# Dassault Service Bulletin F20-790: No revision named

- Rights: © Dassault Aviation. Filed by the FAA in regulations.gov docket FAA-2016-9500; AD 2017-21-01 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- Document: [Dassault Service Bulletin F20-790](https://openairdocs.org/service-documents/dassault/f20-790.md)
- Title as filed: SB F20-790
- Pages: 11
- PDF: https://openairdocs.org/files/sha256/2b/bb/2bbb2912c63588d6d6803aa7862d6b1c4a7f3db4e6132f352c4a31291765eeaa
- Page: https://openairdocs.org/service-documents/dassault/f20-790/file/2bbb2912c635

## 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 20
No 790
SEPTEMBER 14, 2016
MANDATORY
ATA 26-16
FIRE PROTECTION
REPLACEMENT OF FIRE EXTINGUISHER TUBES P/N
MY20791-121 AND -122
FALCON SERVICE BULLETIN
Copyright © 2016 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.
084

### Page 2

FIRE PROTECTION
REPLACEMENT OF FIRE EXTINGUISHER TUBES P/N MY20791-121 AND -122
Initial issuance September 14, 2016
List of effective pages :
1 to 7
FALCON 20 F20 -790
F20 -26-16

### Page 3

FIRE PROTECTION
REPLACEMENT OF FIRE EXTINGUISHER TUBES P/N MY20791-121 AND -122
 
1. PLANNING INFORMATION
A. EFFECTIVITY
This Service Bulletin is applicable to all FAN JET FALCON series, all MYSTERE-FALCON 20-()5
series, and MYSTERE-FALCON 20 GF aircraft.
B. REASON
Several defective extinguisher tubes have been found on Fan Jet Falcon aircraft. The result of the
investigations concluded that these occurrences were due to corrosion from very active halogen
extinguishing agents.
This condition, if not corrected, could impact the capability to extinguish a fire in the rear compartment
of the aircraft, possibly resulting in damage to the aircraft and injury to the occupants.
C. DESCRIPTION
The operation consists in replacing the affected tubes with improved fire extinguisher tubes.
Affected Parts P/N (AG5 material) Serviceable Parts P/N (5086 material)
MY20791-121 MY20791-121-1
MY20791-122 MY20791-122-1
NOTE: This Service Bulletin prohibits (re)installation of the affected fire extinguisher tubes on an
aircraft.
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 modifications MYSTERE-FALCON 20 M7007 and
FALCON 20-5() M3574 (partially) that 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.
F. LABOR
Estimated labor-hours: Refer to Service Bulletin Commercial Summary.
NOTE: These labor-hours only concern the work described in this Service Bulletin and do not include
other maintenance work that may be performed on this occasion.
FALCON 20 F20 -790
September 14, 2016 F20 -26-16
Initial issuance Page 1 / 7
DASSAULT AVIATION Proprietary Data

### Page 4

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
E/H dafsorder@dassault-aviation.com
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
Illustrated Parts Catalog:
• SYSTEM, FIRE EXTINGUISHING, FR33 TO FR35 IPC 26-20-10-20
Aircraft Maintenance Manual:
• 20-00-0-2 "Summary of mandatory precautions to be taken during aircraft maintenance
operations",
• 26-20-2-3 "EXTINGUISHING SYSTEM - SERVICING".
FALCON 20 F20 -790
September 14, 2016 F20 -26-16
Initial issuance Page 2 / 7
DASSAULT AVIATION Proprietary Data

### Page 5

K. OTHER PUBLICATIONS AFFECTED
None.
FALCON 20 F20 -790
September 14, 2016 F20 -26-16
Initial issuance Page 3 / 7
DASSAULT AVIATION Proprietary Data

### Page 6

2. ACCOMPLISHMENT INSTRUCTIONS
A. PRELIMINARY STEPS
(1) The aircraft must be in the maintenance configuration (refer to Maintenance Manual, chapter
20-00-0-2).
(2) Make sure that the aircraft is de-energized.
(3) Make sure that the A/C batteries and the external power sources are disconnected.
(4) On the cockpit circuit breaker panel (RH side), disengage circuit breaker "FIRE EXTINGUISH"
(31W).
(5) In the rear compartment, on the battery box, disengage circuit breaker (32W).
(6) Install a "DO NOT ENERGIZE" warning placard in the cockpit.
B. REPLACEMENT OF THE FIRE EXTINGUISHER TUBES
Refer to fig. 1
(1) Removal
(a) Disconnect LH fire extinguisher tube (1-fig. 1) from LH fire extinguisher discharge head side,
NOTE: The end of this line is identified by means of green paint applied on LH fire
extinguisher discharge head side.
(b) Unscrew clamp (C-fig. 1),
(c) Disconnect RH fire extinguisher tube (2-fig. 1) from RH fire extinguisher discharge head side 
(A-fig. 1),
NOTE: The end of this line is identified by means of green paint applied on RH fire
extinguisher discharge head side.
(d) Disconnect RH fire extinguisher tube (2-fig. 1) from fire extinguisher multi-hole spray pipe
side (B-fig. 1),
(e) Unscrew clamp (D-fig. 1).
(2) Installation
(a) Connect LH fire extinguisher tube P/N MY20791-121-1 (1-fig. 1) to LH fire extinguisher
discharge head side,
(b) Install clamp (C-fig. 1),
(c) Connect RH fire extinguisher tube P/N MY20791-122-1 (1-fig. 1) to RH fire extinguisher
discharge head side (A-fig. 1),
(d) Connect RH fire extinguisher tube P/N MY20791-122-1 (2-fig. 1) to fire extinguisher multi-
hole spray pipe side (B-fig. 1),
(e) Install clamp (D-fig. 1).
(3) Tests
(a) Perform a flow test (refer to Maintenance Manual, chapter 26-20-2-3 paragraphs 4C and
4D).
FALCON 20 F20 -790
September 14, 2016 F20 -26-16
Initial issuance Page 4 / 7
DASSAULT AVIATION Proprietary Data

### Page 7

C. FINAL STEPS
(1) Check the paint for condition for each RH/LH fire extinguisher discharge head side,
(2) Repaint if necessary.
(3) Engage circuit breakers (31W) and (32W).
(4) Remove the "DO NOT ENERGIZE" warning placard.
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 electronic Service Bulletin reply form located in the ”Service Bulletin"
page on the Falcon portal.
FALCON 20 F20 -790
September 14, 2016 F20 -26-16
Initial issuance Page 5 / 7
DASSAULT AVIATION Proprietary Data

### Page 8

3. MATERIAL INFORMATION
A. MODIFICATION KIT
NOTE: Compliance with this Service Bulletin by substituting the part numbers below with
interchangeable subsequent part numbers is acceptable, provided the subsequent part
numbers have the same effectivity as the original ones.
NEW P/N
Q
T
Y
KEY WORD OLD P/N INSTRUCTIONSDISPOSITION ITEMFIG
MY20791-121-1 1 LH TUBE MY20791-121 Connect to the LH
fire extinguisher
discharge head
(1-fig. 1) 
MY20791-122-1 1 RH TUBE MY20791-122 Connect to the RH
fire extinguisher
discharge head
(2-fig. 1)  
FALCON 20 F20 -790
September 14, 2016 F20 -26-16
Initial issuance Page 6 / 7
DASSAULT AVIATION Proprietary Data

### Page 9 (OCR)

DASSAULT  SERVICE BULLETIN
AVIATION
FALCON 20  F20 -790
REAR COMPARTMENT
LH TUBE  RH TUBE
P/N MY20791-121  P/N MY20791-122
to be replaced  to be replaced
Figure 1: FIRE EXTINGUISHER TUBES - REMOVAL/INSTALLATION
September 14, 2016  F20 -26-16
END OF DOCUMENT
Initial issuance  Page 7/7

### Page 10 (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 11

SERVICE BULLETINS COMPLIANCE FALCON 20 A/C S/N    
DASSAULT AVIATION Number  ATA Number   
F20 790  F20 26 16   
        
        
        
        
Coding: C complete compliance
 
T partial compliance
   
Performed by:   
Remarks: Initial issuance 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 20 A/C S/N    
DASSAULT AVIATION Number
Numero DASSAULT AVIATION  
ATA Number
Numero ATA   
F20 790  F20 26 16   
        
        
        
        
Coding: C complete complianceapplication totale
 
T partial complianceapplication partielle
   
Performed by:
Fait par:
  
Remarks: Initial issuance Date: Signature:
Remarques: Edition originale

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