Honeywell Mark III manual Regions

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to use for message transmission. The user also can specify the set of VHF frequencies to use for that region. Figure 28 shows an example.

Figure 28 Regions

In this example, 5 regions are defined: Europe, US, Canada, Mexico, and Cuba. The OTHER region is used for all portions of the world not covered by the other user-defined regions. The DEFAULT region is used for the entire world when the aircraft position data is unavailable.

In this example if the aircraft is in the Mexico region, SATCOM would be the preferred subnetwork. However, if SATCOM is not available, VHF would be used with a frequency of 131.725. If that frequency is not available, then 131.550 would be used. If VHF is not available, then HF would be used.

This is a general algorithm based upon location within the world and is independent of message type. However, there may be cases where a user does not want certain messages to use certain subnetworks. For instance, the user may not wish to utilize HF for Divert Reports. The downlink message encoding property of the message allows the user to specify the set of allowable subnetworks.

Regions are defined to be the union of a set of areas with each area specified by a rectangle using latitude/longitude pairs. The capability to define areas within a region allows the user to more accurately define an irregularly shaped region. Using the map in Figure 29, the example USA region is comprised of three areas (Figure 30). Area 1 defines the continental US, area 2 defines Alaska, and area 3 Hawaii.

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Contents Honeywell Aerospace Electronic Systems Honeywell Aerospace Electronic Systems Introduction Mark III CMU OverviewDatalink Capability for Today and Tomorrow Honeywell Datalink Experience, Products, and Services Page Hardware Overview ArincSystem Interfaces Mark III CMU Interfaces DeviceArinc Interface Baseline Specificati GrowthSubnetwork Interfaces Arinc VDR SDU HfdrCMU Arinc 750 VHF Data Radio VDRFlight Deck Devices Interfaces UHFControl and Display Unit CDU Mcdu Midu CDULRU Interfaces Flight Management Computer FMCPerformance Computer PZ Aircraft Condition Monitoring System AcmsOther Interfaces Software Overview MIL-STD-1553BPcmcia OooiCMF VIACMU AOC HGI AMI Fidb Gbst Database DesignCertification Baseline Functionality AOA VDLM2Operations Uplink ProcessingDownlink Processing World RegionsBite System PagesDMT and DLT VDL Mode Growth FunctionalityAPM Data LoadingPcmcia Data Loading Arinc 761 SatcomMil-STD Weather GraphicsRRI Encryption/AuthenticationATN Page Databases FidbGbst Fidb ArchitectureFidb HGI AMI Menus Main MenuMain Menu CDU Main Menu Supporting Regional / Business Jet CDUs ATS Menu System Menu Uplinks Clearance UplinkClearance Message Elements Clearance Message References Reject Reasons Reject Reasons Values Downlinks Diversion Report DownlinkDiversion Reasons Divert Message Elements Print Definition Logic UnitsPreferred Channel Management Oooi Logic UnitRegions US Map Areas Mechanical Design Interconnect CCAInput/Output CCA Power Supply CCAProcessor CCA Spare CCAs Growth Detailed Interface DefinitionMcdu PrntrCMC ADLSDI PGM VHF PGM OooiVOICE/DATA MON SEL CMUMechanical Packaging Unit Weight Unit Connectors and MountsUnit Size Cooling RequirementsEnvironmental Specifications Power Input DO-160D Section Induced Signal Susceptibility DO-160D SectionWaterproofness DO-160D Section Fluids Susceptibility DO-160D Section2 28 Vdc Input Power Requirements Power Requirements1 115 Vac Input Power Requirements 3 28 Vdc Backup Input Power Requirements Power Interrupt RequirementsTechnical Summary