Honeywell Mark III manual Downlink Processing, World Regions

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Once an AOC message has been viewed by the flight crew (and any required user action has been taken), it can be placed in one of 8 user defined review categories. ATC messages have a separate review category. The flight crew can access messages placed in the review categories at any time.

A useful analogy for ACARS message processing is an email system. When a new email arrives, the user is alerted ("you have mail") and the message goes into an inbox. Once the message is read, the user will typically file the message into one of several email folders. The review categories can be thought of as email folders.

Downlink Processing

The flight crew can create downlink messages to be transmitted to ground systems. As with uplink messages, the definition of the display format and the downlink message format is defined by the user in the AMI. The downlink message can include any aircraft parameters defined in the FIDB and specified in the AMI.

Once all required data is entered on the downlink screen, the SEND prompt becomes active. After selecting the SEND prompt, the message status transitions to SENDING. The flight crew will be notified of successful receipt by the ground when the message status transitions to SENT.

A downlink message is placed in a user-defined queue for transmission to the ground. The user can define the downlink queue based on any number of criteria. For instance, a downlink queue can be defined for a particular message type. By defining different queues for different message types, a user can ensure equitable transmission of different message types.

A user is also able to define the preferred subnetwork (and even service provider) to be used for transmitting a message to the ground. This preference can vary depending upon the current aircraft position. The user can define regions of the world by specifying a series of latitude and longitude coordinates. For a given region, the user can then specify the preferred subnetwork and frequency (See Figure 8 for an example). The baseline subnetworks include VHF (mode 0/A), SATCOM, and HFDL.

Figure 8 World Regions

HONEYWELL Aerospace Electronic Systems

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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