Dassault SB 7X-600: No revision named

FALCON 8X No 600-R1 NOVEMBER 23, 2022

ATA 00

GENERAL

ENHANCED AVIONICS SYSTEM

EASY IV

FALCON SERVICE BULLETIN Copyright © 2022 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 IV Initial issuance November 07, 2022 List of effective pages:

1 to 17 Revision 1 November 23, 2022 List of effective pages:

1 to 17 REASON: - Modification of "REASON" paragraph.

- Record compliance with DASSAULT AVIATION Service Bulletin 7X-590 "EASy III - 4TH CERT".

This revision is applicable to aircraft that have already implemented the initial issuance of this Service Bulletin.

FALCON 7X 7X -600 ATA 00

GENERAL

ENHANCED AVIONICS SYSTEM

EASY IV

1. PLANNING INFORMATION A. EFFECTIVITY This Service Bulletin is applicable to FALCON 8X aircraft with serial numbers 402 and subsequent:

• that have already implemented:

• DASSAULT AVIATION modification M1925 or Service Bulletin 7X-550 "EASy III - 3RD CERT" or subsequent equivalent Service Bulletin, and

• DASSAULT AVIATION modification M2026 or Service Bulletin 7X-535 "RDR-4000 MOD2 UPGRADE", and

• that have not previously implemented DASSAULT AVIATION Modification M2055.

B. REASON The purpose of this Service Bulletin is to upgrade the aircraft avionics to the EASy IV load 18.0 standard that includes the following features:

• an advanced version of the INAV moving map with interactive Vertical Situation Display, combined with new Vivid Displays,

• a combination of the most advanced versions of Honeywell’s NextGen FMS and Communication Management Function,

• improved Jeppesen charts function with a new Night mode, a Panoramic mode, as well as the display of the aircraft symbol on all georeferenced terminal charts (dual charts required),

• dual charts function which introduces redundancy for the use of the electronic Jeppesen charts,

• Runway Overrun Awarness and Alerting System (ROAAS) which analyzes the aircraft trajectory and the TOLD landing performance to determine if the aircraft can safely come to a full stop within the remaining runway length,

• VSA (Visual Separation on Approach) for specific traffic information relative to select traffic, to facilitate visual separation,

• enhanced ADS-B IN Cockpit Display of Traffic Information (CDTI) with 2 applications:

• Visual Separation on Approach (VSA): displays specific traffic information relative to select traffic, to facilitate visual separation,

• AIRB: displays ADS-B airborne traffic on the INAV moving map,

• enhanced TOLD function,

• weak point fix in the Falcon 7X EASy avionics architecture (equivalent to DASSAULT AVIATION Service Bulletin 7X-590 "EASy III - 4th Cert"). This weak point can lead to the display of misleading data on the display units.

FALCON 7X 7X -600 November 23, 2022 ATA 00 Revision 1 Page 1 / 17 DASSAULT AVIATION Proprietary Data

C. DESCRIPTION The operation consists in:

• modifying the aircraft wiring,

• modifying the hardware configuration:

• replacement of modules in MAU 1 and 2,

• replacement of TCAS transceiver.

• performing a full software load and an upgrade of the RDR-4000.

D. COMPLIANCE If you choose to comply with this Service Bulletin, accomplishment can be performed at your convenience.

E. APPROVAL This Service Bulletin covers DASSAULT AVIATION modifications:

• M-OPT1142, M-OPT1144 and M2055 that have been approved by EASA.

• M2035 and M2060 that have been approved under the authority of the DOA ref. EASA.21J.051.

The technical content of this document is approved under the authority of the DOA ref. 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. 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:

• U.S.A. and CANADA: 1-800-800-4036

• MEXICO: 001-800-800-4036

• Other countries: 1-201-541-4809 Email to: Customer.Care@DassaultFalconJet.com Other continents: DASSAULT AVIATION Falcon Spares 54, AVENUE MARCEL DASSAULT B.P. 24 33701 MERIGNAC Cedex (FRANCE) Telephone: 33 (0)5.56.18.44.44 FALCON 7X 7X -600 November 23, 2022 ATA 00 Revision 1 Page 2 / 17 DASSAULT AVIATION Proprietary Data

Email to: dafsorders@dassault-aviation.com Price and availability on request.

H. TOOLING - PRICE AND AVAILABILITY TOOL BOX (TO-20-008) I. WEIGHT AND BALANCE Change in weight: None.

Change in balance with respect to 25% MAC: None.

J. REFERENCES Aircraft Maintenance Manual:

• GENERAL MAINTENANCE AND SAFETY PRECAUTIONS (Refer to TASK 20-00-00-910-801)

• USE OF THE AIRCRAFT MAINTENANCE PROCEDURES (Refer to TASK 20-00-00-910-803)

• UNPLUGGING / PLUGGING OF THE MAU BACKSHELLS (Refer to TASK 20-92-00-910-801)

• INSERTION AND EXTRACTION OF A WIRE FITTED WITH A LOCK-IN CONTACT (Refer to TASK 20-95-00-910-801)

• ENERGIZATION / DE-ENERGIZATION OF THE AIRCRAFT SYSTEMS (Refer to TASK 24-00-00-860-801)

• REMOVAL / INSTALLATION OF THE POWER SUPPLY MODULES (Refer to TASK 31-41-05-900-801)

• REMOVAL / INSTALLATION OF THE PROCESSOR MODULES (Refer to TASK 31-41-09-900-802)

• OPERATIONAL TEST OF THE DATA ACQUISITION SYSTEM - MAU (Refer to TASK 31-42-00-710-801)

• REMOVAL / INSTALLATION OF THE ADVANCED GRAPHICS MODULES (AGM) (Refer to TASK 31-60-17-900-801)

• OPERATIONAL TEST OF THE WEATHER RADAR SYSTEM (Refer to TASK 34-41-00-710-801)

• OPERATIONAL TEST OF THE TRAFFIC / COLLISION AVOIDANCE SYSTEM (TCAS) (Refer to TASK 34-44-00-710-801)

• REMOVAL / INSTALLATION OF THE TCAS TRANSCEIVER (Refer to TASK 34-44-01-900-801)

• OPERATIONAL TEST OF THE ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) (Refer to TASK 34-45-00-710-801)

• 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)

• USE OF THE APM SETTINGS TOOL (Refer to TASK 45-91-00-910-801)

• REMOVAL / INSTALLATION OF THE CABIN FLOOR PANELS (Refer to TASK 53-04-01-900-801)

• OPENING / CLOSING OF THE NOSE CONE (Refer to TASK 53-10-09-860-801) FALCON 7X 7X -600 November 23, 2022 ATA 00 Revision 1 Page 3 / 17 DASSAULT AVIATION Proprietary Data

Wiring Diagram Manual:

• Refer to WD 34-23-50

• Refer to WD 34-40-00

• Refer to WD 34-45-00 DASSAULT AVIATION Service Bulletin:

• 7X-603 "LOADING THE LATEST AMI DATABASE AND SWITCHING AMI DATABASE PROVIDER" K. OTHER PUBLICATIONS AFFECTED The following publication is revised to account for the changes introduced by this Service Bulletin:

• Airplane Flight Manual revision 6 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 6,

• QRH 1 revision 6,

• QRH 2 revision 7,

• Illustrated Parts Catalog,

• Aircraft Maintenance Manual,

• Fault Isolation Manual,

• Wiring Diagram Manual.

Operational Suitability Data:

• Operational Suitability Data - Flight Crew:

• OSM-FC revision 7 or subsequent revision,

• Operational Suitability Manual - Master Minimum Equipment List:

• MMEL-CP0292-PUB.

FALCON 7X 7X -600 November 23, 2022 ATA 00 Revision 1 Page 4 / 17 DASSAULT AVIATION Proprietary Data

2. ACCOMPLISHMENT INSTRUCTIONS A. GENERAL INSTRUCTIONS AND SAFETY PRECAUTIONS

(1) Obey the general maintenance and safety precautions (Refer to TASK 20-00-00-910-801).

(2) Obey the general electrical instructions:

(a) New wires that are installed alongside existing wires should be secured with the existing clamp.

(b) Check that all connections are properly protected to ensure proper insulation, and that markings are visible and appropriate.

(c) Connector wires should be inserted and extracted as per the recommendations in Standard Practices (Refer to TASK 20-95-00-910-801).

(d) Electrical and electronic equipment should be removed and installed as per the recommendations in Standard Practices (Refer to TASK 20-00-00-910-801).

(e) Visually inspect the work area for particles or debris, then vacuum-clean the area. Blowing compressed air is prohibited since it could move metal chips into inaccessible areas.

B. PRELIMINARY STEPS

(1) The aircraft must be in the maintenance configuration (Refer to TASK 20-00-00-910-803).

(2) Open the nose cone ( 210) (Refer to TASK 53-10-09-860-801).

(3) Remove the necessary equipment and interior accommodation items to get access to cabin floors (121EZ), (121FZ), (121GZ), (131BZ) and (131CZ).

(4) Remove the cabin floors listed above (Refer to TASK 53-04-01-900-801).

(5) Remove the TCAS transceiver ( 103NP) (Refer to TASK 34-44-01-900-801).

(6) Remove the backshells from the AGM modules (2101FD), (2201FD), (2301FD) and (2401FD) (Refer to TASK 20-92-00-910-801).

(7) Remove the backshell from the EGPWS 1 module ( 101FW) (Refer to TASK 20-92-00-910-801).

(8) Check the Mod version of Power Supply modules (1101FY), (1201FY), (1301FY) and (1401FY) as follows:

(a) Remove the backshells from the power supply modules.

(b) For each power supply module, check that mod version of PN 7038248-1901 is B or higher.

NOTE: If not, the power supply module must be replaced by a PN 7038248-1901 Mod B or higher.

C. ELECTRICAL MODIFICATIONS

(1) Perform the following modification on each AGM backshell 1:

(a) Fill the new connector ( 2-fig. 1) with blanking pins.

NOTE: This new connector has no wire connected to it.

(b) Open the backshell 1.

FALCON 7X 7X -600 November 23, 2022 ATA 00 Revision 1 Page 5 / 17 DASSAULT AVIATION Proprietary Data

(c) Remove the blank backplate ( a-fig. 1).

(d) Install the connector backplate ( 1-fig. 1) and the connector (2-fig. 1).

(e) Close the backshell 1.

(2) Perform the following modification on each AGM backshell 2:

(a) Open the backshell 2.

(b) Disconnect the two wires from the backshell as per wiring diagram ( item 1-fig. 2)

(c) Cap and stow the two wires inside the backshell.

(d) Close the backshell 2.

(3) Perform the following modification on the backshell of the EGPWS 1 module ( 101FW):

(a) Open the backshell.

(b) Disconnect the two wires from the backshell as per wiring diagram ( item 2-fig. 2).

(c) Cap and stow the two wires to wiring bundle under the cabin floor.

(d) Discard the backshell.

(4) Perform the electrical modification as per wiring diagrams fig. 3 and fig. 4.

(5) Perform an electrical continuity check of the aircraft wiring.

D. HARDWARE / EQUIPMENT MODIFICATIONS

(1) Install the new TCAS transceiver ( 103NP) (Refer to TASK 34-44-01-900-801).

(2) Remove and replace the following MAU 1 modules:

• AGM modules ( 2101FD) and (2201FD) (Refer to TASK 31-60-17-900-801),

• If needed (see step 2.B.(8)), power supply modules (1101FY) or/and (1201FY) (Refer to TASK 31-41-05-900-801),

• processor 10 module (2051FY) in slot 13 in place of EGPWS 1 module (101FW) (Refer to TASK 31-41-09-900-802).

(3) Remove and replace the following MAU 2 modules:

• AGM modules ( 2301FD) and (2401FD) (Refer to TASK 31-60-17-900-801),

• If needed (see step 2.B.(8)), power supply modules (1301FY) or/and (1401FY) (Refer to TASK 31-41-05-900-801).

E. SOFTWARE LOADING CAUTION: PRIOR TO STARTING THE SOFTWARE LOADING, MAKE SURE THAT YOU HAVE ALL THE REQUIRED CD-ROMS MENTIONED IN PARAGRAPH 3.

(1) Energize the aircraft systems (Refer to TASK 24-00-00-860-801 - "Connection of the electrical ground power unit" and “Energization with the electrical ground power unit”).

(2) Record the current APM Settings configuration of the aircraft (Refer to TASK 45-91-00-910-801).

(3) Uninstall the old version of the Remote Terminal software from the client laptop.

CAUTION: USING AN INAPPROPRIATE VERSION OF CMC-RT / DLS TO LOAD THE

SOFTWARE OR DATABASE CAN LEAD TO AGM FAILURES WHICH MAY REQUIRE AGM REPLACEMENT.

FALCON 7X 7X -600 November 23, 2022 ATA 00 Revision 1 Page 6 / 17 DASSAULT AVIATION Proprietary Data

(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) 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:

CAUTION: PRIOR TO STARTING THE OPERATIONAL SOFTWARE LOADING, MAKE SURE THAT THE “CRC32” VALUE CONTAINED ON THE LOAD CD-ROM MATCHES THE CRC VALUE SHOWN ON FALCON PORTAL (REFER TO TASK 45-90-00-860-804).

SOFTWARE KEY WORD EFFECTIVITY Operational Software Top Level System Part Number EB60007394-0116 Load 18.0 All aircraft Creation of the APM Settings files:

• Create and save the APM Settings file on the hard drive using the APM Settings Tool included in the HONEYWELL EPIC Tools CD-ROM and the configuration noted previously. Use the settings.def definition file from the load 18.0 Operational Software located in the apm_defn folder.

NOTE: The create and load feature should not be used.

• Load the settings 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.text" file generated by the APM Settings Tool to keep a record of the latest settings configuration.

TT60005561-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).

18.0* LDI Refer to 7X-603 Airline Modifiable Information (AMI)database Aircraft with Datalink installed V0015* FLT (Fault Code database) All aircraft V0014* OPS (Consequences database) V0036* ECL Latest applicable version ECB PS60002397-0004* FMS AEDB PS60001004-0004* FMS MAGVAR PS60004646-003* FMS TOLD Aircraft with SB 7X-411 DS7-YYCC-RRR*

INDS EPIC AIRSPACE & COMM NAVIGATION DATA A/C without RNP-AR FALCON 7X 7X -600 November 23, 2022 ATA 00 Revision 1 Page 7 / 17 DASSAULT AVIATION Proprietary Data

SOFTWARE KEY WORD EFFECTIVITY DS8-YYCC-RRR* A/C with RNP-AR (RNP-AR=0.3 or RNP-AR<0.3) Full charts INDS Electronic Terminal Charts All aircraft DO69002412-0XXX* (EGPWF database) INDS EGPWF Data 996-0114-5XX* (envelope modulation) 996-0146-6XX* INDS Terrain server PS60001005-0015* ATC Database Aircraft with CPDLC ATN-B1 P1148 Issue 2* ACMF Optional but recommended to allaircraft for troubleshooting SWC69003872-040* EGPWF ROAAS Database All aircraft * 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).

(6) Discard all of the previous versions of the software, Options, Settings, Operator Tools and Database CD-ROMs.

(7) Due to the Operational Software to EB60007394-0116, contact INDS to request the Navigation database changes from (refer to Service Bulletin Commercial Summary):

• DS3 to DS7 for A/C without RNP-AR, or

• DS4 to DS8 for A/C with RNP-AR.

F. RDR-4000 UPGRADE

(1) Upload the RP-1 software according to HONEYWELL Service Bulletin 930-1006-34-0240 attached, paragraph 3.B.(1) "Configuration File Load on the Aircraft".

G. TESTS

(1) Perform the operational test of the TCAS system (Refer to TASK 34-44-00-710-801).

(2) Perform the test after installation relative to the following MAU modules:

• AGM modules (Refer to TASK 31-60-17-900-801)

• processor 10 and power supply modules (Refer to TASK 31-42-00-710-801)

(3) Perform the operational test of the EGPWS (Refer to TASK 34-45-00-710-801).

(4) Perform the operational test of the weather radar system (Refer to TASK 34-41-00-710-801).

H. FINAL STEPS

(1) De-energize the aircraft systems (Refer to TASK 24-00-00-860-801 - “De-energization with the electrical ground power unit” and "Disconnection of the electrical ground power unit").

(2) Install the floors listed in step 2.B.(4) (Refer to TASK 53-04-01-900-801).

FALCON 7X 7X -600 November 23, 2022 ATA 00 Revision 1 Page 8 / 17 DASSAULT AVIATION Proprietary Data

(3) Install all the interior accommodation removed for access.

(4) Close the nose cone ( 210) (Refer to TASK 53-10-09-860-801).

I. DOCUMENTATION Incorporate Airplane Flight Manual revision 6 or subsequent revision pages.

Incorporate fig. 2 in Wiring Diagram Manual chapter 34-23-50.

Incorporate fig. 3 and fig. 4 in Wiring Diagram Manual chapters 34-40-00 and 34-45-00.

J. RECORDING Record compliance with DASSAULT AVIATION Service Bulletin 7X-590 "EASy III - 4TH CERT".

Record compliance with this Service Bulletin in the appropriate aircraft documents.

Fill out the electronic Service Bulletin reply form accessible from the ”Service Bulletin" page on the Falcon portal or register SB implementation at Sbconfiguration@dassault-aviation.com, providing all useful information for aircraft identification:

• aircraft type and serial number,

• SB compliance: complete or section(s) applied,

• remarks,

• compliance date,

• service center.

FALCON 7X 7X -600 November 23, 2022 ATA 00 Revision 1 Page 9 / 17 DASSAULT AVIATION Proprietary Data

3. MATERIAL INFORMATION NOTE: Compliance with this Service Bulletin by substituting the part numbers below with interchangeable subsequent part numbers (as per the Master List or Dassault-approved supply list) is acceptable, provided that subsequent part numbers have the same effectivity as the original ones.

A. MODIFICATION OF EQUIPMENT PART NUMBER

NEW P/N QTY KEY WORD OLD P/N INSTRUCTION/DISPOSITION 60000770-1907 4 AGM module 7036410-1903 7034056-1903 1 PROC module 7028419-1904 processor 10 module (2051FY) 7038248-1901 mod B or more up to 4 Power Supply Module 7038248-1901 If needed (see step

2.B.(8)) 940-0452-001 with software version 01/04 or subsequent 1 TCAS Computer 940-0451-001 620-1974-154 1 Label, Part Number 718-1761-020 1 Configuration feature software CF card 718-1761-012 930-1006-015 with mod 2 1 RDR-4000 930-1006-012 NOTE: Refer to Service Bulletin Commercial Summary to send back the modules removed.

B. SOFTWARE

NEW CD-ROMS

NEW CD-ROMS

NEW P/N SOFTWARE KEY WORD EFFECTIVITY SUPPLIER TM7035297-107 EPIC Tools including:

• Remote Terminal - RT 33, DLS 8.7.0

• APM Settings Tool - V 3.0

• APM Restoration Tool - V 2.2 All aircraft

HONEYWELL MM7034838-020 Operational Software Top Level System Part Number EB60007394-0116 Load 18.0 TT60005561-XXXXX APM Options parameter configuration HONEYWELLthrough FALCON 7X 7X -600 November 23, 2022 ATA 00 Revision 1 Page 10 / 17 DASSAULT AVIATION Proprietary Data