Honeywell Mark III manual Reject Reasons Values

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There are a number of different types of objects that can be placed on a display. As an example, for the Main Menu, page prompts are used to link to other pages. The Main Menu also used a constant text string for the title. The Clearance Uplink display had RETURN and PRINT prompts as well as the ACCEPT, REJECT, and RESP REASONS action prompts. Real-time parameters (such as from the FMS, or internally computed within the CMU, or received from other subsystems) can be displayed on screens. As an example, the Clearance Uplink display also contained a parameter being the value of the Clearance uplink text block.

The Response Reasons screen illustrates several other objects: mandatory entry box, optional entry box, and scrolling prompt. The mandatory entry box is indicated by boxes while the optional entry box is indicated with dashes. Alternatively, brackets can be used for optional data instead of dashes. A scrolling prompt object is preceded by a down arrow and provides the capability to scroll through a number of values. Figure 21 shows the values for the reject reason scroll prompt. The Reject Reasons page also utilizes conditional logic for field display. The optional entry box is only displayed for entry when the value of the reject reason is "other".

Figure 21 Reject Reasons Values

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 RegionsBite System PagesDMT and DLT APM VDL ModeGrowth Functionality Data LoadingMil-STD Pcmcia Data LoadingArinc 761 Satcom 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 Uplink Clearance 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 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 Section2 28 Vdc Input Power Requirements Power Requirements1 115 Vac Input Power Requirements 3 28 Vdc Backup Input Power Requirements Power Interrupt RequirementsTechnical Summary