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FALCON 2000 No 382-R2 MAY 12, 2011
MANDATORY ATA 32-33
LANDING GEAR
MAIN LANDING GEAR
INSTALLATION OF PROTECTIVE WRAPS ON BRAKING
SYSTEM FLEXIBLE HOSES
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.
LANDING GEAR
MAIN LANDING GEAR
INSTALLATION OF PROTECTIVE WRAPS ON BRAKING SYSTEM FLEXIBLE HOSES Initial issuance January 30, 2009 List of effective pages :
1 to 5 Revision 1 December 15, 2010 List of effective pages :
1 to 5 List of modified pages :
1 REASON:This Service Bulletin becomes mandatory in accordance with an EASA Airworthiness Directive to be released.
This revision is not applicable to aircraft already modified per the initial issuance of this Service Bulletin.
Revision 2 May 12, 2011 List of effective pages :
1 to 7 List of modified pages :
1, 2, 4 and 7 REASON:To add inspection criteria on the braking system hoses.
This revision is not applicable to aircraft already modified per a previous revision of this Service Bulletin.
FALCON 2000 F2000 -382 F2000 -32-33
LANDING GEAR
MAIN LANDING GEAR
INSTALLATION OF PROTECTIVE WRAPS ON BRAKING SYSTEM FLEXIBLE HOSES
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, and which have not implemented DASSAULT AVIATION modification F2000 M3237.
B. REASON Several cases of hydraulic fluid leaks recently occurred on the MLG braking system hoses, due to chafing between the external steel braids and the main landing gear torque link.
The purpose of this Service Bulletin is to prevent damage to the steel braid and torque link by installing a spiral wrap made of Teflon, in order to avoid:
• any cancellation of flight if leakage occurs,
• and any additional maintenance workload on damaged torque link and braking system hoses.
C. DESCRIPTION The operation consists in:
• inspecting each MLG brake external steel braid hose and,
• installing a spiral wrap made of Teflon to each MLG brake external steel braid hose (two per main landing gear leg).
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.
E. APPROVAL This Service Bulletin covers DASSAULT AVIATION modification F2000 M3237 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.
F. LABOR Estimated labor-hours:
• 1 hour for the modification.
• No specific access.
FALCON 2000 F2000 -382 May 12, 2011 F2000 -32-33 Revision 2 Page 1 / 7 DASSAULT AVIATION Proprietary Data
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.
I. WEIGHT AND BALANCE Change in weight: None.
Change in balance with respect to 25% MAC: None.
J. REFERENCES Standard Practices:
• Procedure 20-000 (Refer to TASK 20-00-00-910-801).
Dassault Aviation Service Bulletin F2000-368 FALCON 2000 F2000 -382 May 12, 2011 F2000 -32-33 Revision 2 Page 2 / 7 DASSAULT AVIATION Proprietary Data
K. OTHER PUBLICATIONS AFFECTED The Ilustrated Parts Catalog will be revised as a consequence of this Service Bulletin.
FALCON 2000 F2000 -382 May 12, 2011 F2000 -32-33 Revision 2 Page 3 / 7 DASSAULT AVIATION Proprietary Data
2. ACCOMPLISHMENT INSTRUCTIONS A. PRELIMINARY STEPS
(1) The aircraft must be in the maintenance configuration (refer to Standard Practices, procedure 20-000 (Refer to TASK 20-00-00-910-801)).
B. PROCEDURE
(1) In the cockpit, make sure that the park brake handle is released.
(2) Inspect each braking system hose (A-fig. 1):
• If no damage is found, or
• If some strands of various braids are broken and/or damaged but if elastomer hose cannot be seen (see fig. 2, detail A), install a protective wrap (1-fig. 1) on the braking system hose (A-fig. 1) as follows:
CAUTION: TAKE ALL PRECAUTIONS TO AVOID STRETCHING OR BENDING OVER A
TIGHT RADIUS A BRAKING SYSTEM HOSE, WHEN INSTALLING A PROTECTIVE WRAP.
• Place the protective wrap approximately near the hose to be protected and cut it to length (hose length or slightly more).
NOTE: A 24 in. (600 mm) long protective wrap is required to protect each braking system hose.
• Slide the hose identification ring fully down.
• Fit the top of the protective wrap below the torque link lower guide (B-fig. 1).
• Once 4 to 6 in. (10 to 15 cm) of protective wrap are in place, slide the wrap up through the torque link’s lower guide (B-fig. 1), rotating the sheath so as to loosen friction along the hose.
• Repeat step (c) for the next spiral section, passing the wrap through the guides (B-fig. 1) and (C-fig. 1) up to the top of the hose, below the bridge (D-fig. 1).
• Wrap the remaining section around the bottom of the hose and cut any excess length, if necessary.
• If all strands in same braid are broken and if elastomer hose can be seen (see fig. 2, detail B), replace the braking system hose(A-fig. 1) according to Dassault Aviation Service Bulletin F2000-368 “Landing gear - Main landing gear - Improvement of braking hoses and corresponding assemblies”.
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, or fill out the electronic Service Bulletin reply form located in the “Service Bulletin" page on the Falcon portal.
FALCON 2000 F2000 -382 May 12, 2011 F2000 -32-33 Revision 2 Page 4 / 7 DASSAULT AVIATION Proprietary Data
3. MATERIAL INFORMATION A. MODIFICATION KIT KIT SBF2000-0382A
NEW P/N Q T Y
KEY WORD I T E M F I G 3P-PTFE 1 A 3 m (9.84 ft) protective wrap roll 1 1 B. LOCAL PROCUREMENT None FALCON 2000 F2000 -382 May 12, 2011 F2000 -32-33 Revision 2 Page 5 / 7 DASSAULT AVIATION Proprietary Data
DASSAULT SERVICE BULLETIN
AVIATION FALCON 2000 F2000 -382 1
• B Figure 1: INSTALLATION OF PROTECTIVE WRAPS May 12, 2011 F2000-32-33 Revision 2 Page 6 / 7
DASSAULT SERVICE BULLETIN
AVIATION FALCON 2000 F2000 -382 Strands of various braids damaged and elastomere hose not seen Strands of various braids broken and/or damaged and elastomere hose not seen
DETAIL A Strands in same braid broken and elastomere hose seen
DETAIL B Figure 2: INSTRUCTION OF BRAKING SYSTEM HOSE May 12, 2011 END OF DOCUMENT F2000 -32-33 Revision 2 Page 717
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 FALCON 2000 A/C S/N DASSAULT AVIATION Number ATA Number F2000 382 F2000 32 33
Coding: C complete compliance
T partial compliance
Performed by:
Remarks: Revision 2 Date: Signature:
SERVICE BULLETINS COMPLIANCE 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 applique ce Bulletin de Service sur votre avion, veuillez avoir l'amabilite de nous en informer:
- Utiliser la carte reponse superieure pour continent americain (Dispensee de timbrage pour postage depuis les U.S.A.) ou le fax pour Dassault Falcon Jet : 1-201-541-4700.
- Ou la carte reponse inferieure pour autres continents ou le fax pour Dassault Aviation : 33 (0)1.47.11.65.21.
Eventuellement, si d'autres Bulletins de Service ont ete appliques simultanement, vous pouvez les mentionner dans les cases vierges prevues a cet effet.
APPLICATION DES BULLETINS DE SERVICE SERVICE BULLETINS COMPLIANCE FALCON 2000 A/C S/N DASSAULT AVIATION Number Numero DASSAULT AVIATION ATA Number Numero ATA F2000 382 F2000 32 33
Coding: C complete complianceapplication totale
T partial complianceapplication partielle
Performed by:
Fait par:
Remarks: Revision 2 Date: Signature:
Remarques: Revision 2