Honeywell Mark III manual Hardware Overview, Arinc

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2 SYSTEM OVERVIEW

2.1 Hardware Overview

The Mark III CMU is based upon the Multiple Application Processing System (MAPS) platform which is the new generation hardware that will be used for introduction of new Honeywell datalink products. This common hardware platform will facilitate the introduction of communication products that integrate new capabilities with the Mark III CMU.

The Mark III CMU is a single Line Replaceable Unit (LRU) housed in a standard 4 MCU ARINC 600 form factor. The Mark III CMU contains 4 Circuit Card Assemblies (CCAs): (1) Processor; (2) I/O; (3) Power Supply; and (4) Interconnect. There is expansion capacity for two spare CCAs.

The main processor is a 266 MHz Pentium while the I/O is handled by two MPC 860 microprocessors. These two I/O processors are able to concurrently process all I/O effectively eliminating throughput bottlenecks. Additionally, there are two dedicated digital signal processors (DSPs), one each for the VHF and UHF modems. There is a total of 64 MB of DRAM along with 48 MB of Flash EPROM.

The front panel of the Mark III CMU (see Figure 1) contains a "PUSH TO TEST" button for initiating Test Mode, two LEDs to indicate Test Mode Pass and Fail, an ARINC 615 connector, and a PCMCIA connector. The ARINC 615 connector can be used for a portable data loader, a Debug and Maintenance Terminal

ARINC 615

(DMT), or for a Data Logging Terminal (DLT).

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 ProcessingDMT and DLT System PagesBite Data Loading VDL ModeGrowth Functionality APMWeather Graphics Pcmcia Data LoadingArinc 761 Satcom Mil-STDATN Encryption/AuthenticationRRI 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 DesignProcessor CCA Power Supply CCAInput/Output 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 Section1 115 Vac Input Power Requirements Power Requirements2 28 Vdc Input Power Requirements Power Interrupt Requirements 3 28 Vdc Backup Input Power RequirementsTechnical Summary