# Sikorsky Alert Service Bulletin 76-31-4 Copy: Revision A ("Sikorsky ASB 76-31-4 Rev A"), 40 pages: PDF https://openairdocs.org/files/sha256/23/3b/233b0ce7ee280085f0e921353792b5416b3cf1da117db19e760aa93c03507035; text https://openairdocs.org/service-documents/sikorsky/sb-76-31-4/file/233b0ce7ee28.md. Rights: © Sikorsky. Filed by the FAA in regulations.gov docket FAA-2020-0212; AD 2020-15-17 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. ## Details - Manufacturer: [Sikorsky](https://openairdocs.org/service-documents/sikorsky.md) - Type: Service bulletin (Alert Service Bulletin) - Number: 76-31-4 - Latest revision known: 76-31-4, Revision A, dated May 30, 2018 (OpenAirDocs) - Page: https://openairdocs.org/service-documents/sikorsky/sb-76-31-4 ## ADs that cite it (1) (OpenAirDocs) Newest first, with the revision each names, as OpenAirDocs read it from the AD's text. - [AD 2020-15-17](https://openairdocs.org/ad/2020-15-17.md), effective Sep 9, 2020: Revision A Also cited in [1 proposed AD](https://openairdocs.org/service-documents/sikorsky/sb-76-31-4/proposed.md). ## Text (40 pages) Rights: © Sikorsky. Filed by the FAA in regulations.gov docket FAA-2020-0212; AD 2020-15-17 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. 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 ATA 31-60-01 SOFTWARE UPDATE S-76® HELICOPTER ALERT SERVICE BULLETIN NOTICE TO ALL PERSONS RECEIVING THIS DOCUMENT: WARNING: THIS DOCUMENT, OR AN EMBODIMENT OF IT IN ANY MEDIA, DISCLOSES INFORMATION WHICH IS PROPRIETARY, IS THE PROPERTY OF LOCKHEED MARTIN CORPORATION AND/OR ITS SUBSIDIARIES, IS AN UNPUBLISHED WORK PROTECTED UNDER APPLICABLE COPYRIGHT LAWS, AND IS DELIVERED ON THE EXPRESS CONDITION THAT IT IS NOT TO BE USED, DISCLOSED, REPRODUCED, IN WHOLE OR IN PART (INCLUDING REPRODUCTION AS A DERIVATIVE WORK), OR USED FOR MANUFACTURE FOR ANYONE OTHER THAN LOCKHEED MARTIN CORPORATION AND/OR ITS SUBSIDIARIES WITHOUT ITS WRITTEN CONSENT, AND THAT NO RIGHT IS GRANTED TO DISCLOSE OR SO USE ANY INFORMATION CONTAINED HEREIN. ALL RIGHTS RESERVED. ANY ACT IN VIOLATION OF APPLICABLE LAW MAY RESULT IN CIVIL AND CRIMINAL PENALTIES. SOFTWARE LICENSE AGREEMENT: BY ACTIVATING, ACCESSING, OR USING THE SOFTWARE AND/OR RELATED DOCUMENTATION ("SOFTWARE"), YOU HEREBY AGREE TO BE BOUND BY THE TERMS AND CONDITIONS OF THIS AGREEMENT WITH SIKORSKY AIRCRAFT CORPORATION (“SIKORSKY”) AND THAT YOUR ACTIVATION, ACCESS OR USE OF THE SOFTWARE ("USE") IS SUBJECT TO THE FOLLOWING RESTRICTIONS AND LIMITATIONS. YOU MAY NOT USE THE SOFTWARE IF YOU DO NOT AGREE WITH THE TERMS AND CONDITIONS OF THIS AGREEMENT AND THE RESTRICTIONS AND LIMITATIONS ON USE OF THE SOFTWARE. THE SOFTWARE AND ALL SOURCE OR OBJECT CODE ASSOCIATED THEREWITH ARE THE INTELLECTUAL PROPERTY OF SIKORSKY. USE OF THE SOFTWARE IS SOLELY PURSUANT TO LICENSE AND NO OWNERSHIP RIGHTS IN OR TO SUCH SOFTWARE ARE TRANSFERRED TO YOU. FURTHER, USE OF THE SOFTWARE IS LIMITED SOLELY TO USE IN CONNECTION WITH AND FOR THE PURPOSE OF OPERATING AIRCRAFT BEARING THE TAIL NUMBERS SET FORTH BELOW. UNITED STATES COPYRIGHT AND TRADE SECRET LAWS AND INTERNATIONAL TREATY PROVISIONS PROTECT THE SOFTWARE. YOU ACKNOWLEDGE AND AGREE THAT THE SOFTWARE INCLUDES PROPRIETARY INFORMATION, TRADE SECRETS, KNOW-HOW AND CONFIDENTIAL INFORMATION, THAT IS THE EXCLUSIVE PROPERTY OF SIKORSKY. YOU FURTHER AGREE THAT, WITHOUT THE PRIOR WRITTEN CONSENT OF SIKORSKY, YOU WILL NOT GRANT ACCESS TO THE SOFTWARE TO ANY PERSONS OR ENTITIES EXCEPT FOR YOUR EMPLOYEES AND AGENTS WHO HAVE A BUSINESS NEED TO HAVE SUCH ACCESS AND WHO ARE OBLIGATED TO MAINTAIN THE CONFIDENTIALITY THEREOF. YOU AGREE THAT YOU WILL NOT: (A) DISTRIBUTE, COPY, DISASSEMBLE, DECOMPILE, REVERSE ENGINEER, MODIFY, ADAPT OR CREATE DERIVATIVE WORKS OF THE SOFTWARE; (B) RECONFIGURE, TRANSFER OR ACTIVATE THE SOFTWARE FOR USE IN CONNECTION WITH ANY OTHER AIRCRAFT; (C) ALLOW OR ASSIST ANY OTHER PERSON IN ANY OF THE FOREGOING ACTS. ANY ATTEMPT TO DO SO IS A VIOLATION OF THE LEGAL RIGHTS OF SIKORSKY. THE SOFTWARE CONTAINS TECHNOLOGICAL MEASURES THAT RESTRICT ACCESS TO THE SOFTWARE. YOU ARE NOT AUTHORIZED TO ACCESS THE SOFTWARE WITHOUT THE EXPRESS PERMISSION OF SIKORSKY. ANY ATTEMPT TO CIRCUMVENT SUCH TECHNOLOGICAL MEASURES IS STRICTLY PROHIBITED UNDER THE U.S. COPYRIGHT ACT, 17 U.S.C. 101, ET SEQ, AND OTHER LAWS AND MAY SUBJECT YOU TO CIVIL AND CRIMINAL PENALTIES. USE OF CERTAIN FEATURES OF THE SOFTWARE REQUIRE ACTIVATION MEASURES THAT ARE TRADE SECRETS OF SIKORSKY. YOU MUST HAVE THESE ACTIVATION MEASURES PERFORMED BY ONLY SIKORSKY OR ITS AUTHORIZED REPRESENTATIVE. OTHERWISE, YOU DO NOT HAVE A RIGHT TO USE THESE SOFTWARE FEATURES. YOU AGREE THAT YOU WILL NOT ATTEMPT TO ACQUIRE, DISCLOSE, OR USE THE ACTIVATION MEASURES. USE OF SUCH SOFTWARE FEATURES WITHOUT ACTIVATION MEASURES PERFORMED BY SIKORSKY OR ITS AUTHORIZED REPRESENTATIVE IS AN UNAUTHORIZED USE AND CONSTITUTES A MATERIAL BREACH OF THIS AGREEMENT AND APPLICABLE LAW. S-76® IS A REGISTERED TRADEMARK OF SIKORSKY AIRCRAFT CORPORATION. ASB 76-31-4 May 17/18 Revision A ▪ May 30/18 SUBJECT: INDICATING/RECORDING SYSTEMS – Remote Data Acquisition Unit (RDAU) – One-Time Software Update Section 1. P LANNING INFORMATION A. Effectivity S- 76C+/C++ model helicopters with serial numbers 760471 through 760822, equipped with RDAU (76450-01098-107). B. Purpose To update the RDAU software to prevent erroneous Caution Advisory System (CAS) messages and parameter indications due to degraded internal power supply. Sikorsky Aircraft Corporation 6900 Main Street P.O. Box 9729 Stratford, Connecticut 06615-9129 (203) 386-4000 Page 1 of 32 WARNING ‒ This document contains technical data subject to the EAR. Authorization is required prior to providing this technical data to any company, entity, person, or destination. EAR Export Classification: ECCN EAR99 ### Page 2 S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A ▪ May 30/18 ATA 31-60-01 SOFTWARE UPDATE Section 1. P LANNING lNFORMATION (Continued) C. Background An update to the RDAU software was developed that monitors the status of the power supply and will shut down affected channels if degraded power supply is detected. D. Description Helicopter is prepared for maintenance. RDAU software is updated. RDAU is re- identified. Helicopter is returned to service. E. Compliance Compliance is essential. The software update outlined herein is to be accomplished no later than June 30, 2019. F. Approval The design change specified by this document is FAA approved in accordance with the applicable requirements of United States Federal Aviation Regulations 14 CFR Part 29. G. Manpower (Estimated) Task No. of Men No. of Hours Man-Hours* Removal of electrical compartment access cover 1 0.10 0.10 Installation of software onto RDAU 1 2.00 2.00 Re-identification of RDAU 1 0.10 0.10 Installation of electrical compartment access cover 1 0.10 0.10 Total Man-Hours 2.30 *Estimate does not include time required to prepare helicopter or return it to flight status. H. Tooling Refer to Parker Service Bulletin 367-111-77-003, dated January 4, 2018. Qty Nomenclature Part No. Source 1 Roller Commercially available or equivalent (1) 1 Personal Computer-Pentium 4, 1G or better, with Windows 7 or Windows 10 (64 bit installed) Commercially available or equivalent (2) 1 Thunderlinx1000 USB To Serial Adapter THX1000 (2) 1 Remote Signal Processing Unit (RSPU) Maintenance Interface Harness (Programming Cable to RDAU) 199-914-001 (2)(3) 1 Software CD with the following folders: 553-096-008 (2) Page 2 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 3 ASB 76-31-4 S-76 ALERT Revision A ▪ May 30/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 1. P LANNING lNFORMATION (Continued) Qty Nomenclature Part No. Source 555-096 -009 Rev B HOST Software for the S76 RDAU 555-096-010 Rev B EPP Software for the S76 RDAU 555-096 -003 Rev D FUEL Software for the S76 RDAU 555-096-004 Rev A BOOT software for the S76 RDAU (4) 1 Emulator Program Accuterm 7 (standard edition) (2) (1) Available through normal supply channels. (2) C ontact local Field Service Representative (FSR) for details required to accomplish update. These tools are kitted and available via kit No. 17076A88P001-001 for FSR use. (3) Refer to Figure 1 for wiring diagram of RSPU maintenance interface harness for local fabrication. (4) 555-096-004 Rev A BOOT software has not been updated as part of this software update and does not need not be uploaded to the RDAU. I. Weight and Balance Not affected. J. Electrical Load Data Not affected. K. Software Load Data Refer to Parker Service Bulletin 367-111-77-003, dated January 4, 2018. L. References None. M. Publications Affected (1) Temporary Revision No. 31-07 against Illustrated Parts Catalog, SA 4047-76C-4, Figure 31-60-00-1 is released concurrently with this ASB. Page 3 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 4 S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A ▪ May 30/18 ATA 31-60-01 SOFTWARE UPDATE Section 1. PLANNING lNFORMATION (Continued) (2) Temporary Revision No. 39-04 against Illustrated Parts Catalog, SA 4047-76C-4, Figure 39-10-01-3 is released concurrently with this ASB. N. Attachment Parker Service Bulletin 367-111-77-003, dated January 4, 2018. Section 2. M ATERIAL INFORMATION A. Basis for Material Data Per helicopter. B. Bill of Material New Part No. Qty Nomenclature Old Part No. Instructions/ Disposition 76070-60084-012 REF M/K, RDAU (1) Consisting of: 696-863-007 1 Identification Plate 696-863-002 (2)(3) 696-493-001 1 Modification Label 696-493-001 (2)(3)(4) (1) RDAU modification kit (76070-60084-012) is listed for reference only, and is not a procurable item. (2) I dentification plate (696-863-007) and modification label (696-493-001) are available at no cost until June 30, 2019. Parts shall be available after June 30, 2019 at standard Sikorsky Commercial Inc. (SCI) rates. For part availability and lead time requirements contact your Customer Service Representative at SCI. Submit a no-cost purchase order referencing this ASB number and the helicopter serial number(s) on which these parts will be used. This will allow SCI and the operator to track shipment and receipt of parts. Orders will be accepted by letter, telephone, or through the SCI website: https://customerportal.sikorsky.com. For prompt shipment, reference address of each shipping destination. Direct your order to: Sikorsky Aircraft Corporation Commercial Systems and Services Mailstop K100 124 Quarry Road Trumbull, CT 06611 U.S.A. Attn: Account Service Manager Telephone: (203) 416-4000 33TU33TU33TUhttps://customerportal.sikorsky.comUUU33T33T33 Page 4 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 5 ASB 76-31-4 S-76 ALERT Revision A ▪ May 30/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 2. M ATERIAL INFORMATION (Continued) (3) Sikorsky advises adherence to Shelf Life Expiration Date (SLED) provided on packaging. The SLED is due in part to 3M adhesive tape on labels. If labels are suspected to expire prior to the adherence of this ASB, Sikorsky recommends performing Section 3, steps I.(4) and/or I.(8) of this ASB. (4) If existing modification label states “MOD 0” there is no need to order a new modification label. C. Consumable Material Qty Nomenclature Part No. Source A/R Acetone ASTM-D329 or equivalent (1) A/R Cheesecloth CCC-C-440 or equivalent (1) A/R Isopropyl Alcohol TT-I-735 or equivalent (1) A/R Adhesive cleaner 3M General Purpose Adhesive Cleaner or equivalent (1) A/R Acrylic Adhesive 3M High Performance Acrylic Adhesive 200MP or equivalent (1) (1) Available through normal supply channels. Section 3. A CCOMPLISHMENT INSTRUCTIONS A. Define COMM Port as follows: (1) Turn on laptop. (2) Attach Thunderlinx1000 USB to Serial Adapter (THX1000) to laptop USB port. (3) Select START MENU. (4) In the search Windows box, type CONTROL PANEL. (5) Select DEVICES and PRINTERS. (6) In UNSPECIFIED DEVICES area, select UART DEVICE. (7) Select HARDWARE tab. (8) Record COMM PORT number. B. Load RDAU software to laptop as follows: (1) Transfer RDAU software PN 553-096-008 to laptop desktop from www.sikorsy360.com or software CD (553-096-008). Page 5 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 6 S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A ▪ May 30/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) (2) Confirm that folders identified in Section 1 Planning Information are present. C. Prepare helicopter for modification: (1) Turn off all helicopter electrical and hydraulic power. (2) Engage rotor brake. (3) Remove electrical compartment access panel from aft bulkhead in baggage compartment. D. Update RDAU software as follows: (1) Connect laptop with Accuterm 7 (standard edition) software to RDAU using RSPU maintenance interface harness (199-914-001). (Refer to Figure 2). (2) Set RSPU maintenance interface harness (199-914-001) switches as follows (Refer to Figure 3): S1 to PGM ENB S2 to DH ENB S3 to RS232 WRAP-BACK (3) Double-click Accuterm 7 desktop icon. (4) When Accuterm 7 has completed start up, select “File”, then click “New” to create a new session. (5) Select “Serial Port” from “Connection Type” drop down menu, then click “Next”. (Refer to Figure 4). NOTE: COMM port defined and recorded in Section A, “Define COMM Port”. (6) Select recorded COMM as the “Serial Port”, then click “Next”. (Refer to Figure 5). (7) Set the following parameters, then click “Next” (Refer to Figure 6): “Baud rate” to 38400 “Data bits” to 8 “Stop bits” to 1 “Parity” to “Odd” TO PREVENT ELECTRICAL SHOCK OF PERSONNEL OR POSSIBLE DAMAGE TO HELICOPTER COMPONENTS, MAKE SURE TO TURN OFF ALL ELECTRICAL POWER. Page 6 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 7 ASB 76-31-4 S-76 ALERT Revision A ▪ May 30/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) “Handshake” to “None” Set “Terminal Type” to “TTY” then click “Finish”. (Refer to Figure 7). (8) Select “Tools”, then click “Settings” in the options at the top of the page. (9) Select the “Connection” category and set the “Echo (duplex)” to “local echo (half duplex)”, then click “Apply”. (Refer to Figure 8). (10) Select the “File Transfer” category and set the following parameters in the “ASCII OPTIONS” (Refer to Figure 9): “End-of-line” to “CR” “Interline delay” to 30 (11) Click “Apply” then “OK”. NOTE: Configuration settings can be saved for future programming by selecting “File” then “Save”. Enter desired name and select location prior to pressing “Save”. E. Perform software upload as follows: (1) Turn on EXT PWR. (2) Pull out the following circuit breakers: (a) DC ESS BUS PLT IIDS PRI CTR IIDS PRI CPLT IIDS PRI IIDS HTR CTR IIDS HTR PLT PLT IIDS CONT CTR IIDS CONT (b) NO. 1 DC PRI CPLT IIDS HTR (c) NO. 2 DC PRI CPLT IIDS CONT Page 7 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 8 S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A ▪ May 30/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) (3) Pull out PLT IIDS SEC (NO. 2 DC PRI bus). Wait at least five (5) seconds. (4) Push in PLT IIDS SEC (NO. 2 DC PRI bus). (5) Pull out CPLT IIDS SEC (NO. 2 DC PRI bus). Wait at least five (5) seconds. (6) Push in CPLT IIDS SEC (NO. 2 DC PRI bus). (7) Pull out CTR IIDS SEC (NO. 2 DC PRI bus). Wait at least five (5) seconds. (8) Push in CTR IIDS SEC (NO. 2 DC PRI bus). (9) Check IIDS display units. All should be at start up page with the software revision to the HOST, ENGINE and FUEL set to dashes. (Refer to Figure 10). (10) Set S3 switch on RSPU maintenance interface harness (199-914-001) to TRANSMIT. F. Program host Operational Flight Program (OFP) as follows: (1) Select “Tools”, “Upload”, “Browse”, “555-096-009 Rev. B”. (Refer to Figure 11). (2) Select “SHT1.CHA” file and click “Open”. (Refer to Figure 12). (3) Click on “Upload”. Wait for the file to finish uploading then click “OK”. (4) Wait for the message to be displayed as seen in Figure 13 and below: “HOST OFP FILE 1 IS DOWNLOADED SUCCESSFULLY, SEND FILE 2:” “PROC = 4, DEVICE = 0” (a) If the above is verified then the software is loaded correctly. (5) Select “Tools”, “Upload”, “Browse”, “555-096-009 Rev. B”. (6) Select “SHT2.CHA” file and click “Open”. (7) Click “Upload”. Wait for file to finish uploading and click “OK”. (8) Wait for the following message to be displayed as seen in Figure 14, and below: “HOST OFP FILE 1 IS DOWNLOADED SUCCESSFULLY, SEND FILE 2:” “PROC = 4, DEVICE = 0” “OFP IS DOWNLOADED SUCCESSFULLY:” “PART = 555096009” “VER = 2A44” Page 8 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 9 ASB 76-31-4 S-76 ALERT Revision A ▪ May 30/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) “CHECKSUM = 733DAB02” “PROC = 4, DEVICE = 0” (a) If the above is verified then the software is loaded correctly. (9) Select “Tools”, “Upload”, “Browse”, “555-096-009 Rev. B”. (10) Select “SHT1.CHB” file and click “Open”. (11) Click on “Upload”. Wait for the file to finish uploading then click “OK”. (12) Wait for the following message to be displayed: “HOST OFP FILE 1 IS DOWNLOADED SUCCESSFULLY, SEND FILE 2:” “PROC = 8, DEVICE = 0” (a) If the above is verified then the software is loaded correctly. (13) Select “Tools”, “Upload”, “Browse”, “555-096-009 Rev. B”. (14) Select “SHT2.CHB” file and click “Open”. (15) Click on “Upload”. Wait for the file to finish uploading then click “OK”. (16) Wait for the following message to be displayed: “OFP IS DOWNLOADED SUCCESSFULLY:” “PART = 555096009” “VER = 2A44” “CHECKSUM = 733DAB02” “PROC = 8, DEVICE = 0” (a) If the above is verified then the software is loaded correctly. (17) Select “Tools”, “Upload”, “Browse”, “555-096-009 Rev. B”. (18) Select “SHT1.CHC” file and click “Open” (19) Click on “Upload”. Wait for the file to finish uploading then click “OK”. (20) Wait for the following message to be displayed: “HOST OFP FILE 1 IS DOWNLOADED SUCCESSFULLY, SEND FILE 2:” Page 9 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 10 S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A ▪ May 30/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) “PROC = C, DEVICE = 0” (a) If the above is verified then the software is loaded correctly. (21) Select “Tools”, “Upload”, “Browse”, “555-096-009 Rev. B”. (22) Select “SHT2.CHC” file and click “Open”. (23) Click on “Upload”. Wait for the file to finish uploading then click “OK”. (24) Wait for the following message to be displayed: “OFP IS DOWNLOADED SUCCESSFULLY:” “PART = 555096009” “VER = 2A44” “CHECKSUM = 733DAB02” “PROC = C, DEVICE = 0” (a) If the above is verified then the software is loaded correctly. G. Program fuel OFP as follows: (1) Select “Tools”, “Upload”, “Browse”, “555-096-003 Rev. D”. (2) Select “SFUEL.CHA” file and click “Open”. (3) Click on “Upload”. Wait for the file to finish uploading then click “OK”. (4) Wait for the following message to be displayed: “OFP IS DOWNLOADED SUCCESSFULLY:” “PART = 555096003” “VER = 2A12” “CHECKSUM = AD595737” “PROC = 6, DEVICE = 0” (a) If the above is verified then the software is loaded correctly. (5) Select “Tools”, “Upload”, “Browse”, “555-096-003 Rev. D”. (6) Select “SFUEL.CHB” file and click “Open”. Page 10 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 11 ASB 76-31-4 S-76 ALERT Revision A ▪ May 30/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) (7) Click on “Upload”. Wait for the file to finish uploading then click “OK”. (8) Wait for the following message to be displayed: “OFP IS DOWNLOADED SUCCESSFULLY:” “PART = 555096003” “VER = 2A12” “CHECKSUM = AD595737” “PROC = A, DEVICE =0” (a) If the above is verified then the software is loaded correctly. (9) Select “Tools”, “Upload”, “Browse”, “555-096-003 Rev. D”. (10) Select “SFUEL.CHC” file and click “Open”. (11) Click on “Upload”. Wait for the file to finish uploading then click “OK”. (12) Wait for the following message to be displayed: “OFP IS DOWNLOADED SUCCESSFULLY:” “PART = 555096003” “VER = 2A12” “CHECKSUM = AD595737“ “PROC = E, DEVICE = 0” (a) If the above is verified then the software is loaded correctly. H. Program EPP OFP as follows: (1) Select “Tools”, “Upload”, “Browse”, “555-096-010 Rev. B”. (2) Select “SEPP.CHA” file and click “Open”. (3) Click on “Upload”. Wait for the file to finish uploading then click “OK”. (4) Wait for the following message to be displayed: “OFP IS DOWNLOADED SUCCESSFULLY:” “PART = 555096010” Page 11 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 12 S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A ▪ May 30/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) “VER = 3A14” “CHECKSUM = 2D155FA6” “PROC = 5, DEVICE = 0” (a) If the above is verified then the software is loaded correctly. (5) Select “Tools”, “Upload”, “Browse”, “555-096-010 Rev. B”. (6) Select “SEPP.CHB” file and click “Open”. (7) Click on “Upload”. Wait for the file to finish uploading then click “OK”. (8) Wait for the following message to be displayed: “OFP IS DOWNLOADED SUCCESSFULLY:” “PART = 555096010” “VER = 3A14” “CHECKSUM = 2D155FA6” “PROC = 9, DEVICE =0” (a) If the above is verified then the software is loaded correctly. (9) Select “Tools”, “Upload”, “Browse”, “555-096-010 Rev. B”. (10) Select “SEPP.CHC” file and click “Open”. (11) Click on “Upload”. Wait for the file to finish uploading then click “OK”. (12) Wait for the following message to be displayed: “OFP IS DOWNLOADED SUCCESSFULLY:” “PART = 555096010” “VER = 3A14” “CHECKSUM = 2D155FA6” “PROC = D, DEVICE = 0” (a) If the above is verified then the software is loaded correctly. (13) Turn off EXT PWR. Page 12 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 13 ASB 76-31-4 S-76 ALERT Revision A ▪ May 30/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) (14) Set RSPU maintenance interface harness (199-914-001) switches as follows: S1 to OFF S2 to OFF (15) Turn on EXT PWR. (16) IIDS display units shall display on the top row the following RDAU version numbers for the software, as shown in Figure 16. NOTE: Disregard DU S/W VER DATA, as they are not modified by this service bulletin. (a) If this is verified the programming is complete for the RDAU. (b) If the above is not verified, then the RDAU shall be returned to Parker Fluid Systems Division (FSD). (17) Push in the following circuit breakers: (a) DC ESS BUS PLT IIDS PRI CTR IIDS PRI CPLT IIDS PRI IIDS HTR CTR IIDS HTR PLT PLT IIDS CONT CTR IIDS CONT (b) NO.1 DC PRI CPLT IIDS HTR (c) NO. 2 DC PRI CPLT IIDS CONT (18) Turn off EXT PWR. (19) Disconnect laptop and RSPU maintenance interface harness (199-914-001) from helicopter. Page 13 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 14 S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A ▪ May 30/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) I. Re-identify RDAU 76450-01098-107 to 76450-01098-112 using new identification plate (696- 863-007) and modification label (696-493-001) as follows (Refer to Figure 17): NOTE: If existing modification label (696-493-001) states “MOD 0” there is no need to install a new modification label (696-493-001). (1) Remove existing identification plate and modification label, if applicable. (2) Clean bonding surface thoroughly with cheesecloth (CCC-C-440 or equivalent) moistened with isopropyl alcohol (TT-I-735 or equivalent) or acetone (ASTM-D329 or equivalent). (3) Using a rubber stamp and indelible ink, mark identification plate (696-863-007) with serial number found on removed identification plate. NOTE: Sikorsky advises adherence of SLED provided on packaging. The SLED is due in part to 3M adhesive tape on labels. If identification plate adhesive is expired prior to compliance of this ASB, it is recommended to replace identification plate adhesive. (4) If adhesive on identification plate has expired and need replacing, do the following: (a) Using adhesive cleaner (3M General Purpose Adhesive Cleaner or equivalent) , remove existing adhesive from identification plate (696-863-007). (b) Using isopropyl alcohol (TT-I-735 or equivalent) clean identification plate (696-863- 007). (c) Apply acrylic adhesive (3M High Performance Acrylic Adhesive 200MP or equivalent) to surface of identification plate (696-863-007). (5) If adhesive on identification plate (696-863-007) has not expired and does not need replacing, remove adhesive backing from identification plate (696-863-007). (6) In stall identification plate (696-863-007) onto RDAU (76450-01098-112). (7) Using roller (commercially available or equivalent) apply firm pressure to identification plate (696-863-007) to obtain intimate contact of adhesive to RDAU (76450-01098-112). NOTE: Sikorsky advises adherence of SLED provided on packaging. The SLED is due in part to 3M adhesive tape on labels. If identification plate adhesive is expired prior to compliance of this ASB, it is recommended to replace identification plate adhesive (8) If adhesive on modification label (696-493-001) has expired and need replacing, do the following: (a) Using adhesive cleaner (3M General Purpose Adhesive Cleaner or equivalent) remove existing adhesive from modification label (696-493-001). Page 14 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 15 ASB 76-31-4 S-76 ALERT Revision A ▪ May 30/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) (b) Using isopropyl alcohol (TT-I-735 or equivalent) clean modification label (696-493- 001). (c) Apply acrylic adhesive (3M High Performance Acrylic Adhesive 200MP or equivalent) to surface of modification label (696-493-001). (9) If adhesive on modification label (696-493-001) has not expired and does not need replacing, remove adhesive backing from modification label (696-493-001). (10) In stall modification label (696-493-001) onto RDAU (76450-01098-112), if applicable. (11) Using roller (commercially available or equivalent) apply firm pressure to modification label (696-493-001) to obtain intimate contact of adhesive to RDAU (76450-01098-112). J. Install electrical compartment access panel on baggage compartment aft bulkhead. K. Return helicopter to service. Page 15 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 16 (OCR) S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A - May 30/18 Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) TO RDAU → O 1 CHASSIS GND PRG_ENABLE • 2 PRG_ENAB DH_ENABLE S2 -• 3 DH_ENAB - TO PC • WRAP 10 S3 • 7 RXD + •RXD 2 O n XMIT - TXD 3 O 8 TXD GND 5 -O 6.9 GND 199-914-001 CONNECTOR P / N: MS27473E10B13S STRAIN RELIEF P/N: M85D49 / 49210W CONNECTOR P / N: 171DE9S BACKSHELL P/N: 17-310-1 ALL WIRING 20AWG TD4426 PROGRAMMING CABLE WIRING HARNESS FIGURE 1 ATA SOFTWARE Page 16 31-60-01 UPDATE This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 17 ASB 76-31-4 S-76 ALERT Revision A ▪ May 30/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. A CCOMPLISHMENT INSTRUCTIONS (Continued) LAPTOP TO RDAU INTERFACE FIGURE 2 Page 17 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 18 S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A ▪ May 30/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. A CCOMPLISHMENT INSTRUCTIONS (Continued) RSPU MAINTENANCE INTERFACE HARNESS FIGURE 3 Page 18 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 19 (OCR) ASB 76-31-4 S-76 ALERT Revision A • May 30/18 SERVICE BULLETIN Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) A AccuTerm 7 File Edit View Tools Mutvalue Window accuer connecton wizara - connecuon ontons Please select the desired type of connection from this Most terminal sessions use Telnet over a local network (or the Internet) to connect to the host computer. For secure network connections, choose Secure Shell (if your host supports this protocol). If your PC is directly connected to the host computer using a 9 or 25 pin plug, select Serial Port. If you need to dial-up from your PC direcuy to a modem autached to the nost computer select Modem. Connection type: Serial Port the wizard and enter settings directly Secure Shell At any time, you can click the iSessi Telnet e future, do not you never want to use the wizard to SSL/Telnet his wizard Session settings.. < Back Einish Create a new session or open an existing one ACCUTERM 7 - Inbox - mario.a.. ) Skype for Busin. Kronauer, BRA.. A AccuTerm 7 Pa Presentation ... OR 7/19/2017 1:57 PM TD4429 CONNECTION OPTIONS WINDOW FIGURE 4 SOFTWARE ATA UPDATE 31-60-01 Page 19 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 20 (OCR) S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A • May 30/18 Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) A AccuTerm 7 File Edit View Tools MultiValue Window Help ecton Wizard - Port Selection Please select the serial port that is connected to your nost computer. Most PC's have two serial ports. A PC serail port is normally a "D" shaped 9-pin male connector. If you can't determine which port is connected to your host computer, you can try all of the avalable ports, or ask your system administrator. Serial port: Session settings... Cancel Next > Einish * Create a new session or open an existing one Skype for Bus... Kronauer, BRA.. A AccuTerm 7 Pa Presentation - TD4430 SA PORT SELECTION WINDOW FIGURE 5 ATA SOFTWARE Page 20 31-60-01 UPDATE This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 21 (OCR) ASB 76-31-4 S-76 ALERT Revision A • May 30/18 SERVICE BULLETIN Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) A AccuTerm 7 File Edit View Tools MultiValue Window Help 1 - Baud Rate Selection Please select the desired port settings. The Baud Rate is the speed that your PC uses to talk to the host computer. Data Bits, Stop Bits and Parity describe the data format used between the computers, and Handshake controls the flow of data from one computer to the other. The port settings on your PC and the host computer must match for a reliable connection. Baud rate: 38400 Data bits: Stop bits: 1 Parity: Handshake: one Cancel < Back Next > Einish - Create a new session or open an existing one S Skype for Bu. Kronauer, B.. AccuTerm 7 I AccuTerm... Pa Presentation... | = CR 719201 TD4431 BAUD RATE SELECTION WINDOW FIGURE 6 SOFTWARE ATA UPDATE 31-60-01 Page 21 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 22 (OCR) S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A • May 30/18 Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) A AccuTerm 7 File Edit View Tools Multvalue window Help AccuTerm Connection Wizard - Terminal Type I that's left is to choose the type of terminal yo ant to emulate from the list below. Then click on th Finish button! Each terminal speaks a different language. In order to get things working correctly, you need to know what type of terminal your host computer application is designed to use and select the corresponding terminal type here. Most Unix systems use VT220, and most MultiValue systems use ADDS Viewpoint A2 Enhanced (Wyse 50 and 60 are also common). If you choose the wrong type, your menus and screens may appear scrambled. If this happens, just try a different terminal type. Terminal type: Session settings... Cancel Finish * Create a new session or open an existing one ACCUTERM 7 Inbox - mario.a. Skype for Busin.. • Kronauer, BRA. Pa Presentation .. A AccuTer 7 * CR 7/19/2017 TD4432 TERMINAL TYPE WINDOW FIGURE 7 ATA SOFTWARE Page 22 31-60-01 UPDATE This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 23 (OCR) ASB 76-31-4 S-76 ALERT Revision A • May 30/18 SERVICE BULLETIN Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) ^ AccuTerm Z-Irdau Z_19_20171 File Edit Vie AccuTerm Settings Category: Connection Settings General Options I rdau_7_19 Files & Folders Connection Connection type: Serial port Connection settings... • < - Telnet Secure Shell - Private Key Connection Options - SSL/Telnet Echo (duplex): Serial Port local echo (half duplex) Modem Terminal - Screen • Clear bigh bit of received data - Colors • Attribute Colors • Palette - Background • Display connection warnings • Keyboard - Font & Character Set • Sounds - Close session on disconnect - Printer - Screen Print • Slave Printer Cipboard Mouse File Transter MultiValue Rules Windows Apply ₴ • 1,1,1 _ Start • ACCUTERM 7 • Inbox - mario.a.. S Skype for Busin.. • Kronauer, BRA... Po Presentation 1 .. A AccuTerm 7 - [.. * UP 7/19/2017 2:11 PM TD4433 CONNECTION SETTINGS FIGURE 8 SOFTWARE ATA UPDATE 31-60-01 Page 23 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 24 (OCR) S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A - May 30/18 Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) Л AccuTerm Z-Irdau Z_19_20171 File Edit Vie AccuTerm Settings Category: General Options - Fie Transfer Settings • Files & Folders - ASCI Options i rdau_7_19 Connection nterline delay - Telnet 30 ÷ mș Secure Shell - Private Key SSL/Telnet - Kermit Options Serial Port 10 ÷ sec - Screen / Quote eighth bit Colors 30 - • Attribute Colors • Use data compression • Palette • Use CBC block check • Background Keyboard - Font & Character Set - X/Y/Zmodem Options Sounds modem timeout: Zmodem timeout: 10 sec 10 sec 10 sec • Screen Print • Slave Printer Initiate Zmodem downloads automatically Clipboard • Mouse - Defaults File Transfer Transfer mode: • Iext C Binary • MultiValue Rules • Windows Text file encoding No encoding • Oyerwrite existing files Cancel Apply 8 • 1,1,1 ACCUTERM 7 OC Inbox - mario.a..ù Skype for Busin. © Kronauer, BRA.. Pa Presentation 1-. * CR 7/19/2017 2:16 PM TD4434 FILE TRANSFER SETTINGS FIGURE 9 ATA SOFTWARE Page 24 31-60-01 UPDATE This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 25 ASB 76-31-4 S-76 ALERT Revision A ▪ May 30/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. A CCOMPLISHMENT INSTRUCTIONS (Continued) PRE-UPLOAD IIDS DISPLAY UNIT FIGURE 10 Page 25 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 26 (OCR) S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A • May 30/18 Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) Compressed Folder Tools 000008 eV - • x File Home share Extract • • • Pictures NEMASTER REF DOCT FLIGHT TESTI ASB 107 Extract To + → • 1 • › Network › sussffOu > shflsvc2eng > S-76 Project 1022 › Mission Systems Integration > S-76 RDAU > Parker Docs > Contents of SW CD 553-096-008 Rev - zip » 553096008 Rev• & Search 553096008 Rev - P • Nar Password... Size Ratio Date modified * Quick acce 11/9/2017 2:09 PM 11/9/20172:09 PM 11/9/2017 2:09 PM 11/9/2017 2:09 PM TD4491 SELECT FOLDER WINDOW FIGURE 11 ATA SOFTWARE Page 26 31-60-01 UPDATE This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 27 (OCR) ASB 76-31-4 S-76 ALERT Revision A • May 30/18 SERVICE BULLETIN Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 0100:1 Compressed holder Tools 555096009 Rev B File Home Share View Extract • Documents | MASTER REF DOC FLIGHT TEST L ASB 10: ARCHIVE Extract To + → = + I « suffOu > shfisceng > 5:76 Project 1022 › Mission Systems Integration > 576RDAU › Parker Docs › Contents of SW CD 553-096-008 Rev-zip > 553096008 Rev- > 555096009 RevB & [Search 555096009 Rev B P • Name Ratio Date modified ar Ouick acces • SHT1.CHA 289 KB 74% 8/1/2017 6:16 PM 289 KB 7478 8/1/2017 6:16 PM 289 KB 7498 ASHTO CHA 289 KB 95% 8/1/2017 6:16 PM 289 KB 9578 8/1/2017 6:16 PM = ENTERPRISE (SUS: TD4490 SELECT FILE TO UPLOAD WINDOW FIGURE 12 SOFTWARE ATA UPDATE 31-60-01 Page 27 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 28 (OCR) S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A • May 30/18 Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) ]El AccuTerm 2K2 - [576_STE (1)) -/#|× 2082080405891 HOST OFP FILE 1 IS DOWNLOADED SUCCESSFULLY, SEND FILE 2 Proc=4, Device=0 D 576_STE (1) g 1,3,1 80,24,1 DEC VT100 bIde by Capture Off a Comg ≥ 38400,0,8,1,0 100O.102 Microsaft Office «53 (8 9:30 AM TD4492 SUCCESSFUL DOWNLOAD OF SHT1.CHA FILE FIGURE 13 ATA SOFTWARE Page 28 31-60-01 UPDATE This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 29 (OCR) ASB 76-31-4 S-76 ALERT Revision A • May 30/18 SERVICE BULLETIN Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) El AccuTerm 2K2 - [576_STE (1)] File EdR Yew Iook Beset Window Help OFP IS DOWNLOADED SUCCESSFULLY: PART = 555096009 VER = 2A44 CHECKSUM = 733DAB02 Proc=4, Device=0 it Start e @ @ * [ AccuTerm 2K2 - [576. 3] Document - Microsoft... ] Microsoft Office * « 03 C: 12:57 PM TD4493 SUCCESSFUL DOWNLOAD OF SHT1.CHB FILE FIGURE 14 SOFTWARE ATA UPDATE 31-60-01 Page 29 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 30 (OCR) S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A • May 30/18 Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) Parker ULL ELECTRONIC SYSTEMS DIVISIDI COPYRIGHT © 1996, 199 RDAU S/W VERS: 2.44. 3.14 2.12 DU S/W VERS: 2.10 2.11 A/C MODEL: S-76-C++ POSITION: CENTER TEST: PASS 00PO-2 MENU TD4494 IIDS DISPLAY UNIT WITH SOFTWARE VERSION NUMBERS FIGURE 15 ATA SOFTWARE Page 30 31-60-01 UPDATE This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 31 (OCR) ASB 76-31-4 S-76 ALERT Revision A • May 30/18 SERVICE BULLETIN Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) REMOVE: 696-863-002 IDENTIFICATION PLATE (1) INSTALL: 696-863-007 IDENTIFICATION PLATE - 1 REQ'D J10 STATIC AIR 150 VOLTS REMOVE: 696-493-001 MODIFICATION LABEL (1) INSTALL: 696-493-001 NOTE MODIFICATION LABEL - 1 REQ'D IF EXISTING MODIFICATION LABEL (SEE NOTE) STATES "MOD O" THERE IS NO NEED TO INSTALL A NEW MODIFICATION LABEL. TD4442 SA IDENTIFICATION PLATE AND MODIFICATION PLATE INSTALLATION FIGURE 17 SOFTWARE ATA UPDATE 31-60-01 Page 31 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 32 S-76 ALERT ASB 76-31-4 SERVICE BULLETIN Revision A ▪ May 30/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. A CCOMPLISHMENT INSTRUCTIONS (Continued) L. Record of compliance: (1) Make helicopter logbook entries to show compliance with this ASB as follows: (a) Make helicopter level logbook entry on form SA7343-15 (Aircraft ASB Release Signoff). (b) When ASB modifies a component that can be removed from this helicopter: 1. Make component log card entries on forms SA7343-22 (Aircraft Component Log Cards) and SA7343-21 (Component Log Cards), as applicable. 2. If a component modified by this ASB does not have a log card and the ASB does not create one, then annotate compliance on the next higher assembly that the component belongs to which does have a log card. NOTE: If access to www.Sikorsky360.com is unavailable, complete attached ALERT SERVICE BULLETIN COMPLIANCE RECORD CARD and return it to Sikorsky Aircraft Corporation. (2) Make an appropriate electronic compliance entry in the E-Notification section at www.Sikorsky360.com. Refer to User Guide located on the www.Sikorsky360.com/E- Notification Search page. Page 32 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 33 (Fold over and tape closed) SIKORSKY AIRCRAFT CORPORATION FACSIMILE NUMBER (817) 762-6715 EMAIL ADDRESS: product_safety.gr-sik@lmco.com ATTENTION: Gr-SIK, Product_Safety SIKORSKY AIRCRAFT CORPORATION (Fold Up to Arrows) IMPORTANT NOTICE Upon COMPLIANCE with the attached ASB, Sikorsky requests your cooperation in completing and returning this ENTIRE PAGE by MAIL, FAX, or scan & EMAIL. Please fill in the requested information at the bottom of the page, so we may maintain proper records documenting the configuration of your aircraft. This information is useful when determining configuration and effectivity of issues affecting fielded aircraft. This request is in keeping with our policy to assure that our customers receive the latest information applicable for the maintenance of your aircraft. Thank you. ALERT SERVICE BULLETIN: ________________ Compliance Record Card TITLE: ___________________________________________________________________ ___________________________________________________________________ ___________________________________________________________________ OWNER/OPERATOR: _____________________________________________________ SUBMITTED BY: ___________________________ DATE: ____________________ FOLLOWING SERIAL NUMBERS ARE NOT AFFECTED BY THIS ASB ASB HAS BEEN COMPLIED WITH ON HELICOPTER SERIAL NUMBERS: ___________ ___________ ___________ ___________ ___________ ___________ ___________ ___________ ___________ ___________ ___________ ___________ No. 76-31-4A INDICATING/RECORDING SYSTEMS – Remote Data Acquisition Unit (RDAU) – One-Time Software Update This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 34 No Postage Necessary BUSINESS REPLY MAIL FIRST-CLASS MAIL PERMIT NO. 432 BRIDGEPORT CT POSTAGE WILL BE PAID BY ADDRESSEE SIKORSKY AIRCRAFT CORPORATION Commercial Systems and Services Mailstop K100 124 QUARRY ROAD TRUMBULL, CT 06611 U.S.A. ATTENTION: Gr-SIK, Product_Safety Please complete the form on the reverse side and FAX to FACSIMILE NUMBER (817) 762-6715 Or scan and email to: EMAIL ADDRESS: product_safety.gr-sik@lmco.com or fold and return ENTIRE form to Sikorsky Aircraft Corporation This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 35 Customer Support Operations SERVICE BULLETIN Initial Issue Jan 4, 2018 367-111-77-003 Page 1 of 6 THIS DOCUMENT CONTAINS INFORMATION THAT IS CONFIDENTIAL AND PROPRIETARY TO PARKER-HANNIFIN CORPORATION. THIS DOCUMENT IS FURNISHED ON THE UNDERSTANDING THAT THE DOCUMENT AND THE INFORMATION IT CONTAINS WILL NOT BE COPIED OR DISCLOSED TO OTHERS EXCEPT WITH THE WRITTEN CONSENT OF PARKER, WILL NOT BE USED FOR ANY PURPOSE OTHER THAN CONDUCTING BUSINESS WITH PARKER, AND WILL BE RETURNED AND ALL FURTHER USE DISCONTINUED UPON REQUEST BY PARKER. COPYRIGHT PARKER. YEAR OF COPYRIGHT IS FIRST YEAR INDICATED ON THIS DOCUMENT. ALL RIGHTS RESERVED. ENGINE INDICATING REMOTE DA TA ACQUISITION UNIT ASSEMBLY PARKER PART NUMBER 367-111-002 SOFTWARE UPGRADE 1. PLANNING INFORMATION A. Effectivity This Service Bulletin is applicable to the Parker Hannifin Corporation, Remote Data Acquisition Unit (RDAU) Part Number (P/N) 367-111-002, Sikorsky P/N 76450-01098-107. B. Concurrent Requirements None. C. Reason The RDAU P/N 367-111-002 has been updated to 367-111-102 (Sikorsky P/N 76450-01098- 107 updated to 76450-01098-112) to introduce a software change that allows a red fail screen to be displayed in flight if an internal power supply is degraded, thus preventing the display of misleading information to the pilot. The updated software will now mon itor ±5V and ±15 VDC for degraded voltage level. If a lost or degraded voltage is detected either in Air and /or on Ground, the software will latch a Red Box "FAIL" within the same power cycle. In addition, the Master Caution Trip, CAS Message and Audio Alerts for the affected channel will be turned off to prevent nuisance indications to the pilot. The following code/design errors were also addressed and corrected as part of this change: (a) N1 issue on the C++ Power As surance performance. N1 Bias number after power assurance is 0.0 and is out of range. (b) Test Button on IIDS show s RED BOX failure display. (c) Start Page Timeout not triggerin g from same logic from side to side. (d) Power Assurance page incorrect. Labe l 300 sent erroneously. (e) Fuel Quantity sometimes will drop for no reason. (f) Power Assurance Repeat 10 second timer does not reset to 2:45 (2 minutes 45 seconds) when N1 goes to 70% or below. (g) PO Values from IIDS are not stable upon power up. (h) T5 Coefficient Error 100 and 101 fault stored. (i) Occasionally RDAU is not saving T5 Coefficients. WARNING ‒ This document contains technical data subject to the EAR. Authorization is required prior to providing this technical data to any company, entity, person, or destination. EAR Export Classification: ECCN EAR99 ### Page 36 Customer Support Operations SERVICE BULLETIN Initial Issue Jan 4, 2018 367-111-77-003 Page 2 of 6 THIS DOCUMENT CONTAINS INFORMATION THAT IS CONFIDENTIAL AND PROPRIETARY TO PARKER-HANNIFIN CORPORATION. THIS DOCUMENT IS FURNISHED ON THE UNDERSTANDING THAT THE DOCUMENT AND THE INFORMATION IT CONTAINS WILL NOT BE COPIED OR DISCLOSED TO OTHERS EXCEPT WITH THE WRITTEN CONSENT OF PARKER, WILL NOT BE USED FOR ANY PURPOSE OTHER THAN CONDUCTING BUSINESS WITH PARKER, AND WILL BE RETURNED AND ALL FURTHER USE DISCONTINUED UPON REQUEST BY PARKER. COPYRIGHT PARKER. YEAR OF COPYRIGHT IS FIRST YEAR INDICATED ON THIS DOCUMENT. ALL RIGHTS RESERVED. (j) Low rotor Advisory update. A djust Low NR threshold from 95% to 91. Inhibit Low NR on Ground. (k) Power Assurance in flight look up table correction. D. Description This Service Bulletin provides instructions to modify, test, and re-identify the RDAU. Modification consists of installing the revised software only, hardware is not affected. After completion of this Service Bulletin, the RDAU P/N 367-111-002 will be upgraded to P/N 367-111-102 configuration. E. Compliance This modification is not mandatory, but is recommended at the earliest practical maintenance period. F. Approval This Service Bulletin has been reviewed by the appropriate governmental authority, and the repairs and modifications herein comply with the applicable Aviation Regulations. G. Manpower This modification may be accomplished by a crew of one (1) in approximately 2.0 hours. H. Weight and Balance None. I. Electrical Load Data Not affected. J. Software Accomplishment Summary Load software into RDAU. Verify checksum upon completion. Re-identify RDAU. K. References Parker Hannifin, Operators Manual - C+ Model: Pub No. IIDS S-76 PM004 Rev. B, October 4, 2017. Parker Hannifin, Operators Manual - C++ Model: Pub No. IIDS S-76 PM003 Rev. B, October 4, 2017. This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 37 Customer Support Operations SERVICE BULLETIN Initial Issue Jan 4, 2018 367-111-77-003 Page 3 of 6 THIS DOCUMENT CONTAINS INFORMATION THAT IS CONFIDENTIAL AND PROPRIETARY TO PARKER-HANNIFIN CORPORATION. THIS DOCUMENT IS FURNISHED ON THE UNDERSTANDING THAT THE DOCUMENT AND THE INFORMATION IT CONTAINS WILL NOT BE COPIED OR DISCLOSED TO OTHERS EXCEPT WITH THE WRITTEN CONSENT OF PARKER, WILL NOT BE USED FOR ANY PURPOSE OTHER THAN CONDUCTING BUSINESS WITH PARKER, AND WILL BE RETURNED AND ALL FURTHER USE DISCONTINUED UPON REQUEST BY PARKER. COPYRIGHT PARKER. YEAR OF COPYRIGHT IS FIRST YEAR INDICATED ON THIS DOCUMENT. ALL RIGHTS RESERVED. L. Other Publications Affected None. M. Interchangeability and In termixability of Parts Parker RDAU, P/N 367-111-002 (Sikorsky P/N 76450-01098-107) is completely interchangeable with RDAU P/N 367-111-102 (Sikorsky P/N 76450-01098-112). 2. MATERIAL INFORMATION A. Material - Price and Availability RDAU, P/N 367-111-002 (Sikorsky P/N 76450-01098-107) software upgrade is a chargeable upgrade to operators, with a delivery time of 30 days from receipt of purchase order at the address below. PARKER HANNIFIN CORPORATION AOG HOTLINE (949) 851-4357 Fluid System Division – Hauppauge FAX: (631) 434-4706 300 Marcus Blvd. TECHNICAL FAX HOTLINE: (949) 809-8444 Hauppauge, NY 11788 TECHNICAL E-MAIL HOTLINE: csoengineering@parker.com USA REPAIR STATION NO.: FX1R156K B. Industry Support Information Operators are requested to cont act their respective Parker Hannifin Customer Service Administrator to schedule implementation of this Service Bulletin. Damage from mishandling and/or a bnormal use, and parts or work required outside the scope of this Service Bulletin is subject to time and material charges. C. Material Necessary for Each Component Programming procedure. Table 1 TEST ITEM NOMENCLATURE FSD P/N S-76 IIDS RDAU 367-111-102 Test equipment requirement. Table 2 ITEM DESCRIPTION MODEL MANUFACTURER AMLCD Systems Production Test Set 199-382-001 FSD Parker RDAU Interface Harness 467-743-001 or 467-743-002 FSD Parker Oscilloscope TDS440A Tektronix STE ATP Software (For 367-111-002 and 367-111-102) 577-096-012 FSD Parker This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 38 Customer Support Operations SERVICE BULLETIN Initial Issue Jan 4, 2018 367-111-77-003 Page 4 of 6 THIS DOCUMENT CONTAINS INFORMATION THAT IS CONFIDENTIAL AND PROPRIETARY TO PARKER-HANNIFIN CORPORATION. THIS DOCUMENT IS FURNISHED ON THE UNDERSTANDING THAT THE DOCUMENT AND THE INFORMATION IT CONTAINS WILL NOT BE COPIED OR DISCLOSED TO OTHERS EXCEPT WITH THE WRITTEN CONSENT OF PARKER, WILL NOT BE USED FOR ANY PURPOSE OTHER THAN CONDUCTING BUSINESS WITH PARKER, AND WILL BE RETURNED AND ALL FURTHER USE DISCONTINUED UPON REQUEST BY PARKER. COPYRIGHT PARKER. YEAR OF COPYRIGHT IS FIRST YEAR INDICATED ON THIS DOCUMENT. ALL RIGHTS RESERVED. Microcontroller OFP (External F LASH PROM) Software for P/N 367-111-102 and 553-096-008. Table 3 S76 RDAU SOFTWARE P/N DESCRIPTION REVISION 553-096-008 Software Control Drawing - S76 RDAU 367-111-102 Hardware Assembly Drawing - HOST 548-123-001 Unit Part Number P Software P/N 555-096-009 Software Revision B Software Version 2.44/1.13 Checksum 733DAB0216 EPP 548-124-001 Unit Part Number W Software P/N 555-096-010 Software Revision B Software Version 3.14/1.14 Checksum 2D155FA616 FUEL 548-125-001 Unit Part Number M Software P/N 555-096-003 Software Revision D Software Version 2.12/3.5 Checksum AD59573716 BOOT 548-(123,124,125)-001 Unit Part Number See above Software P/N 555-096-004 Software Revision A Software Version 2.10/NA Checksum DBD7533B16 Remove Plate, Identification , P/N 696-863-002 and replace with Plate, Identification, P/N 696- 863-007 as shown in Table 4. Table 4. NEW P/N KEYWORD OLD P/N QTY DISPOSITION 696-863-007 Plate, Identification 696-863-002 1 Scrap 696-493-001* Label, Modification Same 1 Scrap NOTE: * If existing Label, Modification, P/N 696-493-001 is not at 'Mod 0', replace it with a new Label, Modification, P/N 696-493-001 and mark as 'Mod 0”. D. Material Necessary for Each Spare See Table 1 through 4 above. E. Re-identified Parts After the ACCOMPLISHMENT INSTRUCTIONS in Paragraph 3 of this Service Bulletin are complete, the RDAU P/N 367-111-002 (Sikorsky P/N 76450-01098-107) will be re-identified as P/N 367-111-102 (Sikorsky P/N 76450-01098-112). This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 39 Customer Support Operations SERVICE BULLETIN Initial Issue Jan 4, 2018 367-111-77-003 Page 5 of 6 THIS DOCUMENT CONTAINS INFORMATION THAT IS CONFIDENTIAL AND PROPRIETARY TO PARKER-HANNIFIN CORPORATION. THIS DOCUMENT IS FURNISHED ON THE UNDERSTANDING THAT THE DOCUMENT AND THE INFORMATION IT CONTAINS WILL NOT BE COPIED OR DISCLOSED TO OTHERS EXCEPT WITH THE WRITTEN CONSENT OF PARKER, WILL NOT BE USED FOR ANY PURPOSE OTHER THAN CONDUCTING BUSINESS WITH PARKER, AND WILL BE RETURNED AND ALL FURTHER USE DISCONTINUED UPON REQUEST BY PARKER. COPYRIGHT PARKER. YEAR OF COPYRIGHT IS FIRST YEAR INDICATED ON THIS DOCUMENT. ALL RIGHTS RESERVED. F. Tooling – Price and Availability None. 3. ACCOMPLISHMENT INSTRUCTIONS A. Option 1: Return the RDAU to Parker for on-bench software upgrade. B. Option 2: For customers who wish to perform the upgrade themselves (on aircraft), detailed instructions will be provided by Sikorsky Aircraft Corporation. C. Operation Flight Program (OFP) programming procedure. On the 199-382-001 test set, select the following switch posit ions to: (a) MAIN POWER: OFF. (b) UUT POWER: AUTO. (c) COMPUTER POWER: ON. (d) MONITOR POWER: ON. (e) SORENSEN D.C. SUPPLY POWER: ON. The 553-096-008 w ill display software numbers and other info needed for programming. On the test set, turn the “MAIN POWER” switch to “ON”. The test set computer will initialize and display the “MAIN MENU”. On the test set computer, select: (a) Sikorsky S-76 C++ RDAU. (NOTE: this selection supports bot h -002 and -102 part numbers). (b) OFP Download. (c) Board A, B and C for the HOST. (d) The computer will prompt for entry of various information, such as the serial number of the RDAU. Enter all information as requested. (e) When the download is complete, the computer will display a message indicating the download was successful. On the test set computer, select: (a) Board A, B and C for the EPP. (b) When the download is complete, the computer will display a message indicating the download was successful and will prompt for the next step. This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 40 (OCR) Parker Customer Support Operations SERVICE BULLETIN (б) On the test set computer, select: (a) Board A, B and C for the FUEL. (0) The computer will prompt for entry of software. (c) When the download is complete, the computer will display a message indicating the download was successful and will prompt for the next step. (d) Press Escape key (ESC) to exit. 4. APPENDIX NO CONNECTION STE P3B J1 STE P1 P1 J1 J8 STE P8 P2 J2 J3 STE P3 P3 J3 TEST SET J4 STE P4 P4 J4 RDAU 199-382-001 367-111-002 J10 P10 J5 STE P5 P5 J5 OR 367-111-102 J6 STE P6 P6 J6 J7 STE P7 P7 J7 J8 J9 STE P9 P8 J8 P9 J9 115V/60Hz CABLE 487-833-001 115V/60Hz SOURCE NOTE: CABLE 467-743-001 OR 467-743-002 IS THE CABLE THAT CONNECTS THE TEST SET 199-382-001 TO THE RDAU 367-111-002 OR 367-111-102. 367-111-77-003SB_R0 Fig1 Figure 1 Test Set and RDAU Connection Diagram. This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. Initial Issue Jan 4, 2018 367-111-77-003 Page 6 of 6 THIS DOCUMENT CONTAINS INFORMATION THAT IS CONFIDENTIAL AND PROPRIETARY TO PARKER-HANNIFIN CORPORATION. THIS DOCUMENT IS FURNISHED ON THE UNDERSTANDING THAT THE DOCUMENT AND THE INFORMATION IT CONTAINS WILL NOT BE COPIED OR DISCLOSED TO OTHERS EXCEPT WITH THE WRITTEN CONSENT OF PARKER, WILL NOT BE USED FOR ANY PURPOSE OTHER THAN CONDUCTING BUSINESS WITH PARKER, AND WILL BE RETURNED AND ALL FURTHER USE DISCONTINUELT JPON REQUEST BY PARKER. COPYRIGHT PARKER. YEAR OF COPYRIGHT IS FIRST YEAR INDICATED ON THIS DOCUMENT. ALL RIGHTS RESERVED --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.