E90400259-1-A DEVELOPMENT - Release - 23 Sep 2014 12:14:52 MST - Printed on 14 Nov 2014 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-34. JetWave™ System Interconnect Diagram - FMA (KRFU Inside Aircraft Fuselage) (Sheet 1 of 8) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90400259-4-A SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-34. JetWave™ System Interconnect Diagram - FMA (KRFU Inside Aircraft Fuselage) (Sheet 4 of 8) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90400259-5-A SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-34. JetWave™ System Interconnect Diagram - FMA (KRFU Inside Aircraft Fuselage) (Sheet 5 of 8) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90400259-6-A SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-34. JetWave™ System Interconnect Diagram - FMA (KRFU Inside Aircraft Fuselage) (Sheet 6 of 8) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90400259-7-A SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-34. JetWave™ System Interconnect Diagram - FMA (KRFU Inside Aircraft Fuselage) (Sheet 7 of 8) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90401047-1-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-35. JetWave™ System Interconnect Diagram - Boeing Specific FMA (External KRFU) (Sheet 1 of 8) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90401047-5-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-35. JetWave™ System Interconnect Diagram - Boeing Specific FMA (External KRFU) (Sheet 5 of 8) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90401047-7-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-35. JetWave™ System Interconnect Diagram - Boeing Specific FMA (External KRFU) (Sheet 7 of 8) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90401047-8-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-35. JetWave™ System Interconnect Diagram - Boeing Specific FMA (External KRFU) (Sheet 8 of 8) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90403590-1-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-36. JetWave™ System Interconnect Diagram - A350 FMA (Sheet 1 of 10) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90403590-2-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-36. JetWave™ System Interconnect Diagram - A350 FMA (Sheet 2 of 10) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90403590-3-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-36. JetWave™ System Interconnect Diagram - A350 FMA (Sheet 3 of 10) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90403590-7-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-36. JetWave™ System Interconnect Diagram - A350 FMA (Sheet 7 of 10) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90403590-8-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-36. JetWave™ System Interconnect Diagram - A350 FMA (Sheet 8 of 10) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90403590-9-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-36. JetWave™ System Interconnect Diagram - A350 FMA (Sheet 9 of 10) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90403590-10-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-36. JetWave™ System Interconnect Diagram - A350 FMA (Sheet 10 of 10) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System JETWAVE™ AES SYSTEM CONFIGURATION 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • ARINC • MCN (for the China market) • INMARSAT (for Lufthansa, Germanwings, Swiss, Austrian, and Eurowings) • Distribution Partners: • Satcom1 • Satcom Direct • SITA OnAir • Gogo Business Aviation • ARINC Direct The actual throughputs achieved by the GXA terminal are dependent on the Airline Operator subscription. Each subscription will have a defined Committed Information Rate which is the minimum throughput guaranteed to each subscriber.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System The JetWave™ system is manufactured by Honeywell as sole supplier of Inmarsat GX Aviation equipment. Honeywell manufactures and sells this hardware to end customers, as well as to VARs and DPs. B.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 132 Yes True heading Hybrid 110 50 324 Yes Pitch angle INS 50 20 325 Yes Roll angle INS 50 20 330 Yes Yaw rate INS 50 20 326 Yes Pitch rate INS 50 20 327 Yes Roll rate INS 50 20 331 Yes INS 60 20 332 Yes INS 60 20 0.001 g 333 Yes Body longitudinal acceleration Body lateral acceleration Body vertical Acceleration 0.015 degrees/sec 0.015 degrees/sec 0.015 degrees/sec 0.001 g INS 60 20 0.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 3-1. AES User Level, Aircraft ID Display/Update Information Page B. View AES System Configurations The AES system configuration includes the aircraft installation information. NOTE: The AES System configuration file update is not a field activity. This is done by the equipment supplier as part of production process.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System There are a number of functions that an Ethernet port can support namely, data traffic, data loading, GUI, AES logs extraction (maintenance function) and status/control (through the SNMP). The terminal can be configured to indicate whether an Ethernet port supports traffic, data loading, SNMP etc, such as AG1 SNMP, and data loading, EG1 traffic, using the aircraft service configuration file.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • Weight on Wheels discrete input availability and its polarity • User Ethernet Ports which are to be configured and the type of services to be enabled (such as Dataload, SNMP and GUI). • Particulars of VAR/DPs providing the IP services • Aircraft blockage data. Refer to APPENDIX E on page D-1 for more details. 5. ARINC 615A Software Dataload Process A.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System This section contains the instructions for data loading of JetWave™ software to any of the JetWave™ LRUs through the ARINC 600 AV1 (Maintenance Port) Ethernet interface of Modman. Data loading of JetWave™ system can be performed while: • JetWave™ system is in normal operation • During system initialization • When in critical fault mode.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-2.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System D. JetWave™ Data Load Procedure (1) General Preparation (a) Power up the AES system. (b) Power up the ARINC 615A compliant data loader and ensure data loader is interfaced with Modman and is ready to upload. (c) Load the media CD with the copy of the released JetWave™ software and configuration file. The media (CD) contains a configuration file and a file containing the software to be uploaded.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (2) (3) Preparation for Loading Software (a) Click to bring up the 665 Media window on the data loader. (b) Select Media Repository and click OK button. Most of the data loader will automatically select the media repository folder and brings up the Select Media Set window. (c) In the Select Media Set window, the operator will be able to see the packaged software data files.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (4) Getting Target Information (a) The ARINC 615A INFORMATION operation is used to retrieve software configuration information from a loadable target. (b) The Modman advertise two data load hardware targets, one for the Modman and the other for the AES Configuration, as follows: Modman LRU: • Target Hardware Identifier: "HNIGXMODMAN0" • Target Type Name: "MODMAN" • Target Position: "0" • Literal Name: "JetWave™ MODMAN" • Manufacture Code: "HNI".
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (a) The ARINC 615A UPLOAD operation is used to transfer the data files to the Modman. The AIT F-SIM-LDR ARINC 615A data upload information dialog box screen shot is shown in Figure 3-5. Figure 3-5. AIT F-SIM-LDR ARINC 615A Data Upload Information Dialog Box (b) The UPLOAD process is initiated by selecting an individual LSAP or ARINC 665 media set containing one or more LSAPs.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (e) Update the field for target IP address of the JetWave™ Modman as 172.29.55.1 for loading the entire JetWave™ AES media set. (f) Update the field for target IP address of the JetWave™ LRUs for respective LRU IP address and by choosing the Load Header (.LUH) (Header Files (*.LUH)) file associated for data load of respective JetWave™ AES LRUs. (g) Click Upload LSAPs.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System When calibration is completed successfully, the ACM proceeds to its configured mode of operation as if it had been restarted. When commissioning is not completed successfully, either due to an error condition or a user cancellation, the ACM enters an inactive state. One Touch Commissioning (OTC) is available on the AES Menu Access System. 7. Post Installation System Checkout Procedures A.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System On completion of AES system installation activities, the installer can view and make sure that the JetWave™ LRUs status, AES configuration settings, discrete input and output status, and antenna alignment status through the GUI as described in this section. Once the Modman is powered up, the JetWave™ GUI page can be accessed. The JetWave™ system GUI service is supported on AV1 10/100 Base T Ethernet interface.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • Ground status • Mute Reason • Link start and end time • Heath status of the system LRUs. The GUI AES Home page screen, as shown in Figure 3-7, lets the operator navigate to all applicable options depending on the access level. Figure 3-7. AES Home and Status Info Page View and verify the AES configuration data, navigate to the "Configuration Files" formation pages under the other information and control menu.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 3-8. 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 let you to view and make sure of the health status of the JetWave™ system. The AES summary and interlink status are shown in Figure 3-9. 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 3-9. Health Statuses (excerpt), AES Summary and Link Statuses To see the AES LRUs hardware and software version and part number, navigate to the Version and Manufacturing Information menu. Figure 3-10 shows the typical Modman Version and Manufacturing Information page. Make sure the vesion and manufacturing information are current for all the LRUs. 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 3-10. AES Modman and Manufacturing Information Page Update the aircraft tail number, navigate to the "Aircraft Tail Number" page under the other information and control menu. The aircraft tail number page is shown in Figure 3-11. Figure 3-11. Aircraft Tail Number Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Modman Reset Input (1) Activate the Modman Reset by toggling Modman reset switch on the JetWave™ AES control panel. (2) Monitor the Modman ”power” and “status” LEDs flash continuously. (3) Toggle the Modman Reset switch on the Satcom test panel to the open/non-grounded position. (4) Monitor the “status” LED on the front of the Modman, progresses from red color to steady state green as seen during initial power-on.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 429 interface through which the required ARINC 429 labels as defined in APM configuration file are made available. Navigate to the AES Summary and Link Status page and scroll down to see the aircraft status. Refer to Figure 3-13. This page will be updated with current latitude and longitude position of the aircraft.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 3-14. Manual Antenna Steering E. Antenna Calibration Testing Do the Antenna Calibration in accordance with the detailed instructions in TMA Alignment or FMA Alignment section. Navigate to Antenna Calibration Status under the commanded test menu and make sure that the current calibration status, calibration is “Aligned”. F.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 3-15. Calibrate Transmit Cable Status Page G. ARINC 615 Data Load Do the data load as detailed in ARINC 615A Software Dataload Process section. Make sure that the data load operation is completed successfully. H. 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. I.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Make sure that the network connectivity in accordance with the aircraft configuration plan. With the use of another laptop, make sure that the network connectivity on each active port once the data link available output is available. Begin a two way (Rx and Tx) video conference call with a tool such as Microsoft Lync or Skype. Make sure that the availability of the uninterrupted data connectivity.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (5) 8. In case of any RF interference, there will be significant variation of the C/N and Eb/No parameters. Post-Installation Troubleshooting A. System Fails Post-installation Checks (1) To make sure that the system is correctly installed, do as follows: (a) Make sure that the APM has been correctly configured and loaded.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (1) (2) If the system is reporting labels missing, do as follows: (a) Check that the APM is configured to have correct labels on the correct bus. (b) Make sure that the labels are present on bus. If the system is reporting an incorrect label status on the bus (FW, NCD, FT), do as follows: (a) C. Wait for equipment providing the labels to report Normal Operation.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 3-17. Contents of Aircraft Services Configuration File There are a number of functions that an Ethernet port can support namely, data traffic, data loading, GUI, AES logs extraction (maintenance function) and status/control (through the SNMP). The terminal can be configured to indicate whether an Ethernet port supports traffic, data loading, SNMP, etc, such as port PA1 configured for engineering SNMP and AES access services.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • User Port IP filter 1 thru 150. Once the items have been loaded into the APM the Modman reads the APM once at power-on and passes the appropriate data to the relevant LRU or uses the information locally. (1) If the Ethernet port is not active, do as follows: (a) (b) (2) 9. 1 Make sure that the port is enabled. 2 Check system errors. 3 Check for system reporting No layer 1 or No traffic faults.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System C. Airworthiness Limitations (1) Installation of the JetWave™ AES OAE assembly and LRUs on an aircraft by supplemental type certificate (STC) or Form 337 obligates the aircraft operator to include the maintenance information supplied by this manual in the operator’s Aircraft Maintenance manual and the operator’s Aircraft Scheduled Maintenance Program. (2) It is recommended that this section be appended to the Airplane Maintenance Manuals.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (4) It is recommended to follow the Standard Practices Chapter of the Aircraft Maintenance Manual and do all required inspections and repairs. Table 3-12. Scheduled Maintenance SI No. G.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-13. Unscheduled Maintenance Item Potential Damage Inspection JetWave™ AES FMA OAE/TMA OAE Heavy rain / hail Paint erosion External visual bird strike Paint damage/radome puncture External visual JetWave™ AES system Failure NA NA Removal (2) JetWave™ AES system status can be viewed through the GUI. Refer to Checking Status Information section for description.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Only qualified avionics personnel who are knowledgeable in the technical and safety issues related to the troubleshooting of aircraft communications equipment should do the troubleshooting procedures supplied in this manual. NOTE: If any of the KANDU unmonitored voltage rails are not working the troubleshooting output of the JetWave™ system would not identify the problem directly. A.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • Access the user interface with Username: "User" and no password. (7) User may press Log out button to log out. Upon logging off, log in page will be presented by default. Figure 3-19 shows the log out page. Figure 3-19. JetWave™ Logout Page B. Checking Status Information (1) The health status of the JetWave™ system can be monitored by selecting AES Summary and Link Status under the Health Status pane menu.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 3-20. JetWave™ Summary and Link Status (Sheet 1 of 2) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 3-18. JetWave™ Summary and Link Status (Sheet 2 of 2) (2) C. The JetWave™ system status can be viewed through the GUI. Refer to AES system status verification section on page 3-5 for description. Downloading LRU Logs (1) To view the hystorical fault logs, under the AES historical logs pane, select the "Fault Log". A screenshot of fault log page is shown in Figure 3-19.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 3-19. 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 3-20 for an example of a viewable fault log. 23-15-29 © Honeywell International Inc.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 3-20. 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 3-21 will come into view. Save to the computer to open and view the fault log. Figure 3-21. JetWave™ Fault Log Download Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System D. System Dataload 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 615A data loader is connected to the correct port: NOTE: AV1 by default, but this may have been modified by the configuration loaded on the APM. (4) 11. Make sure you are trying to load a valid set of files into the correct LRU.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (a) Remove the unit (b) Secure cables and wiring (c) Collar applicable switches and circuit breakers (d) Placard the JetWave™ AES LRU and associated items as “inoperative” in accordance with the aircraft maintenance manual (e) Before flight, do as follows: 1 Record the removal of the unit in the log book 2 Revise the equipment list. Refer to section 91.213 of the FAR or the aircraft’s minimum equipment list.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (2) Visually examine the FMA or TMA radome for any damage or defects. (a) Remove the JetWave™ AES OAE FMA or TMA assembly and LRUs from service if you find: • Punctures in the radome • Cracks in the radome • Chips, nicks, or gouges more than 0.250 inch (6.35 mm) across in any direction • Erosion lamination because of impact more than 0.250 inch (6.35 mm) across in any direction • Erosion of lamination because of impact more than 0.031 inch (0.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (a) The JetWave™ AES consists of the Modman, KANDU, KRFU, TMA or FMA LRUs, plus the APM. (b) 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. (c) The BITE system divides the responsibility for BITE and historical logs in a BITE hierarchy as illustrated in Figure 3-22. Figure 3-22.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 3-23. AES and LRU Controller Interaction (g) The AES Controller resides in the Modman LRU. (h) 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). • (i) Events: These are BITE events which occur but do not have a set or clear state.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (k) 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. This is mentioned in some reaction tables described below. (l) The AES controller has its own historical logs which allow it to record events about the whole system.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (2) Status Memory (a) The AES Controller remembers the following information: • The AES Controller maintains an overall mode of operational state, of UNKNOWN (Default), DATA LOAD, CRITICAL FAULT, COMMANDED MODE, OPERATIONAL MODE. • The AES controller maintains an overall service state, of AVAILABLE (default) or UNAVAILABLE. This service state, when set to UNAVAILABLE, disables user servicer and transmission.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • For every ARINC 429 label the LRU understands, it records the status: DISABLED, UNKNOWN (default after power on), ACTIVE, SSMERROR, MISSING. It also records if the label is causing a mute of the system. • For every input discrete the LRU possesses, it records the status: ASSERTED, DEASSERTED. • The LRU maintains in memory the reason, if any, for muting. B. LRU Codes BITE event information is encoded by the LRUs in three values.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-15.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-15. L1 Codes (Cont) 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. D.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-16.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-16.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-17.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-18.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-19. L2 Codes – User Interface E.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action System (00) Regulatory Log (07) 0x 0000 Regulatory log upload failure 0x 0001 Reg log full NO ACTION –System will continue to try and upload the file as directed by the regulatory log requirements on frequency of upload attempts.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action Modman (01) Controller/router (02) 0x 0004 Ethernet PIES Switch 0x 0005 Ethernet AISD Switch Hardware faults and events: - Replace the Modman.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action Modman (01) Reset (FC) 0x 0003 Reset Pin 0x 0004 SW exception Info events - Recording what happened in the LRU. 0x 0001 HW SW compatibility 0x 0002 LRU SW compatibility 0x 0003 Configuration parameter missing Reload the configuration data with the A615A data loading process.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action KRFU (02) 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, then a fresh data load of software is required to load the fresh image. 0x 0007 Data load 0x 000A Operating image list Unit configuration events: - Critical, something needs to be done (reload software).
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action TMA (03) LNA (03) 0x 0001 LNA current Motor and sensors (04) 0x 0001 AZ sensor detection 0x 0002 EL INIT sensor detection 0x 0003 EL LIMIT sensor detection Hardware faults and events: - Replace the TMA. NOTE: Before removing the Tail Mount Radome, Honeywell recommends manually steering the TMA through GUI to a safe antenna orientation position.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action TMA (03) Software Configuration (FD) 0x 0003 Configuration parameter missing Reload the configuration data with the A615A data loading process. 0x 0004 Primary image corruption warning - Reboot the LRU to load valid primary image and check if fault goes away. - If not, then a fresh data load of software is required to load the fresh image.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action FMA (04) MDU (0B) 0x 0004 12V positive voltage 0x 0005 12V negative voltage Hardware faults and events: - Replace the FMA. 0x 0006 38.5V voltage 0x 0007 1.5V current 0x 0008 3.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action FMA (04) Software runtime (FE) 0x 0000 Heartbeat failure 0x 0001 General module failure 0x 0020 File system full 0x 0021 thru 0x 007F Other SW errors Software events: - Critical, will cause the unit to reset. -Warning, then the event was unexpected, but will sort itself out. -Info, recording what happened in the LRU.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action KANDU (06) ASC (01) 0x 0021 ASC 1.5 V: Out-of-spec 0x 0022 ASC 1.8 V: Out-of-spec Hardware faults and events: - Replace the KANDU. 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 1.2 V current: Out-of-spec 0x 0028 ASC 1.5 V current: Out-of-spec 0x 0029 ASC 1.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action KANDU (06) ASC BITE A429 AUX (13) 0x 0000 ARINC 429 AUX post unresponsive Hardware faults and events: - Replace the KANDU.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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, then a fresh data load of software is required to load the fresh image.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action Modman KANDU Ethernet bus (20) KANDU input (02) 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 on traffic has been seen on the bus, but layer 1 is established so a physical link exists.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action KANDU OAE Ethernet Bus (30) KANDU input (01) 0x 0003 Ethernet normal System is good. OAE input (02) 0x 0000 Ethernet no layer 1 Indicates nothing is connected: - Check wiring between boxes. - Check TX box is operating. - Check RX box is operating.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action KANDU OAE Serial IMU Bus (32) OAE input (02) 0x 0003 Serial Normal System is good. KANDU KRFU Serial Bus (33) KANDU input (01) 0x 0001 Serial Inactive Is a warning that on 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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. IRU Input Bus (70) Unknown (00) 0x 0000 Inactive link Aircraft Interconnect.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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. If fault is a warning, the label is expected but not there, the system will continue to operate.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Body longitudinal acceleration (06) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Body vertical acceleration (07) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Body lateral acceleration (09) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Latitude label (11) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Longitude label (12) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Vertical velocity (14) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) N-S velocity (15) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) E-W velocity (16) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Time label (31) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Date label (32) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) Flight phase (41) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action IRU Input Bus (70) GNSS sensor status word (80) 0x 0007 Fault Will be available in future revision IRS discrete word (81) 0x 0000 Align mode/Not ready 0x 0001 Revisionary altitude mode 0x 0002 Normal mode Unknown (00) 0x 0000 Inactive link Aircraft Interconnect. Means we see no labels on the bus: - Check wiring - Check source - Check KANDU and Modman.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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. If fault is a warning, the label is expected but not there, the system will continue to operate.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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. If fault is a warning, the label is expected but not there, the system will continue to operate.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action Aircraft State Input Bus (71) 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action AISD Network: Ethernet AG1 (80) 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 on traffic has been seen on the bus, but layer 1 is established so a physical link exists.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action PIESD Network: Ethernet EG1 (88) 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 on traffic has been seen on the bus, but layer 1 is established so a physical link exists.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action PIESD Network: Ethernet EN8 (8C) 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 on traffic has been seen on the bus, but layer 1 is established so a physical link exists.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-20. L3 Codes (Cont) L1 L2 L3 Code L3 Description Repair Action PODD Network: Ethernet PA3 (93) 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 on traffic has been seen on the bus, but layer 1 is established so a physical link exists.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System APPENDIX A 1. RTCA/DO-160G Environmental Characteristics A. Modman Section Condition Category 4 Temperature and altitude A1(V) NOTE: Below 5˚F (-15˚C), user services are not offered. 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.
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.
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.
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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Condition Category 20 Radio frequency susceptibility RY NOTE: - 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 a 1 Hz rate and 50% duty cycle). Pulse width is 10 μsec (1% of 1 kHz). - 0.3 to 6 GHz: 20 V, (Pulse repetition frequency of 200 Hz and a duty cycle of 12.5%). Pulse width is 625 μsec (12.5% of 200 Hz).
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. 7 Operational shocks and crash safety 8 Vibration E and B CAT R, CURVE E CAT R, CURVE E1 NOTE: The sinusoidal sweep rate not to exceed 0.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Condition Category 20 Radio frequency susceptibility MY NOTEL: - 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 a 1 Hz rate and 50% duty cycle). Pulse width is 10 μsec (1% of 1 kHz). - 0.3 to 6 GHz: 20 V/m, (Pulse repetition frequency of 200 Hz and a duty cycle of 12.5%). Pulse width is 625 μsec (12.5% of 200 Hz).
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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Condition Category 22 Lightning induced transient susceptibility A3K3L3 modified NOTE: Pin Injection waveform 5A level 2. Single stroke WF 4, level 3 (extended to 300V/1000A), Multi-stroke WF4 level 3 (extended to 120V/400A 1st stroke, 75V/150A subsequent strokes), Extend WF5A level 3 (extended 120V/400A 1st stroke, 75V/150A subsequent strokes).
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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Condition Category 21 Emissions of RF energy H NOTE: Extension of conducted emissions limits to 200 MHz at 20 dBμA and power line limits from 30MHz to 152MHz at 20 dBμA. All conducted emissions limits, including interconnecting bundles limits, are set in accordance with Category H power line limit levels. Radiated emissions to start at 40 dBμV/m at 2 MHz to 35 dBμV/m at 25 MHz, and at 35 dBμV/m at 25 MHz to 44.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System APPENDIX B 1. MIB Objects A. MIB Structure (1) SNMP applications can monitor the MIB objects. The Modman implements the Honeywell engineering SNMP MIB with OIDs as shown in Figure B-1. Figure B-1. MIB Object Structure (2) The Honeywell engineering SNMP service provides information to the external entity covering two areas of concern, link/service status and maintenance/BITE status.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System B. Detailed MIB Definition (1) Object Types This section describes all the special object types in individual sections and tables, which are not defined in the SNMP and MIB standard. (a) Link Status Type Definician The SNMP Type HonAkSatLinkState reports the network link state and link state of the terminal. It is an enumerated integer value with the structure shown in Table B-1. Table B-1.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (c) Health Status Type definition The SNMP type HonAkHealthStatus report the health status of the AES. It is an enumerated integer value with the structure as shown in Table B-3. Table B-3.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (g) Tenths Unsigned32 Type definition The SNMP type HonAkTenthsUnsigned32 cause an Unsigned32 that expresses something in tenths to be displayed in a floating point way. • For example, consider the case where an object that uses this TC and contains a value of '1234'. This object would be displayed as '123.4'.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (k) Satellite Handover Type definition The SNMP honAkSatHandoverPending reports the satellite handover state. It is an enumerated integer value with the structure as shown in Table B-9. Table B-9. Satellite Handover Enumeration Type Number 1 2 3 SNMP Type yes no unavailable (l) Description Satellite Handover is pending.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System The .honAkLinkStatus (1) folder contains object as shown in the details below: Object Identifier .honAkServSatLinkState (1) Type HonAkSatLink State honAkServTxO nGround .honAkServTxOnGround (2) 2 Range Description This object shows the state of the satellite link. This object indicates whether RF Transmission is allowed on Ground or not. System Related Sub Branch The .
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System .honAkModmanHealthStatus(2) HonAkHealthStatus .honAkKanduHealthStatus(3) HonAkHealthStatus .honAkKrfuHealthStatus(4) HonAkHealthStatus .honAkOaeHealthStatus(5) HonAkHealthStatus .honAkApmHealthStatus(6) .honAkAesFailureCode(7) HonAkHealthStatus DisplayString .honAkAesFailureText(8) DisplayString .honAkModmanToKanduEthernet(9) TruthValue .honAkModmanToKanduTxFilterSelectRs422(10) TruthValue .
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System .honAkModmanToKrfuRfLink(19) TruthValue .honAkKrfuToModmanRfLink(20) TruthValue .honAkOaeToKrfuRfLink(21) TruthValue .honAkApmToModman(22) TruthValue .honAkIrsStatus(23) honAkIrsStatus .honAkAesReset(24) TruthValue .honAkModmanThermalState(25) HonAkThermalStat e HonAkThermalStat e HonAkThermalStat e HonAkThermalStat e .honAkKanduThermalState(26) .honAkKrfuThermalState(27) .honAkOaeThermalState(28) 3 The Modman to KRFU RF link state.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System .honAkLinkTxCount(7) Unsigned32 .honAkLinkRxCount(8) Unsigned32 .honAkLinkSignalQuality(9) HonAkTenthsUnsigned32 .honAkLinkSignalLevel(10) HonAkTenthsInteger32 .honAkLinkEbNoSignalQuality(11) HonAkTenthsUnsigned32 .honAkTxCtrlState(12) HonAkDiscreteInputState .honAkWowState(13) HonAkDiscreteInputState .honAkCellularTxState(14) HonAkDiscreteInputState .honAkGroundTxState(15) HonAkDiscreteInputState .
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System .honAkAircraftOnGround(30) TruthValue .honAkAircraftGroundSpeed(31) Unsigned32 4 0..1500 | 9999 Indicates whether or not the aircraft is on the ground Reports the ground speed of the aircraft. The range of the object is from 0 to 1,500 knots. 9,999 indicates that the data is not available System Configuration Related Sub Branch The .
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System .honAkKrfuSwPnSwValid(20) DisplayString 0..32 .honAkKrfuSwSubpartVer(21) .honAkKrfuOemId(22) DisplayString DisplayString 0..255 0..32 .honAkKrfuHoneywellHwPn(23) DisplayString 0..32 .honAkOaeLruName(24) DisplayString 0..32 .honAkOaeOemHwPn(25) DisplayString 0..32 .honAkOaeSn(26) DisplayString 0..32 .honAkOaeSwPnSwValid(27) DisplayString 0..32 .honAkOaeSwSubpartVer(28) DisplayString 0..255 .honAkOaeOemId(29) DisplayString 0.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System b Port Info Table The .honAkPortInfoTable (2) table supports information pertaining to various Ethernet ports. This table has objects as shown in the below detail: Object Identifier .honAkPortInfoIndex(1) Type Unsigned32 Range 1..4294 967295 .honAkPortInfoName(2) DisplayString 0..16 .honAkPortInfoUserDataSupported(3) TruthValue .honAkPortInfoOperStatus(4) honAkPortInfoOperStatu s .honAkPortInfoVlanIdList(5) DisplayString .
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (3) Traps under Engineering Notification Branch This honAkEngNotifications(3) branch contain service and maintenance notification’s folder for maintenance and service related traps. (a) Service Trap Related Sub Branch The .honAkServTrap(0)Branch contains the object as shown in the below details: Trap (OID) .
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System APPENDIX C 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.
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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System APPENDIX D 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, a maintenance panel is required.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA B. Modman Physical Examine for physical damage. √ Value Environmental conditions, refer to Figure 2-24. 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 2-1.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA C. APM (Cont) Electrical wiring Electrically wire and interconnect in accordance with Figure 2-25 and Figure 2-33. √ Value Electrical wiring Connect the APM to the Modman with - APM to two twisted shielded 24 AWG pairs with Modman Teflon insulation or aerospace grade shielded CAT5/CAT5e cable, maximum length 9.8 feet (3 m). D. KANDU Physical Examine for physical damage.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA E. KRFU Physical Examine for physical damage. √ Value Environmental conditions, refer to Figure 2-27, Figure 2-28, or Figure 2-29 depending on configuration used. Install the thermal pad in accordance with KRFU Thermal Pad Kit on page 2-9. The KRFU is installed with the TMA, refer to OAE TMA Installation Procedure on page 2-15. The KRFU feet are configured differently depending on the part number ordered.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter J. OAE TMA Installation TMA install Procedure (Cont) TMA radome and radome fairing Item NA √ Value Refer to JetWave™ System LRU Installation, OAE TMA Installation Procedure. 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. Radome and fairing installation is aircraft specific. Refer to aircraft specific SDIM for details.
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, a maintenance panel is required.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA B. 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 2-1.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA C. APM (Cont) Electrical wiring Connect the APM to the Modman with - APM to two twisted shielded 24 AWG pairs with Modman Teflon insulation or aerospace grade shielded CAT5/CAT5e cable, maximum length 9.8 feet (3 m). D. KANDU Physical √ Value Examine for physical damage. Environmental conditions, refer to Figure 2-26 E. KRFU Mounting Install location of KANDU is airframe specific.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA E. 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. √ Value Electrical wiring Electrically wire and interconnect in accordance with outline drawing Figure 2-27, Figure 2-28, or Figure 2-29 and interconnect drawing Figure 2-34, Figure 2-35, or Figure 2-36. N.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA A. Maintenance Panel Applicability If the system is not wired to another aircraft system, a maintenance panel is required.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA B. Modman (Cont) Electrical bonding Bonding, refer to page 2-5 √ Value Electrical wiring Electrically wire and interconnect in accordance with Figure 2-24 and Figure 2-34, Figure 2-35, or Figure 2-36. Electrical RF coaxial Equalizer in the TX path TX path loss, refer to Table 2-2. Modman Cable Loss Values Attenuator in the RX path RX path loss, refer to Table 2-2. Modman Cable Loss Values C.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA D. KANDU Physical Examine for physical damage. √ Value Environmental conditions, refer to Figure 2-26 Electrical wiring Electrically wire and interconnect in accordance with Figure 2-26 and Figure 2-34, Figure 2-35, or Figure 2-36. Mounting Install location of KANDU is airframe specific.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter E. 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 Item NA √ Value Make sure the waveguide is connected before powering the KRFU Waveguide Connection must be WR28 for TX and KRFU to FMA coaxial cable for RX.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Section Parameter Item NA N. 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 (8). FMA radome Attach the radome assembly onto the radome skirt fairing. FMA bonding Electrically bond in accordance with page 2-29.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System APPENDIX E 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.
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Weight on Wheels Weight on Wheels Discrete Input Available Yes/No User Ethernet Port Configuration User Ethernet Port Enable/ Disable User Traffic Yes/No EN5 PIESD Ethernet Polarity of Weight on Wheels Discrete Signal User Services to be Enabled Dataload Yes/No SNMP Yes/No GUI Yes/No EN6 PIESD Ethernet EN7 PIESD Ethernet EN8 PIESD Ethernet AV1 AISD Ethernet AV2 AISD Ethernet AV3 AISD Ethernet PA1 PODD Ethernet PA2 PODD Ethernet PA3 PODD Ethe
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blockage Angle c Blockage Angle d Blockage Angle e Blockage Angle f Blockage Angle h Blockage Angle i Blockage Angle k Blockage Angle m Blockage Angle p Angle "c" refers to the point of the wing, where an antenna radiating at -10 degrees elevation would find the wing’s leading edge. Angle "d" refers to the outer, aft-most tip of the wing (including vortex eliminators, if present).
SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
