FCS
standard upgraded but considered as faulty and must be replaced.
• The uploading procedure is successfully completed when the whole displayed slots are notched
4 FCS Uploader
Slot  Current P/N  S/N  New P/N
≤ 13  ENS7X101-11  9999  ENS7X101-12
N 12  ENS7X102-11  9999  ENS7X102-12
≤ 11  ENS7X101-11  8888  ENS7X101-12
≤ 10  ENS7X102-11  8888  ENS7X102-12
109  ENS7X101-11  7777  ENS7X101-12
/ 08  ENS7X102-11  7777  ENS7X102-12
/ 0Б  ENS7X501-18  9999  ENS7X501-20  FCS Uploader
/ 04  ENS7X501-18  8888  ENS7X501-20
The upload operation is successful.
Please disconnect the laptop and switch off the power
supplies.
(A) DASSAULT  Retry  Quit  Ok  Cancel
• Clic on "Quit", the application "FCS UPLOADER" closes
IMPORTANT :
• Inside the LH FRONT RACK, unstick the MFCCA, MFCC3B, MFCC2A, MFCC2B,
MFCCIA; MFCC1B, MAIC2A and MAIC4A modules labels scanned at step SCAN1
Then go to chapter 4.1.3.
2.1.3 Sticking of labels
Approved  4. PROCEDURE  31
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### Page 43

REFERENCE INDICE DATE 
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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 remote loading has failed must mandatory be 
identified by the new label of the uploaded standard. They will be considered broken down and the 
procedure of installation/remove modules will have being applied 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 4

### Page 44 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
• Tool name,
• Tool version,
• Module Part Number,
• Module Serial Number,
• Upload status.
Laptop directory : My Documents\Dassault-Aviation\FCS Uploader\Logs\Falcon 7X\n°A/C
(A/C serial number entered by the operator at the beginning of the procedure)
Dossiers  ×  Nom  Taille  • Type  Date de modific... 4
Of Bureau  E LH FRONT RACK_2010_01_05, 10g  1 Ko Document texte  05/01/2010 12:10
= 1 Mes documents
+ • CD Designer
• • DASSAULT Aviation
DIO FCS Uploader
•O Logs
• Falcon 7X
Modules
) 2010-01-05
If more than one report is recorded in the directory, the last one 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 reports available in the Laptop directory:
"My Documents \ Dassault-Aviation \ FCS Uploader \ Modules".
Dossiers  × Nom  Taille Type  Date de modific... 4
G Bureau  E) ENS7X501-18#8888 2010-01-05 12_06_45.log  3 Ko Document texte  05/01/2010 12:06
• L Mes documents  E) ENS7X501-18#9999 2010-01-05 12_07_01.log  3 Ko Document texte  05/01/2010 12:07
# D CD Designer  E ENS7X51-18*8888 2010-01-05 12_09_13. log  3 Ko Document texte  05/01/2010 12:09
• O DASSAULT Aviation  E ENS7X501-18#9999 2010-01-05 12_09_35./og  3 Ko Document texte  05/01/2010 12:09
• a FCS Uploader  E ENS7X501-18#8888 2010-01-05 12_10_49. log  3 Ko Document texte  05/01/2010 12:10
eÒ Logs  E ENS7X501-18#9999 2010-01-05 12_10_49.log  3 Ko Document texte  05/01/2010 12:10
• O Falcon 7X
• a Modules
• 2010-01-05
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.
Approved  4. PROCEDURE  33
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### Page 45

REFERENCE INDICE DATE 
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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 :

### Page 46

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 the 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 4.3

### Page 47 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
2.2 Software RH FRONT Rack uploading
NOTE : see hereafter the RHF Rack layout.
RHF
Power Supples
E1  ЕЗ  Е4
P/N  CFI
ATA #  TOP  Slot #
27-02-0100  Spare  1
27-02-0200  Spare  2
27-02-0300  RHF_PWR4  3  00A051-xx (302 CZ)
27-02-0400  SFCI4  4  0877X601-xx (402 CZ)
27-02-0500  SFCI3  5  0877X601-xx (502 CZ)
27-02-0600  FDC1-A  0877X301-xx (602 CZ)
27-02-0700  FDC3-A  7  0877X301-xx (702CL)
27-02-0800  SFCC1  8  ENS7X201-xx (802CZ)
27-02-0900  SFCC2  9  ENS7X201-xx (902CZ)
27-02-1000  SFCC3  10  ENS7X201-xx (1002 CZ)
27-02-1100  FDC5-A  11  0877X301-xx (1102CZ)
27-02-1200  МАІС3_А  12  ENS7X501-xx (1202CZ)
27-02-1300  MAI_3  13  0877X502-xx (1302 CZ)
27-02-1400  MAIC1_A  14  ENS7X501-xx (1402 CZ)
27-02-1500  MAI_1  15  0877X502-xx (1502C2)
27-02-1600  RHF_PWR1  16  00A051-xx (1602CZ)
27-02-1700  RHF_PWR3  17  00A051-xx (1702CL)
BOTTOM
Approved  4. PROCEDURE  36
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### Page 48 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
FCS UPLOADER
MEM 405-01
RHF RACK INSTALLATION
FIG 2  RH FRONT  RACK
Slot 1
MEM 40506-01
RHF INTERFACE
Module
MEM 40501-01
ELECTRONIC UNIT
Movable connector  B type USB port [
128 contacts  MEM 40501-01 - PC
between RHF  Portable ]
interface module
MEM40506-01 and
Electronic Unit
MEM40501-01  A type USB port
to plug the hand-held
scanner
MEM 40504-01
FCS Labels  Hand-held scanner  MEM 40504-01
paperbook
DDM00102-XX
A type USB port [ PC
Portable - MEM
40501-011
FCS software
DDM00101-XX
Approved  4. PROCEDURE  37
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### Page 49

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 Initialization (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 (electrical connection 110V/220V AC) if 
its own battery is not charged enough to ensure 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 drive 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 connector 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 required connections to 
upload. A message drawing attention on the laptop running on its own battery can be displayed 
NOTE : the aircraft is de-energized.

### Page 50 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913 D  28/05/2010
4 FCS Uploader
DASSAULT Aviation FCS Uploader
1.0.46.0
Welcome to DASSAULT AVIATION FCS Uploader.
Please ensure that this laptop is properly connected to the Flight Control System
rack.
The aircraft power supplies shall be switched off.
(8) DASSAULT  Next>  Quit
• Clic on "Next"
4 FCS Uploader
Please select your name in the list
Add  Remove
- DASSAULT  Quit
• Clic on "Add" and enter the uploading operator's name
Add user  Add user
Name:  Name: Jérôme CAPPELLE
Cancel  OK  Cancel
Approved  4. PROCEDURE  39
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### Page 51 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913 D  28/05/2010
4 FCS Uploader
Please select your name in the list
Jérôme CAPPELLE
Add  Remove
A DASSAULT  AVIATION  Quit
• Select your name in the list
• Clic on "Next"
• Enter the aircraft serial number
• Select the RH FRONT RACK
4 FCS Uploader
Aircraft serial number:
Select the rack to upload:
= * Falcon 7X
1 LH FRONT RACK
RH FRONT RACK
A DASSAULT  ‹Previous  Quit
• If the aircraft power supplies are still "ON", this red message occurs
4 FCS Uploader
Aircraft serial number: 0
Select the rack to upload:
= * Falcon 7X
LH FRONT RACK
RH FRONT RACK
Please switch off the aircraft power supplies.
(4) DASSAULT  ‹Previous  Next›  Quit
Approved  4. PROCEDURE 40
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### Page 52

REFERENCE INDICE DATE 
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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 automatically 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: 
ƒ SFCC and MAIC, go to chapter 4.2.2.3 
ƒ SFCC only, go to chapter 4.2.2.1 
ƒ MAIC only, go to chapter 4.2.2.2 
 
2.2.2.1  Uploading SFCC 1 - SFCC 2 - SFCC 3 modules 
 
• Notch the case SFCC

### Page 53

REFERENCE INDICE DATE 
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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 supplies 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 laptop

### Page 54 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
4 FCS Uploader
Please perform the following tasks in chronological order.
Notch the case when done:
• Power-on the aircraft power supplies.
• Set the switches TEST E1 and TEST E2 to the ON position.
• Close H5 breaker (FBW RF E4) on RH Front SPDB
- Close H3 breaker (FBW RF E3) on LH Front SPDB
BY PASSAULT  ‹Previous  Quit
4 FCS Uploader
Please perform the following tasks in chronological order.
Notch the case when done:
• Power-on the aircraft power supplies.
• Set the switches TEST E1 and TEST E2 to the ON position.
• Close H5 breaker (FBW RF E4) on RH Front SPDB
• Close H3 breaker (FBW RF E3) on LH Front SPDB
• DASSAULT  ‹Previous
Clic on "Next" when the "Next" button is enable
4 FCS Uploader
Please scan the labels of the modules in the following order:
Slot  Designation  P/N  S/N
08  SFCC1
09  SFCC2
10  SFCC3
8) DASSAULT  ‹Previous  Next>  Quit
SCAN 1 :scan the modules SFCC1 (slot 8), SFCC2 (slot 9) and SFCC3 (slot 10). To facilitate
the scan, lift the right locking lever.
Approved  4. PROCEDURE 43
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### Page 55 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
FCS Uploader
Please scan the labels of the modules in the following order:
Slot  Designation  P/N  S/N
08  SFCC1  ENS7X201-14  9999
09  SFCC2  ENS7X201-14  8888
10  SFOC3  ENS7X201-14  7777
(4) DASSAULT  ‹Previous  Next>  Quit
• Clic on "Next"
NOTE: if the operator make an error as wrong slot scanned, scanning order 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
FCS Uploader  FCS Uploader
This bar code was already scanned. Please check the
Please insert the FCS software update media.  list.
Ok  Cancel
FCS Uploader
The bar code does not match the expected part
number.
• In this case, clic on OK and start again the operation 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"
Approved  4. PROCEDURE  44
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### Page 56

REFERENCE INDICE DATE 
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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 the 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 doesn't match with the one expected in the 
column"NEW P/N", the following message is displayed. In this case clic"OK" and start again 
the operation starting from the module which caused the error message

### Page 57 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
FCS Uploader  FCS Uploader
The bar code does not match the expected part  number.  The serial numbers do not match.
Cancel  Ok Cancel
FCS Uploader
The new P/N does not belong to this FCS standard.
Please check either the label or the FCS standard
media
Cancel
Bar code reading is finished.
A message warns that an uploading operation is to begin.
NOTE: if you click on "NO", uploading is aborted and the application goes back to screen
SCAN 2
You are about to perform an upload operation. Do you
contirm the operation?
Yes  No
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 window. A correctly uploaded module is notched
4 FCS Uploader
Do not disconnect the laptop.
Do not switch off the aircraft power supplies.
Slot  Current P/N  S/N  New P/N
→ 08  ENS7X201-14  9999  ENS7X201-14
09  ENS7X201-14  8888  ENS7X201-14
10  ENS7X201-14  7777  ENS7X201-14
The upload is in progress...
8) DASSAULT
• A failed uploading sequence is notched X . A warning message asks to check the connections
and electrical powers but the next module uploading sequence goes on
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.

### Page 58 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
4 FCS Uploader
Do not disconnect the laptop.
Do not switch off the aircraft power supplies.
Slat  Current P/N  | S/N  New P/N
· 08  ENS7X201-14  9999  ENS7X201-14
× 09  ENS7X201-14  8888  ENS7X201-14
→ 10  ENS7X201-14  7777  ENS7X201-14
The upload is in progress...
(9) DASSAULT
FCS Uploader
Upload errors have occurred !
Please check the connections and the aircraft power
supplies
• When one or several slots are notched X clic on "Retry" to re-start the related modules failed
uploading sequences.
CAUTION : The operator can apply a "Retry". If a failure 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 related uploaded module is however new FCS
standard upgraded but considered as faulty and must be replaced.
4 FCS Uploader
Slat  Current P/N  S/N  New P/N
· 08  ENS7X201-14  9999  ENS7X201-14
× 09  ENS7X201-14  8888  ENS7X201-14
≤ 10  ENS7X201-14  7777  ENS7X201-14
(9) DASSAULT  Retry  Quit
• The uploading procedure is successfully completed when the whole displayed slots are notched
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.

### Page 59 (OCR)

NOT CLASSIFIED
DASSAULT  REFERENCE  INDICE  DATE
AVIATION  DT EQUIP 43913  28/05/2010
4 FCS Uploader
Slat  Current P/N  S/N  New P/N
· 08  ENS7X201-14  9999  ENS7X201-14
· 09  ENS7X201-14  8888  ENS7X201-14
/ 10  ENS7X201-14  7777  ENS7X201-14
FCS Uploader
The upload operation is successfu
Please disconnect the laptop and switch off the powe
supplies.
(S) DASSAULT  Retry  Quit  Cancel
• Clic on "Quit", the application "FCS UPLOADER" closes
IMPORTANT :
• Inside the RH FRONT RACK slot 8, 9 and 10,unstick the SFCCI, SFCC2 and SFCC3 modules
labels scanned at step SCANI
Then go to chapter 4.2.3.
2.2.2.2 Uploading MAIC 1A - MAIC 3A modules
• Notch the case MAIC
FCS Uploader
Please select the modules to upload:
Name  Designation
• SFCC SECONDARY FOC Set
• MAIC MAINT.AV.INT.CPU Set
S DASSAULT  ‹Previous  Next  Quit
• Clic on "Next"
• Perform the following steps in chronological order
• Energize the aircraft (refer to 24-00-00-860-801)
• On the maintenance panel (1010TP) set the TEST E1 switch (R511CZ) and TEST E2
switch(L511CZ) to the ON position (UP position)
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.

### Page 60

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 supplies 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 laptop

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