# Dassault Service Bulletin F7X-214: No revision named

- Rights: © Dassault Aviation. Filed by the FAA in regulations.gov docket FAA-2013-0464, the docket of AD 2014-16-23. Not covered by OpenAirDocs’ CC0 dedication.
- Document: [Dassault Service Bulletin F7X-214](https://openairdocs.org/service-documents/dassault/f7x-214.md)
- Title as filed: U.S. DOT/FAA - SB F7X-214 Erratum
- Pages: 11
- PDF: https://openairdocs.org/files/sha256/e1/c1/e1c19c95b0836582d8905748f696baf65cb286e7ec99739ebbfc38eb3eb63c8d
- Page: https://openairdocs.org/service-documents/dassault/f7x-214/file/e1c19c95b083

## Text

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### Page 1

FALCON 7X
No 214
JANUARY 26, 2012
MANDATORY
ATA 27
FLIGHT CONTROLS
MODULAR ELECTRONIC FLIGHT CONTROL SYSTEM
FCS STANDARD 2.1.7.3
FALCON SERVICE BULLETIN
Copyright © 2012 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
Erratum January 26, 2012
List of effective pages :
1 to 9
List of modified pages :
1
REASON:Modification of NOTE 1 (para. 1. A.), Dassault Aviation recommends to load
simultaneously the latest applicable Electronic CheckList (ECL) database version
when complying with Service Bulletin 7X-214.
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 recommends to load simultaneously the latest applicable Electronic
CheckList (ECL) database version.
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:
• This Service Bulletin is rendered mandatory by EASA Airworthiness Directive No 2011-0241.
• As prescribed by the Airworthiness Authorities of the country of registration of the aircraft.
E. APPROVAL
This Service Bulletin covers DASSAULT AVIATION modification FALCON 7X M1245 which has been
approved by EASA.
FALCON 7X 7X-214
January 26, 2012 ATA 27
Initial issuance Page 1 / 9
DASSAULT AVIATION Proprietary Data

### Page 4

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.
• maintenance computer (TO-45-100) including software application media installed with
MEM40507-01 installation media.
• Standard USB cable.
FALCON 7X 7X-214
January 26, 2012 ATA 27
Initial issuance Page 2 / 9
DASSAULT AVIATION Proprietary Data

### Page 5

• 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
January 26, 2012 ATA 27
Initial issuance Page 3 / 9
DASSAULT AVIATION Proprietary Data

### Page 6

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
January 26, 2012 ATA 27
Initial issuance Page 4 / 9
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
January 26, 2012 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
January 26, 2012 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
January 26, 2012 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
January 26, 2012 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
January 26, 2012  ATA 27
Initial issuance  Page 9 / 9
END OF DOCUMENT

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