Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-36. (Sheet 8 of 8) JetWave™ System Interconnect Diagram - FMA (KRFU Outside Aircraft Fuselage), (90401047-1, REV F) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-37. (Sheet 1 of 12) Alternative KRFU Outside Aircraft Fuselage Configuration (90405210, REV D) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-37. (Sheet 2 of 12) Alternative KRFU Outside Aircraft Fuselage Configuration (90405210, REV D) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-37. (Sheet 3 of 12) Alternative KRFU Outside Aircraft Fuselage Configuration (90405210, REV D) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-37. (Sheet 4 of 12) Alternative KRFU Outside Aircraft Fuselage Configuration (90405210, REV D) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-37. (Sheet 5 of 12) Alternative KRFU Outside Aircraft Fuselage Configuration (90405210, REV D) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-37. (Sheet 6 of 12) Alternative KRFU Outside Aircraft Fuselage Configuration (90405210, REV D) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-37. (Sheet 7 of 12) Alternative KRFU Outside Aircraft Fuselage Configuration (90405210, REV D) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-37. (Sheet 8 of 12) Alternative KRFU Outside Aircraft Fuselage Configuration (90405210, REV D) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-37. (Sheet 9 of 12) Alternative KRFU Outside Aircraft Fuselage Configuration (90405210, REV D) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-37. (Sheet 10 of 12) Alternative KRFU Outside Aircraft Fuselage Configuration (90405210, REV D) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-37. (Sheet 11 of 12) Alternative KRFU Outside Aircraft Fuselage Configuration (90405210, REV D) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-37. (Sheet 11 of 12) Alternative KRFU Outside Aircraft Fuselage Configuration (90405210, REV D 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System SECTION 5 SOFTWARE CONFIGURATION 5.1 ARINC 615A Software Data Load Process A. Introduction As a minimum, APM system configuration files need to be loaded onto the JETWAVE™ system. The JetWave™ LRUs are preloaded with a full software load and there may be a need to perform a field data load under normal conditions during installation.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System as an Electronic Flight Bag (EFB) or other portable computing device, an on-board portable device, or an avionics device. Since the Aircraft loading procedures can vary due to different type of uploading means, it is recommended to refer to the appropriate Aircraft Maintenance Manual before attempting data loading of JetWave™ AES system. C.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System : Table 5-1.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System For the ARINC 615A data load operations, an A615A target connection must be defined. Target connection defines a TFTP client on the Modman and TFTP server on the data loader that will be used for file transfer. D. Procedure (AIT Flight Simulyzer v3.0.0) (1) Refer to the latest revision of SBs JETWAVE-23-0001, JETWAVE-23-0002, and JETWAVE-23-0003 or later SB for the software upload procedures.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (c) Right click “Lan Configuration” and select “Import HostLan Configuration…” (d) Browse to the “LanConfig.hex” file and select “Open”. (This file needs to be present by the installer on the data loader computer.) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (e) Expand “Lan Configurations” and then also expand “TFTP” on the left side of the screen. 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (f) Select “Client Configurations” on the left side of the screen and verify the settings appear as in the screenshot below. 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (g) (3) Select “Server Configurations” on the left side of the screen and verify the settings appear as in the screenshot below. Data-loading GXA with the AIT Flight Simulyzer Software NOTE: Replace “” below with the LRU to be loaded. (a) Power on the system. (b) Wait until the Modman front panel LEDs (‘POWER’ and ‘STATUS’) are both solid green in color.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Log in and view the system status info at the top of the GUI window. At the GUI login, the username is "User" and there is no password. (e) Wait until all of the LRUs indicate a status of “OK” before continuing, to ensure the system has booted up fully.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (f) In the AIT ‘Flight Simulyzer’ application, select the “Simulation” button on the left side of the screen. 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (g) The LRU name (i.e. ‘GXA ’) should now be visible in the left side window pane under “A615A Data Loader”. (h) Right click the LRU name (‘GXA ’) on the left side window pane and select “Load Operations…” 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (i) Select the “Refresh” button near the bottom right part of the screen. (j) Verify that the “Target Information” for the LRU appears on the right side of the screen. This will ensure communication between the 615A Data Loader and the Modman. 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (k) Select “Add LSP…” and browse to the .luh file in the 665 data load package for the LRU, select it and click “Open”. 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (l) The package should now be visible in the “File Transfer” window. (m) Select the “Upload” button when ready to begin the transfer to the LRU. (n) When complete, the “Status” heading in the “File Transfer” window will indicate “Complete” and a green status bar at the bottom of the screen will indicate “Data load 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System has completed successfully. Once all LRUs are updated, de-assert the data load discrete to reset the system (100%)”. (o) If loading additional software, again execute the steps above starting with Step (h). (p) Once all software upgrades are completed, toggle the ‘Data Load Enable’ discrete to the ‘Disabled’ state. This will cause a system reboot.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System the VDDs which were loaded. For details on the software versions, refer to the applicable SB. E. A615 LanConfig.Hex File Creation and Settings (1) Open the AIT Flight Simulyzer Tool and select the ‘Settings’ pushbutton. Under the local host tree, select the “A615A DataLoader”. Select “ADD” to add the seven entries as shown in Step (b).
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (2) Enter all the A615A DataLoader settings as shown in the following screenshots. 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (3) In the Local Host Tree, select “ Lan Configuration”, “TFTP”, “Client Configurations”. Enter the settings as shown in the following screenshots. 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (4) In the Local Host Tree, select “ Lan Configuration”, “TFTP”, “Server Configurations”. Enter the settings as shown in the following screenshots. 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (5) Once all settings have been entered, select “LAN Configuration” from the tree and right click, “Export HostLan Configuration to a file.” Save to a folder and name the file LanConfig.hex. (6) This configuration file can now be loaded anytime you want to run a data load. 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System SECTION 6 SYSTEM COMMISSIONING 6.1 Provisioning of User Services Within the JetWaveTM system, the Modman LRU is responsible for bringing Inmarsat satellite network IP access to onboard users through In-flight Entertainment Systems or through Onboard Network Systems.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • Satcom1/GoDirect • Satcom Direct • SITA OnAir • Thales • ARINC Direct The actual throughputs achieved by the GXA terminal are dependent on the Operator subscription. Each subscription will have a defined Committed Information Rate which is the minimum throughput guaranteed to each subscriber. The delivered services will be able to exceed those CIRs where the resources allow up to defined Maximum Information Rate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System B. 6.2 Terminal Activation (1) To activate the terminal with your service provider you need to provide the ACM TPK. (2) The TPK is written on the test report document delivered with the MODMAN. (3) The TPK may be viewed using the MODMAN GUI. Certification and Approvals All antenna installations must obtain the approval of the appropriate government air/radio authority, such as the FAA, EASA, or Transport Canada.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System The GUI AES status summary screen lets the user navigate to all applicable options. At the User level, the Other Information & Control has an option to display the current Aircraft ID stored in the AES Configuration data. Refer to Figure 6-1 for the AES aircraft ID information page. Figure 6-1. Aircraft ID Display/Update Information Page The JetWave™ system LRUs are shipped with the operational software preloaded.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System There are two LEDs on the front panel of Modman. One is for the power and the second one is for status. Use Table 6-1 to identify the current operating mode of Modman with the power LED indicating powered up status. Table 6-1. Modman LED Status Indications Status LED Mode Off No electrical power/electrical power is supplied but prior to boot.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 6-2. AES GUI Login Page (a) The GUI is configured to have the login accounts that follow: • User interface with Username: “User” and Password: empty (no) password • Maintenance interface with Username: “Maintenance” and Password: “Earthbound”. On successful login, the AES Home page screen is shown. Refer to Figure 6-3.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 6-3. AES Home and Status Info Page View and verify the AES configuration data, navigate to the "Configuration Files" information pages under the other information and control menu. The typical configuration file information page is shown in Figure 6-4. To view and make sure that the AES configuration settings are current, click the AES configuration file to display.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 6-4. View Configuration Files Page To view the health status of the JetWave™ system, navigate to the “AES Summary and Link Status” under the Health Statuses menu on the left. This will allow you to view and make sure of the health status of the JetWave™ system. The AES summary and interlink status are shown in Figure 6-5. Figure 6-5.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System To see the AES LRUs hardware and software version and part number, navigate to the Version and Manufacturing Information menu. Figure 6-6 shows the typical Modman Version and Manufacturing Information page. Make sure the version and manufacturing information are current for all the LRUs. NOTE: Follow appropriate Jetwave Service Bulletin reference to validate the SW currently installed on the Jetwave system. Figure 6-6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System C. Discrete Input Testing (1) If wired, activate the Modman Reset by toggling Modman reset switch on the JetWave™ AES control panel. (2) If the Modman Reset is not wired, then reset the system from the GUI. (3) Monitor the Modman ”power” and “status” LEDs flash continuously. (4) Toggle the Modman Reset switch on the Satcom test panel to the open/non-grounded position.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Once the JetWave™ system starts receiving the valid navigational input from aircraft IRS system, make sure that the values are correct as compared to the aircraft navigational system outputs. Figure 6-9. Aircraft Statuses E. Manual Steering of the Antenna To do a commanded test to manually steer the antenna, navigate to "Manual Antenna Steering" under the commanded test menu.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 6-10. Manual Antenna Steering F. System Available (Cockpit Control Panel) Output Once the JetWave™ system is powered up, monitor the “System Available” status discrete. Make sure that the discrete state agrees with the discrete output in the GUI. Refer to Figure 6-11. 6.4 Cable Calibration The Modman will not transmit until it has been calibrated, with the transmit cable calibration.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System initiate the "Calibrate Transmit Cable" commanded test. The recommendation is not mandatory and Jetwave will continue to operate at a high level of performance over the service life. To maintain a fully optimized Jetwave system, it is recommended to perform a single cable calibration in the 20 year service life, at around 8,000 to 12,000 hours of operation.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (3) It is required to do the automatic antenna alignment calibration with the Radome installed. The antenna alignment process can be initiated through the GUI interface. The JetWave™ system GUI service is supported on AV1 10/100 Base T Ethernet interfaces (AV1 being default configuration, ports may vary depending on specific APM configuration).
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 6-13. GUI Calibrate Antenna Alignment Page (2) For the automatic antenna alignment calibration, it is recommended to tow and put the aircraft in an open area away from aircraft hangars such that there is clear visibility to the open sky with the true heading (not magnetic heading) of the aircraft pointed in one of four recommended aircraft true heading values displayed on the GUI antenna calibration page.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (4) The recommended values are dependent on the radome and these values are calculated by the KANDU based on the input from the aircraft IRS and the selected satellite coordinates and the APM configuration data. The Auto Alignment application automatically presents the four true headings to the operator when a target satellite is selected from the “recommended” target which is also location dependent.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 6-14. GUI Antenna Alignment Calibration Page Extract 6.6 On-ground Testing and Commissioning NOTE: There are restrictions to testing the JetWave™ system for the commissioning process. Each country has its own restrictions to on-ground testing and transmission. Verify regulations before testing the system. Particular attention must be observed the first time the system is turned on and able to transmit.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • If AES Configuration System wow is configured to be connected and it is indicating it is in the air. (3) B. Ground transmission can be enabled by asserting the ground transmit enable discrete of the JetWave™ system. (a) The ground operation depends on location and country of aircraft registration.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System NOTE: Based on the geographical location, surrounding obstructions, etc., the 360 degree connectivity access can be limited. Verify that the connectivity remains available through the 360-degree turn by monitoring the datalink status discrete. Connect to each of the configured Ethernet ports to make sure there is data connectivity. Figure 6-15. Network Statuses B.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System SECTION 7 TROUBLESHOOTING 7.1 Post-installation Troubleshooting This section supplies troubleshooting procedures for the JetWave™ system. Airline maintenance engineers can troubleshoot the JetWave™ system on the ground, with the health status information and Fault Details and Isolation assistance displayed on the AES GUI.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (6) Use the applicable login account with well defined password in the login page for accessing the interface level required. The login for the maintenance interface and user interface is as follows: • Access maintenance interface with Username: “Maintenance” and Password: “Earthbound”. • Access the user interface with Username: “User” and no password. (7) User may press Log out button to log out.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System configuration data is supplied. Figure 7-3 shows the AES Summary and Link Status page. Figure 7-3. JetWave™ Summary and Link Status (Sheet 1 of 2) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 7-3. JetWave™ Summary and Link Status (Sheet 2 of 2) (2) B. The JetWave™ system status can be viewed through the GUI. Refer to AES system status verification section on page 6-3 for description.SUmmary and link status Downloading LRU Logs (1) To view the historical fault logs, under the AES historical logs pane, select the "Fault Log". A screenshot of fault log page is shown in Figure 7-4.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 7-4. JetWave™ Fault Log Download Configuration Page (5) The fault log contains the details that follow: • LRU POST and BITE fault codes • Watch dog reset events • Software exception events • LRU Recorded Temperature, if available • LRU Recorded Time, if available • LRU Antenna pointing information, if applicable • Fault count. Refer to Figure 7-5 for an example of a viewable fault log.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 7-5. JetWave™ Fault Log Data (6) To download the fault log data for analysis and trouble shooting, press the “Download” button. The window as shown in Figure 7-6 will come into view. Save to the computer to open and view the fault log. Figure 7-6. JetWave™ Fault Log Download Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System C. System Data Load Failure (1) Make sure that the system is configured for ground operation. (2) Make sure that the local data load enable switch is closed. (3) Make sure that the ARINC 615A data loader is connected to the correct port: NOTE: Port AV1 is by default the Modman Maintenance Port, but this may have been modified by the APM configuration loaded. D.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System G. JetWave™ System Fault Codes (1) BITE Philosophy (a) Description 1 The JetWave™ AES consists of the Modman, KANDU, KRFU, TMA or FMA LRUs, plus the APM. 2 The APM is a simple memory device with no software and performs no BITE by itself. Any BITE required for the APM is performed by the Modman. The APM is not shown in these diagrams.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 7-8. AES and LRU Controller Interaction 7 The AES Controller resides in the Modman LRU. 8 Each LRU Controller monitors the LRU for BITE events. BITE events are classified into two categories: • Faults: These are BITE events which have a SET state (occurring) or CLEAR state (fault has disappeared). • 9 Events: These are BITE events which occur but do not have a set or clear state.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 11 The AES controller has a sub-part called the AES controller fault and event handler which is in charge of responding to BITE events reported by the AES controller or a LRU controller. 12 The AES controller has its own historical logs which allow it to record events about the whole system.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • For each unique L1 thru L3 code, maintained across reset/power down, it records if the code has occurred (SET), cleared after occurring (CLEAR), or never seen (NO_ERROR). • For each unique L1 thru L3 code, maintained across reset/power down, it records the number of occurrences and the time of the last occurrence.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (2) LRU Codes BITE event information is encoded by the LRUs in three values. The values are named L1 thru L3: • L1 denotes the LRU or interface (generated by an LRU on its behalf) which is generating the event • L2 denotes the Shop Replaceable Module within an LRU for a event relating to an LRU, or for interfaces it denotes a particular part of the interface which is generating the event.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-1.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-1. L1 Codes (Continued) Group L1 Code L1 Description PODD Network 0x 90 PODD Network: Ethernet PG1 0x 91 PODD Network: Ethernet PA1 0x 92 PODD Network: Ethernet PA2 0x 93 PODD Network: Ethernet PA3 0x 94 PODD Network: Ethernet PA4 NOTE: All other codes not explicitly stated are spare.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-2.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-2.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-3.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (c) The event L2 code further identifies ARINC 429 and ARINC 791 discrete interfaces, coded as follows: Table 7-4.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-4. L2 Codes – ARINC Discrete Interfaces L1 L2 Code L2 Description Modman Aircraft Discrete Input (72) 0x 06 WOW 0x 07 Cell TX OK 0x 08 Ground transmit enable 0x 09 Public services disable 0x 0A Remote manager 0x 0B Cooling available 0x 0C Local data load 0x 0C TX control KANDU Aircraft Discrete Input (73) (d) The event L2 code further identifies user interfaces, coded as follows Table 7-5.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (5) L3 Codes (a) The L3 code is four hexadecimal digits, used to uniquely identify the fault or event against an L1, L2 code pair. (b) Each LRU defines their own L3 codes. These are given in the fault table, refer to Table 7-6. Table 7-6. L3 Codes L1 L2 L3 Code L3 Description Repair Action System (00) Unknown (00) 0x 0001 OAE not pointed correctly Try a manual point and see if it works.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action System (00) AES menu access level (02) 0x 0023 Log clearance AES usage historical log - Info events - Recording what happened in the LRU. - If it is a warning, it is info only.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action System (00) Regulatory Log (07) 0x 0000 Regulatory log upload failure NO ACTION –System will continue to try and upload the file as directed by the regulatory log requirements on frequency of upload attempts.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Modman (01) Unknown (00) 0x 0000 Mute state 0x 0011 LRU menu access - maintenance Info events - Recording what happened in the LRU.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Modman (01) Controller/router (02) 0x 0004 Ethernet PIES Switch Hardware faults and events: - Replace the Modman.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Modman (01) Controller /router (02) 0x 0023 RSSI control in/out IO 0x 0024 Unique ID chip Hardware faults and events: - Replace the Modman.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Modman (01) Software configuration (FD) 0x 0001 HW SW compatibility 0x 0002 LRU SW compatibility Reload compatible software with the A615A data loading process. 0x 0003 Configuration parameter missing Reload the configuration data with the A615A data loading process.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action KRFU (02) Unknown (00) 0x 0000 Mute state 0x 0001 Primary power interruption Info events - Recording what happened in the LRU.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action KRFU (02) Software configuration (FD) 0x 0007 Data load 0x 000A Operating image list Info events - Recording what happened in the LRU. 0x 0008 Data loader connected 0x 0009 Data loader disconnected 0x 000B Secondary image corruption warning A reloading of software is required to load a fresh image.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action TMA (03) Unknown (00) 0x 0001 Primary power interruption 0x 0011 LRU menu access - maintenance Info events - Recording what happened in the LRU.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action TMA (03) Position control unit (05) 0x 0001 DSP fault 0x 0002 AZ motor current draw 0x 0003 El motor current draw 0x 0004 Initialization incomplete 0x 0003 OMAP PWR 3.3V: Out-of Spec 0x 0004 OMAP PWR 5V: Out-of Spec 0x 0005 MOT PWR 12V: Out-of Spec 0x 0006 LNA PWR 12V: Out-of Spec Hardware faults and events: - Replace the TMA.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action TMA (03) Software Configuration (FD) 0x 0001 HW SW compatibility 0x 0002 LRU SW compatibility Reload compatible software with the A615A data loading process. 0x 0003 Configuration parameter missing Reload the configuration data with the A615A data loading process.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action TMA (03) Temperature (FF) 0x 0001 Motor driver circuit 0x 0002 Ambient - If is a warning, it is for info only. - If it is critical, the LRU shut itself down functionally: suggest the LRU is not correctly installed or a subassembly in the LRU may be generating too much heat.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action FMA (04) MDU (0B) 0x 0001 1.25V voltage 0x 0002 1.5V voltage Hardware faults and events: - Replace the FMA . 0x 0003 3.3V voltage 0x 0004 12V positive voltage 0x 0005 12V negative voltage 0x 0006 38.5V voltage 0x 0007 1.5V current 0x 0008 3.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action FMA (04) Software runtime (FE) 0x 0000 Heartbeat failure 0x 0001 General Module Failure 0x 0006 Application Controller Database Invalid 0x 0007 Application Not Present 0x 0008 Application Unable to Start 0x 0009 Application fails during monitoring Software events: - Critical, will cause the unit to reset.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action FMA (04) Software runtime (FE) 0x 0023 Alignment - corrupt file 0x 0024 Alignment - write fail 0x 0026 Configuration Data Manager ICC open failure 0x 0027 Configuration Data Manager Database not consistent 0x 0028 FMA Controller ICC open failure Software events: - Critical, will cause the unit to reset.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action FMA (04) Software runtime (FE) 0x 080D APM Client - Data not validated 0x 080E RSSI Manager unable to open well known socket Software events: - Critical, will cause the unit to reset. -Warning, then the event was unexpected, and may cause shortened life but does not stop current function. -Info, recording what happened in the LRU.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action KANDU (06) ASC (01) 0x 0001 DSP fault 0x 0020 ASC 1.2 V: Out-of-spec Hardware faults and events: - Replace the KANDU. 0x 0021 ASC 1.5 V: Out-of-spec 0x 0022 ASC 1.8 V: Out-of-spec 0x 0023 ASC 2.5 V: Out-of-spec 0x 0024 ASC 3.3 V: Out-of-spec 0x 0025 ASC 5.0 V: Out-of-spec 0x 0026 ASC 12 V input: Out-of-spec 0x 0027 ASC 1.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action KANDU (06) ASC BITE A429 IRS (12) 0x 0002 ARINC 429 IRS post OK Hardware faults and events: - Replace the KANDU.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action KANDU (06) Software configuration (FD) 0x 0006 LRU PRI-SEC image mismatch - Reboot the LRU to load valid primary image and check if fault goes away. - If not, reloading of software is required to load a fresh image.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Modman KANDU Ethernet bus (20) Modman input (01) 0x 0000 Ethernet no layer 1 Indicates nothing is connected: - Check wiring between boxes. - Check TX box is operating. - Check RX box is operating.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action KANDU OAE Serial Control Bus (31) KANDU input (01) 0x 0001 Serial Inactive Is a warning that no traffic has been seen on the bus: - Far end is not talking. - Wiring problem. - Input problem. 0x 0002 Serial High packet loss There is an intermittent wiring problem or hardware fault. 0x 0003 Serial Normal System is good.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action KANDU KRFU Serial Bus (33) KANDU input (01) 0x 0001 Serial Inactive Is a warning that no traffic has been seen on the bus: - Far end is not talking. - Wiring problem. - Input problem. 0x 0002 Serial High packet loss There is an intermittent wiring problem or hardware fault. 0x 0003 Serial Normal System is good.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action KRFU Input Discrete from KANDU (41) Filter Select (03) 0x 0000 Asserted 0x 0001 De-asserted System interconnect: Is a Debug aid to allow maintainer or installer to see inputs on various boxes on system interconnect. If not working correctly: - Check cables. - Check TX LRU. - Check RX LRU.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Roll angle label (02) 0x 0001 Missing Expected label is not there: - Make sure that the system configuration expects the correct label. - Check aircraft system is supplying the correct label on the bus. If fault is critical, the system will not work.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Pitch rate label (03) 0x 0002 SSM FT Expected label is in functional test: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Roll rate label (04) 0x 0004 SSM FW Expected label is in failure warning: If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate. 0x 0005 SSM NO Normal operation, system is good.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Body longitudinal acceleration (06) 0x 0001 Missing Expected label is not there: - Make sure that the system configuration expects the correct label. - Check aircraft system is supplying the correct label on the bus. If fault is critical, the system will not work.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Body vertical acceleration (07) 0x 0002 SSM FT Expected label is in functional test: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) True heading label (08) 0x 0004 SSM FW Expected label is in failure warning: If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate. 0x 0005 SSM NO Normal operation, system is good.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Latitude label (11) 0x 0001 Missing Expected label is not there: - Make sure that the system configuration expects the correct label. - Check aircraft system is supplying the correct label on the bus. If fault is critical, the system will not work.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Longitude label (12) 0x 0002 SSM FT Expected label is in functional test: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Altitude (13) 0x 0004 SSM FW Expected label is in failure warning: If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate. 0x 0005 SSM NO Normal operation, system is good.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) N-S velocity (15) 0x 0001 Missing Expected label is not there: - Make sure that the system configuration expects the correct label. - Check aircraft system is supplying the correct label on the bus. If fault is critical, the system will not work.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) E-W velocity (16) 0x 0002 SSM FT Expected label is in functional test: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Horizontal stabilization (21) 0x 0004 SSM FW Expected label is in failure warning: If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate. 0x 0005 SSM NO Normal operation, system is good.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Date label (32) 0x 0001 Missing Expected label is not there: - Make sure that the system configuration expects the correct label. - Check aircraft system is supplying the correct label on the bus. If fault is critical, the system will not work.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Flight phase (41) 0x 0002 SSM FT Expected label is in functional test: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) MLG ground condition (42) 0x 0004 SSM FW Expected label is in failure warning: If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate. 0x 0005 SSM NO Normal operation, system is good.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 Body Roll Acceleration (51) Body Yaw Acceleration (52) L3 Code L3 Description Repair Action 0x 0003 SSM NCD Expected label is in no computed data: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 GNSS sensor status word (80) IRS discrete word (81) L3 Code L3 Description Repair Action 0x 0002 SSM FT Expected label is in functional test: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) Unknown (00) 0x 0000 Inactive link Aircraft Interconnect. Means we see no labels on the bus: - Check wiring - Check source - Check KANDU and Modman. Pitch angle label (01) 0x 0001 Missing Expected label is not there: - Make sure that the system configuration expects the correct label.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) Pitch angle label (01) 0x 0003 SSM NCD Expected label is in no computed data: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) Pitch rate label (03) 0x 0001 Missing Expected label is not there: - Make sure that the system configuration expects the correct label. - Check aircraft system is supplying the correct label on the bus. If fault is critical, the system will not work.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) Roll rate label (04) 0x 0002 SSM FT Expected label is in functional test: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) Yaw rate label (05) 0x 0004 SSM FW Expected label is in failure warning: If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate. 0x 0005 SSM NO Normal operation, system is good.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) Body vertical acceleration (07) 0x 0001 Missing Expected label is not there: - Make sure that the system configuration expects the correct label. - Check aircraft system is supplying the correct label on the bus. If fault is critical, the system will not work.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) True heading label (08) 0x 0002 SSM FT Expected label is in functional test: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) Body lateral acceleration (09 0x 0004 SSM FW Expected label is in failure warning: If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate. 0x 0005 SSM NO Normal operation, system is good.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Latitude label (11) 0x 0001 Missing Expected label is not there: - Make sure that the system configuration expects the correct label. - Check aircraft system is supplying the correct label on the bus. If fault is critical, the system will not work. If fault is a warning, the label is expected but not there, the system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) Longitude label (12) 0x 0002 SSM FT Expected label is in functional test: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) Altitude (13) 0x 0004 SSM FW Expected label is in failure warning: If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate. 0x 0005 SSM NO Normal operation, system is good.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) N-S velocity (15) 0x 0001 Missing Expected label is not there: - Make sure that the system configuration expects the correct label. - Check aircraft system is supplying the correct label on the bus. If fault is critical, the system will not work.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) E-W velocity (16) 0x 0002 SSM FT Expected label is in functional test: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Horizontal stabilization (21) 0x 0001 Missing Expected label is not there: - Make sure that the system configuration expects the correct label. - Check aircraft system is supplying the correct label on the bus. If fault is critical, the system will not work.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) Horizontal stabilization (21) 0x 0004 SSM FW Expected label is in failure warning: If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate. 0x 0005 SSM NO Normal operation, system is good.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) Date label (32) 0x 0001 Missing Expected label is not there: - Make sure that the system configuration expects the correct label. - Check aircraft system is supplying the correct label on the bus. If fault is critical, the system will not work.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) Flight phase (41) 0x 0002 SSM FT Expected label is in functional test: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Aircraft State Input Bus (71) Ground Speed (43) 0x0001 Missing 0x0002 SSM FT Expected label is in functional test: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Aircraft State Input Bus (71) Body Yaw Acceleration (52) 0x0001 Missing 0x0002 SSM FT Expected label is in functional test: This is expected, but is recorded as a debug aid. If a fault is critical, the system will not work. If the fault is a warning, the label is expected but not there, system will continue to operate.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action Modman Aircraft Discrete Input (72) WOW (06) 0x 0000 Asserted 0x 0001 De-asserted Ground transmit enable (08) 0x 0000 Asserted 0x 0001 De-asserted Public Svr disable (09) 0x 0000 Asserted 0x 0001 De-asserted Aircraft interconnect: This is an aid to installation.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action AISD Network: Ethernet AV2 (82) Modman Input (01) 0x 0000 Ethernet no layer 1 Indicates nothing is connected: - Check wiring between boxes. - Check TX box is operating. - Check RX box is operating. 0x 0001 Ethernet no traffic Is a warning that no traffic has been seen on the bus, but layer 1 is established so a physical link exists.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action PIESD Network: Ethernet EN6 (8A) Modman Input (01) 0x 0000 Ethernet no layer 1 Indicates nothing is connected: - Check wiring between boxes. - Check TX box is operating. - Check RX box is operating. 0x 0001 Ethernet no traffic Is a warning that no traffic has been seen on the bus, but layer 1 is established so a physical link exists.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action PODD Network: Ethernet PA1 (91) Modman Input (01) 0x 0000 Ethernet no layer 1 Indicates nothing is connected: - Check wiring between boxes. - Check TX box is operating. - Check RX box is operating. 0x 0001 Ethernet no traffic Is a warning that no traffic has been seen on the bus, but layer 1 is established so a physical link exists.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 7-6. L3 Codes (Continued) L1 L2 L3 Code L3 Description Repair Action RF TX Modman to KRFU (B0) Unknown (00) 0x 0001 TX IF 0x 0002 50 MHz Ref Check the interconnecting RF connection between the Modman and KRFU LRUs. RF TX KRFU to OAE (B1) Unknown (00) 0x 0001 TX Ka Band Check the interconnecting RF connection between the KRFU and OAE LRUs.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (i) 7.4 Make sure that the connecting equipment is operating correctly. 3 Check the wiring. Make sure that the system has the correct software loaded. The GUI screen has a Software Validity Flag, which if it is clear, then ALL system software is OK. If so, do as follows: 1 Check for LRU software errors. 2 Check for LRU hardware/software incompatibilities.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System To view and verify the AES system configuration, a web based GUI is supplied. The JetWave™ Ethernet configuration data can be viewed and verified by navigating to the “Contents of Aircraft Services Configuration Files” page from “Configuration Files” under the Other Information & Control menu. Figure 6-4 shows the typical configuration file Information page.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • User Port PA1/2/3/4/PG1/EN5/6/7/8/EG1/AV1/2/3/AG1 AES services IP Modman • User Port PA1/2/3/4/PG1/EN5/6/7/8/EG1/AV1/2/3/AG1 AES services IP KANDU • User Port PA1/2/3/4/PG1/EN5/6/7/8/EG1/AV1/2/3/AG1 AES services IP OAE • User Port AES services IP subnet • User Port PA1/2/3/4/PG1/EN5/6/7/8/EG1/AV1/2/3/AG1 traffic services • User Port IP filter 1 thru 150.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System SECTION 8 MAINTENANCE AND REPAIR 8.1 Maintenance Requirements (1) The maintenance-free design of the JetWave™ AES system does not require field maintenance to maintain airworthiness. (2) Maintenance of the JetWave™ AES system is limited to replacement of LRUs on verified failure. (3) OAE do not require field maintenance, such as lubrication of moving parts.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (2) It is recommended that this section be appended to the Airplane Maintenance Manuals. The information contained herein supplements the Airplane Maintenance Manuals in areas covered by the JetWave™ AES FMA/TMA installation. (3) It is recommended to consult basic Airplane Maintenance Manuals for limitations and procedures not contained in this supplement.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 8.5 Electrical and Mechanical Inspection and Check Periodic inspections of the mechanical and electrical interfaces of the JetWave™ AES OAE assembly and LRUs to the aircraft should be completed as defined by the governing airworthiness body (such as Transport Canada, the FAA, or the JAA) Instructions for Continued Airworthiness for the installation.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 8.7 (a) Recommended periodic scheduled servicing tasks: None required. (b) Recommended periodic inspections: (c) Scheduled maintenance inspections supplied in Table 8-1 and in accordance the aircraft’s inspection and maintenance schedule. (d) Recommended periodic scheduled preventative maintenance tests (to determine system condition and/or latent failures): None required.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 8-1. Scheduled Maintenance (Continued) SI No.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 8.9 Unscheduled Maintenance (1) Follow the Standard Practices Chapter of the Aircraft Maintenance Manual and do all the required inspections and repairs, as shown in Table 8-2. Table 8-2.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System APPENDIX A 1. RTCA/DO-160G Environmental Characteristics A. Modman The following characteristics are taken from the core equipment qualification program and do not reflect any additional qualification conducted on a per installation basis. Section Condition Category 4 Temperature and altitude A1(V) NOTE: Below 5˚F (-15˚C), user services are not offered.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Condition Category 20 Radio frequency susceptibility RR (custom) NOTE: Radiated: Additional subjections SW: 0.4 to 8 GHz: 28 V/m (1 kHz square mod with greater than 90% depth switched on and off at 1 Hz rate and 50% duty cycle). PM: 0.4 to 8 GHz: 150 V/m (Pulse repetition frequency of 1 kHz and a duty cycle of 1%, switched on and off at 1 Hz rate and 50% duty cycle). Pulse width is 10 µsec (1% of 1 kHz). PM: 0.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System B. APM Section Condition Category 4 Temperature and altitude A1(V) NOTE: Altitude test extended to 50,000 feet (15,240 m). Overpressure 28.9 PSI (199 kPa), Decompression 6,000 to 55,000 (1828.8 to 16,764 m) in 2 seconds.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System C. KANDU Section Condition Category 4 Temperature and altitude D2 NOTE: Altitude test extended to 51,000 feet (15,544.8 m). Overpressure 28.9 PSI (199 kPa), Decompression 6,000 to 55,000 (1,828.8 to 16,764.0 m). 5 Temperature variation A 6 Humidity B 7 Operational shocks and crash safety E and B 8 Vibration CAT R, CURVE E CAT R, CURVE E1 NOTE: The sinusoidal sweep rate not to exceed 0.5 octaves/minute.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Condition Category 21 Emissions of RF energy Q NOTE: Extension of conducted emissions limits to 200 MHz at 20 dBμA and power line limits from 30 MHz to 108 MHz at 20 dBμA. Extension of radiated emissions to start at 45 dBμV/m at 150 kHz to 40 dBμV/m at 2 MHz, and at 30 dBμV/m at 2 MHz to 25 dBμV/m at 25 MHz, and at 25 dBμV/m at 25 MHz to 26.3 dBμV/m at 30 MHz, and at 36.3 dBμV/m at 30 MHz to 44.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System D. KRFU Section Condition Category 4 Temperature and altitude D2 NOTE: Altitude test extended to 51,000 feet (15,544.8 m). Overpressure 28.9 PSI (199 kPa), Decompression 6,000 to 55,000 (1,828.8 to 16,764.0 m). 5 Temperature variation A 6 Humidity B NOTE: At least six spot checks required.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Condition Category 21 Emissions of RF energy P NOTE: Extension of conducted emissions limits to 200 MHz at 20 dBμA and power line limits from 30MHz to 108MHz at 20 dBμA. Extension of radiated emissions to start at 45 dBμV/m at 150 kHz to 40 dBμV/m at 2 MHz, and at 30 dBμV/m at 2 MHz to 25 dBμV/m at 25 MHz, and at 25 dBμV/m at 25 MHz to 26.3 dBμV/m at 30 MHz, and at 36.3 dBμV/m at 30 MHz to 44.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System E. TMA Section Condition Category 4 Temperature and altitude F2 5 Temperature variation A 6 Humidity B 7 Operational shocks and crash safety E 8 Vibration CAT R, CURVE E CAT R, CURVE E1 9 Explosive atmosphere E and H 10 Waterproofness Y and W 11 Fluid susceptibility F (de-icing fluids) NOTE: Ethylene Glycol.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Condition Category 23 Lightning direct effects X - not required 24 Icing B 25 Electrostatic discharge A 26 Fire, flammability C - covers 4 CFR 25.853 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System F. FMA Section Condition Category 4 Temperature and altitude F2 NOTE: Extended operating high to 194˚F (90˚C). 5 Temperature variation A 6 Humidity B NOTE: At least six spot checks are required. 7 Operational shocks and crash safety B and E 8 Vibration CAT S, CURVE C CAT R, CURVE C1 NOTE: The sinusoidal sweep rate not to exceed 0.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Condition Category 22 Lightning induced transient susceptibility A3K3L3 NOTE: Pin Injection waveform 5A level 125V/125A and 400V/4A. Single stroke WF 4, level 3 (extended to 300V/1000A), Multi-stroke WF4 level 3 (extended to 120V/400A 1st stroke, 60V/120A subsequent strokes).
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System APPENDIX B NOTE: The JetWave™ LRU labels do contain data such as Software Part No., Software Version No. or Software Mod dots. To see the JetWave™LRUs hardware and software version and part number, navigate to the Version and Manufacturing Information menu on the GUI. 1. Aircraft Information Sheet Owner Tail Number Serial Number Model/Type 2. JetWave™ AES Subsystem Components A.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System D. JetWave™ AES Modman Installation Information Sheet Part Number Serial Number Hardware Revision Mod Status E. JetWave™ AES APM Installation Information Sheet Part Number Serial Number Hardware Revision Mod Status 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System APPENDIX C 1. Installation Checklist Aircraft Identification: Name Signature Date Installation/Checks completed by: Approved/Witnessed by: A. OAE-TMA Checklist Section Parameter Item NA A. Maintenance Panel Applicability If the system is not wired to another aircraft system, an installer provided maintenance panel is required.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA A. Modman Physical Examine for physical damage. √ Value Environmental conditions, refer to Figure 4-22. Mounting tray Install applicable 4-MCU tray, supplied by customer. Clearance Minimum 1 inch (25.4 mm) from top surface and 0.5 inch (12.7 mm) from all other surfaces Electrical connector ARINC 600 mating connector and pins, refer to Table 4-1.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA NOTE: Input signal range: -79 to -5 dBm. Output signal range -30 to +5 dBm. Incross talk requirement: -25 dBc. Output cross talk requirement: -40 dBc. (Cont) Electrical wiring Electrically wire and interconnect in accordance with Figure 4-24 and Figure 4-34. 4.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA 4.6 KRFU Physical Examine for physical damage. √ Value Environmental conditions, refer to Figure 4-27, Figure 4-28, or Figure 4-29 depending on configuration used. Install the thermal pad in accordance with KRFU on page 4-16. The KRFU is installed with the TMA, refer to OAE TMA Installation Procedure on page 4-30. The KRFU feet are configured differently depending on the part number ordered.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA (b) OAE TMA Installation Procedure (Cont) TMA install Refer to OAE TMA Installation Procedure. TMA radome and radome fairing Depending on the airframe, there may be a need to install radome fairing which adapts to the tail empennage of the aircraft, consult aircraft OEM. √ Value Radome and fairing installation is aircraft specific. Refer to aircraft specific SDIM for details.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System B. A791 Based OAE-FMA with the AIM Checklist Section Parameter Item NA A. Maintenance Panel Applicability If the system is not wired to another aircraft system, an installer provided maintenance panel is required.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA A. Modman (Cont) Clearance Minimum 1 inch (25.4 mm) from top surface and 0.5 inch (12.7 mm) from all other surfaces Electrical connector ARINC 600 mating connector and pins, refer to Table 4-1.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA NOTE: Input signal Electrical range: -79 to -5 dBm. wiring - APM to Output signal range -30 Modman to +5 dBm. Incross talk requirement: -25 dBc. Output cross talk requirement: -40 dBc. (Cont) APM to Modman interconnect cable shall use ARINC 664 compliant 2 Shielded Twisted Pair 24 AWG (or Aerospace Grade Shielded Cat 5/Cat 5E Minimum). Part No.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter 4.6 KRFU (Cont) Waveguide The RX interconnect path loss KRFU to FMA RX connection at the KRFU requires a (Cont) WR42 to coax transition adapter at the KRFU J4. N.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System C. Non-A791 Based OAE-FMA with the LAIM Checklist Section Parameter Item NA A. Maintenance Panel Applicability If the system is not wired to another aircraft system, an installer provided maintenance panel is required.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA A. Modman (Cont) Electrical bonding Bonding, refer to page 4-3 Electrical wiring Electrically wire and interconnect in accordance with Figure 4-21 or Figure 4-22 and Figure 4-35thru Figure 4-37, depending on the configuration being used. Electrical RF coaxial Equalizer in the TX path √ Value TX path loss, refer to Table 4-2.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA 4.3 KANDU Physical Examine for physical damage. √ Value Environmental conditions, refer to Figure 4-25 or Figure 4-26. Electrical wiring Electrically wire and interconnect in accordance with Figure 4-25 or Figure 4-26 and Figure 4-34, thru Figure 4-37, depending on the configuration being used. Mounting Install location of KANDU is airframe specific.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA 4.6 KRFU (Cont) Physical (Cont) The KRFU feet are configured differently depending on the part number ordered. Make sure feet are in the correct configuration for the aircraft application. Waveguide Make sure the waveguide is connected before powering the KRFU. √ Value Waveguide Connection must be WR28 for TX and KRFU to FMA coaxial cable for RX.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter I. FMA Installation Procedure (Cont) Install radome Install and attach the radome skirt skirt fairing fairing to fuselage with 39 fasteners. FMA install Refer to Fuselage Mount Antenna (If FMA radome Item NA √ Value applicable) (8). Attach the radome assembly onto the radome skirt fairing. FMA bonding Electrically bond in accordance with page 4-16.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System APPENDIX D 1. List of Airframe Specific Information Required for JetWave™ System Configuration A Honeywell proprietary configuration tool is used to generate the JetWave™ configuration files. Information as listed in the tables below is to be provided to Honeywell for generation of JetWave™ configuration files. Table D-1. Value Added Reseller (VAR/DP) Name of the Service Provider Table D-2.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table D-4.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table D-5. Airframe Structural Blockage Information Blockage Angle Value in Degrees Remarks Blockage Angle a Angle “a” is the angle between the horizontal plane where the antenna emitting point is located and outer tip of the Horizontal Tail Plane (HTP). Blockage Angle b Angle “b” is between horizontal plane where antenna emitting point is located and outer tip of wing (including vortex eliminators, if present).
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System NOTE: • All zenith view (from above) angles, except for “e,” are measured from the aircraft longitudinal axis, being 0 degrees at the stern. • All side view angles are measured from the aircraft longitudinal axis, being 0 degrees at the plane where the antenna emitter is located.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table D-10. Modman Serial Number Modman Serial Number Table D-11. Modman Ethernet Configuration Table Modman Ethernet Interface AISD Ethernet AV1 10/100 Mbps User OTA Traffic Enabled / Disabled AES Services to be Enabled Static IP / Local IP Address (Modman/KAND U/FMA or TMA) 615A DL (Data Load) AESSFTP SNMP GUI 172.29.55.1/.2/.3 615A DL (Data Load) AESSFTP SNMP GUI 172.29.55.1/.2/.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table D-11. Modman Ethernet Configuration Table NOTE 3: Select the appropriate AES services. AES services available are: (a) 615A DL (Data Load) (b) AESSFTP (c) SNMP and (d) GUI. NOTE 4: The Static/local IP addresses shown are the default values the terminal uses until it has read a non-blank APM. Table D-12. KRFU Location Inside Cabin Inside Radome Table D-13. Antenna Location Fuselage Mount Tail Mount Table D-14.
