Honeywell Mark III manual Software Overview, MIL-STD-1553B, Pcmcia, Oooi

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future to define Warm and Hot spare requirements. This effort has not yet started. As the Mark III CMU hardware was designed to support Dual capability, Updated dual capability could be provided with a software upgrade.

Ethernet

ARINC 646 defines an Ethernet Local Area Network (ELAN) aboard an aircraft. The Mark III CMU provides four 10BaseT Ethernet ports that can be used for various applications which could include Gatelink connectivity, ARINC 615A data loading, ARINC 744A printer and ELAN connectivity. Software support for the Ethernet ports will require a software upgrade.

MIL-STD-1553B

Mil-Std-1553B is a military standard interface used to communicate with onboard end systems such as an FMC, MCDUs and remote annunciators. This hardware interface is only available in the military version of the Mark III CMU. Software support of this interface requires a software upgrade. This is applicable for only specific Military aircraft.

Debug Maintenance Terminal (DMT) / Data Logging Terminal (DLT)

A Debug Maintenance Terminal and Debug Logging Terminal can be used to access BITE information, program the APM, and for general debug capability. The Mark III CMU provides two RS-232 ports that can be used for a DMT and a DLT. The RS-232 ports are accessible both from the front and rear connectors and can interface with a laptop computer executing terminal emulation software. The DMT is a device that is used for Honeywell debugging and testing, and is not a device required by our airline customers.

Data Loader

The Mark III CMU supports an interface to both an ARINC 615 compliant Airborne Data Loader (ADL) and an ARINC 615 compliant Portable Data Loader (PDL) via high speed ARINC 429. The ADL interface is accessible through the rear connector while the PDL is accessible from the front connector.

High speed data loading via PCMCIA and Ethernet are software growth options.

PCMCIA

The Mark III CMU hardware is equipped with a PCMCIA interface that can be used, to provide a faster means of data loading than an ARINC 615 data loader. The PCMCIA interface is accessible only from the front panel. PCMCIA is Honeywell’s recommended method of performing complete full software loads.

OOOI

The Mark III CMU provides up to 6 high speed ARINC 429 inputs and a number of analog discrete inputs that can be used to determine Out/Off/On/In events. Data available on these interfaces typically include oil pressure, weight on wheels (WOW), flaps, parking brake, and doors.

2.3 Software Overview

In order to meet the system/safety requirements of future CNS/ATM upgrades, all of the Mark III CMU software has been developed to support a future DO-178B Level C. Today, the Mark III CMU is certified to Level D, which is the standard used for certification of ACARS and CMU units. Partitioning in the Mark III CMU is supported by the DEOS operating system which has been previously certified to DO-178B Level A.

The underlying fundamental goal for the Mark III CMU software development was to develop a single software system that could be used with minor modification on other platforms. Honeywell was able to achieve this goal through the use of advanced software development techniques, including model-based development. The model-based approach allowed the developers to design the system independent of the target hardware, capturing the requirements in a model database. The requirements/design are then turned into source code

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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 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 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