Honeywell Mark III manual

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The Mark III CMU is designed to provide airlines with a hardware platform with the best growth potential of any system in the market. Not only does it contain significantly more processing power than other systems; it is also designed to support such future capabilities as Gatelink. The software within the Mark III CMU is also designed to provide customers with more control over AOC functional changes. This is accomplished using the GBST reconfiguration tool, which allows airlines to modify the logical processing in addition to such items as MCDU screens and downlink messages.

As the leading provider of Datalink systems, with over 100 customers, Honeywell provides our customers with extensive experience in the area of datalink. This includes our unique ability to be able to offer datalink systems which span every possible aircraft you may operate, including providing ATSU AOC software for the new Airbus aircraft, the datalink functions within the AIMS B-777 aircraft, to CMUs for aircraft ranging form Embraer 135/145s to wide body aircraft such as 747s. In addition, Honeywell’s Mark III CMU software is also being used as the software for our latest integrated avionics platforms such as the EPIC and VIA platforms. This includes providing the datalink function for the VIA platforms to be used on C-5 and KC-10 aircraft. Honeywell also is investing in the future. As an example, the future ATN software to be used in the future CNS/ATM-1 environment, is currently being developed by an international consortium of companions, including Honeywell, the only CMU manufacturer involved in it’s development.

In addition to offering all of today’s datalink avionics, Honeywell also offers ground-based solutions to airlines, ranging from services provided by our Global Data Center (which currently supports over 2,200 datalink-equipped aircraft); to on-site systems such as our AMOSS system. If more information on the Mark III CMU is needed, or on any other information on our Datalink products and service, please contact your Honeywell representative.

HONEYWELL Aerospace Electronic Systems

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Contents Honeywell Aerospace Electronic Systems Honeywell Aerospace Electronic Systems Mark III CMU Overview IntroductionDatalink Capability for Today and Tomorrow Honeywell Datalink Experience, Products, and Services Page Arinc Hardware OverviewInterface Baseline Specificati Growth System InterfacesMark III CMU Interfaces Device ArincArinc 750 VHF Data Radio VDR Subnetwork InterfacesArinc VDR SDU Hfdr CMUUHF Flight Deck Devices InterfacesMcdu Midu CDU Control and Display Unit CDUAircraft Condition Monitoring System Acms LRU InterfacesFlight Management Computer FMC Performance Computer PZOther Interfaces Oooi Software OverviewMIL-STD-1553B PcmciaVIA CMFDatabase Design CMU AOC HGI AMI Fidb GbstCertification AOA VDLM2 Baseline FunctionalityUplink Processing OperationsWorld Regions Downlink ProcessingBite System PagesDMT and DLT Data Loading VDL ModeGrowth Functionality APMWeather Graphics Pcmcia Data LoadingArinc 761 Satcom Mil-STDRRI Encryption/AuthenticationATN Page Fidb DatabasesFidb Architecture GbstFidb HGI AMI Main Menu MenusMain Menu CDU Main Menu Supporting Regional / Business Jet CDUs ATS Menu System Menu Clearance Uplink UplinksClearance Message Elements Clearance Message References Reject Reasons Reject Reasons Values Diversion Report Downlink DownlinksDiversion Reasons Divert Message Elements Logic Units Print DefinitionOooi Logic Unit Preferred Channel ManagementRegions US Map Areas Interconnect CCA Mechanical DesignInput/Output CCA Power Supply CCAProcessor CCA Detailed Interface Definition Spare CCAs GrowthADL McduPrntr CMCSEL CMU SDI PGM VHF PGMOooi VOICE/DATA MONCooling Requirements Mechanical Packaging Unit WeightUnit Connectors and Mounts Unit SizeEnvironmental Specifications Fluids Susceptibility DO-160D Section Power Input DO-160D SectionInduced Signal Susceptibility DO-160D Section Waterproofness DO-160D Section2 28 Vdc Input Power Requirements Power Requirements1 115 Vac Input Power Requirements Power Interrupt Requirements 3 28 Vdc Backup Input Power RequirementsTechnical Summary
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