# Dassault Service Bulletin 7X-600: No revision named - Rights: © Dassault Aviation. Filed by the FAA in regulations.gov docket FAA-2025-1729, the docket of AD 2025-22-05. Not covered by OpenAirDocs’ CC0 dedication. - Document: [Dassault Service Bulletin 7X-600](https://openairdocs.org/service-documents/dassault/7x-600.md) - Title as filed: SB_7X-600_R2_12-18-2023 - Pages: 38 - PDF: https://openairdocs.org/files/sha256/9d/69/9d6905e6a1030bfec5e0d52a9315322897b1a09bba29c2f310c8fadff8734fcd - Page: https://openairdocs.org/service-documents/dassault/7x-600/file/9d6905e6a103 ## Text Some pages are OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 FALCON 8X No 600-R2 DECEMBER 18, 2023 A TA 00 GENERAL ENHANCED AVIONICS SYSTEM EASY IV FALCON SERVICE BULLETIN Copyright © 2023 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. 769 ### Page 2 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. Erratum January 10, 2023 List of effective pages: 1 to 18 REASON: Note added in "APPROVAL" paragraph for aircraft not under EASA or FAA regulations. Note added in "SOFTWARE LOADING" paragraph regarding "System Config ID" pages accessibility. One item in kit P/N SBF7X0600A replaced by another in local procurement. Erratum May 12, 2023 List of effective pages: 1 to 17 REASON: Modification of INDS EPIC AIRSPACE & COMM NAVIGATION DATA effectivity. Revision 2 December 18, 2023 FALCON 7X 7X -600 ATA 00 ### Page 3 List of effective pages: 1 to 17 REASON: Addition of new equipment kit. Update of database part numbers. This revision is not applicable to aircraft that have already implemented a previous revision of this Service Bulletin. FALCON 7X 7X -600 ATA 00 ### Page 4 PAGE INTENTIONALLY LEFT BLANK FALCON 7X 7X -600 ATA 00 ### Page 5 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, • a dual charts function on aircraft already equipped with single charts, which introduces redundancy for the use of the electronic Jeppesen charts, • 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), • 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, • 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 December 18, 2023 ATA 00 Revision 2 Page 1 / 17 DASSAULT AVIATION Proprietary Data ### Page 6 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-OPT22, M-OPT640, 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. NOTE: For aircraft not under EASA and FAA regulations, please refer to the Falcon Service Advisory that lists the countries for which EASy IV is approved. 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 FALCON 7X 7X -600 December 18, 2023 ATA 00 Revision 2 Page 2 / 17 DASSAULT AVIATION Proprietary Data ### Page 7 B.P. 24 33701 MERIGNAC Cedex (FRANCE) Telephone: 33 (0)5.56.18.44.44 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) FALCON 7X 7X -600 December 18, 2023 ATA 00 Revision 2 Page 3 / 17 DASSAULT AVIATION Proprietary Data ### Page 8 • OPENING / CLOSING OF THE NOSE CONE (Refer to TASK 53-10-09-860-801) 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 December 18, 2023 ATA 00 Revision 2 Page 4 / 17 DASSAULT AVIATION Proprietary Data ### Page 9 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 P/N 7038248-1901 is B or higher. NOTE: If not, the power supply module must be replaced by a P/N 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 December 18, 2023 ATA 00 Revision 2 Page 5 / 17 DASSAULT AVIATION Proprietary Data ### Page 10 (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 SOFTWARE/DATABASES 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 December 18, 2023 ATA 00 Revision 2 Page 6 / 17 DASSAULT AVIATION Proprietary Data ### Page 11 (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). NOTE: The "System Config ID" pages to check APM Data and Database Config ID can only be accessed after all the FMS databases (FMS AEDB / Magvar / TOLD Database / INDS EPIC AIRSPACE & COMM NAVIGATION DATA) have been loaded. 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). 18.0.1* 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 FALCON 7X 7X -600 December 18, 2023 ATA 00 Revision 2 Page 7 / 17 DASSAULT AVIATION Proprietary Data ### Page 12 SOFTWARE KEY WORD EFFECTIVITY PS60004646-003* FMS TOLD Aircraft with SB 7X-411 DS7-YYCC-RRR* or DS8-YYCC-RRR* (1) INDS EPIC AIRSPACE & COMM NAVIGATION DATA (1) for operator with RNP AR OPS APPROVAL (RNP AR=0.3 or RNP AR DOWN TO RNP 0.1 APPROACH) 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 P1182 Issue 1* ACMF Optional but recommended to allaircraft for troubleshooting 69003872-040* 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, or • DS4 to DS8 for operator with RNP-AR OPS APPROVAL. 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). FALCON 7X 7X -600 December 18, 2023 ATA 00 Revision 2 Page 8 / 17 DASSAULT AVIATION Proprietary Data ### Page 13 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). (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 December 18, 2023 ATA 00 Revision 2 Page 9 / 17 DASSAULT AVIATION Proprietary Data ### Page 14 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 940-0452-001 with software version 01/04 or subsequent 1 TCAS Computer 940-0451-001 930-1006-015 with mod 2 1 RDR-4000 930-1006-012 Refer to HONEYWELL VSB 930-1006-34-0240 Kit P/N SBF7X0600B Effectivity: All aircraft Kit P/N SBF7X0600B 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 4 Power Supply Module 7038248-1901 If needed (see step 2.B.(8)) 620-1974-154 1 Label, Part Number For RDR-4000 upgrade (refer to HONEYWELL VSB 930-1006-34-0240) 718-1761-020 1 Configuration feature software CF card 718-1761-012 For RDR-4000 upgrade (refer to HONEYWELL VSB 930-1006-34-0240) NOTE: Refer to Service Bulletin Commercial Summary to send back: • the removed modules, and • the not used power supply modules (see step 2.B.(8)). FALCON 7X 7X -600 December 18, 2023 ATA 00 Revision 2 Page 10 / 17 DASSAULT AVIATION Proprietary Data ### Page 15 B. SOFTWARE NEW SOFTWARE/DATABASES NEW SOFTWARE/DATABASES 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 through DASSAULT AVIATION MM7034838-020 Operational Software Top Level System Part Number EB60007394-0116 Load 18.0 TT60005561-XXXXX APM Options parameter configuration HONEYWELL through DASSAULT AVIATION PUB: 1001 18.0.1* LDI DASSAULT AVIATION available on Falcon eData Refer to Service Bulletin 7X-603 AMI database Aircraft withDatalink installed GDC or ARINC Direct or SATCOM DIRECT PUB: 1001 V015* FLT (Fault Codedatabase) All aircraft DASSAULT AVIATION available on Falcon eData PUB: 1001 V0014* OPS (Consequences database) PUB: 1001 V0036* ECL Database Full charts INDS ElectronicTerminal Charts Integrated Navigation Data Service (INDS) EGPWF Data DO69002412-0XXX* (EGPWF Database) INDS EGPWF Data996-0114-5XX* (envelope modulation) EGPWF Terrain Server 996-0146-XXX* (terrain server) INDS Terrain server DS7 or DS7-YYCC-RRR* or INDS EPIC (1) for operatorwith RNP AR FALCON 7X 7X -600 December 18, 2023 ATA 00 Revision 2 Page 11 / 17 DASSAULT AVIATION Proprietary Data ### Page 16 NEW SOFTWARE/DATABASES NEW P/N SOFTWARE KEY WORD EFFECTIVITY SUPPLIER DS8 (1) DS8-YYCC-RRR* (1) AIRSPACE & COMM NAVIGATION DATA OPS APPROVAL (RNP AR=0.3 or RNP AR DOWN TO RNP 0.1 APPROACH) DM60004646-003 PS60004646-003* TOLD Database Aircraft with SB7X-411 HONEYWELL through DASSAULT AVIATION SWC69003872-040 69003872-040* EGPWF ROAASDatabase All aircraft HONEYWELL through DASSAULT AVIATION * 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). DATABASES REQUIRED ONLY IF NOT PREVIOUSLY PROCURED DATABASES REQUIRED ONLY IF NOT PREVIOUSLY PROCURED P/N SOFTWARE KEY WORD EFFECTIVITY SUPPLIER DM60002397-0004* PS60002397-0004* FMS AEDB All aircraft HONEYWELL through DASSAULT AVIATION DM60001004-0004* PS60001004-0004* Magvar All aircraft HONEYWELL through DASSAULT AVIATION DM60001005-0015* PS60001005-0015* ATC database Aircraft with CPDLC ATN-B1 HONEYWELL through DASSAULT AVIATION PUB: 804 Latest applicable version ECB All aircraft DASSAULTAVIATION PUB: 1001 P1182 Issue 1* ACMF Optional but recommended for AP troubleshooting DASSAULT AVIATION available on Falcon eData *or latest applicable version (the most current software and database versions which can be loaded on the aircraft are now tracked in the "SOFTWARE & DATABASES - Software & Databases Status" section of the Falcon Portal, where you will be given the most up-to-date versions depending on the aircraft configuration). FALCON 7X 7X -600 December 18, 2023 ATA 00 Revision 2 Page 12 / 17 DASSAULT AVIATION Proprietary Data ### Page 17 C. MODIFICATION KIT Kit P/N SBF7X0600A Effectivity: All aircraft Kit P/N SBF7X0600A - Electrical kit P/N QTY KEY WORD DISPOSITION/ITEM-FIG 01C0K600-22P01 3 Contact 103NPE 01C0K501-20S01 2 Contact SP2102NH1 01EQTPRL16B01 - Unused* 2 Splice SP2102NH1 01EQTPRL08R01 1 Splice SP103NPF-7K 01EQTRB23-1R 4 Soldering sleeve SP2102NH1, 103NPE 01EQTEC1-1 11 Insulation cap 01CAN203-1-24W 0.5 m Wire 01CAB211-2-24 3.5 m Wire 01CAN211-1-24 1 m Wire 103NPE-5E/SP103NPF-7K 2 Wire identification sleeve (01PR0TMS1G1-8) 103NPE-15C-15D/2102NH-32-33 2 Wire identification sleeve (01PR0TMS1G1-8) SP103NPF-7K 1 Splice identification sleeve (01PR0TMS1G3-32) 01C0A507CPC11A8-01 4 Connector backplate (1-fig. 1) 01C0F501U62BS001L 4 Connector (2-fig. 1) 01C0A54148FC22 256 Blanking pin 2101FD, 2201FD, 2301FD, 2401FD *Replaced by reference 01EQTPRL08R01 (see local procurement). D. LOCAL PROCUREMENT • Splice P/N 01EQTPRL08R01, Qty: 2 FALCON 7X 7X -600 December 18, 2023 ATA 00 Revision 2 Page 13 / 17 DASSAULT AVIATION Proprietary Data ### Page 18 (OCR) DASSAULT SERVICE BULLETIN AVIATION FALCON 7X 7X -600 001200/91 n--4-0 GAU-7-9 210148 2 Figure 1: AGM BACKSHELL December 18, 2023 ATA 00 Revision 2 Page 14 / 17 ### Page 19 (OCR) DASSAULT SERVICE BULLETIN AVIATION FALCON 7X 7X -600 2301FD 2401FD AGM2 AGM4 BEFORE MODIFICATION FOR COMPLEMENT, SEE WDM CHAP. 34-23-50 108FT *AGM3- T2201FD TERRAIN SERVER C 0 511712457_ R5511FD - 524512457-0.0 AGM1 2101FD EGPWM1 101FW TERRAIN SERVER L5511FD UNLESS OTHERWISE SPECIFIED : ALL WIRE IS AWG 24 2301FD 2401FD AFTER MODIFICATION AGM2 AGM4 INCORPORATE IN WDM, CHAP.34-23-50 ADDED ELEMENTS AGM3 2201FD TERRAN SEED T 5117/24S7 5245/24S7 R5511FD AGM1 | 2101FD O EGPWM1 101FW TERRAIN SERVED A 25 E 5131/24S7 L5511FD 125 OHM • WIRES CAPPED AND STOWED INSIDE T F WIRES CAPPED AND STOWED TO WIRING BUNDLE UNLESS OTHERWISE SPECIFIED : ALL WIRE IS AWG 24 Figure 2: WDM 34-23-50 - TERRAIN SERVER BUS WIRING MODIFICATION December 18, 2023 ATA 00 Revision 2 Page 15 / 17 ### Page 20 (OCR) DASSAULT SERVICE BULLETIN AVIATION FALCON 7X 7X -600 BEFORE MODIFICATION FOR COMPLEMENT, SEE WDM CHAP. 34-40-00 & 34-45-00 103NP 75- 5E 10A 10E TCAS/XPDR2 H 14A 14B _203J5 RA VALID DISABLE 4G PROG AUDIO LVL 6DB 7B PROG COMMON PIN OUT 7K OP ANT TOP ANTENNA 603NF 153FT BOT ANTENNA 503NP SD 31-51-00, 45-32-00 * 2102NH UNLESS OTHERWISE SPECIFIED: ALL WIRE IS AWG 24 1 THE FOUR COAXIAL MUST HAVE THE SAME LENGTH. 2 THE FOUR COAXIAL MUST HAVE THE SAME LENGTH. SHIELDED WIRES CONNECTED BY A TERMINAL JUNCTION OR SPLICE HAVE THE SHIELDING JOINED TOGETHER (THIS JUNCTION IS NOT ILLUSTRATED IN THIS WD) - 77J/P LH FR1 BASIC ELEC CUT-OFF CONNECTOR F1, LH - 751J BASIC/OPTION CUT-OFF CONNECTOR CABIN AREA, F14 UNDER FLOOR, RH - 103NP TCAS TRANSCEIVER F12-16, UNDER CABIN FLOOR, LH - 603NP UPPER TCAS ANTENNA F12-30, OVER CABIN FLOOR, LH - 503NP LOWER TCAS ANTENNA F26-27, FUEL EQUIPMENT BAY - 2102NH ADAHRS UNIT F8-12, UNDER CABIN FLOOR, LH - 203J TERMINAL STRIP F8-9, OVER FLOOR, LH CABINET Figure 3: WDM 34-40-00 & 34-45-00 - BEFORE WIRING MODIFICATION December 18, 2023 ATA 00 Revision 2 Page 16 / 17 ### Page 21 (OCR) DASSAULT SERVICE BULLETIN AVIATION FALCON 7X 7X -600 INCORPORATE IN WDM, CHAP.34-40-00 & 34-45-00 AFTER MODIFICATION 103NP FOR COMPLEMENT, SEE WDM CHAP. 34-40-00 & 34-45-00 751 10A 10E 2102NH-32-33 TCAS/XPDR2 H 14A 14B} 103NPE-5E/SP103NPF-7K 203J5 RA VALID DISABLE 4G PROG AUDIO LVL 6DB 7B PROG COMMON PIN OUT SP103NPF-7K 'OP ANT TOP ANTENNA 603NP 153FT BOT ANTENNA 503NP SD 31-51-00, 45-32-00 * 2102NH UNLESS OTHERWISE SPECIFIED : ALL WIRE IS AWG 24 ADDED ELEMENTS 1 THE FOUR COAXIAL MUST HAVE THE SAME LENGTH. MODIFIED ELEMENTS 2) THE FOUR COAXIAL MUST HAVE THE SAME LENGTH. SHIELDED WIRES CONNECTED BY A TERMINAL JUNCTION OR SPLICE HAVE THE SHIELDING JOINED TOGETHER (THIS JUNCTION IS NOT ILLUSTRATED IN THIS WD) - 77J/P LH FR1 BASIC ELEC CUT-OFF CONNECTOR F1, LH - 751J BASIC/OPTION CUT-OFF CONNECTOR CABIN AREA, F14 UNDER FLOOR, RH - 103NP TCAS TRANSCEIVER F12-16, UNDER CABIN FLOOR, LH - 603NP UPPER TCAS ANTENNA F12-30, OVER CABIN FLOOR, LH - 503NP LOWER TCAS ANTENNA F26-27, FUEL EQUIPMENT BAY - 2102NH ADAHRS UNIT F8-12, UNDER CABIN FLOOR, LF - 203J TERMINAL STRIP F8-9, OVER FLOOR, LH CABINET Figure 4: WDM 34-40-00 & 34-45-00 - AFTER WIRING MODIFICATION December 18, 2023 END OF DOCUMENT ATA 00 Revision 2 Page 17 / 17 ### Page 22 (OCR) Honeywell Honeywell International Inc. 15001 N.E. 36 Street Redmond, Washington 98052-6450 U.S.A. CAGE: 97896 Telephone: 800-601-3099 (Toll Free U.S.A./Canada) Telephone: 602-365-3099 (International Direct) Website: https://aerospace.honeywell.com SERVICE BULLETIN NAVIGATION - RP-1 RADAR PROCESSOR (RP-1) - CONVERSIONS OF PN 930-1006-010/-012 TO PN 930-1006-015 Legal Notice Export Control These items are controlled by the U.S. government and authorized for export only to the country of ultimate destination for use by the ultimate consignee or end-users) herein identified. They may not be resold, transferred, or otherwise disposed of, to any other country or to any person other than the authorized ultimate consignee or end-user(s), either in their original form or after being incorporated into other items, without first obtaining approval from the U.S. government or as otherwise authorized by U.S. law and regulations. ECCN: 6E991. Proprietary Information HONEYWELL - CONFIDENTIAL COPYRIGHT BY HONEYWELL INTERNATIONAL INC. ("HONEYWELL"). ALL RIGHTS RESERVED. THIS DOCUMENT AND ALL INFORMATION CONTAINED HEREIN ARE THE CONFIDENTIAL AND PROPRIETARY INFORMATION OF HONEYWELL AND CONTAIN HONEYWELL TRADE SECRETS. NEITHER THIS DOCUMENT NOR THE INFORMATION CONTAINED HEREIN MAY, IN WHOLE OR IN PART, BE USED, DUPLICATED, OR DISCLOSED FOR ANY PURPOSE WITHOUT PRIOR WRITTEN PERMISSION OF HONEYWELL. PLEASE REVIEW THE TERMS OF THIS AGREEMENT CAREFULLY BEFORE USING THIS DOCUMENT, AS BY USING IT, YOU ACKNOWLEDGE THAT YOU HAVE REVIEWED THIS AGREEMENT AND AGREE TO BE BOUND BY ITS TERMS AND CONDITIONS. 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 1 of 17 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 23 (OCR) Honeywell SERVICE BULLETIN 930-1006 HONEYWELL MATERIALS LICENSE AGREEMENT This document and the information contained herein ("the Materials") are the proprietary data of Honeywell. These Materials are provided for the exclusive use of Honeywell-authorized Service Centers; Honeywell-authorized repair facilities; owners of a Honeywell aerospace product that is the subject of these Materials ("Honeywell Product) that have entered into a written agreement with Honeywell relating to the repair or maintenance of Honeywell Product; and direct recipients of Materials from Honeywell via https://aerospace.honeywell.com/en/learn/about-us/about-myaerospace that own a Honeywell Product. The terms and conditions of this Honeywell Materials License Agreement ("License Agreement") govern your use of these Materials, except to the extent that any terms and conditions of another applicable agreement with Honeywell regarding the maintenance or repair of a Honeywell Product and that is the subject of the Materials conflict with the terms and conditions of this License Agreement, in which case the terms and conditions of the other agreement will govern. The terms of this License Agreement supersede any other Material License Agreement previously provided with the Materials, regardless of what form the Materials were provided, including without limitation when received in hard copy, downloaded via the MyAerospace portal or CD-ROM. However, this License Agreement will govern in the event of a conflict between these terms and conditions and those of a purchase order or acknowledgement. Your access or use of the Materials represents your acceptance of the terms of this License Agreement. 1. License Grant - If you are a party to an applicable written agreement with Honeywell relating to the repair or maintenance of the subject Honeywell Product, subject to your compliance with the terms and conditions of this License Agreement, Honeywell hereby grants you, and you accept, a limited, personal, non-transferrable, non-exclusive license to use these Materials only in accordance with that agreement. If you are a direct recipient of these Materials from Honeywell's MyAerospace Technical Publication website and are not a party to an agreement related to the maintenance or repair of the subject Honeywell Product, subject to your compliance with the terms and conditions of this License Agreement, Honeywell hereby grants you, and you accept, a limited, personal, non-transferrable, non-exclusive license to use a single copy of these Materials to maintain or repair only the subject Honeywell Product installed or intended to be installed on the aircraft you own and/or operate and only at the facility to which these Materials have been shipped ("the Licensed Facility"). Transfer of the Materials to another facility owned by you is permitted only if the original Licensed Facility retains no copies of the Materials, the transferee accepts all of your obligations and liabilities under this License Agreement, and you provide prior written notice to Honeywell with the name and address of the transferee. You agree not to use these Materials for commercial purposes. 2. Restrictions on Use - You may not sell, rent, lease, or (except as authorized under any applicable airworthiness authority regulation) lend the Materials to anyone for any purpose. You may not use the Materials to reverse engineer any Honeywell product, hardware or software, and may not decompile or disassemble software provided under this License Agreement, except and only to the extent that such activity is expressly permitted by applicable law notwithstanding this limitation. You may not create derivative works or modify the Materials in any way. You agree that Materials shall only be used for the purpose of the rights granted herein. The Material furnished hereunder may be subject to U.S. export regulations. You will adhere to all U.S. export regulations as published and released from time to time by the U.S. Government. You may not design or manufacture a Honeywell part or detail of a Honeywell part, to create a repair for a Honeywell part, design or manufacture any part that is similar or identical to a Honeywell part, compare a Honeywell part or design of a Honeywell part to another part design, or apply for FAA PMA or other domestic or foreign governmental approval to manufacture or repair a Honeywell part. Honeywell International Inc. and its affiliates comply fully with all applicable export control laws and regulations of the United States and of all countries where it conducts business. In order to satisfy US export control laws, you confirm that you are not an entity that meets the definition of a military end user in China, Russia, or Venezuela ("Military End User") or sells items that support or contribute to a Military End Use by a Military End User. Military End User includes any entity that is part of the national armed services (army, navy, marine, air force, or coast guard), as well as the national guard and national police, government intelligence or reconnaissance organizations, 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 2 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 24 (OCR) Honeywell SERVICE BULLETIN 930-1006 or any person or entity whose actions or functions are intended to support "military end uses." "Military End Uses" includes use of an item to support or contribute to the operation, installation, maintenance, repair, overhaul, refurbishing, development, or production of military items. In addition, you will not divert or in any way utilize or sell Honeywell products, materials, technology, or technical data to any entity that is a Chinese, Russian, or Venezuelan Military End User or for Military End Uses, as stated above. You shall immediately notify Honeywell and cease all activities associated with the transaction in question if it knows or has a reasonable suspicion that the products, materials, technical data, plans, or specifications may be exported, reexported, or transferred in support of a prohibited Military End Use or to a Military End User. Failure to comply with this provision is a material breach of your order and agreement with Honeywell and Honeywell is entitled to immediately seek all remedies available under law and in equity (including without limitation, termination), without any liability to Honeywell. 3. Rights In Materials - Honeywell retains all rights in these Materials and in any copies thereof that are not expressly granted to you, including all rights in patents, copyrights, trademarks, and trade secrets. The Materials are licensed and not sold under this License Agreement. No license to use any Honeywell trademarks or patents is granted under this License Agreement. 4. Changes - Honeywell reserves the right to change the terms and conditions of this License Agreement at any time, including the right to change or impose charges for continued use of the Materials. Honeywell may add, delete or otherwise modify any portion of the Materials ("Updated Materials) at any time. You agree to stop using outdated Materials upon issuance of any Updated Materials. 5. Confidentiality - You acknowledge that these Materials contain information that is confidential and proprietary to Honeywell. You agree to take all reasonable efforts to maintain the confidentiality of these Materials. 6. Assignment and Transfer - This License Agreement may be assigned to a service center approved and formally designated as a service center by Honeywell, provided, however, that you retain no copies of the Materials in whole or in part. However, the recipient of any such assignment or transfer must assume all of your obligations and liabilities under this License Agreement. No assignment or transfer shall relieve any party of any obligation that such party then has hereunder. Otherwise, neither this License Agreement nor any rights, licenses or privileges granted under this License Agreement, nor any of its duties or obligations hereunder, nor any interest or proceeds in and to the Materials shall be assignable or transferable (in insolvency proceedings, by merger, by operation of law, by purchase, by change of control or otherwise) by you without Honeywell's written consent. 7. Copies of Materials - Unless you have the express written permission of Honeywell, you may not make or permit making of copies, digital or printed, of the Materials. You agree to return the Materials and any such copies thereof to Honeywell upon the request of Honeywell. 8. Term - This License Agreement is effective until terminated as set forth herein. This License Agreement will terminate immediately, without notice from Honeywell, if you fail to comply with any provision of this License Agreement or will terminate simultaneously with the termination or expiration of your applicable agreement with Honeywell relating to the repair or maintenance of the subject Honeywell Product. Upon termination of this License Agreement, you will return these Materials to Honeywell without retaining any copies, in whole or in part, and will have one of your authorized officers certify that all Materials have been returned with no copies retained. 9. Audit Rights - Honeywell, through its authorized representatives, with no less than thirty (30) calendar days notice from Honeywell, has the right during normal business hours during the term of this License Agreement and for three (3) years thereafter to visit you and have access to the inside and outside of your facility for the purpose of inspecting, observing and evaluating your compliance under this License Agreement. 10. Remedies - Honeywell reserves the right to pursue all available remedies and damages resulting from a breach of this License Agreement. 11. Limitation of Liability - Honeywell makes no representations or warranties regarding the use or sufficiency of the Materials. THERE ARE NO OTHER WARRANTIES, WHETHER WRITTEN OR ORAL, EXPRESS, IMPLIED OR STATUTORY, INCLUDING, BUT NOT LIMITED TO (i) WARRANTIES ARISING FROM COURSE OF 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 3 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 25 (OCR) Honeywell SERVICE BULLETIN 930-1006 PERFORMANCE, DEALING, USAGE, OR TRADE, WHICH ARE HEREBY EXPRESSLY DISCLAIMED, OR (ii) WARRANTIES AGAINST INFRINGEMENT OF INTELLECTUAL PROPERTY RIGHTS OF THIRD PARTIES, EVEN IF HONEYWELL HAS BEEN ADVISED OF ANY SUCH INFRINGEMENT. IN NO EVENT WILL HONEYWELL BE LIABLE FOR ANY INCIDENTAL DAMAGES, CONSEQUENTIAL DAMAGES, SPECIAL DAMAGES, INDIRECT DAMAGES, LOSS OF PROFITS, LOSS OF REVENUES, OR LOSS OF USE, EVEN IF INFORMED OF THE POSSIBILITY OF SUCH DAMAGES. TO THE EXTENT PERMITTED BY APPLICABLE LAW, THESE LIMITATIONS AND EXCLUSIONS WILL APPLY REGARDLESS OF WHETHER LIABILITY ARISES FROM BREACH OF CONTRACT, WARRANTY, INDEMNITY, TORT (INCLUDING BUT NOT LIMITED TO NEGLIGENCE), BY OPERATION OF LAW, OR OTHERWISE. 12. Controlling Law - This License Agreement shall be governed and construed in accordance with the laws of the State of New York without regard to the conflict of laws provisions thereof. 13. Severability - In the event any provision of this License Agreement is determined to be illegal, invalid, or unenforceable, the validity and enforceability of the remaining provisions of this License Agreement will not be affected and, in lieu of such illegal, invalid, or unenforceable provision, there will be added as part of this License Agreement one or more provisions as similar in terms as may be legal, valid and enforceable under controlling law. 14. Integration and Modification - This License Agreement sets forth the entire agreement and understanding between the parties on the subject matter of the License Agreement and merges all prior discussions and negotiations among them. Safety Advisory WARNING: BEFORE THE MATERIALS CALLED OUT IN THIS PUBLICATION ARE USED, KNOW THE HANDLING, STORAGE AND DISPOSAL PRECAUTIONS RECOMMENDED BY THE MANUFACTURER OR SUPPLIER. FAILURE TO OBEY THE MANUFACTURERS' OR SUPPLIERS' RECOMMENDATIONS CAN RESULT IN PERSONAL INJURY OR DISEASE. This publication describes physical and chemical processes which can make it necessary to use chemicals, solvents, paints, and other commercially available materials. The user of this publication must get the Safety Data Sheets (OSHA Hazard Communication Standard (HCS) 29 CFR 1910.1200(g) or equivalent) from the manufacturers or suppliers of the materials to be used. The user must know the manufacturer/ supplier data and obey the procedures, recommendations, warnings and cautions set forth for the safe use, handling, storage, and disposal of the materials. Warranty/Liability Advisory WARNING: WARNING: HONEYWELL ASSUMES NO RESPONSIBILITY FOR ANY HONEYWELL EQUIPMENT WHICH IS NOT MAINTAINED AND/OR REPAIRED IN ACCORDANCE WITH HONEYWELL'S PUBLISHED INSTRUCTIONS AND/OR HONEYWELL'S FAA/ODA REPAIR AUTHORIZATION. NEITHER DOES HONEYWELL ASSUME RESPONSIBILITY FOR SPECIAL TOOLS AND TEST EQUIPMENT FABRICATED BY COMPANIES OTHER THAN HONEYWELL. WARNING: INCORRECTLY REPAIRED COMPONENTS CAN AFFECT AIRWORTHINESS OR DECREASE THE LIFE OF THE COMPONENTS. INCORRECTLY FABRICATED SPECIAL TOOLING OR TEST EQUIPMENT CAN RESULT IN DAMAGE TO THE PRODUCT COMPONENTS OR GIVE UNSATISFACTORY RESULTS. Copyright - Notice Copyright 2022 Honeywell International Inc. All rights reserved. Honeywell is a registered trademark of Honeywell International Inc. All other marks are owned by their respective companies. 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 4 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 26 (OCR) Honeywell SERVICE BULLETIN 930-1006 Transmittal Information ATA Number 930-1006-34-0240 (Publication Number D202202002219) Summary This revision is a FULL replacement. This revision includes the changes that follow: • Updated Paragraph 1.F.(1). • Updated CMM 34-41-68 revision number from "7" to "9" in Paragraph 1.K. (2). • Updated CMM 34-41-68 revision number from "7" to "9" in Paragraph 1 .L. (1). • Added Paragraph 3.B.(1)(a)5. • Added TSO Acronym in Table 4. The information that is identified with revision bars is listed in the Revision History section. Revision bars are not used before Paragraph 1.A. The editorial changes and information that was moved, removed, or reformatted are not identified with revision bars. Refer to Paragraph 4.A. for a list of the acronyms and abbreviations used in this service bulletin. Revision History This service bulletin has had one revision(s) as shown in Table 1. Table 1. Revision History Revision Number Revision Date 23 Mar 2022 1 Nov 2022 Highlights This section issues Revision 1 to Service Bulletin, ATA Number 930-1006-34-0240 (Publication Number D202202002219), and contains these changes: The list of highlights tells the users about the changes that the revision makes. The list has three columns. The "Page" column shows the block of data that the revision changes and the page on which the block begins. The block can be a section, subsection, graphic, table, etc. Revision marks give the location of the change in the block. The "Description" column tells the user about the change or changes in each block. A paragraph, table, or figure reference often comes before the description. The "Effectivity" column tells the user about the part number(s) to which the block of information applies. The default value for this column is "All." "All" means that the block applies to all parts. Page Description Effectivity Paragraph 1.F. (1) . Updated Paragraph. All Paragraph 1.K. (2) . Updated CMM 34-41-68 revision number from "7" to "9". All 8 Paragraph 1.L. (1) . Updated CMM 34-41-68 revision number from "7" to "9". All 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 5 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 27 (OCR) Honeywell SERVICE BULLETIN 930-1006 Page Description Effectivity 13 Paragraph 3.B. (1)(a)5 . Added Paragraph. All 16 Paragraph 4.A. (1) . Added TSO Acronym in Table 4. All 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 6 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 28 (OCR) Honeywell SERVICE BULLETIN 930-1006 Planning Information Effectivity (1) This service bulletin is applicable to the RP-1 PN 930-1006-010/-012 SW MOD 1, 2. B. Concurrent Requirements (1) Not applicable. C. Reason (1) This conversion is to use update AGM software with hazard display. D. Description (1) A summary of the work necessary to do this conversion is given below: (a) The new configuration file is loaded in to the RP-1. NOTE: This is a configuration file change only. The RP-1 is not disassembled and the inspection seals are not broken. NOTE: This conversion can be done at a shop location or at a customer location (in the aircraft). E. Compliance (1) This is a must to do conversion to be used on EASy IV configuration. F. Approval (1) This service bulletin has been reviewed by the Honeywell Radar Systems FAA TSO Specialist. The conversion information herein meets the requirement of TSO. G. Manpower (1) This conversion can be completed in the approximate times that follow: (a) If this conversion is done at a customer location (in the aircraft): • 0.5 hour for the labor to convert to the PN 930-1006-015. NOTE: The time identified above does not include the time to get access to the RP-1 on the aircraft. (b) If this conversion is done at a shop location: • 0.5 hour for the labor to do the modification of the RP-1 • 2.0 more hours for the labor to do a test of the RP-1. H. Weight and Balance (1) None. 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 7 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 29 (OCR) Honeywell SERVICE BULLETIN 930-1006 Electrical Load Data (1) Not applicable. Software Accomplishment Summary (1) A software accomplishment summary has been completed to agree with the necessary conditions of RTCA document DO-178B, Software Considerations in Airborne Systems and Equipment Certification. K. References (1) To find, see, and download Honeywell Technical Publications, go to https://aerospace.honeywell.com. (2) The document that follows is necessary to complete this conversion. Unless specified differently, you can use subsequent revisions. • CMM, ATA Number 34-41-68 (Publication Number 012-0746-001), Revision 9 or Latest, RP-1 Radar Processor. Other Publications Affected (1) CMM, ATA Number 34-41-68 (Publication Number 012-0746-001), Revision 9 or Latest, RP-1 Radar Processor, will be revised because of this service bulletin. (2) This service bulletin has no effect on the test procedure. M. Interchangeability or Intermixability of Parts (1) The operator must speak to the OEM about the interchangeability and intermixability of the RP-1 part numbers identified in this service bulletin. 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 8 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 30 (OCR) Honeywell SERVICE BULLETIN 930-1006 2. Material Information Material - Price and Availability (1) For available parts, supply times, necessary test documentation, applicable test material prices, and repair support information, go to: https://aerospace.honeywell.com. Registered users can enter their Honeywell ID and password. New users must register to create a Honeywell ID. NOTE: To speak with Honeywell personnel: Honeywell Aerospace Contact Team Telephone: 800-601-3099 (Toll Free U.S.A./Canada) Telephone: 602-365-3099 (International Direct) (2) This conversion can be done at a Honeywell service center, Honeywell-authorized repair location or in the aircraft for the price given at the time of the order. (3) Honeywell can supply the parts necessary to do this conversion. The price for parts will be given at the time of the order. When you make an order for parts, send a purchase order that refers to this service bulletin, ATA Number 930-1006-34-0240 (Publication Number D202202002219). The purchase order must include only the applicable parts specified in Table 2 of this service bulletin. Industry Support Information (1) Honeywell will give no reimbursement to do this conversion. The customer will receive an applicable invoice for the conversion of each RP-1 radar processor done at a Honeywell service center or Honeywell-authorized repair location. C. Material Necessary for Each Component (1) The parts identified in Table 2 are necessary to do this service bulletin. Table 2. Operator-Purchased Material Instructions/ Keyword/ List Disposition New PN2, 3, 4 Nomenclature Old PN Qty Price' Codes 620-1974-154 Label, Part Number 620-1956-138/620-1974-136 1 F 718-1761-020 Configuration 718-1761-012 1 Features List File NOTES: 1. The list price is applicable to the parts that Honeywell has available at the time of the order. Refer to the Honeywell, Aerospace Contact Team (Paragraph 2.A.) for the applicable material prices, available parts, supply times, and minimum order quantities. 2. Refer to the Honeywell Aerospace Contact Team (Paragraph 2.A.) when you need data about available parts, supply times, or minimum order quantities. 3. Different supply-times are necessary to supply the parts. Honeywell Aerospace Contact Team (Paragraph 2.A.) or your local Honeywell service center for schedules, applicable prices, and available parts. 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 9 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 31 (OCR) Honeywell SERVICE BULLETIN 930-1006 4. The customer or local regulatory authority can make decisions about what to do with the used parts. Discard or erase the used software and do not use it again. Table 3. Instructions/Disposition Codes Code Description Disposition Code F Discard the removed part and replace with a new part. D. Material Necessary for Each Spare (1) Same as Paragraph 2.C. E. Reidentified Parts (1) Not applicable. F. Tooling - Price and Availability (1) The equipment that is necessary to do this conversion is specified in the documents given in Paragraph 1.K. of this service bulletin. 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 10 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 32 (OCR) Honeywell SERVICE BULLETIN 930-1006 3. Accomplishment Instructions A. General WARNING: TO AVOID INJURY TO PERSONNEL, BE AWARE THAT VOLTAGES ARE PRESENT IN THE UNIT AND IN THE TEST EQUIPMENT. VOLTAGES AS LOW AS 28 VOLTS CAN CAUSE SERIOUS INJURY UNDER SOME CONDITIONS. DO NOT BE MISLED BY THE TERM "LOW VOLTAGE." WARNING: BEFORE YOU USE A MATERIAL, REFER TO THE MANUFACTURER'S MATERIAL SAFETY DATA SHEETS. SOME MATERIALS CAN BE DANGEROUS. CAUTION: DO NOT USE A MATERIAL THAT IS NOT EQUIVALENT TO THE MATERIAL SPECIFIED BY HONEYWELL. A MATERIAL THAT IS NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN MAKE THE WARRANTY NOT APPLICABLE. CAUTION: THE RP-1 CONTAINS ELECTROSTATIC DISCHARGE SENSITIVE ITEMS. USE INDUSTRY APPROVED PRECAUTIONS. (1) Obey the precautions. (2) Refer to the RP-1 CMM, ATA Number 34-41-68 (Publication Number 012-0746-001), for procedures and precautions. Use all CAUTIONS and WARNINGS. Refer to the IPL in the CMM for the location of the parts, unless specified differently. (3) Keep all hardware for use in assembly unless specified differently. (4) Obey standard established shop practices during conversion of the RP-1 unless specified differently. (5) When the compact flash card is used for dataloading, the system automatically uploads the software from the card into system memory. When the flash card is detected the only functions that the RP-1 will perform are those of uploading software. (6) This is a configuration file change only. The RP-1 is not disassembled and the inspection seals are not broken. (7) This conversion can be done at a shop location or at a customer location (in the aircraft). (8) Paragraph 3.B. (1) is applicable for the installation of this conversion in RP-1 units when the installation is performed on the aircraft. (9) Paragraph 3.B. (2) is applicable for the installation of this conversion in RP-1 units when the installation is performed at a service center. 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 11 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 33 (OCR) Honeywell SERVICE BULLETIN 930-1006 B. Procedure WARNING: MAKE SURE ALL PERSONNEL AND OBJECTS ARE AT A SAFE DISTANCE FROM THE ANTENNA DRIVE ASSEMBLY SCAN VOLUME. NOTE: Complete the instructions in Paragraph 3.B. one time for each unit. (1) Configuration File Load on the Aircraft (a) Configuration Assembly Load 1 Make sure the RDR-4000 is not transmitting by verifying the radar is in "Standby". Make sure no power is applied to the RP. Put the configuration feature software CF card, PN 718-1761-020, in the vertical slot under the right port cover. The right port cover is on the front panel of the RP. Refer to Figure 1. DISPLAY / MODIFICATION LEFT PORT DOTS LABEL COVER - RIGHT PORT COVER SW/VERSION DATABASE LABEL • SERIAL NUMBER LABEL • PART NUMBER LABEL PNR 930-1003-RXX ICN-97896-0000382486-001-01 Figure 1. RP-1 Radar Processor, Front View Apply power to the RP. 4 The transfer process can take up to 2 minutes. This can change when the amount of data to be uploaded changes. The data load is complete when the LCD shows the message "Upload Successful". If "Upload Fail", or "Invalid Card" appear then return to Paragraph 3.B. (1)(a)1 in this section. If a proper load is not achevied after a few attempts send the RP to Honeywell for repair. 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 12 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 34 (OCR) Honeywell SERVICE BULLETIN 930-1006 5 When the data load is complete, remove power from the RP-1 and extract the CF card. (b) Data Load Check NOTE: The instructions in this paragraph use the RP-1 front panel display to make sure the software part numbers are correct. Refer to Figure 1 for the location of the RP-1 front panel display. During data load check, make sure the RDR-4000 is not transmitting by verifying the radar is in "Standby" mode. 1 Apply power to the RP. Press the scroll button. Scroll to the word CONFIGURATION. Press Select to make a selection of the CONFIGURATION. Press the scroll button. Scroll to the RP/IOP config. Press select for the RP/IOP config. 4 You will see the RP SER and PNR. 5 Press the scroll button until you see APP, the number should be one of PN 996-4061-504/-505/-506/-507. Press the scroll button until you see DB, the number should be PN 996-1232-547. Select NEXT to get to the RP/MP Config. Press the scroll button until you see APP, the number should be one of PN 996-4061-504/-505/-506/-507. Press the scroll button until you see DB, the number should be PN 996-0175-502. 10 Press the scroll button until you see CFG, this number should be PN 996-4061-707. 11 Select NEXT to get to the TR. 12 Press the scroll button until you see APP, the number should be one of PN 996-4061-504/-505/-506/-507. 13 Select NEXT to get to the DA. 14 Press the scroll button until you see APP, the number should be one of PN 996-4061-504/-505/-506/-507. (c) Replacement of Label 1 Remove the power from all of the equipment. Replace part number label with PN 620-1974-154 for PN 930-1006-015. 23 Mar 2022 930-1006-34-0724013 Revision 1, 1 Nov 2022 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 35 (OCR) Honeywell SERVICE BULLETIN 930-1006 (2) Configuration File Load at a Service Center (a) Configuration Assembly Load 1 Make sure no power is applied to the RP. Put the configuration feature software CF card, refer to Table 2 the CF card part number, in the vertical slot under the right port cover. The right port cover is on the 2 Apply power to the RP. 3 The transfer process can take up to 2 minutes. This can change when the amount of data to be uploaded changes. The data load is complete when the LCD shows the message "Upload Successful", "Upload Fail", or "Invalid Card". Any other text means that the transfer is still in work. (b) Data Load Check NOTE: The instructions in this paragraph use the RP-1 front panel display to make sure the software part numbers are correct. Refer to Figure 1 for the location of the RP-1 front panel display. 1 Apply power to the RP-1. Press the scroll button. Scroll to the word CONFIGURATION. Press Select to make a selection of the CONFIGURATION. Press the scroll button. Scroll to the RP/IOP. Select the RP/OP. Press the select button to see the IOP part numbers. 5 Scroll through the part numbers. Scroll to the line that starts with APP. Make sure the part number on this line is one of the SW PN 996-4061-504/-505/-506/-507. Scroll to the line that starts with DB. 9 Make sure the part number on this line is PN 996-1232-547. 10 Select NEXT to get to the RP/MP. 11 Scroll to the line that starts with APP. 12 Make sure the part number on this line is one of the SW PN 996-4061-504/-505/-506/-507. 13 Scroll to the line that starts with DB. 14 Make sure the part number on this line is PN 996-0175-502. 15 Scroll to the line that starts with CFG, this number should be PN 996-4061-707. NOTE: If the RP-1 does not have the correct part numbers as verified in this section, go to the applicable section and repeat the instructions to upload the correct software. 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 14 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 36 (OCR) Honeywell SERVICE BULLETIN 930-1006 (c) Replacement of Label 1 Remove the power from all of the equipment. Replace part number label with PN 620-1974-154 for PN 930-1006-015. C. Test (1) Do a test of the RP-1. Refer to the instructions in the TESTING AND FAULT ISOLATION section of the CMM 34-41-68. 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 15 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 37 (OCR) Honeywell SERVICE BULLETIN 930-1006 4. Appendix A. Appendix A, Acronyms and Abbreviations (1) Refer to Table 4 for a list of the acronyms and abbreviations used in this service bulletin. Table 4. Acronyms and Abbreviations Term Full Term ATA Air Transport Association CAGE Commercial and Government Entity CF Compact Flash CFG Configuration CFR Code of Federal Regulations CMM Component Maintenance Manual DA Drive Assembly ECCN Export Control Classification Number FAA Federal Aviation Administration HCS Hazard Communication Standard NID Identification Inc. Incorporated IPL Illustrated Parts List LCD Liquid Crystal Display LRU Line Replaceable Unit MOD Modification OEM Original Equipment Manufacturer OSHA Occupational Safety and Health Administration PMA Parts Manufacturer Approval PN Part Number PNR Part Number Qty Quantity RP Radar Processor RTCA Radio Technical Commission for Aeronautics SER Serial SW Software TR Transmitter Receiver TSO Technical Standard Order 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 16 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. ### Page 38 (OCR) Honeywell SERVICE BULLETIN 930-1006 Appendix B, Customer Support Service Report (1) If the modification given in this service bulletin is done at a location other than a Honeywell service center, complete the CSSR. LRU/SRU Model/Nomenclature: RP-1 radar processor * LRU/SRU Part No. (Before modification): * LRU/SRU Part No. (After modification): * LRU/SRU Serial Number: * Hardware/Software MOD Level (Before modification): * Hardware/Software MOD Level (After modification): Aircraft Type, Serial Number, Tail Number: * End User Company Name: Company Address: * Service Provider Person to Contact: Company Name: Company Address: Company Phone No.: Date of modification: * Required Information Fields Honeywell Internal Use Only SAR Number.: QDS Customer Number.: Honeywell Mail or Fax Aerospace Electronic Systems Attn: Order Management Completed Form to: P.O. Box 21111 Phoenix, AZ 85036-1111 FAX: 1-602-822-7272 23 Mar 2022 930-1006-34-0240 Revision 1, 1 Nov 2022 Page 17 Publication Number D202202002219 © Honeywell International Inc. Do not copy without express permission of Honeywell. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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