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FALCON SERVICE BULLETIN
FALCON 2000EX FALCON 2000EX EASy FALCON 2000DX
No 171-R3
MARCH 10, 2010
MANDATORY
MANDATORY
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 57-5
WING
WING TANK MODIFICATION
FALCON 2000EX
SERVICE BULLETIN F2000EX–171
F2000EX–57–5 WING
WING TANK MODIFICATION ________________________________________________________________________________ INITIAL ISSUANCE date: July 6, 2009 List of effective pages: 1 to 6.
________________________________________________________________________________ COMPLETE ISSUANCE: REVISION 1 date: October 30, 2009 List of effective pages: 1 to 7.
List of modified pages: 1 to 7.
REASON: The Service Bulletin is updated to give precise details about compliance and training.
This revision is not applicable to aircraft already modified per the original issue.
________________________________________________________________________________ COMPLETE ISSUANCE: REVISION 2 date: February 15, 2010 List of effective pages: 1 to 7.
List of modified pages: 6 and 7.
REASON: Addition/correction of information in appendix 1, 2, 5 following installations performed during training.
This revision is not applicable to aircraft already changed per the original issue.
________________________________________________________________________________ COMPLETE ISSUANCE: REVISION 3 date: March 10, 2010 List of effective pages: 1 to 7.
List of modified page: 3.
REASON: Modification of paragraph “TRAINING”.
This revision is not applicable to aircraft already changed per the original issue or revision 1 or revision 2.
DASSAULT AVIATION Proprietary Data
SERVICE BULLETIN FALCON 2000EX F2000EX–171
March 10, 2010 F2000EX–57–5 Revision 3 Page 1 WING
WING TANK MODIFICATION ________________________________________________________________________________ 1 . PLANNING INFORMATION A . EFFECTIVITY This Service Bulletin is applicable to:
– FALCON 2000EX aircraft with serial numbers 1 through 600 (F2000EX, F2000EX EASy), – FALCON 2000EX aircraft with serial numbers 601 through 700 (F2000DX), which have not previously implemented DASSAUL T A VIATION modification F2000EX M3072.
B . REASON An analysis of rare high-speed runway excursions has revealed that, in case of a main landing gear leg failure due to overloads, the subsequent wing damage may cause a potential fuel spill.
The purpose of this Service Bulletin is to prevent such a fuel spill in the event of such an exceptional occurence by installing a sealed boundary between ribs No. 4 and 5 in front of the rear wing spar.
C . DESCRIPTION The operation consists in:
– removing the structural removable lower wing panel, – installing a drainage capability, – installing a boundary between ribs No 4 and 5, – applying a sealant around the boundary , – performing a test for leakage, – replacing the instruction placards on the wings and on the refueling door (186CR).
The Accomplishment Instructions and the tests are included in the five Appendices to this Service Bulletin.
DASSAULT AVIATION Proprietary Data FALCON 2000EX
SERVICE BULLETIN F2000EX–171
March 10, 2010 F2000EX–57–5 Revision 3 Page 2 D . COMPLIANCE Mandatory:
Compliance with this Service Bulletin should be done no later than 12 years and 6 months of its release date.
It is anticipated that this Service Bulletin will be rendered mandatory by an EASA Airworthiness Directive. The Airworthiness authorities of other countries may also elect to mandate compliance with this Service Bulletin and compliance timelines will be established by those authorities.
Each person applying this Service Bulletin must have successfully completed a training program. For more details refer to the training section of paragraph F .
E . APPROVAL This Service Bulletin covers DASSAULT AVIATION modifications F2000EX M3072 which has been approved by EASA and M3206 which have 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.
DASSAULT AVIATION Proprietary Data
SERVICE BULLETIN FALCON 2000EX F2000EX–171
March 10, 2010 F2000EX–57–5 Revision 3 Page 3 F . LABOR Estimated labor–hours:
– Access time: 300 hours – Modification: 300 hours – 40 hours for paint touch (including lower wing panels and upper wings reworked areas) 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.
NOTE: The Service Bulletin instructions contained in the five APPENDICES constitute complex structural rework activity that should only be accomplished at Service Centers that have relevant experience working on Falcon aircraft and have a high level of competency in the following areas:
– Work on primary structure.
– Metal work.
– Precision adjustment.
– Non-destructive-Testing (NDT) for cracks.
– Use of S-class screws and repair dimensions.
Failure to utilize an experienced Service Center with a high level of proficiency in the above disciplines and specialized training in the operations covered hereby, could result in inadvertent damage during the Service Bulletin procedure, possibly requiring extensive aircraft repairs.
TRAINING: Each person applying this Service Bulletin must have successfully completed a training program. This training program consists of applying this Service Bulletin in the person’s facility under the supervision of a trainer from Dassault Aviation, and/or Dassault Aircraft Services (DAS) personnel that have received training from Dassault A viation.
Each facility applying this Service Bulletin must maintain capable individuals on staff that have successfully completed the Dassault training program prior to attempting this modification.
However, it is acceptable that a person from a facility that has successfully completed the training program to be designated to serve as a trainer for that facility . As a consequence, it is the responsibility of each maintenance facility applying this Service Bulletin to define an internal training program of its technicians and maintain familiarization of the application of the SB to maintain the required knowledge over the years.
DASSAULT AVIATION Proprietary Data FALCON 2000EX
SERVICE BULLETIN F2000EX–171
March 10, 2010 F2000EX–57–5 Revision 3 Page 4 G . MATERIAL – PRICE AND AVAILABILITY The modification kit will be delivered to the Service Centers approved 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 The specific tooling are listed in the APPENDIX 5.
I . WEIGHT AND BALANCE Change in weight: + 6.4 lb (+ 2.9 kg).
Change in balance with respect to 25% MAC : + 32 ft.lb (+ 4,3 m.daN) nose up moment.
DASSAULT AVIATION Proprietary Data
SERVICE BULLETIN FALCON 2000EX F2000EX–171
March 10, 2010 F2000EX–57–5 Revision 3 Page 5 J . REFERENCE Aircraft Maintenance Manual:
– procedure 27-510, – procedure 27-811, – procedure 57-011.
Standard Practices:
– procedure 20-305, – procedure 20-306, – procedure 20-320, – procedure 20-602, – procedure 20-650.
Illustrated Parts Catalog:
– chapter 11-20-10, – chapter 11-20-20, – chapter 53-20-20.
Airplane Flight Manual:
– F2000EX Airplane Flight Manual (DGT84278) rev .7 or subsequent.
– F2000EX Easy Airplane Flight Manual (DGT88898) rev .6 or subsequent.
AMM chap. 12, Ingredients and consumable products.
K . OTHER PUBLICATIONS AFFECTED The following publications will be revised at a later date to account for the changes introduced by this Service Bulletin:
– AMM – IPC
DASSAULT AVIATION Proprietary Data FALCON 2000EX
SERVICE BULLETIN F2000EX–171
March 10, 2010 F2000EX–57–5 Revision 3 Page 6 2 . ACCOMPLISHMENT INSTRUCTIONS A . ACCOMPLISHMENT INSTRUCTIONS ARE DESCRIBED IN THE FOLLOWING APPENDICES:
(1) APPENDIX 1 DRY BAY – ASSEMBLY OF BOUNDARY AND DRAINING CAPABILITY REVISION 2
(2) APPENDIX 2 DRY BAY – SEALANT APPLICATION ON BOUNDARY REVISION 3
(3) APPENDIX 3 DRY BAY – LEAKAGE PRESSURE TEST FOR THE SEAL BOUNDARY REVISION 2
(4) APPENDIX 4 DRY BAY – REPORT OF DRILLING THE PR INJECTION HOLES REVISION 1 B . REPLACEMENT OF INSTRUCTION PLACARDS
(1) LH and RH wings – Remove the instruction placards Item 50 as per Illustrated Parts Catalog, Chap. 11-20-20, fig. 10.
– For F2000EX aircraft, install the new instruction placards F2MB090200003A3 at the same location as per Procedure 20-306.
– For F2000DX aircraft, install the new instruction placards F2ME090200003A1 at the same location as per Procedure 20-306.
(2) Refueling access door (186CR) – Open the refueling access door (186CR) as per Illustrated Parts Catalog, Chap. 53-20-20, fig. 35 for F2000EX aircraft or Illustrated Parts Catalog, Chap. 53-20-20, fig. 14 for F2000DX aircraft.
– Remove the instruction placard Item 100 as per Illustrated Parts Catalog, Chap. 11-20-10, fig. 30.
– For F2000EX aircraft, install the new instruction placard F2MB090100023A3 as per Procedure 20-305.
– For F2000DX aircraft, install the new instruction placard F2ME090100024A1 as per Procedure 20-305.
C . DOCUMENTATION Update, if not already done, the Airplane Flight Manual with:
– Airplane Flight Manual (DGT84278) rev.7 or subsequent for a F2000EX – Airplane Flight Manual (DGT88898) rev.6 or subsequent for a F2000EX Easy
DASSAULT AVIATION Proprietary Data
SERVICE BULLETIN FALCON 2000EX F2000EX–171
March 10, 2010 F2000EX–57–5 Revision 3 Page 7END OF DOCUMENT D . 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, or fill out the Compliance Form on line on the Dassault Falcon website.
3 . MATERIAL INFORMATION Refer to DRY BAY APPENDIX 5 REVISION 3.
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
SERVICE BULLETINS COMPLIANCE
SERVICE BULLETINS COMPLIANCE
SERVICE BULLETINS COMPLIANCE FALCON 2000EX
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 2000EX 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 :
171 171 F2000EX 57 57 5 5 Revision 3 Revision 3 Révision 3 F2000EX F2000EX F2000EX
PAGE 1/49
ASSEMBLING DRY BAY AND DRAINING CAPABILITY Revision 2 February 15, 2010 DRY BAY APPENDIX-1 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.