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
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
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

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DASSAULT AVIATION Proprietary Data
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
• 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
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
(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

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DASSAULT 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

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DASSAULT AVIATION Proprietary Data
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

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DASSAULT AVIATION Proprietary Data
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

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DASSAULT AVIATION Proprietary Data
Figure 1: SPEED LIMITATION PLACARDS

END OF DOCUMENT

FALCON 7X 7X-214

August 30, 2011 ATA 27

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DASSAULT AVIATION Proprietary Data
NOT CLASSIFIED

Procedure 

FCS DATA LOADING PROCEDURE 

SCOPE 

Falcon 7X 

 

Approved 

Division Dassault Equipements - Direction Technique 

 

 

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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 
REFERENCE INDICE DATE 

DT EQUIP 43913 D 28/05/2010

NOT CLASSIFIED

Approved TABLE OF CONTENTS 2

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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
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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. 
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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 
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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 installation 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') 
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2. PROCEDURE 

2.1 Software LH FRONT Rack uploading 

NOTE : see hereafter the LHF Rack layout. 
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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. 
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• Clic on "Next" 

• Clic on "Add" and enter the uploading operator's name 

 
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• 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 
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• Clic on "Next" 

2.1.2 Uploading 

Depending of the upload requested for the new standard 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 MAIC 2A / MAIC 4A modules 

• Notch the case MAIC 
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• 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 
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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 

• SCAN 1 : scan the modules MAIC2A (slot 6) and MAIC4A (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 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 

 
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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" 

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

• SCAN 2 : scan the labels MAIC2A and MAIC4A on the related FCS labels paperbook 

(DDM00102-xx)
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• 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 
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• 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 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. 
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• The uploading procedure is successfully completed when the whole displayed slots are notched 

 

• Clic on "Quit", the application "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 MFCC 1A/B - MFCC 2A/B - MFCC 3A/B modules 

• Notch the case MFCC 
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• 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 
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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. 
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• 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" 
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• 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 
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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 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 on 
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• 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 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. 
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• The uploading procedure is successfully completed when the whole displayed slots are 

notched

 

• Clic on "Quit", the application "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 modules labels scanned at step SCAN1

Then go to chapter 4.1.3. 

2.1.2.3 Uploading MAIC 2A - MAIC 4A - MFCC 1A/B - MFCC 2A/B - MFCC 3A/B modules 

• Notch the cases MFCC and MAIC 
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• 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 
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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. 
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• 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" 
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• 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 
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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 notched 
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• 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. 
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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 

 

• Clic on "Quit", the application "FCS UPLOADER" closes 

IMPORTANT : 

• Inside the LH FRONT RACK, unstick the 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 labels 
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• 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 
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o Tool name, 

o Tool version, 

o Module Part Number, 

o Module Serial Number, 

o 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) 

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”. 

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. 
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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 : 
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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 
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2.2 Software RH FRONT Rack uploading 

NOTE : see hereafter the RHF Rack layout. 
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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. 
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• Clic on "Next" 

• Clic on "Add" and enter the uploading operator's name 

 
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• 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 still "ON", this red message occurs 
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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 standard 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 - SFCC 3 modules 

• Notch the case SFCC 
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• 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 
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• Clic on "Next" when the "Next" button is enable 

• SCAN 1 :scan the modules SFCC1 (slot 8), SFCC2 (slot 9) and SFCC3 (slot 10). To facilitate 

the scan, lift the right locking lever. 
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• 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 three modules are correctly recognized 

• Clic on "Next" 
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• 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 
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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

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 

• 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 
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• 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 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 
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• Clic on "Quit", the application "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 MAIC 1A - MAIC 3A modules 

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

• SCAN 1 scan the modules MAIC3A (slot 12) and MAIC1A (slot 14) bar code (to facilitate the 

scan, lift the right locking lever) 

• Clic on "Next" 
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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 two modules are correctly recognized 

• Clic on "Next" 

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

• SCAN 2 : Scan the labels MAIC3A and MAIC1A on the related FCS labels paperbook 

(DDM00102-xx)
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• 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 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
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• 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 

• 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 
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• 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 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 

 

• Clic on "Quit",the application "FCS UPLOADER" closes 
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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 - SFCC 3 - MAIC 1A - MAIC 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 done 
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• After electrical power supplies 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/DONG" can be heard from the 

laptop 

• Clic on "Next" when the "Next" button is enable 
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• SCAN 1 : scan the modules SFCC1 (slot 8), SFCC2 (slot 9), SFCC3 (slot 10), MAIC3A (slot 

12) and MAIC1A (slot 14) bar codes (to facilitate the scan, lift the right locking lever) 

• 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 

 
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• 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 five modules are correctly recognized 

• Clic on "Next" 

• Clic on "Next". The screen below could be displayed during the 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" 
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Column "NEW P/N" is automatically fed with scanned SFCC1, SFCC2, SFCC3, MAIC3A, 

MAIC1A label information from the 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 notched 
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• 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 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. 
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• The uploading procedure is successfully completed when the whole displayed slots are notched 

 

• Clic on "Quit", the application "FCS UPLOADER" closes 

IMPORTANT : 

• Inside the RH FRONT RACK, unstick the SFCC1 (slot 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 applied in this case (refer to 27-90-01-

900-803). 
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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 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) 

See examples on LH FRONT rack in chapter 4.1.4 

If more than one report is recorded in the directory, the last one in time shall be considered. 

This report is to be : 

MAIC3A 

slot 12 

MAIC1A 

Slot 14 

SFCC1 

SFCC2 

SFCC3 

Slot 8 to 10 
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- 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”. 

See examples on LH FRONT rack in chapter 4.1.4 

NOTE :If no LH FRONT rack module to upload or if LH FRONT rack modules are already 

uploaded, go to item § 4.2.5 else go to § 4.1. 
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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 : 
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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 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 conector 128 contacts 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 FRONT 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 test on the CMC screen “FCS ELECTRONIC 

FAILURES (1/4)” 

A part of this automatic test checks the consistency of all the modules versions (Hardware 

and Software) with a compatibility table embedded in the MAIC4 module. 
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• 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”) associated 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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