REV DCA DATE DRAWN CHECKED APPROVED PUBLISHED A W /14/2014 Don Mathiesen Jay Jensen Robert Davis Linda Andujo

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NEITHER RECEIPT NOR POSSESSION OF THIS DOCUMENT CONFERS ANY RIGHT TO REPRODUCE, USE OR DISCLOSE, IN WHOLE OR IN PART, ANY INFORMATION CONTAINED IN THIS DOCUMENT WITHOUT WRITTEN AUTHORIZATION FROM

1 REVISION HISTORY Refer to the DCA and associated markups for a complete description of the changes incorporated in a revision. REV DCA DATE DRAWN CHECKED APPROVED PUBLISHED A W /14/2014 Don Mathiesen Jay Jensen Robert Davis Linda Andujo THIS DOCUMENT CONTAINS PROPRIETARY INFORMATION. NEITHER RECEIPT NOR POSSESSION OF THIS DOCUMENT CONFERS ANY RIGHT TO REPRODUCE, USE OR DISCLOSE, IN WHOLE OR IN PART, ANY INFORMATION CONTAINED IN THIS DOCUMENT WITHOUT WRITTEN AUTHORIZATION FROM WULFSBERG ELECTRONICS. Chelton Avionics, Inc. dba Wulfsberg Electronics Division Prescott, AZ CAGE CODE 1WZE2 A PRINTED COPY OF THIS DOCUMENT MAY NOT BE THE LATEST REVISION. IT IS THE USER S RESPONSIBILITY TO ENSURE THAT HE OR SHE IS USING THE LATEST DOCUMENT REVISION. THE LATEST REVISION MAY BE VIEWED OR PRINTED FROM THE ELECTRONIC DOCUMENT DISTRIBUTION SYSTEM. DOCUMENT TITLE SERVICE BULLETIN, CSB JETLAN- AVIOP-01 AvioIP V2.2 SW Installation SIZE A LRU JETLAN DOCUMENT NUMBER REV A Typed signatures indicate approval. Handwritten signature approval of this document is on file at Wulfsberg Electronics, Prescott, Arizona. SCALE: NONE DO NOT SCALE DRAWING Rev A Page 1 of 10

2 SERVICE BULLETIN EQUIPMENT: PAR-6259, PAS-6273 DATE: 7/15/2014 BULLETIN NUMBER: CSB JETLAN-AVIOP-01 REVISION: A Section 1 Planning Information 1.0 Implementation Approval Factory Repair Station Only 1.1 Compliance Upon customer request or any PAR-6259 or PAS-6273 received with AvioIP Revision 2.2 Software previously installed. 1.2 Description Load Satcom1 AvioIP Version 2.2 software on to the JetLAN. 1.3 Applicability Model(s) PAR-6259, Part Number B09 and PAS-6273, Part Number AS Reason To provide the customer with this revision (2.2) of AvioIP Software when requested by the customer or when there is no other applicable Service Bulletin for the installation of a newer revision of AvioIP Software. 1.5 Approval This modification does not affect the original approval. 1.6 Costing/Parts and Labor N/A Rev A Page 2 of 10

3 1.7 Equipment Required Quantity Description Part Number 1 USB Flash Drive with AvioIP V2.2 Installer CheckSum: 4a39a280be1a3afb0c1677e1 796a785c Part Number can be created using document # _648-0 (latest rev.), Software Configuration Index for the AviopIP V2.2 Installer USB Flash Drive. 1.8 Software Configuration Software Component (SWID N/A) Location Description Device Type Ver Rev Load Module Part Number N/A N/A N/A N/A N/A N/A N/A 1.8 Weights and Balance There is no appreciative change to the weight or balance of the unit. 1.9 Electrical Load Data There is no appreciative change to the Electrical Load Data of the unit Other Publications Affected N/A 1.11 Reference Documents Document Number Description CMM for the PAR-6259 Section 2 Procedure Instructions 2.1 Modification Procedure UUT CONFIGURATION PRIOR TO LOADING AVIOIP SOFTWARE 1. The UUT (Unit Under Test) must have successfully completed all steps in the ATP called out in the Test CID applicable to the unit. 2. Connect the rear ARINC connector on the ATP Test Cable to the AX250 rear ARINC Connector. 3. Connect the ATP test cable s ZIF connector to the Server Test Set. 4. Be prepared to connect the ATP cables power connections to the 28VDC Power supply when directed to apply UUT power per this procedure. 5. Connect the round maintenance connector on the test cable to the AX250 front maintenance connector Rev A Page 3 of 10

The steps in this paragraph are done using the keyboard connected to the UUT. The results will show on the Video monitor connected to the UUT. 2.

4 6. Connect the VGA monitor to the VGA monitor connector that comes from the ARINC connector on the ATP Cable. 7. Connect the PS-2 Keyboard to the Keyboard connector that comes from the rear of the ARINC connector AVIOIP SOFTWARE LOAD PROCEDURE 1. The steps in this paragraph are done using the keyboard connected to the UUT. The results will show on the Video monitor connected to the UUT. 2. Be prepared to select the DELETE key after applying power to the AX Apply power to the UUT. 4. Press DELETE to enter the BIOS setup utility. 5. Load the factory default BIOS settings. 6. Change the BIOS settings to that in BIOS SETTINGS, column Settings for Loading. 7. Exit BIOS setup utility, saving the settings. The video display will sequence to a screen that says No bootable device available. R Reboot S Setup. 8. Now, connect the USB Flash Drive (PN: ) to the USB connector that comes from the front maintenance connector. [The USB is not connected until this step, to get around a problem with some flash drives not being identified as boot devices.] 9. Press r to reboot the unit. 10. Wait for the prompt Do you want to install AvioIP 11. Select yes with the arrow 12. Press enter. It will take more than 40 minutes to complete the loading process. 13. Wait until INSTALLATION FINISHED appears. 14. Press Enter Rev A Page 4 of 10

5 15. Wait until Will now Halt. System halted. appears. 16. Power Off the target JetLAN 17. Remove the USB Flash drive. Apply power to the UUT. 18. Attach UUTs P9 Ethernet 3 cable directly to NIC 1 on the test PC. The NIC on the test PC should be configured to automatically obtain the IP address. It may be necessary to disable the Network Connection (NIC), then enable it, for the change to be affective. 19. Power-up the UUT. 20. Press DELETE to enter the BIOS setup utility. 21. Change the BIOS settings to that in BIOS SETTINGS, column Settings for AvioIP. 22. Exit BIOS setup utility, saving the settings. Wait until the UUT boots up to the login screen. 23. Open a web browser (such as MS Internet Explorer, or Firefox). On the web browser address line, enter: then Enter. 24. The SATCOM1 web page, shown below, should appear. If the web page does not appear, then the software load has failed. 25. Select Skip Wizard repeatedly until a page with the About selection is available. 26. Select About and verify that the version of AvioIP is that which you installed Rev A Page 5 of 10

6 27. Power down the UUT Rev A Page 6 of 10

7 2.1.3 BIOS SETTINGS Changes from the Factory Default are highlighted. Section Parameter Factory Default Settings For Loading Date and Time Date Time Drive Assignment Drive A 1.44 MB 3.5" (none) (none) Drive B (none) (none) (none) Settings For AvioIP Drive C HDD Pri Master USB HDD HDD/CF Sec Slave Drive D (none) (none) USB HDD Drive E (none) (none) (none) Drive F (none) (none) (none) Drive G (none) (none) (none) Boot Order Boot 1st Drive A (Drive C (none) Boot 2nd Drive C (none) Drive D Boot 3rd (none) (none) Drive C Boot 4th (none) (none) (none) Boot 5th (none) (none) (none) Boot 6th (none) (none) (none) Drive and Boot Options Floppy Seek Disabled Disabled Disabled Hard Disk Seek Disabled Disabled Disabled Floppy Swap Disabled Disabled Disabled Boot Method Boot Sector Boot Sector Boot Sector Primary IDE Cable Auto Auto Auto Sec IDE Cable Auto Auto Auto Sec Master ATA Mode LBA LBA LBA Sec Slave ATA Mode LBA LBA LBA Keyboard and Mouse Num Lock Disabled Disabled Disabled Typematic Enabled Enabled Enabled Delay 250 ms 250 ms 250 ms Rate 30 cps 30 cps 30 cps Initialize PS/2 Mouse Enabled Enabled Enabled User Interface Show 'Hit Delete ' Enabled Enabled Enabled F1 Error Wait Disabled Disabled Disabled Config Box Enabled Enabled Enabled Splash Screen Disabled Disabled Disabled Rev A Page 7 of 10

8 Section Parameter Factory Default Settings For Loading Settings For AvioIP Memory Memory Test Fast Fast Fast Memory Hole Disabled Disabled Disabled Shadow D000-D3FF Disabled Disabled Disabled Shadow D400-D7FF Disabled Disabled Disabled Shadow D800-DBFF Disabled Disabled Disabled Shadow DC00-DFFF Disabled Disabled Disabled Power Management ACPI Enabled Enabled Enabled APM Disabled Disabled Disabled Advanced Features Post Memory Manager Disabled Disabled Disabled CPU Serial Number Enabled Enabled Enabled Watchdog Timeout (secs) Disabled Disabled Disabled Serial Console Hot Cable Hot Cable Hot Cable Port 3F8h 3F8h 3F8h SMM Support Enabled Enabled Enabled USB Boot Support Disabled Enabled Enabled Lan Boot Disabled Disabled Disabled On-Board Serial Ports Serial 1 3F8h 3F8h 3F8h IRQ Mode RS-232 RS-232 RS-232 Serial 2 2F8h 2F8h 2F8h IRQ Mode RS-232 RS-232 RS-232 Serial 3 3E8h 3E8h 3E8h IRQ Mode RS-232 RS-232 RS-232 Serial 4 2E8h 2E8h 2E8h IRQ Mode RS-232 RS-232 RS-232 On-Board LPT Port LPT1 378h 378h 378h IRQ DMA Mode Standard Standard Standard On-Board Controllers Floppy (irq 6) Enabled Enabled Enabled Primary IDE (irq 14) Enabled Enabled Enabled Sec IDE (irq 15) Enabled Enabled Enabled Rev A Page 8 of 10

9 Section Parameter Factory Default Settings For Loading Settings For AvioIP PS/2 Mouse (irq 12) Enabled Enabled Enabled USB 4 Ports 4 Ports 4 Ports Audio Enabled Disabled Disabled On-Board Video Framebuffer Size 16 MB 16 MB 16 MB AGP Aperature 128MB 128MB 128MB Off-Board Primary Disabled Disabled Disabled Display CRT CRT CRT Panel Type None none none PCI INTA IRQ INTB IRQ INTC IRQ INTD IRQ INTE IRQ INTF IRQ INTH IRQ Plug and Play PnP BIOS Enabled Enabled Enabled PnP OS Enabled Enabled Enabled Assign IRQ 1 Disabled Disabled Disabled Assign IRQ 3 Enabled Enabled Enabled Assign IRQ 4 Enabled Enabled Enabled Assign IRQ 5 Enabled Enabled Enabled Assign IRQ 6 Disabled Disabled Disabled Assign IRQ 7 Enabled Enabled Enabled Assign IRQ 9 Enabled Disabled Disabled Assign IRQ 10 Enabled Enabled Enabled Assign IRQ 11 Enabled Enabled Enabled Assign IRQ 12 Disabled Disabled Disabled Assign IRQ 14 Disabled Disabled Disabled Assign IRQ 15 Disabled Disabled Disabled Assign DMA 0 Disabled Disabled Disabled Assign DMA 1 Disabled Disabled Disabled Assign DMA 2 Disabled Disabled Disabled Assign DMA 3 Enabled Enabled Enabled Assign DMA 5 Enabled Enabled Enabled Assign DMA 6 Enabled Enabled Enabled Rev A Page 9 of 10

10 Section Parameter Factory Default Settings For Loading Settings For AvioIP Assign DMA 7 Enabled Enabled Enabled 2.2 Identification Procedure N/A 2.3 Acceptance Test procedures N/A Section 3 Material Information/Parts Required N/A Section 4 Warranty Information This modification is covered under warranty. Section 5 Illustrations All applicable illustrations provided throughout the modification procedure END Rev A Page 10 of 10

REV DCA DATE DRAWN CHECKED APPROVED PUBLISHED A W /09/2014 John Rodriguez Jay Jensen Robert Davis Linda Andujo

REVISION HISTORY Refer to the DCA and associated markups for a complete description of the changes incorporated in a revision. REV DCA DATE DRAWN CHECKED APPROVED PUBLISHED A W13998 07/09/2014 John Rodriguez