Dassault SB F2000EX-322: Revision 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.

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.

FALCON 2000EX F2000EX -322 F2000EX -00-19

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 FALCON 2000EX F2000EX -322 June 21, 2017 F2000EX -00-19 Revision 1 Page 5 / 14 DASSAULT AVIATION Proprietary Data

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) FALCON 2000EX F2000EX -322 June 21, 2017 F2000EX -00-19 Revision 1 Page 6 / 14 DASSAULT AVIATION Proprietary Data

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 FALCON 2000EX F2000EX -322 June 21, 2017 F2000EX -00-19 Revision 1 Page 7 / 14 DASSAULT AVIATION Proprietary Data

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) FALCON 2000EX F2000EX -322 June 21, 2017 F2000EX -00-19 Revision 1 Page 8 / 14 DASSAULT AVIATION Proprietary Data

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 FALCON 2000EX F2000EX -322 June 21, 2017 F2000EX -00-19 Revision 1 Page 9 / 14 DASSAULT AVIATION Proprietary Data

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 “Deenergization 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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