# Dassault Service Bulletin F2000EX-322: Revision 1

- Rights: © Dassault Aviation. Filed by the FAA in regulations.gov docket FAA-2017-1250; AD 2018-02-06 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- Document: [Dassault Service Bulletin F2000EX-322](https://openairdocs.org/service-documents/dassault/f2000ex-322.md)
- Title as filed: SB F2000EX-322 R1
- Pages: 18
- PDF: https://openairdocs.org/files/sha256/b9/09/b90997fdd46ff1abfb240cebd996edc2cedeba4b38ae2ad58d112150efa41218
- Page: https://openairdocs.org/service-documents/dassault/f2000ex-322/file/b90997fdd46f

## Text

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### Page 1

FALCON 2000EX EASy
FALCON 2000LX
FALCON 2000LXS
FALCON 2000DX
FALCON 2000S
No 322-R1
JUNE 21, 2017
 
ATA 00-19
GENERAL
ENHANCED AVIONICS SYSTEM
EASY II LOAD 16.4
FALCON SERVICE BULLETIN
Copyright © 2017 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.
671

### Page 2

GENERAL
ENHANCED AVIONICS SYSTEM
EASY II LOAD 16.4
Initial issuance October 17, 2016
List of effective pages :
1 to 13
Revision 1 February 23, 2017
List of effective pages :
1 to 13
List of modified pages :
1, 6, 8, 9, 10, 11 and 12
REASON:Modification of the effectivity.
Correction of discrepancies.
This revision is not applicable to aircraft already modified per the initial issuance of
this Service Bulletin.
Erratum June 21, 2017
List of effective pages :
1 to 14
List of modified pages :
5 to 10
REASON:Additional information for APM settings update.
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F2000EX -00-19

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GENERAL
ENHANCED AVIONICS SYSTEM
EASY II LOAD 16.4
 
1. PLANNING INFORMATION
A. EFFECTIVITY
This Service Bulletin is applicable to:
• F2000EX aircraft with serial numbers 6, 28 through 292 (F2000EX EASy, F2000LX, F2000LXS),
• F2000EX aircraft with serial numbers 601 through 604 (F2000DX),
• F2000EX aircraft with serial numbers 702 through 730 (F2000S),
that have already implemented DASSAULT AVIATION Service Bulletin F2000EX-300 and,
that have not previously implemented DASSAULT AVIATION modification F2000EX M3688.
NOTE: Before operating an aircraft equipped with this new load 16.4, the crew must have followed a
specific training.
B. REASON
The purpose of this Service Bulletin is to upgrade the aircraft avionics to the EASy II load 16.4
standard that includes the following features:
• TOGA,
• Automatic Descent Mode capability (through DASSAULT AVIATION Service Bulletin FALCON
2000EX-304),
• TOLD for F2000S and F2000LXS,
• TOLD increased to 14,000 ft,
• TOLD increased to 42,800 lb (A/C with M3390 or M3622),
• various improvements: Full Charts database for all aircraft, FMS, CAS, displays,
communication...
• new AMI database for GDC and ARINC Direct providers (through DASSAULT AVIATION
Service Bulletin F2000EX-147).
C. DESCRIPTION
The operation consists in:
• performing a full load of software,
• changing the pilot and copilot wheel labels (from "GA" to "TOGA").
D. COMPLIANCE
If you choose to comply with this Service Bulletin, accomplishment should be performed at the first
opportunity.
E. APPROVAL
This Service Bulletin covers DASSAULT AVIATION modification F2000EX M3688 that has been
approved by EASA.
The technical content of this document is approved under the authority of DOA nr. EASA.21J.051.
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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.
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.
Scalpel.
I. WEIGHT AND BALANCE
Change in weight: None.
Change in balance with respect to 25% MAC: None.
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J. ELECTRICAL LOAD ANALYSIS
None.
K. REFERENCES
Aircraft Maintenance Manual:
• GENERAL MAINTENANCE AND SAFETY PRECAUTIONS (Refer to TASK 20-00-00-910-801)
• ENERGIZATION / DE-ENERGIZATION OF THE AIRCRAFT (Refer to TASK 24-00-00-860-801)
• AIRCRAFT PERSONALITY MODULE (APM) SETTINGS TOOL USER GUIDE (Refer to TASK
31-42-25-910-801)
• INSTALLATION OF AVIONICS SOFTWARE TOOLS (Refer to TASK 45-10-00-860-801)
• PERIODIC DATABASE LOADING (Refer to TASK 45-90-00-860-801)
• DATABASE LOADING (Refer to TASK 45-90-00-860-803)
• SOFTWARE LOADING (Refer to TASK 45-90-00-860-804)
DASSAULT AVIATION Service Bulletins
• F2000EX-065 "INSTALLATION OF A BRAKE HEATING SYSTEM" 
• F2000EX-117 "VIDEO INTERFACE CAPABLE OF HANDLING EIGHT CAMERAS" 
• F2000EX-147 "LOADING THE LATEST AMI DATABASE AND SWITCHING THE AMI
DATABASE PROVIDER" 
• F2000EX-304 "AUTOMATIC DESCENT MODE" 
• F2000EX-300 "ENHANCED AVIONICS SYSTEM EASY II" 
• F2000EX-329 "INCREASE OF WEIGHT AND BALANCE ENVELOPE FOR TAKE-OFF" 
L. OTHER PUBLICATIONS AFFECTED
The following publication is revised to account for the changes introduced by this Service Bulletin:
• Airplane Flight Manual revision 21 or subsequent revision (or Change Proposal 76)  or
subsequent revision.
• Master Minimum Equipment List Change Proposal 204 or subsequent revision.
The following publications will be revised at a later date to account for the changes introduced by this
Service Bulletin:
• CODDE 2 revision 19
• CODDE 3:
• QRH 1 revision 21
• QRH 2 revision 21
• Maintenance Manual.
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2. ACCOMPLISHMENT INSTRUCTIONS
A. PRELIMINARY STEPS
(1) The aircraft must be in the maintenance configuration (Refer to TASK 20-00-00-910-801).
B. REPLACEMENT OF THE "GA" LABEL
(1) On pilot control column/wheel (10CR) and copilot control column/wheel  (20CR), unstick the "GA"
label:
(a) Degrease the adjacent area of the label with cleaner.
(b) Apply adhesive tape 1790 all around the glue beads of the label to be removed.
(c) Carefully remove the beads of glue around the label with a scalpel, as shown below:
CAUTION: TAKE CARE NOT TO SCRATCH THE PAINT ON THE SURRONDING AREA.
(d) Slide the scalpel under the label then unstick it.
(2) Clean the area:
CAUTION: TAKE CARE NOT TO SCRATCH THE PAINT ON THE SURROUNDING AREA.
(a) Remove glue, paint and sealant from the label area with the scalpel.
(b) Clean the label area with a clean cloth moistened with cleaner.
(3) Stick the “TOGA” label:
(a) Mark the label area with adhesive tape 1790.
(b) Stick the “TOGA” label on the pilot or copilot wheel with glue ( araldite AV138M + hardener
HV998).
NOTE: Use the remaining beads of glue to correctly position the label.
(c) Remove the adhesive tape.
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(d) Restore the beads of glue at the area perimeter with ( araldite AV138M + hardener HV998).
(e) Allow the glue to cure during 16 hours.
(f) Remove the protective film from the “TOGA” label.
(4) On pilot control column/wheel (10CR) and copilot control column/wheel  (20CR) , write the letter
“A” after the part number with a vibro-engraver:
C. SOFTWARE LOADING
(1) Prior to starting the software loading, make sure that you have all the required CD-ROMs
mentioned in the “MATERIAL INFORMATION” paragraph and the previous APM Options CD-
ROM (this CD-ROM will be used to update the new APM settings configuration).
(2) Energize the aircraft systems (Refer to TASK 24-00-00-860-801 , paragraphs "Connection of the
electrical ground power unit" and “Energization with the electrical ground power unit”).
(3) Write the APM Settings configuration of the aircraft (Refer to TASK 31-42-25-910-801) using the
new table below:
NOTE 1: Parameters in grey cells:
• are either new, and will be completed during the full load,
• or, were previously incorporated in the APM Options (new APM settings name
and previous APM Options name are written in the cell). Refer to the Options.txt
file included in the previous APM Options CD-Rom for the parameter value.
NOTE 2: Parameters in bold text can be changed (the other values are the default values).
NOTE 3: The APM Settings tool cannot be used to download the current APM Settings file from
the aircraft to create the new settings.bin file for the Load 16.4. All the parameters
should be noted in the table below.
New load 16.4 Remarks Value
Aircraft Registration Number XXXXXX
Aircraft S/N XXX
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New load 16.4 Remarks Value
Mode S Transponder ICAO Address XXXXXX [hex]
2 Character IATA Airline ID 0
If Datalink is installed:
• XA (with ARINC Direct)
• GS (with GDC)
• ZD (with SATCOM DIRECT)
3 Character ICAO Airline ID 0
If Datalink is installed:
• XAA (with ARINC Direct)
• GDC (with GDC)
• SDI (with SATCOM DIRECT)
Audio Panel 3 Installed 0 (not installed)
1 (Installed)
Audio Panel 4 Installed 0 (Not installed)
Audio Panel 5 Installed 0 (Not installed)
Audio Panel 6 Installed 0 (Not installed)
Audio Panel 7 Installed 0 (Not installed)
Audio Panel 8 Installed 0 (Not installed)
Auto-Brake Installed 0 (Not installed)
1 (Installed with M3556)
Avionics Battery Removal 0 (Disable)
1 (Enable with M3336)
Bleed Air System Controller Type 0 (BASC 600 or 700)
1 (BASC 800 installed with M3086)
GPU Battery Charging Installed 0 (not installed)
1 (Installed with M2518)
Battery Voltage Drop Suppression 0 (Disable)
1 (Enable with M3147)
Battery Temp Control Installed 0 (Not installed with M2674)
1 (Installed)
Aircraft S/N Digit Thousands X [Dec]
Aircraft S/N Digit Hundreds X [Dec]
Aircraft S/N Digit Tens X [Dec]
Aircraft S/N Digit Ones X [Dec]
Brake System Anti-Ice Installed 0 (Not installed)
1 (Installed with SB F2000EX-065
(M2529) or M3195)
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New load 16.4 Remarks Value
Video Camera 1 Installed 0 (Not installed)
1 (Installed with SB F2000EX-117*
(M2516))
1 (Installed with SB F2000EX-189**
(M2308))
Video Camera 1 Name
Video Camera 2 Installed
Video Camera 2 Name
Video Camera 3 Installed
Video Camera 3 Name
Video Camera 4 Installed
Video Camera 4 Name
Video Camera 5 Installed Camera X (0 to 10 characters)
with SB F2000EX-117 (M2516)* or
Installed with SB F2000EX-189**
(M2308)
Video Camera 5 Name
Video Camera 6 Installed
Video Camera 6 Name
Video Camera 7 Installed
Video Camera 7 Name
Video Camera 8 Installed
Video Camera 8 Name
DMU Type 0
EVS LAT Offset 0
X [Dec] with ELBIT EVS
EVS Minimums 0
EVS Offset CRC 1 1
X [Dec] with ELBIT EVS
31701 with Rockwell Collins EVS
EVS Offset CRC 2 1
X [Dec] with ELBIT EVS
50799 with Rockwell Collins EVS
EVS Roll Offset 0 with Rockwell Collins EVS
X [Dec] with ELBIT EVS
EVS Vert Offset 0 with Rockwell Collins EVS
X [Dec] with ELBIT EVS
EVS Zoom percent 0
A/C Performance DBS Config. ID F2000EX EASy: 124100
F2000EX EASy with M3622: 124103
F2000DX: 124101
F2000LX: 124102
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New load 16.4 Remarks Value
F2000LXS: 125300
HUD Installed 0 (not installed)
1 (Installed with HGS)
HUD LAT Offset 0
HUD Offset CRC 1 1
31701 with HGS
HUD Offset CRC 2 1
50799 with HGS
HUD Roll Offset 0
HUD Verf Offset 0
Ice Detector System Installed 0 (Not installed)
1 (installed with M2533)
Barometric Default Units
(APM Options previous name:
jaaConfigEnabled)
0 (Disable - Baro units defaulted to
inches (JAA) with M2699)
1 (Enable - Baro units defaulted to
HPa (EASA) with M2699)
Number of Audio Panel
(APM Options previous name:
numAudioPanel)
2
3 (If third audio panel installed)
Number of COM
(APM Options previous name:
numCOM)
2
3 (If third VDR installed)
Number of VDR
(APM Options previous name:
numVDR)
2
3 (If third VDR installed)
Number of Video Camera 0
X [Dec] with SB F2000EX-117*
(M2516)
Printer Installed 0 (Not installed)
1 (Installed)
ECS Remote Temp Ctrl Installed 0 (not installed)
1 (Installed with M2613)
Selective Call
(APM Options previous name:
selcalEnable)
0 (Disable)
1 (Enable with M2662)
VDR 3 Installed 0 (Not installed)
1 (Installed if third VDR installed)
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New load 16.4 Remarks Value
(APM Options previous name:
vdr3Installed)
VHF 2 Cabin Transfer installed 0 (Not installed)
1 (Installed with M2615)
* A/C with SB F2000EX-117 (M2516), for the Video Camera channels assigned:
• set the Video Camera Installed statuses to "1" (Installed)
• fill in the Video Camera Names according to your choice.
** A/C with SB F2000EX189 (M2308), for the Video Camera channel chosen for EVS, set:
• Video Camera Installed status to "1" (Installed),
• Video Camera Name to "EVS".
(4) Remove the old version of the Remote Terminal software from the customer's laptop.
(5) Install the new version of the Remote Terminal software included in the HONEYWELL EPIC Tools
CD-Rom (Refer to TASK 45-10-00-860-801).
(6) Load the new software and databases in accordance with the data loading procedures (Refer to
TASK 45-90-00-860-801 ), (Refer to TASK 45-90-00-860-803 ), (Refer to TASK
45-90-00-860-804) and following the sequence hereafter:
SOFTWARE KEY WORD EFFECTIVITY
Operational Software Top Level
System Part Number
EB7036889-00210
Load 16.4 All Aircraft
TT600003571-XXXXX
APM Options parameter configuration
NOTE: If an authorization code is required, it will
be specified on the CD ROM label (Refer
to TASK 45-90-00-860-803)
All Aircraft
Creation of the APM Settings files:
• Create and save the APM Settings file on the hard drive using the APM
Settings Tool version 2.1 included in the HONEYWELL EPIC Tools CD-ROM
and the configuration noted previously. Use the settings.def definition file from
the Load 16.4 Operation Software located in the apm_defn folder.
NOTE: The create and load feature should not be used.
• Load the setting file created from the hard drive using DLS.
• Make a copy of this file generated by the APM Settings Tool on a media (e.g.
CD-ROM) and keep a copy on-board the aircraft.
NOTE: It is recommended to print the “settings.txt” file generated by the APM
Settings Tool to keep a record of the latest settings configuration.
All aircraft
16.3.1* LDI All aircraft
Refer to SB F2000EX-147 Airline Modifiable Information (AMI) database Aircraft with Datalink installed
V0004* Status Page - Fault Codes Database All aircraft
V0006* Status Page - Consequences Database F2000EX EASy / DX / LX
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SOFTWARE KEY WORD EFFECTIVITY
V0007* F2000LXS / S
V0033*
ECL database
F2000LXS / S
V0032* F2000EX EASy / DX / LX
60000704-005 FMS ACDB All aircraft
EPICM12-3CC INDS EPIC AIRSPACE & COMM NAVIGATIONDATA All aircraft
CHART DISK CC-20YY
(Full charts)
INDS Electronic Terminal Charts All aircraft
996-0145-5XX
(threat)
INDS EGPWS Data All aircraft
996-0114-5XX
(enveloppe modulation)
996-0146-5XX
(terrain server)
69000767-505 ATC Database
Aircraft with SB F2000EX-308
CPDLC ATN-B1
ACMF R1878* ACMF Optional but recommended to allaircraft for AP troubleshooting
* or latest applicable version (the most current software and database versions which can be loaded on the aircraft are
now tracked in the "MAINTENANCE DOCUMENTATION - Documentation Status" section of the Falcon Portal, where
you will be given the most up-to-date versions depending on the aircraft configuration).
NOTE: For aircraft with SB F2000EX-329 (M3622), the APM Options parameter configuration
must be updated as follows (Refer to TASK 45-90-00-860-803):
APM Parameter APM Value
aircraftTypeText F2000EX_M3622
(7) De-energize the aircraft systems (Refer to TASK 24-00-00-860-801  , paragraphs “De-
energization with the electrical ground power unit” and "Disconnection of the electrical ground
power unit").
(8) Discard all of the previous versions of the software, Options, Settings, Operator Tools and
Database CD-ROMs.
D. DOCUMENTATION
If not already done, update:
• the Airplane Flight Manual with revision 21 pages (or Change Proposal 76) or subsequent
revision,
• the Master Minimum Equipment List with Change Proposal 204 or subsequent revision.
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E. 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.
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3. MATERIAL INFORMATION
NOTE: Compliance with this Service Bulletin by substituting the part numbers below with interchangeable
subsequent part numbers (as per Master List or by DASSAULT AVIATION referenced supply) is
acceptable, provided the subsequent part numbers have the same effectivity as the original ones.
A. MODIFICATION OF CONTROL WHEEL PART NUMBERS
NEW P/N QTY KEY WORD OLD P/N
VLP202-20A
1 pilot control column/wheel (10CR)
VLP202-20
VLP202-10A VLP202-10
VLP302-10A VLP302-10
VLP402-10A VLP402-10
VLC202-20A
1 copilot control column/wheel (20CR)
VLC202-20
VLC202-10A VLC202-10
VLC302-10A VLC302-10
B. SOFTWARE
NEW P/N SOFTWARE KEY WORD EFFECTIVITY SUPPLIER
TM7035296-104
EPIC Tools including:
• Remote Terminal - RT 26.1, DLS 8.2
• APM Settings Tool - V 2.1
• APM restoration tool - V 2.2
All aircraft HONEYWELL
MM7033340-012
Operational Software
Top Level System
Part Number
EB7036889-00210
Load 16.4 All Aircraft HONEYWELL
TT60003571-XXXXX APM Options parameter configuration All Aircraft
HONEYWELL
through
DASSAULT
AVIATION
PUB: 422 or 690*
16.3.1** LDI
F2000EX EASy
DASSAULT
AVIATION
available on
FALCON portal
PUB: 423 or 690* F2000DX
PUB: 426 or 690* F2000LX
PUB: 431 or 690* F2000LXS
PUB: 432 or 690* F2000S
Refer to Service Bulletin F2000EX-147 
Airline Modifiable
Information (AMI)
database
Aircraft with Datalink
installed
GDC or
ARINC Direct or
SATCOM DIRECT
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NEW P/N SOFTWARE KEY WORD EFFECTIVITY SUPPLIER
PUB: 677 V0004** Status Page - FaultCodes database All aircraft DASSAULTAVIATION
PUB: 678
V0006** Status Page -
Consequences
database
F2000EX EASy / LX /
DX DASSAULT
AVIATION
V0007** F2000LXS / S
PUB: 691
V0033**
ECL database
F2000LXS / S
DASSAULT
AVIATIONV0032** F2000EX EASy / DX /LX
DM60000704-005 60000704-005 FMS ACDB All aircraft HONEYWELL
DS1 EPICM12-3CC
INDS EPIC
AIRSPACE & COMM
NAVIGATION DATA
All aircraft
Integrated Navigation
Data Service (INDS)
Full charts CHART DISKCC-20YY INDS ElectronicTerminal Charts All aircraft
EGPWS Database
996-0145-5XX (threat)
INDS EGPWS Data
All aircraft996-0114-5XX
(envelope modulation)
EGPWS Terrain
Server 996-0146-5XX All aircraft
69000767-505 ATC database
Aircraft with SB
F2000EX-308
CPDLC ATN-B1
HONEYWELL
ACMF r1878 ACMF r1878** ACMF
Optional but
recommended to all
aircraft for AP
troubleshooting
DASSAULT
AVIATION
available on
FALCON portal
* CD-ROM PUB number
** or latest applicable version (the most current software and database versions which can be loaded on the aircraft are
now tracked in the "MAINTENANCE DOCUMENTATION - Documentation Status" section of the Falcon Portal, where
you will be given the most up-to-date versions depending on the aircraft configuration).
C. MODIFICATION KIT
Kit P/N SBF900EX0400E
NEW P/N QTY KEY WORD
2616399887 2 Label for pilot and copilot control wheels
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D. LOCAL PROCUREMENT
As indicated in Consumable Products Manual (CPM):
• cleaner.
• araldite AV138M.
• hardener HV998.
• adhesive tape 1790.
 
END OF DOCUMENT
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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

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SERVICE BULLETINS COMPLIANCE FALCON 2000EX A/C S/N    
DASSAULT AVIATION Number  ATA Number   
F2000EX 322  F2000EX 00 19   
        
        
        
        
Coding: C complete compliance
 
T partial compliance
   
Performed by:   
Remarks: Revision 1 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 2000EX A/C S/N    
DASSAULT AVIATION Number
Numero DASSAULT AVIATION  
ATA Number
Numero ATA   
F2000EX 322  F2000EX 00 19   
        
        
        
        
Coding: C complete complianceapplication totale
 
T partial complianceapplication partielle
   
Performed by:
Fait par:
  
Remarks: Revision 1 Date: Signature:
Remarques: Revision 1

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