Honeywell Mark III manual Areas

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Figure 30 Areas

The Mark III CMU GBST provides the next generation in Airline reconfiguration. It is specifically designed to provide airlines with the freedom and flexibility to customize the AOC functions in the CMU, and to allow users to expand the Mark III CMU as their requirements change. As part of the GBST, there is an extensive configuration control application built into the GBST, which allows airlines to manage the changes to the AMI database using the GBST. This includes both password controls as well as version control at the functional element level.

The GBST is an enhanced version of the GBST used for the B-777 system. As such, although there are more capabilities and features included, it provides the same basic interface as the B-777 GBST. Thus, airlines using the B-777 GBST will find that only minimal training is required due to the common human interface used between the two tools. The GBST for the Mark III CMU is also designed to operate on a PC, using either Windows NT or Windows 2000 (Windows 2000 recommended).

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 RegionsDMT and DLT System PagesBite APM VDL ModeGrowth Functionality Data LoadingMil-STD Pcmcia Data LoadingArinc 761 Satcom 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 Units Preferred Channel Management Oooi Logic UnitRegions US Map Areas Mechanical Design Interconnect CCAProcessor CCA Power Supply 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 Section1 115 Vac Input Power Requirements Power Requirements2 28 Vdc Input Power Requirements 3 28 Vdc Backup Input Power Requirements Power Interrupt RequirementsTechnical Summary