Honeywell Mark III manual Print Definition, Logic Units

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4.2.4 Print Definition

The user can define the print format for a message by specifying the field names and associated parameters. Figure 26 shows the print format for a Flight Initialization uplink. This allows the user to define formats for uplink messages, as well as Mark III CMU generated reports to be easily readable by the flight crew. It also allows the flexibility to modify such formats as user requirements change.

Figure 26 Print Format

4.2.5 Logic Units

In addition to the various display types and the conditional display options, the GBST provides an extremely powerful capability called logic units. Logic units allow a user to generate algorithms that can trigger events based upon certain conditions. This provides significant flexibility to a user as user requirements for datalink change, and more complex functions are required. The use of logic units provides a wide range of capabilities. For instance, a display object could be hidden on a screen and made visible only when a specific parameter exceeds a certain value. Logic units can be used to provide a mini-ACMS capability where a downlink message is generated and sent (without flight crew involvement) when a specific condition has been met (such as an engine exceedance). Further, the specified condition can be turned on and off or even changed based upon the value included in an uplink message.

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 ArincArinc System InterfacesMark III CMU Interfaces Device Interface Baseline Specificati GrowthCMU Subnetwork InterfacesArinc VDR SDU Hfdr Arinc 750 VHF Data Radio VDRFlight Deck Devices Interfaces UHFControl and Display Unit CDU Mcdu Midu CDUPerformance Computer PZ LRU InterfacesFlight Management Computer FMC Aircraft Condition Monitoring System AcmsOther Interfaces Pcmcia Software OverviewMIL-STD-1553B OooiCMF VIACMU AOC HGI AMI Fidb Gbst Database DesignCertification Baseline Functionality AOA VDLM2Operations Uplink ProcessingDownlink Processing World RegionsSystem Pages DMT and DLTBite APM VDL ModeGrowth Functionality Data LoadingMil-STD Pcmcia Data LoadingArinc 761 Satcom Weather GraphicsEncryption/Authentication ATNRRI 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 CCAPower Supply CCA Processor CCAInput/Output CCA Spare CCAs Growth Detailed Interface DefinitionCMC McduPrntr ADLVOICE/DATA MON SDI PGM VHF PGMOooi SEL CMUUnit Size Mechanical Packaging Unit WeightUnit Connectors and Mounts Cooling RequirementsEnvironmental Specifications Waterproofness DO-160D Section Power Input DO-160D SectionInduced Signal Susceptibility DO-160D Section Fluids Susceptibility DO-160D SectionPower Requirements 1 115 Vac Input Power Requirements2 28 Vdc Input Power Requirements 3 28 Vdc Backup Input Power Requirements Power Interrupt RequirementsTechnical Summary