# Dassault Service Bulletin F2000-368: No revision named

- Rights: © Dassault Aviation. Filed by the FAA in regulations.gov docket FAA-2017-0130; AD 2017-16-09 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- Document: [Dassault Service Bulletin F2000-368](https://openairdocs.org/service-documents/dassault/f2000-368.md)
- Title as filed: SB F2000-368
- Pages: 9
- PDF: https://openairdocs.org/files/sha256/b4/d6/b4d6ab4fc15f2e31c2406730afd4531b3829fbd2ce30f6ebd14f2c4e4558e483
- Page: https://openairdocs.org/service-documents/dassault/f2000-368/file/b4d6ab4fc15f

## Text

Some pages are OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

FALCON SERVICE BULLETIN   
 
 
 
554 
 
 
 
 
 
 
FALCON 2000 
 
 
No 368 
 
 
MAY 29, 2009 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
Copyright © 2009 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.  
ATA 32-34 
 
 
 
LANDING GEAR 
MAIN LANDING GEAR 
IMPROVEMENT OF BRAKING HOSES AND 
CORRESPONDING ASSEMBLIES  
0900400080320120 - VALIDATED - Certification Repository

### Page 2

FALCON 2000
SERVICE BULLETIN
F2000–368
 
F2000–32–34
LANDING GEAR
MAIN LANDING GEAR
IMPROVEMENT OF BRAKING HOSES AND CORRESPONDING ASSEMBLIES
________________________________________________________________________________
INITIAL ISSUANCE date: May 29, 2009
List of effective pages:
1 to 5.
________________________________________________________________________________

### Page 3

DASSAULT AVIATION Proprietary Data
SERVICE BULLETIN
FALCON 2000 F2000–368
 
May 29, 2009 F2000–32–34
Initial issuance Page  1
LANDING GEAR
MAIN LANDING GEAR
IMPROVEMENT OF BRAKING HOSES AND CORRESPONDING ASSEMBLIES
________________________________________________________________________________
 1  . PLANNING INFORMATION
 A . EFFECTIVITY
This Service Bulletin is applicable to FALCON 2000 aircraft with serial numbers 1 through 231
which are not equipped with :
– LH main landing gear P/N D23345000-7 Amdt B,
– RH main landing gear P/N D23346000-7 Amdt B.
NOTE: Incorporation of this Service Bulletin makes Service Bulletin F2000-382  not
applicable.
 B . REASON
On several in-service aircraft, damages have been reported on the main landing gear torque
link and the braking system hoses, due to chafing  between the external steel braids of the
hoses and the torque link. In order  to prevent the metallic sleeve from chafing against the
metallic guides of the torque link, the installation of a protective wrap on the hoses has been
recommended through Service Bulletin F2000-382 pending the next landing gear removal
for overhaul or repair. As a permanent solution, brake hoses with Dacron sleeves are installed
on each main landing gear returned for overhaul or repair .
The purpose of this Service Bulletin is to enable the installation of brake hoses with Dacron
sleeves when replacing hoses with metallic sleeves on wing.
 C . DESCRIPTION
The operation consists in installing new hydraulic lines, composed of braking hoses fitted with
ther corresponding stop assemblies and bridges
 D . COMPLIANCE
If you choose to comply with this Service Bulletin, accomplishment can be performed at your
convenience.
 E . APPROVAL
This Service Bulletin covers DASSAUL T AVIATION modification F2000 M3085 which has
been approved under the authority of DOA nr . EASA.21J.051.
The technical content of this document is approved under the authority of  DOA
nr. EASA.21J.051.

### Page 4

DASSAULT AVIATION Proprietary Data
FALCON 2000
SERVICE BULLETIN
F2000–368
 
May 29, 2009 F2000–32–34
Initial issuance Page  2
 F . LABOR
Estimated labor–hours: 2 hours per leg.
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 No 101
AEROPORT DU BOURGET
93352 – LE BOURGET Cedex (FRANCE)
Please contact your Dassault A viation
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.

### Page 5

DASSAULT AVIATION Proprietary Data
SERVICE BULLETIN
FALCON 2000 F2000–368
 
May 29, 2009 F2000–32–34
Initial issuance Page  3
 I . WEIGHT AND BALANCE
Change in weight: + 0.18 lb / 0.08 kg.
Change in balance with respect to 25% MAC : Negligible.
 J . REFERENCES
Standard Practices:
– Procedure 20-001.
Messier-Dowty SA Service Bulletin No. D23345-32-020.
 K . OTHER PUBLICATIONS AFFECTED
The following publication will be revised at a later date to account for the changes introduced
by this Service Bulletin:
– Illustrated Part Catalog.

### Page 6

DASSAULT AVIATION Proprietary Data
FALCON 2000
SERVICE BULLETIN
F2000–368
 
May 29, 2009 F2000–32–34
Initial issuance Page  4
 2  . ACCOMPLISHMENT INSTRUCTIONS
 A . PRELIMINARY STEPS
(1) The aircraft must be in the maintenance  configuration (refer to Standard Practices,
procedure 20-001).
 B . PROCEDURE
(1) Replace MLG braking hoses and corresponding stop assemblies and bridges in
accordance with Messier-Dowty SA Service Bulletin No. D23345-32-020.
 C . RECORDING
Record compliance with this Service Bulletin in the appropriate aircraft documents.
Fill out the card located at the end of the Service Bulletin and mail or fax it to Dassault Aviation
or Dassault Falcon Jet.

### Page 7

DASSAULT AVIATION Proprietary Data
SERVICE BULLETIN
FALCON 2000 F2000–368
 
May 29, 2009 F2000–32–34
Initial issuance Page  5END OF DOCUMENT
 3  .  MATERIAL INFORMATION
 A . MODIFICATION KIT
KIT P/N SBF2000-0368A
NEW P/N
Q
T
Y
KEY WORD
Y220-04043-01-3 1 Kit for LH main landing gear
Y220-04043-02-3 1 Kit for RH main landing gear
 B . LOCAL PROCUREMENT
None

### Page 8 (OCR)

NO POSTAGE
NECESSARY
FROM
IF MAILED
IN THE
UNITED STATES
ZIP CODE
BUSINESS REPLY MAIL
FIRST CLASS MAIL PERMIT NO. 3306 HACKENSACK, NJ 07602
POSTAGE WILL BE PAID BY ADDRESSEE:
DASSAULT FALCON JET CORP.
PO BOX 1946
SO HACKENSACK NJ 07606-9946
ATTENTION:
FIELD SERVICE DEPARTMENT
DASSAULT AVIATION
78, Quai Marcel Dassault
Cedex 300
92552 SAINT-CLOUD Cedex
FRANCE
A l'attention de DSC

### Page 9

SERVICE BULLETINS COMPLIANCE
SERVICE BULLETINS COMPLIANCE
SERVICE BULLETINS COMPLIANCE
FALCON 2000
APPLICATION DES BULLETINS DE SERVICE
DASSAULT AVIATION Number ATA Number
Remarks:
Coding:
A/C S/N
C
T
complete compliance
partial compliance
Date : Signature :
Performed by:
DASSAULT AVIATION Number ATA Number
Remarks:
Coding: C
T
complete compliance
partial compliance
Date : Signature :
Performed by:
FALCON 2000 Avion No
Numéro DASSAULT AVIATION Numéro ATA
Fait par :
application partielle
application totale
Would you be kind enough to inform us that this Service Bulletin is complied with:
– For ”Western Hemisphere”, mail upper card (No postage necessary if mailed in the U.S.A.) or fax to
   Dassault Falcon Jet: 1–201–541–4700.
– For ”Other Continents”, mail card herebelow or fax to Dassault Aviation: 33 (0)1.47.11.65.21.
On the occasion, if other Service Bulletins have been simultaneously complied with could you complete 
the blank spaces provided for this purpose.
APPLICATION DE BULLETINS DE SERVICE
Lorsque vous aurez appliqué ce Bulletin de Service sur votre avion, veuillez avoir l’amabilité
de nous en informer :
– Utiliser la carte réponse supérieure pour continent américain (Dispensée de timbrage pour postage
     depuis les U.S.A.)  ou  le fax  pour Dassault Falcon Jet : 1–201–541–4700.
– Ou la carte réponse inférieure pour autres continents ou le fax pour Dassault Aviation : 33 (0)1.47.11.65.21.
Eventuellement, si d’autres Bulletins de Service ont été appliqués simultanément,
vous pouvez les mentionner dans les cases vierges prévues à cet effet.
Remarques :
368
368 F2000
32
32 34
34
Initial issuance
Initial issuance
Edition originale
F2000
F2000 F2000

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