# Sikorsky Alert Service Bulletin 76-31-5 Copy: No revision named ("Sikorsky ASB 76-31-5"), 41 pages: PDF https://openairdocs.org/files/sha256/07/d3/07d391f3d68e96ff81ae675c00d166b0a1657b2015dab4c8706009861711b0e5; text https://openairdocs.org/service-documents/sikorsky/sb-76-31-5/file/07d391f3d68e.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: 76-31-5 - Page: https://openairdocs.org/service-documents/sikorsky/sb-76-31-5 ## 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: No revision named Also cited in [1 proposed AD](https://openairdocs.org/service-documents/sikorsky/sb-76-31-5/proposed.md). ## Text (41 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INFORMATION WHICH IS PROPRIETARY, IS THE PROPERTY OF LOCKHEED MARTIN CORPORATION AND/OR ITS SUBSIDIARIES, IS AN UNPUBLISHED WORK PROTECTED UNDER APPLICABLE COPYRIGHT LAWS, AND IS DELIVERED ON THE EXPRESS CONDITION THAT IT IS NOT TO BE USED, DISCLOSED, REPRODUCED, IN WHOLE OR IN PART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 76-31-5 Basic Issue ▪ July 31/18 SUBJECT: INDICATING/RECORDING SYSTEMS – Remote Data Acquisition Unit (RDAU) – One Time Software Update Section 1. P LANNING INFORMATION A. Effectivity S- 76C+ model helicopters with serial numbers 760453 through 760606, equipped with RDAU (76450-01098-106). B. Purpose To update the RDAU software to prevent erroneous Caution Advisory System (CAS) messages and parameter indications due to degraded internal power supply. 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. Sikorsky Aircraft Corporation 6900 Main Street P.O. Box 9729 Stratford, Connecticut 06615-9129 (203) 386-4000 Page 1 of 33 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 76-31-5 SERVICE BULLETIN Basic Issue ▪ July 31/18 ATA 31-60-01 SOFTWARE UPDATE Section 1. P LANNING lNFORMATION (Continued) D. Description Helicopter is prepared for maintenance. RDAU software is updated. RDAU is re- identified as part number (P/N) 76450-01098-112. Helicopter is returned to service. NOTE: It is mandatory that Display Units (DUs) (76450-01098-101) be replaced with DUs (76450-01098-108 or 76450-01098-110) to maintain compatibility with RDAU (76450-01098-112). DUs (76450-01098-101) may be updated to DUs (76450-01098-108) by performing Sikorsky Service Bulletin (SB) 76-006, Software Update for Display Unit (DU) (76450- 01098-101), basic issue or later revision. E. Compliance Compliance is essential. The RDAU software update outlined herein is to be accomplished no later than July 31, 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 367-111-77-004, dated May 10, 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) Page 2 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 3 ASB 76-31-5 S-76 ALERT Basic Issue ▪ July 31/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 1. PLANNING lNFORMATION (Continued) Qty Nomenclature Part No. Source 1 Software CD with the following folders: 553-096-008 (2) 555-096-009 Rev B HOST Software for the S76 RDAU 555-096-010 Rev B EPP Software for the S76 RDAU (4) 555-096-003 Rev D FUEL Software for the S76 RDAU 555-096-004 Rev A BOOT Software for the S76 RDAU (5) 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) The 555-096-010 Rev B EPP software for the S76 RDAU is the current software that should be loaded in RDAU. Sikorsky has identified a small population of RDAU in the field with 555-096-010 Rev A software installed. As part of this Alert Service Bulletin (ASB), the latest 555-096-010 Rev B EPP software for the S76 RDAU will be loaded on all RDAU, regardless of existing revision. (5) The 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 367-111-77-004, dated May 10, 2018. Page 3 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 4 S-76 ALERT ASB 76-31-5 SERVICE BULLETIN Basic Issue ▪ July 31/18 ATA 31-60-01 SOFTWARE UPDATE Section 1. PLANNING lNFORMATION (Continued) L. References SB 76-006, Software Update for Display Unit (DU) (76450-01098-101), basic issue or later revision. M. Publications Affected Temporary Revision No. 31-08 against Illustrated Parts Catalog, SA 4047-76C-4, Figure 31-60- 00-01 is released concurrently with this ASB. N. Attachment Parker Service Bulletin 367-111-77-004, dated May 10, 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 76070-60084-013 REF M/K, RDAU (1) Consisting of: 696-863-007 1 Identification Plate 696-794-002 (2)(3) 696-493-001 1 Modification Label 696-493-001 (2)(3)(4) (1) RDAU modification kit (76070-60084-013) is listed for reference only, and is not a procurable item. Page 4 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 5 ASB 76-31-5 S-76 ALERT Basic Issue ▪ July 31/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 2. MATERIAL INFORMATION (Continued) (2) Parts are available at no cost until July 31, 2019. Parts shall be available after July 31, 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 (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) OBSERVE ALL CAUTIONS AND WARNINGS ON CONTAINERS WHEN USING CONSUMABLES. WHEN APPLICABLE, WEAR NECESSARY PROTECTIVE GEAR DURING HANDLING AND USE. IF A CONSUMABLE IS FLAMMABLE OR EXPLOSIVE, MAKE CERTAIN CONSUMABLE AND ITS VAPORS ARE KEPT AWAY FROM HEAT, SPARK AND FLAME. MAKE CERTAIN FIREFIGHTING EQUIPMENT IS READILY AVAILABLE PRIOR TO USE. FOR ADDITIONAL INFORMATION ON TOXICITY, FLASHPOINT AND FLAMMABILITY OF CHEMICALS, CONSULT YOUR MEDICAL DEPARTMENT OR THE MANUFACTURER OF THE CONSUMABLE. Page 5 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 6 S-76 ALERT ASB 76-31-5 SERVICE BULLETIN Basic Issue ▪ July 31/18 ATA 31-60-01 SOFTWARE UPDATE Section 2. MATERIAL INFORMATION (Continued) Qty Nomenclature Part No. Source 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 P/N 553-096-008 to laptop desktop from www.sikorsy360.com or software CD (553-096-008). (2) Confirm that software CD 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. 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 76-31-5 S-76 ALERT Basic Issue ▪ July 31/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 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” “Handshake” to “None” (8) Set “Terminal Type” to “TTY” then click “Finish”. (Refer to Figure 7). (9) Select “Tools”, then click “Settings” in the options at the top of the page. (10) Select the “Connection” category and set the “Echo (duplex)” to “local echo (half duplex)”, then click “Apply”. (Refer to Figure 8). (11) Select the “File Transfer” category and set the following parameters in the “ASCII OPTIONS” (Refer to Figure 9): “End-of-line” to “CR” Page 7 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 8 S-76 ALERT ASB 76-31-5 SERVICE BULLETIN Basic Issue ▪ July 31/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) “Interline delay” to 30 (12) 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 (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). Page 8 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 9 ASB 76-31-5 S-76 ALERT Basic Issue ▪ July 31/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) (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” “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”. Page 9 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 10 S-76 ALERT ASB 76-31-5 SERVICE BULLETIN Basic Issue ▪ July 31/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) (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:” “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”. Page 10 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 11 ASB 76-31-5 S-76 ALERT Basic Issue ▪ July 31/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) (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”. (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” Page 11 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 12 S-76 ALERT ASB 76-31-5 SERVICE BULLETIN Basic Issue ▪ July 31/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) “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” “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”. Page 12 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 13 ASB 76-31-5 S-76 ALERT Basic Issue ▪ July 31/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) (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 of EXT PWR. (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 15. Page 13 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 14 S-76 ALERT ASB 76-31-5 SERVICE BULLETIN Basic Issue ▪ July 31/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) NOTE: Disregard DU S/W VER DATA, as they are not modified by this ASB. (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. I. Re-identify RDAU 76450-01098-106 to 76450-01098-112 using new identification plate (696- 863-007) and modification label (696-493-001) as follows (Refer to Figure 16): 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). Page 14 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 15 ASB 76-31-5 S-76 ALERT Basic Issue ▪ July 31/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) (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 needs replacing, do the following: (a) Using adhesive cleaner (3M General Purpose Adhesive Cleaner or equivalent), remove existing adhesive from the 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) Install 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 needs replacing, do the following: (a) Using adhesive cleaner (3M General Purpose Adhesive Cleaner or equivalent), remove existing adhesive from the modification label (696-493-001). (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 identification plate (696-493-001). (10) Install modification label (696-493-001) onto RDAU (76450-01098-112), if applicable. Page 15 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 16 S-76 ALERT ASB 76-31-5 SERVICE BULLETIN Basic Issue ▪ July 31/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) (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. Update DU (76450-01098-101) per SB 76-006, Software Update for Display Unit (DU) (76450- 01098-101), basic issue or later revision. K. Install electrical compartment access panel on baggage compartment aft bulkhead. L. Return helicopter to service. Page 16 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 17 (OCR) ASB 76-31-5 S-76 ALERT Basic Issue • July 31/18 SERVICE BULLETIN Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) TO RDAU • • 1 CHASSIS GND PRG_ENABLE asy -O 2 PRG_ENAB DH_ENABLE -O 3 DH_ENAB — TO PC • WRAP S3 10 -O 7 RXD + + RXD 2 O • XMIT → TXD 3 O 4 0 O 8 TXD → GND 5 O 6 0 7 0 • 6.9 GND 8 O 9 0 CONNECTOR P / N: MS27473E10B13S 199-914-001 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 SOFTWARE ATA UPDATE 31-60-01 Page 17 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 18 S-76 ALERT ASB 76-31-5 SERVICE BULLETIN Basic Issue ▪ July 31/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) LAPTOP TO RDAU INTERFACE FIGURE 2 Page 18 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 19 ASB 76-31-5 S-76 ALERT Basic Issue ▪ July 31/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) RSPU MAINTENANCE INTERFACE HARNESS FIGURE 3 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 76-31-5 SERVICE BULLETIN Basic Issue • July 31/18 Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) A AccuTerm 7 vizard - Connecton Opuons Please select the desired type of connection from this list. PC directly to a modem attached to the host computer, select Modem. Connection type: Serial Port Serial Port the wizard and enter settings directy Secure Shell At any time, you can click the "Sessi Telnet e future, do not you never want to use the wizard to SSL/Telnet his wizard Session settings... Next > Einish Create a new session or open an existing one ACCUTERM 7 • Inbox - mario, a. Skype for Busin... Kronauer, BRA... • AccuTem 7 Pa Presentation -.. = UR 7/19/2017" 1:57 PM TD4429 CONNECTION OPTIONS WINDOW FIGURE 4 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 76-31-5 S-76 ALERT Basic Issue • July 31/18 SERVICE BULLETIN Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) A AccuTerm 7 File Edit View Tools MultiValue Window Help AccuTerm Connection Wizard - Port Selection Please select the serial port that is connected to your host 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: COM5: Session settings... Cancel < Back Create a new session or open an existing one L start ACCUTERM 7 • Inbox - mario.a... So Skype for Busin... • Kronauer, BRA... A AccuTer 7 Pa Presentation .. = CR 115200 TD4430 PORT SELECTION WINDOW FIGURE 5 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 76-31-5 SERVICE BULLETIN Basic Issue - July 31/18 Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) A AccuTerm 7 on Wizard - 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 lata format used between the computers, and Handshake ontrols the flow of data from one computer to the other. The port settings on your PC and the host computer must match Tor a relable connecton. Baud rate: 38400 Data bits: Stop bits: 1 Parity: Handshake: Session settings.. Cancel Next > Finish Create a new session or open an existing one Start ACCUTERM 7 C Inbox - mari.. S Skype for Bu... • Kronauer, B.. TD4434 BAUD RATE SELECTION WINDOW FIGURE 6 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 76-31-5 S-76 ALERT Basic Issue • July 31/18 SERVICE BULLETIN Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) A AccuTerm 7 ion Wizard - Terminal Type All that's left is to choose the type of terminal you want to emulate from the list below. Then click on the 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: LY Session settings... Cancel < Back Einish Create a new session or open an existing one L Start ACCUTERM 7 Og Inbox - mario,.. S skype for Busin.. • Kronauer, BRA... Pa Presentation ... A AccuTerm 7 = C 7/19/2017 2:06 PM TD1132 TERMINAL TYPE WINDOW FIGURE 7 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 76-31-5 SERVICE BULLETIN Basic Issue • July 31/18 Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) ^ AccuTerm Z-Irdau Z_19_201Z1 File Edit Vie AccuTerm Settings Category: General Options Connection Settings 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 ›cal echo (half duplex) - Modem • Terminal • Clear high bit of received data - Screen - Colors Attribute Colors Palette Keyboard - Background • Display connection warnings Font & Character Set Sounds • Close session on disconnect • Printer .. Screen Print •Slave Printer Clipboard • Mouse • File Transfer • MultiValue Rules • Windows OK Cancel Apply * • 1,1,1 ACCUTERM 7 • Inbox - mario,.. Skype for Busin.. • Kronauer, BRA. : CR 7/19/2017 2:11 PM TD4433 CONNECTION SETTINGS FIGURE 8 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 (OCR) ASB 76-31-5 S-76 ALERT Basic Issue • July 31/18 SERVICE BULLETIN Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) ^ AccuTerm Z-Irdau Z_19_20171 File Edit Vie AccuTerm Settings Category: - File Transfer Settings General Options Files & Folders - ASCII Options i rdau_7_19 Connection - Telnet nterline delay 30 ÷ m • Secure Shell - Private Key Kermit Options Serial Port 10 = sec Terminal - Screen • Quote eighth bit - Colors 30 ÷ Attribute Colors Error retries: • Use data compression • Palette • Use CBC block check - Background - Keyboard - Font & Character Set - X/Y/Zmodem Options • Sounds modem timeout: modem timeout: •• Printe 10 = seC 10 sec • Screen Print - Slave Printer • Initiate Zmodem downloads automatically • Clipboard • Mouse - Defaults • File Transfer • MultiValue Rules • Text C Binary • Windows Text file encoding No encoding • Overwrite existing files Cancel Apply & •1,1,1 • Start 1 Inbox - mario.a.. S Skype for Busin. Kronauer, BRA... Pg Presentation 1 .. = C 7/19/2017 2:16 PM TD4434 FILE TRANSFER SETTINGS FIGURE 9 SOFTWARE ATA UPDATE 31-60-01 Page 25 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 26 S-76 ALERT ASB 76-31-5 SERVICE BULLETIN Basic Issue ▪ July 31/18 ATA 31-60-01 SOFTWARE UPDATE Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) PRE-UPLOAD IIDS DISPLAY UNIT FIGURE 10 Page 26 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 27 (OCR) ASB 76-31-5 S-76 ALERT Basic Issue • July 31/18 SERVICE BULLETIN Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 0100: ^ • FLIGHT TESI → • 1 • Network • sussffOu › shflssveZeng • 5-76 Project 1022 • Mission Systems Integration > S-76 RDAU > Parker Docs › Contents of SW CD 553-096-008 Rev-zip » 553096008 Rev - • © Search 553096008 Rev - Password size Ratio Date modified • 555096003 Rev D 11/9/2017 2:09 PM 555006004 Rev A 11/9/2017 2:09 PM = Document 11/9/2017 2:09 PM • Downloads • 555096010 Rev B File folder 11/9/2017 2:09 PM • Pictures • ASB 107 • FLIGHT TEST • MASTER • MASTER REF DOC = This PC • Desktop E Documents • Downloads J Music • Pictures • Videos OSDisk (C:) = ENTERPRISE (1 SUS: * Network TD4491 SELECT FOLDER WINDOW FIGURE 11 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 76-31-5 SERVICE BULLETIN Basic Issue • July 31/18 Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) 555096009 Rev B Home Extract I MAD ER MASTER REF DOC FLIGHT TEST → • + « sussffOu › shflssvc2eng » S-76 Project 1022 » Mission Systems Integration > S-76 RDAU > Parker Docs of SW CD 553-096-008 Rev - zip > 553096008 Rev - → 555096009 Rev B & Search 555096009 Rev B • Name compressed size Date modified * Quick access • Desktop • SHT1.CHA • SHT1.CHB CHA FilE CHB File 1O KB NO 76KB No 209 KB 1478 289 KB 74% 8/1/20176:16 PM 8/1/2017 6:16 PM • Documents • SHT1.CHC CHC File 76 KB No 289 KB 74% 8/1/2017 6:16 PM • Downloads • SHT2.CHA CHA FIle 15 KB No 289 KB 95% 8/1/2017 6:16 PM • PIctureS I SH12.CHB CHB File 15KB No 289 KB 95% 8/1/2017 6:16 PM • ASB 107 • SHT2.CHC CHC Fille 15 KB No 289 KB 95% 8/1/2017 6:16 PM • FLIGHT TEST MASTER • MASTER REF DOC _ This PC • Desktop • Documents • Downloads f Music • Pictures • Videos - OSDisk (C:) = ENTERPRISE (ASUS: TD4490 SELECT FILE TO UPLOAD WINDOW FIGURE 12 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 76-31-5 S-76 ALERT Basic Issue • July 31/18 SERVICE BULLETIN Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) cuTerm 2K2 - [576_STE e Edr Yew Iooks Beset Window D208208000.? HOST OFP FILE 1 IS DOWNLOADED SUCCESSFULLY, SEND FILE 2 proc=4, Device=0 a g 1,3,1 ¿ Start @ @ * [ AccuTerm 2K2 - [576. 2] DOWN_LOAD. doc - Micr... My Computer 1D CO._102 Microsoft Office * « 0g UP 9:30 AM TD4492 SUCCESSFUL DOWNLOAD OF SHT1.CHA FILE FIGURE 13 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 76-31-5 SERVICE BULLETIN Basic Issue • July 31/18 Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) LE AccuTerm 2K2 - [576_STE (1)] 28200405! OFP IS DOWNLOADED SUCCESSFULLY: PART = 555096009 VER = 2A44 CHECKSUM = 733DAB02 Proc=4, Device=0 • 576_STE (1) 8 g 1,6,1 g 80,24,1 g DEC VT100 Ed Idle [2g Capture Off ga Comg | 3, 38400,0,8,1,N TD4193 Start e 3 a * [ AccuTerm 2k2 ] Document1 - Microsoft... | Macrosoft Ofice » «93 (: 1257 PM SUCCESSFUL DOWNLOAD OF SHT1.CHB FILE FIGURE 14 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 76-31-5 S-76 ALERT Basic Issue • July 31/18 SERVICE BULLETIN Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) Parker GULL ELECTRONIC SYSTEMS DIvIsION COPYRIGHT © 1996, 1997 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 MENU TD4494 IIDS DISPLAY UNIT WITH SOFTWARE VERSION NUMBERS FIGURE 15 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 (OCR) S-76 ALERT ASB 76-31-5 SERVICE BULLETIN Basic Issue • July 31/18 Section 3. ACCOMPLISHMENT INSTRUCTIONS (Continued) REMOVE: 696-794-002 IDENTIFICATION PLATE (1) INSTALL: 696-863-007 IDENTIFICATION PLATE - 1 REQ'D CAUTION J10 CAUTION STATIC AIR PORT 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 0" THERE IS NO NEED TO INSTALL A NEW MODIFICATION LABEL. TD4586 IDENTIFICATION PLATE AND MODIFICATION PLATE INSTALLATION FIGURE 16 ATA SOFTWARE Page 32 31-60-01 UPDATE This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 33 ASB 76-31-5 S-76 ALERT Basic Issue ▪ July 31/18 SERVICE BULLETIN ATA 31-60-01 SOFTWARE UPDATE Section 3. A CCOMPLISHMENT INSTRUCTIONS (Continued) M. 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 33 This Document Contains Technical Data Controlled by the EAR. See WARNING and classifications on first page. ### Page 34 (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. 76-31-5 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 35 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 36 Customer Support Operations SERVICE BULLETIN Initial Issue May 10, 2018 367-111-77-004 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 367-111-001 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) 367-111-001, Sikorsky P/N 76450-01098-106. B. Concurrent Requirements None. C. Reason The RDAU P/N 367-111-001 has been updated to 367-111-102 (Siko rsky P/N 76450-01098- 106 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 Assuranc e page incorrect. Label 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. ### Page 37 Customer Support Operations SERVICE BULLETIN Initial Issue May 10, 2018 367-111-77-004 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 367-111-001 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, S-76 C+ Model: Pub No. IIDS S-76 PM004 Rev. B, October 4, 2017. Parker Hannifin, Operators M anual, S-76 C++ Model: Pub No. IIDS S-76 PM003 Rev. B, October 4, 2017. ### Page 38 Customer Support Operations SERVICE BULLETIN Initial Issue May 10, 2018 367-111-77-004 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 Not applicable. 2. MATERIAL INFORMATION A. Material - Price and Availability RDAU, P/N 367-111-001 (Sikorsky P/N 76450-01098-106) 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 F AX HOTLINE: (949) 809-8444 Hauppauge, NY 11788 TECHNI CAL 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 467-743-0 01 or 467-743-002 FSD Parker Oscilloscope TDS 440A Tektronix STE ATP Software (For 367-111-001 and 367-111-102) 577-096-012 FSD Parker ### Page 39 Customer Support Operations SERVICE BULLETIN Initial Issue May 10, 2018 367-111-77-004 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 696-794-002 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 696-794-002 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 367-111-001 (Sikorsky P/N 76450-01098-106) will be re-identified as P/N 367-111-102 (Sikorsky P/N 76450-01098-112). ### Page 40 Customer Support Operations SERVICE BULLETIN Initial Issue May 10, 2018 367-111-77-004 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 (OF P) programming procedure. On the 199-382-001 test set, sel ect the following switch positions 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 both -001 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 complet e, 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 complet e, the computer will display a message indicating the download was successful and will prompt for the next step. ### Page 41 Customer Support Operations SERVICE BULLETIN Initial Issue May 10, 2018 367-111-77-004 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 DISCONTINUED UPON REQUEST BY PARKER. COPYRIGHT PARKER. YEAR OF COPYRIGHT IS FIRST YEAR INDICATED ON THIS DOCUMENT. ALL RIGHTS RESERVED. On the test set computer, select: (a) Board A, B and C for the FUEL. (b) The computer will promp t for entry of software. (c) When the download is complet e, the computer will display a message indicating the download was successful and will prompt for the next step. (d) Press Escape k ey (ESC) to exit. 4. APPENDIX Figure 1 Test Set and RDAU Connection Diagram. --- 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.