Honeywell Mark III manual Fidb HGI AMI

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FIDB

HGI

AMI

FIDB

Customer

Mark III

Honeywell

CMU

 

 

Figure 11 AMI/HGI Generation

The GST offers a robust set of capabilities that allow the user to completely customize their AOC application. With the GBST, the user can control the functionality of the CMU, including such major items as:

defining the datalink menu structure,

defining the content and characteristics of uplink and downlink messages,

defining the format of printed messages and screen displays,

defining user parameters,

specifying message review categories,

defining areas and regions of the world to be used for specifying preferred frequencies and subnetworks,

specifying the set of downlink buffers, and

generating user-defined algorithms that trigger events when certain conditions are met (such as OOOI algorithms, engine exceedance algorithms, etc).

The GBST provides a wide range of capabilities, and all of the capabilities of the GBST are more than what can easily be described in this product description document. The following sections provides some additional information on how the GBST is used for reconfiguring the Mark III CMU, with the intent of identifying some of the major features of the GBST.

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