Honeywell Mark III manual Diversion Reasons

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Like the Reject Reasons page, the Diversion Report Downlink display contains a scrolling prompt and a conditional display field that is only displayed upon a certain value of the scroll field. Figure 23 shows the Diversion Reasons values. The text field below the diversion reason is only available when the diversion reason is "other".

Figure 23 Diversion Reasons

Two other object types that can be used on a display are toggle prompts and exclusive selector prompts (ESPs). Toggle prompts are a simple way of selecting from among one or more choices (ON/OFF). The Exclusive Selector Prompts are used to pick one (and only one) of two or more mutually exclusive choices. This is similar to the scroll prompt, but requires more display space (each choice must be placed on the display).

In addition to the downlink message screen definition, the user can define the downlink message format and characteristics (encodings). For downlink messages, the user defines the message elements (Figure 24) and the message properties (Figure 25). The message properties allows the user to define the downlink buffer and allowable subnetworks.

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 RegionsDMT and DLT System PagesBite VDL Mode Growth FunctionalityAPM Data LoadingPcmcia Data Loading Arinc 761 SatcomMil-STD Weather GraphicsATN Encryption/AuthenticationRRI 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 CCAProcessor CCA Power Supply CCAInput/Output 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 Section1 115 Vac Input Power Requirements Power Requirements2 28 Vdc Input Power Requirements 3 28 Vdc Backup Input Power Requirements Power Interrupt RequirementsTechnical Summary