Honeywell Mark III manual Baseline Functionality, AOA VDLM2

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3 FUNCTIONAL OVERVIEW

The Mark III CMU is designed to provide complete datalink capability, providing interfaces and support to today’s installed equipment. In addition, Honeywell as well as the industry recognizes that Datalink features will be expanded over time, and is in fact the principle behind the current ARINC 758 characteristic. A Characteristic that was developed to define current operation (referred to as Level O.1A), and allow expansion over time to support new requirements and needs. The Mark III CMU was specifically designed to support such future growth. Growth Functionality describes potential new capabilities for post-baseline software releases. Many of the capabilities described in both the Baseline Functionality and Growth Functionality sections are configurable via the AMI or the HGI.

The Mark III CMU supports an ARINC 739 MCDU, an ARINC 739 MIDU, and a CDU for displaying ACARS information. For the purpose of simplifying the text of this section, 'datalink display' will be used generically to mean MCDU, MIDU, or CDU.

3.1 Baseline Functionality

The baseline Mark III CMU provides functionality defined as level 0.1A in ARINC 758.

For Reference, the level of functionality as defined in the ARINC 758 Characteristic is shown below. This level of functionality is defined, as the CMU is recognized within the industry as evolving over time in order to meet future CNS/ATM requirements.

A758 level

Service Function

 

 

0

ARINC 724B ACARS equivalent

 

 

 

ARINC 618: ACARS

 

 

 

ARINC 716: VHF

 

 

 

ARINC 750: VHF Mode 0

 

 

 

ARINC 741: SATCOM

 

 

0.1

+ VDR Mode A using ARINC 429 I/F

 

 

 

ARINC 750: Mode A

 

 

 

ARINC 761: SATCOM

 

 

 

ARINC 753: HF

 

 

0.2

AOA VDLM2

 

 

1

+ ATN Services

 

 

 

ARINC 750: VDL Mode 2

 

 

2

+ High Speed Services

 

 

 

Not specified at this time

 

 

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 RegionsSystem Pages DMT and DLTBite APM VDL ModeGrowth Functionality Data LoadingMil-STD Pcmcia Data LoadingArinc 761 Satcom Weather GraphicsEncryption/Authentication ATNRRI 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 CCAPower Supply CCA Processor 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 SectionPower Requirements 1 115 Vac Input Power Requirements2 28 Vdc Input Power Requirements 3 28 Vdc Backup Input Power Requirements Power Interrupt RequirementsTechnical Summary