# Dassault Service Bulletin F900EX-423: No revision named

- 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 F900EX-423](https://openairdocs.org/service-documents/dassault/f900ex-423.md)
- Title as filed: SB F900EX-423
- Pages: 34
- PDF: https://openairdocs.org/files/sha256/54/d8/54d8f79cb420d3f2015993c8347f3a3fdf999105cbeb4326936afb4619af0a74
- Page: https://openairdocs.org/service-documents/dassault/f900ex-423/file/54d8f79cb420

## Text

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### Page 1

FALCON 900LX
No 423
DECEMBER 09, 2016
 
ATA 00-22
GENERAL
EASY II LOAD 28.4
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.
573

### Page 2

GENERAL
EASY II LOAD 28.4
Initial issuance December 09, 2016
List of effective pages :
1 to 7
FALCON 900EX F900EX -423
F900EX -00-22

### Page 3

GENERAL
EASY II LOAD 28.4
 
1. PLANNING INFORMATION
A. EFFECTIVITY
This Service Bulletin is applicable to F900LX aircraft with serial numbers 291, 294, 297 and 298 that
have not previously implemented DASSAULT AVIATION modification F900EX M6002.
B. REASON
The purpose of this Service Bulletin is to upgrade the aircraft avionics to the EASy II load 28.4
standard that includes the following features:
• Various improvements for FMS, CAS, displays, communication.
• New AMI database for GDC and ARINC Direct providers (through DASSAULT AVIATION
Service Bulletin F900EX-313).
C. DESCRIPTION
The operation consists in performing a full load of software.
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 F900EX M6002 that has been
approved by EASA.
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.
G. TOOLING - PRICE AND AVAILABILITY
Normal maintenance tooling.
H. WEIGHT AND BALANCE
Change in weight: None.
Change in balance with respect to 25% MAC: None.
I. REFERENCES
Aircraft Maintenance Manual:
FALCON 900EX F900EX -423
December 09, 2016 F900EX -00-22
Initial issuance Page 1 / 7
DASSAULT AVIATION Proprietary Data

### Page 4

• GENERAL MAINTENANCE AND SAFETY PRECAUTIONS (Refer to TASK 20-00-00-910-801)
• BASIC SEALING METHODS (Refer to TASK 20-32-00-390-801)
• ENERGIZATION / DE-ENERGIZATION OF THE AIRCRAFT SYSTEMS (Refer to TASK
24-00-00-860-801)
• AIRCRAFT PERSONALITY MODULE (APM) SETTINGS TOOL USER GUIDE (Refer to TASK
31-42-25-910-801)
• OPERATIONAL TEST OF THE CENTRAL DISPLAY SYSTEM (CDS) (Refer to TASK
31-60-00-710-801)
• INSTALLATION OF AVIONICS SOFTWARE TOOLS (Refer to TASK 45-10-00-860-801)
• DATABASE LOADING (Refer to TASK 45-90-00-860-803)
DASSAULT AVIATION Service Bulletin F900EX-313
J. OTHER PUBLICATIONS AFFECTED
The following publications are revised to account for the changes introduced by this Service Bulletin:
• Maintenance Planning Documentation, Chapter 5-40 DGT113875 CP 16.
• Aircraft Maintenance Manual.
• Master Minimum Equipment List, CP 204.
The following publications will be revised at a later date to account for the changes introduced by this
Service Bulletin:
• Aircraft Maintenance Manual revision 23.
• Maintenance Planning Documentation, Chapter 5-40 DGT113875 revision 10.
• Maintenance Planning Documentation revision 7.
FALCON 900EX F900EX -423
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Initial issuance Page 2 / 7
DASSAULT AVIATION Proprietary Data

### Page 5

2. ACCOMPLISHMENT INSTRUCTIONS
A. PRELIMINARY STEPS
The aircraft must be in the maintenance configuration (Refer to TASK 20-00-00-910-801).
B. SOFTWARE LOADING
(1) Prior to starting the software loading, make sure that you have all the required CD-ROMs
mentioned in paragraph 3.
(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) Remove the old version of the Remote Terminal software from the customer's laptop.
(4) 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).
(5) Perform a full load of software in accordance with the periodic databases, databases and software
loading procedures and following the sequence hereafter.
SOFTWARE KEY WORD EFFECTIVITY
Operational Software Top Level
System Part Number
EB7036889-00121
Load 28.4 All aircraft
TT60003572-XXXXX
(see first note below)
APM Options parameter configuration All aircraft
Creation of the APM Settings files (see second note below):
• Create and load the APM Settings file using the APM Settings Tool
version 2.1 included in the HONEYWELL EPIC Tools CD-ROM and the
configuration noted previously.
• 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
28.4.1 LDI All aircraft
Refer to SBF900EX-313 Airline Modifiable Information (AMI)database Aircraft with Datalink installed
V0003 Status Page - Fault Codes Databasefor Dassault Easy All aircraft
V0005 Status Page - ConsequencesDatabase for Dassault Easy All aircraft
V0007 ECL DATABASE All aircraft
60000704-005 FMS ACDB All aircraft
EPICM12-3CC DS1 All aircraft
FALCON 900EX F900EX -423
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DASSAULT AVIATION Proprietary Data

### Page 6

SOFTWARE KEY WORD EFFECTIVITY
INDS EPIC AIRSPACE
& COMM NAVIGATION DATA
CHART DISK mm-yyyy
(Full charts version)
INDS Electronic Terminal Charts All aircraft
996-0145-5XX
(threat)
INDS EGPWS Data All aircraft
996-0114-5XX
(envelope modulation)
996-0146-5XX
(terrain server)
69000767-505 ATC Database
Aircraft with SB F900EX-408
CPDLC ATN-B1
ACMF r3938 ACMF Optional but recommended to allaircraft for AP troubleshooting
NOTE: Load the new Options parameter configuration in accordance with the dataloading
procedure (Refer to TASK 45-90-00-860-803 ). The following new APM Options
parameters are defined in the table below:
APM parameter Selection Value
dmuType DLMU 2
svsInavVividDisplayEnable Disable 0
NOTE: Update the APM settings file with the following settings data (Refer to TASK
31-42-25-910-801)
APM parameter Selection Value
EVS Minimums Not installed 0
HUD Flare Enabled Disable 0
HUD Type CMC Rockwell Collins HUD 0
(6) 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").
(7) Discard all of the previous versions of the software, Options, Settings, Operator Tools and
Database CD-ROMs.
C. DOCUMENTATION
Incorporate:
• CP 204 in the Master Minimum Equipment List,
FALCON 900EX F900EX -423
December 09, 2016 F900EX -00-22
Initial issuance Page 4 / 7
DASSAULT AVIATION Proprietary Data

### Page 7

• CP 16 attached in the Maintenance Planning Documentation, Chapter 5-40 until revision 10 is
released.
NOTE: For A/C on which operation (31-60-00-710-801-08) has been performed within 1640FH,
the FH have to be counted from the last operation (31-60-00-710-801-08).
• TASK 31-60-00-710-801 attached in the Aircraft Maintenance Manual until revision 23 is
released.
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 900EX F900EX -423
December 09, 2016 F900EX -00-22
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DASSAULT AVIATION Proprietary Data

### Page 8

3. MATERIAL INFORMATION
NOTE: Compliance with this Service Bulletin by substituting the part numbers below with interchangeable
subsequent part numbers (by DASSAULT AVIATION referenced supply) is acceptable, provided
the subsequent part numbers have the same effectivity as the original ones.
A. SOFTWARE
NEW P/N SOFTWARE KEY WORD EFFECTIVITY SUPPLIER
TM7035298-105
EPIC Tools including:
• Remote
Terminal - RT 26.1, DLS 8.2
• APM Settings
Tool - V 2.1
• APM restoration tool
- V 2.2
EPIC TOOLS All aircraft HONEYWELL
MM7031351-021
Operational Software
Top Level System
Part Number
EB7036889-00121
Load 28.4 All aircraft HONEYWELL
TT60003572-XXXXX TT60003572-XXXXX
APM Options
parameter
configuration
All aircraft
HONEYWELL
through
DASSAULT
AVIATION
PUB: 411 or 630* 28.4.1 LDI All aircraft
DASSAULT
AVIATION
available on
FALCON portal
Refer to Service Bulletin F900EX-313
Airline Modifiable
Information (AMI)
database
Aircraft with
Datalink installed
GDC or ARINC
Direct or
SATCOM
DIRECT
PUB: 584 V0003
Status Page -
Fault Codes
Database for
Dassault Easy
All aircraft DASSAULTAVIATION
PUB: 585 V0005
Status Page -
Consequences
Database for
Dassault Easy
All aircraft DASSAULTAVIATION
PUB: 628 V0007 ECL DATABASE All aircraft DASSAULTAVIATION
DM60000704-005 60000704-005 FMS ACDB All aircraft HONEYWELL
FALCON 900EX F900EX -423
December 09, 2016 F900EX -00-22
Initial issuance Page 6 / 7
DASSAULT AVIATION Proprietary Data

### Page 9

NEW P/N SOFTWARE KEY WORD EFFECTIVITY SUPPLIER
DS1 EPICM12-3CC
INDS EPIC
AIRSPACE &
COMM
NAVIGATION
DATA
All aircraft
Integrated
Navigation
Data Service
(INDS)
Full charts CHART DISK mm-yyyy INDS ElectronicTerminal Charts All aircraft
EGPWS Database
996-0145-5XX
(threat) INDS EGPWS
Data
All aircraft
996-0114-5XX
(envelope modulation)
EGPWS Terrain
Server
996-0146-5XX
(terrain server)
INDS EGPWM
Data
69000767-505 ATC Database
Aircraft with SB
F900EX-308
CPDLC ATN-B1
HONEYWELL
ACMF r3938 ACMF r3938 ACMF
Optional but
recommended to
all aircraft for AP
troubleshooting
DASSAULT
AVIATION
available on
FALCON portal
DASSAULT
AVIATION
available on
FALCON portal
* CD-ROM part number
 
END OF DOCUMENT
FALCON 900EX F900EX -423
December 09, 2016 F900EX -00-22
Initial issuance Page 7 / 7
DASSAULT AVIATION Proprietary Data

### 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 900EX A/C S/N    
DASSAULT AVIATION Number  ATA Number   
F900EX 423  F900EX 00 22   
        
        
        
        
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 900EX A/C S/N    
DASSAULT AVIATION Number
Numero DASSAULT AVIATION  
ATA Number
Numero ATA   
F900EX 423  F900EX 00 22   
        
        
        
        
Coding: C complete complianceapplication totale
 
T partial complianceapplication partielle
   
Performed by:
Fait par:
  
Remarks: Initial issuance Date: Signature:
Remarques: Edition originale

### Page 12 (OCR)

Filing instruction:  FALCON 900EX EASY CHAPTER 5
Instead of:  Section 5-40 Mandatory Maintenance Operations
CHANGE PROPOSAL 016
FALCON 900EX EASY / 900LX / 900DX
CHAPTER 5-40
31 : INDICATING - RECORDING SYSTEMS
maintenance  Scheduled  Origin  Title / Operation  First Inspection  Interval  Remarks
task number
31-60-00-710-801-08  CMR  PERATIONAL TEST OF THE CENTRAL DISPLAY SYSTEM (CDS  1640 FH  1640 FH
31-600  EVERSION CONTROLLER (34F
0900400080a1cace - RELEASED - Certification Repository  Effectivity: A/C 97 and >=120 - Reference DGT 113875
Rev. Date: November 2015
Page 20 / 31
"DASSAULT AVIATION Proprietary Data"
Rev. Date: CP 016 draft 1 08/2016

### Page 13 (OCR)

Read:
FALCON 900EX EASY / 900LX / 900DX
CHAPTER 5-40
31 : INDICATING - RECORDING SYSTEMS
maintenance  Scheduled  Origin  Title / Operation  First inspection  Interval  Remarks
task number
31-60-00-710-801-20  CMR  THE THE CURSE CONTE ONE AN DEMAND ELICOST  1640 FH  1640 FH
31-600
Effectivity : A/C 97 and >=120 - Reference DGT 113875
Rev. Date : XX/20XX
Page 20 / 31
'DASSAULT AVIATION Proprietary Data"
Rev. Date: CP 016 draft 1 08/2016

### Page 14

TASK 31-60-00-710-801
OPERATIONAL TEST OF THE CENTRAL DISPLAY SYSTEM (CDS)
 
1. OVERVIEW OF THE JOB
Operation code: 31-60-00-710-801-20 Test of the Cursor Control Device and Reversion commands
NOTE: Even though the test of the Reversion Controller – DU Shutdown is not a scheduled maintenance
task in Maintenance Planning Document (MPD), this test must be done before the test of the
Cursor Control Device and Reversion commands.
2. LOGISTICS
A. References
Reference Designation
• 24-00-00-860-801 ENERGIZATION / DE-ENERGIZATION OF THE AIRCRAFT SYSTEMS
B. Tools and Ground Support Equipment
Reference Designation Quantity
• TO-20-360 MULTIMETER
C.  Energy
• ELECTRICAL
D. Access
Reference Designation
• PAX PASSENGER DOOR
3. JOB SET-UP
A. Connect the electrical ground power unit (Refer to TASK 24-00-00-860-801, paragraph "Connection of
the Electrical Ground Power Unit").
B. Energize the aircraft system (Refer to TASK 24-00-00-860-801 , paragraph "Energization with the
Electrical Ground Power Unit").
4. TEST OF THE REVERSION CONTROLLER – DU SHUTDOWN
Refer to fig. 1
A. To test the LH PFD ( L12FV), do the following steps:
(1) Turn the inner dimming knob on the reversion controller (34FV) for the LH PFD (1-fig. 1) to
"OFF".
(2) Make sure that the LH PFD screen goes blank and that its display data is shown on the upper
MFD.
(3) Turn the inner dimming knob on the reversion controller for the LH PFD (1-fig. 1) away from
"OFF".
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 1 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 15

(4) Make sure that the LH PFD displays data again.
B. To test the upper MFD ( L22FV), do the following steps:
(1) Turn the inner dimming knob on the reversion controller for the upper MFD (2-fig. 1) to "OFF".
(2) Make sure that the upper MFD screen goes blank and that there is no change in the data
displayed on the other DUs.
(3) Turn the inner dimming knob on the reversion controller for the upper MFD (2-fig. 1) away from
"OFF".
(4) Make sure that the upper MFD displays data again.
C. To test the lower MFD ( R22FV), do the following steps:
(1) Turn the inner dimming knob on the reversion controller for the lower MFD (11-fig. 1) to "OFF".
(2) Make sure that the lower MFD screen goes blank screen and that the upper MFD reverts to the
default windows configuration of the lower MFD.
(3) Turn the inner dimming knob on the reversion controller for the lower MFD (11-fig. 1) away from
"OFF".
(4) Make sure that the lower MFD displays data again.
D. To test the RH PFD ( R12FV), do the following steps:
(1) Turn the inner dimming knob on the reversion controller for the RH PFD (3-fig. 1) to "OFF".
(2) Make sure that the RH PFD screen goes blank and that its display data is shown on the upper
MFD.
(3) Turn the inner dimming knob on the reversion controller for the RH PFD (3-fig. 1) away from
"OFF".
(4) Make sure that the RH PFD displays data again.
5. TEST OF THE CURSOR CONTROL DEVICE AND REVERSION COMMANDS
Refer to fig. 1, fig. 2, fig. 3, fig. 4, fig. 5, fig. 6, fig. 7, fig. 8, fig. 9 and fig. 10
NOTE: Each Cursor Control Device (L44FV)/(R44FV) has two equivalent channels, outboard and inboard,
to control the cursor movement on the display units (DU) and to provide CCD input data to the
MAU (including Baro Settings, reversion controller DU/AGM and sensor data).
A. On the guidance panel, turn the Pilot Baro Setting Knob (2-fig. 2) to set a value of 1020 mbar on the
LH PFD (L12FV).
B. On the guidance panel, turn the Copilot Baro Setting Knob (11-fig. 2) to set a value of 1030 mbar on
the RH PFD (R12FV).
C. Check the inner dimming knobs on the reversion controller ( 34FV) as follows:
(1) Turn the inner dimming knob on the reversion controller for the LH PFD (1-fig. 1) to “OFF”.
(2) Make sure that the LH PFD screen goes blank and that its display data is shown on the upper
MFD.
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 2 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 16

(3) Turn the inner dimming knob on the reversion controller for the upper MFD (2-fig. 1) to “OFF”.
(4) Make sure that the upper MFD screen goes blank and that the LH PFD display data is shown on
the lower MFD.
(5) Turn the inner dimming knob on the reversion controller for the LH PFD (1-fig. 1) and the inner
dimming knob on the reversion controller for the upper MFD (2-fig. 1) clockwise from “OFF”.
(6) Make sure that the brightness of the LH PFD and the upper MFD increases and that each DU
displays its usual data.
(7) Turn the inner dimming knob on the reversion controller (3-fig. 1) for the RH PFD to “OFF”.
(8) Make sure that the RH PFD screen goes blank and that its display data is shown on the upper
MFD.
(9) Turn the inner dimming knob on the reversion controller (11-fig. 1) for the lower MFD to “OFF”.
(10) Make sure that the lower MFD screen goes blank.
(11) Push the “PDU/MDU” button (10-fig. 1).
(12) Make sure that the data displayed on the upper MFD is replaced with the display data from the
lower MFD.
(13) Turn the inner dimming knob on the reversion controller for the RH PFD and the inner dimming
knob on the reversion controller for the lower MFD clockwise from “OFF”.
(14) Make sure that the brightness of the RH PFD and the lower MFD increases and that each DU
displays its usual data.
D. Do the following steps to test channel A (outboard channel) of the LH CCD ( L44FV):
(1) Open the "CCD LH" circuit breaker (R41FV) (isolation of the inboard LH CCD channel) on the
right side of the circuit breaker panel (10PP).
(2) Open the "CCD RH" circuit breaker (R31FV) (isolation of the inboard RH CCD channel) on the
right side of the circuit breaker panel (10PP).
(3) Open the "CCD RH" circuit breaker (L41FV) (isolation of the outboard RH CCD channel) on the
left side of the circuit breaker panel (10PP).
(4) Set the channel reversion switch on the rear of the LH CCD to the outboard channel position ( fig.
4).
(5) Make sure that the amber " CCD RH FAIL" CAS message is displayed on the PFDs.
(6) On the CCD, do the following steps:
(a) Use the display switch (5-fig. 5) on the CCD to move the cursor from one DU to a different
DU according to the tables below:
Table 1: LH CCD display switch test
Display switch position Cursor location
Up Upper MFD
Down Lower MFD
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 3 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 17

Display switch position Cursor location
Left LH PFD
Right Upper MFD
Table 2: RH CCD display switch test
Display switch position Cursor location
Up Upper MFD
Down Lower MFD
Left Upper MFD
Right RH PFD
(b) Move the cursor to the center of the MFD and push the “MENU” button (4-fig. 5) on the
CCD.
(c) Make sure that the menu selection is displayed on the MFD ( fig. 6).
(d) Select "INAV" (1-fig. 6) using the left enter pushbutton (1-fig. 5) on the CCD.
(e) Make sure that the INAV window is displayed on the MFD.
(f) Move the CCD trackball (2-fig. 5) randomly and make sure that the cursor follows
accordingly on the INAV window.
(g) Turn the inner and outer data set knobs (3-fig. 5) on the CCD and make sure that the INAV
range increases and decreases accordingly.
(7) On the reversion controller, test the CCD inputs of the display reversion system as follows:
(a) Do the reversion according to the table below and record the results in the PASS/FAIL
column.
AGM manual reversion
Use PFD/MFD outer knob
DU shutdown
Use PFD/MFD inner knob
State after manual AGM and/or DU
reversion
RESUL
TS
LH
PFD
(1-fig.
1)
Uppe
r
MFD
(2-fig.
1)
Lowe
r
MFD
(11-
fig. 1)
RH
PFD 
(3-fig.
1)
LH
PFD 
(1-fig.
1)
Upper
MFD (2-
fig. 1)
Lower
MFD 
(11-fig.
1)
RH PFD
(3-fig.
1)
LH PFD
Format
and
Source
Upper
MFD
Format
and
Source
Lower
MFD
Format
and
Source
RH
PFD
Format
and
Source
PASS/
FAIL
No reversion LH PFD
AGM1
P
MFD
AGM2
P
MFD
AGM3
P
RH
PFD
AGM4
P
REV LH PFD
AGM3
S
MFD
AGM2
P
Red X RH
PFD
AGM4
P
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 4 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 18

AGM manual reversion
Use PFD/MFD outer knob
DU shutdown
Use PFD/MFD inner knob
State after manual AGM and/or DU
reversion
RESUL
TS
LH
PFD
(1-fig.
1)
Uppe
r
MFD
(2-fig.
1)
Lowe
r
MFD
(11-
fig. 1)
RH
PFD 
(3-fig.
1)
LH
PFD 
(1-fig.
1)
Upper
MFD (2-
fig. 1)
Lower
MFD 
(11-fig.
1)
RH PFD
(3-fig.
1)
LH PFD
Format
and
Source
Upper
MFD
Format
and
Source
Lower
MFD
Format
and
Source
RH
PFD
Format
and
Source
PASS/
FAIL
REV LH PFD
AGM3
S
MFD
AGM1
T
Red X RH
PFD
AGM4
P
REV REV LH PFD
AGM1
P
Red X Red X RH
PFD
AGM4
P
REV LH PFD
AGM3
S
MFD
AGM1
T
Red X RH
PFD
AGM2
S
REV OFF Blank LH PFD
AGM2
P
MFD
AGM3
P
RH
PFD
AGM4
P
REV OFF LH PFD
AGM2
T
Blank MFD
AGM3
P
RH
PFD
AGM4
P
REV OFF LH PFD
AGM3
S
RH
PFD
AGM2
P
MFD
AGM4
T
Blank
REV OFF LH PFD
AGM1
P
MFD
AGM4
S
Blank RH
PFD
AGM3
T
REV OFF Blank LH PFD
AGM2
P
MFD
AGM1
S
RH
PFD
AGM4
P
NOTE 1: REV – The outer knob is set to "REV". If nothing is required, the outer knob is set "AUTO".
NOTE 2: OFF – The inner knob is set to "OFF". If nothing is required, the inner knob is set away from "OFF".
NOTE 3: Blank – No data displayed on the DU.
NOTE 4: Red X – Red cross displayed on the DU.
NOTE 5: AGMX P - Primary source
AGMX S - Secondary source
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 5 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 19

AGM manual reversion
Use PFD/MFD outer knob
DU shutdown
Use PFD/MFD inner knob
State after manual AGM and/or DU
reversion
RESUL
TS
LH
PFD
(1-fig.
1)
Uppe
r
MFD
(2-fig.
1)
Lowe
r
MFD
(11-
fig. 1)
RH
PFD 
(3-fig.
1)
LH
PFD 
(1-fig.
1)
Upper
MFD (2-
fig. 1)
Lower
MFD 
(11-fig.
1)
RH PFD
(3-fig.
1)
LH PFD
Format
and
Source
Upper
MFD
Format
and
Source
Lower
MFD
Format
and
Source
RH
PFD
Format
and
Source
PASS/
FAIL
AGMX T - Tertiary source
(b) Put all reversion/dimming knobs ( (1-fig. 1), (2-fig. 1), (3-fig. 1) and (11-fig. 1)) in the normal
configuration as follows:
1 Set the PFD/MFD inner dimming knobs away from "OFF",
2 Set the PFD/MFD outer reversion knobs to "AUTO".
(c) Turn the LH and RH PFD inner dimming knobs ( (1-fig. 1) and (3-fig. 1)) to "OFF":
• Make sure that LH and RH PFD are off.
• Make sure that the upper MFD displays the LH PFD data.
• Make sure that the lower MFD displays the RH PFD data.
(d) Push the "PDU/MDU" button (10-fig. 1) and make sure that the data displayed on the lower
MFD is in MFD format.
(e) Put all buttons and knobs in the normal configuration as follows:
1 Set the LH and RH PFD inner dimming knobs ( (1-fig. 1)  and (3-fig. 1)) away from
"OFF",
2 Set the PFD/MFD outer reversion knobs to "AUTO" (  (1-fig. 1), (2-fig. 1), (3-fig. 1) and 
(11-fig. 1)),
(8) On the reversion controller, test the CCD inputs of the reversion sensors as follows:
(a) Turn the “DAU1” knob (12-fig. 1) on the reversion controller from “AUTO” to “REV”.
(b) Make sure that an amber “ DAU 1” annunciation (21-fig. 7) is displayed next to the top left
corner of the airspeed tape on each PFD.
(c) Turn the “DAU2” knob (9-fig. 1) on the reversion controller from “AUTO” to “REV”.
(d) Make sure that an amber “ DAU 2” annunciation (3-fig. 8) is displayed next to the top right
corner of the altitude tape on each PFD.
(e) Turn the “DAU1” knob and “DAU2” knob to “AUTO”.
(f) Use “IRS” buttons (5-fig. 1) and (16-fig. 1) on the reversion controller to toggle the IRS
source on the LH PFD and RH PFD, and check the annunciation for each of the selections
in the table below:
NOTE: IRS reversion annunciation (13-fig. 8) is displayed adjacent to the bottom right
corner of the altitude tape on each PFD.
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 6 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 20 (OCR)

DASSAULT
FALCON
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
A/C WITH 2 IRS  A/C WITH 3 IRS
Reversion controller  IRS reversion  Reversion controller  IRS reversion
IRS button  annunciation on PFD  IRS button  annunciation on PFD
LH button  RH button  LH PFD  RH PFD  LH button  RH button  LH PFD  RH PFD
Released  Released  Released  Released
1s' push  Released  IRS2  IRS2  1s' push  Released  IRS3
2nd push  Released  2"° push  Released  IRS2  IRS2
2nd push  1st push  IRS1  IRS1  2nd push  Is push  IRS2  IRS3
2°° push  2" push  2nd push  2nd push  IRS2  IRS1
3r push  2nd push  IRS1  IRS1
3rd push  3r push
(g) Make sure that IRS source is back in normal configuration on LH PFD and RH PFD (no IRS
reversion annunciation on PFDs).
Use "FMS" buttons (4-fig. 1) and (17-fig. 1) on the reversion controller to toggle the FMS
source on the LH PFD and RH PFD, and check the annunciation for each of the selections
in the table below:
NOTE 1: FMS reversion annunciation is displayed on the left side of the HSI (9-fig. 9) on
each PFD.
NOTE 2: FMS reversion annunciation is only displayed if "FMS" check box is selected on
"CDI" menu of the HSI control bar (fig. 10).
A/C WITH 2 FMS  A/C WITH 3 FMS
Reversion controller  FMS reversion  Reversion controller  FMS reversion
FMS button  annunciation on PFD  FMS button  annunciation on PFD
LH button  RH button  LH PFD  RH PFD  LH button  RH button  LH PFD  RH PFD
Released  Released  Released  Released
FMS1  FMS2  FMS1  FMS2
1s push  Released  FMS2  FMS2  1s push  Released  FMS3  FMS2
1" push  1s push  FMS2  FMS1  2nd push  Released  FMS2  FMS2
2"d push  1s' push  FMS1  FMS1  2nd push  1° push  FMS2  FMS3
2"° push  2"° push  FMS1  FMS2  2nd push  2°d push  FMS2  FMS1
3* push  2nd push  FMS1  FMS1
3rd push  3rd push  FMS1  FMS2
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 7 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 21

(i) Make sure that FMS source is back in normal configuration on LH PFD and RH PFD
("FMS1" annunciation on LH PFD and "FMS2" annunciation on RH PFD)
(j) (A/C with second radar altimeter) Use “RA” buttons (6-fig. 1) and (15-fig. 1) on the reversion
controller to toggle the radar altimeter source on the LH PFD and RH PFD, and check the
annunciation for each of the selections in the table below:
NOTE: RA reversion annunciation (8-fig. 8) is displayed on the right side of the altitude tape
on each PFD.
(k) Make sure that RA source is back in normal configuration on LH PFD and RH PFD (no RA
reversion annunciation on PFDs).
(l) Use “ADS” buttons (13-fig. 1) and (8-fig. 1) on the reversion controller to toggle the ADS
source on the LH PFD and RH PFD, and check the annunciation for each of the selections
in the table below:
NOTE: ADS reversion annunciation (6-fig. 8) is displayed on the right side of the altitude
tape on each PFD.
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 8 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 22

(m) Make sure that ADS source is back in normal configuration on LH PFD and RH PFD (no
ADS reversion annunciation on PFDs).
(9) Check that the baro-setting value on LH PFD is 1020 mbar.
(10) Check that the baro-setting value on RH PFD is 1030 mbar.
E. Do the following steps to test channel B (inboard channel) of the LH CCD ( L44FV):
(1) Open the "CCD LH" circuit breaker (L31FV) (isolation of the outboard LH CCD channel) on the
left side of the circuit breaker panel (10PP).
(2) Close the "CCD LH" circuit breaker ( R41FV) on the right side of the circuit breaker panel (10PP).
(3) Set the channel reversion switch on the rear of the LH CCD to the inboard channel position ( fig.
4).
(4) Make sure that the amber " CCD RH FAIL" CAS message is still displayed on the PFDs.
(5) Do steps 5.D.(6) thru 5.D.(10).
F. Do the following steps to test channel B (outboard channel) of the RH CCD ( R44FV):
(1) Close the "CCD RH" circuit breaker ( L41FV) on the left side of the circuit breaker panel (10PP).
(2) Make sure that the amber " CCD RH FAIL" CAS message is not displayed on the PFDs.
(3) Open the "CCD LH" circuit breaker (R41FV) (isolation of the inboard LH CCD channel) on the
right side of the circuit breaker panel (10PP).
(4) Set the channel reversion switch on the rear of the RH CCD to the outboard channel position ( fig.
4).
(5) Make sure that the amber " CCD LH FAIL" CAS message is displayed on the PFDs.
(6) Do steps 5.D.(6) thru 5.D.(10).
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 9 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 23

G. Do the following steps to test channel A (inboard channel) of the RH CCD ( R44FV):
(1) Open the "CCD RH" circuit breaker (L41FV) (isolation of the outboard RH CCD channel) on the
left side of the circuit breaker panel (10PP).
(2) Close the "CCD RH" circuit breaker ( R31FV) on the right side of the circuit breaker panel (10PP).
(3) Set the channel reversion switch on the rear of the RH CCD to the inboard channel position ( fig.
4).
(4) Make sure that the amber " CCD LH FAIL" CAS message is still displayed on the PFDs.
(5) Do steps 5.D.(6) thru 5.D.(10).
(6) Close the "CCD LH" circuit breaker ( R41FV) on the right side of the circuit breaker panel (10PP).
(7) Close the "CCD LH" circuit breaker ( L31FV) on the left side of the circuit breaker panel (10PP).
(8) Close the "CCD RH" circuit breaker ( L41FV) on the left side of the circuit breaker panel (10PP).
(9) Set the channel reversion switches on the rear of the LH and RH CCD to the outboard channel
positions (fig. 4).
(10) Make sure that the amber "CCD LH FAIL" CAS message is not displayed on the PFDs.
6. CLOSE-UP
A. De-energize the aircraft (Refer to TASK 24-00-00-860-801 , paragraph "De-Energization with the
Electrical Ground Power Unit").
B. Disconnect the electrical ground power unit (Refer to TASK 24-00-00-860-801 , paragraph
"Disconnection of the Electrical Ground Power Unit").
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 10 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 24

Figure 1: REVERSION CONTROLLER - LOCATION OF CONTROLS
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 11 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 25

Figure 2: GUIDANCE PANEL CONTROLLER - LOCATION OF CONTROLS
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 12 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 26

Figure 3: LOCATION OF CIRCUIT BREAKERS
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 13 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 27 (OCR)

DASSAULT
FALCON
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
LH CCD  ~ RH CCD
LH CCD  RH CCD
TOGGLE SWITCH
OUTBOARD SELECTION
Figure 4: CURSOR CONTROL DEVICE (CCD) - SELECTION OF INBOARD/OUTBOARD CHANNELS
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 14 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 28

Figure 5: CURSOR CONTROL DEVICE (CCD) - LOCATION OF CONTROLS
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 15 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 29 (OCR)

DASSAULT
FALCON
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
- 2
INAV  WPT LIST  WPT LIST  WPT LIST
-3  3
WPT LIST  FLIGHT MGMT  FLIGHT MGMT  FLIGHT MGM
FLIGHT MGM  FULL INAV  FULL INAV  FULL INAV
- 12  11
CHARTS  MEL  CHECKLIS
SYNOPTICS
MF/AFIS
FULL MAIN
VIDEO
(A/C without M5340)
Figure 6: MFD - CCD "MENU" BUTTON SELECTIONS
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 16 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 30 (OCR)

DASSAULT
FALCON
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
- 2
INAV  WPT LIST  WPT LIST  WPT LIST
-3  3
WPT LIST  FLIGHT MGMT  FLIGHT MGMT  FLIGHT MGM
FLIGHT MGM  FULL INAV  FULL INAV  FULL INAV
- 13  — 13  - 13
CHARTS  ATC DTLK  ATC DTLK  ATC DTLK
- 12  - 11
SYNOPTICS  MEL  CHECKLIST
C
:MF/AFIS
FULL MAINT  D
VIDEO
(A/C with M5340)
Figure 6: MFD - CCD "MENU" BUTTON SELECTIONS
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 17 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 31

Figure 7: AIRSPEED TAPE DISPLAY
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 18 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 32

Figure 8: ALTITUDE TAPE DISPLAY
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 19 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 33

Figure 9: FMS HSI DISPLAY
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 20 / 21
"DASSAULT AVIATION Proprietary Data"

### Page 34 (OCR)

DASSAULT
FALCON
F900EX EASY
AIRCRAFT MAINTENANCE MANUAL
FMS3  o In  FMS3
• Hpa  VOR
FMS2  LSS  FMS2
• Mag  SBA2
ADF1  / SV>  BRT  • Tru  Crs  71  ADF2
VOR1  FPL  © Met  OFt  / VOR  SBA1  VOR2
Off  WX  Units  / FMS  Off
E
HSI  Data  Units  CDI
(Opened HSI Control Bar)
HSI
(Closed HSI Bar)
Figure 10: HSI CONTROL BAR
Effectivity: ALL
Rev. Date: MAR 08/2017
31-60-00-710-801
page 21 / 21
"DASSAULT AVIATION Proprietary Data"

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