Honeywell Mark III manual Flight Deck Devices Interfaces, Uhf

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Satellite Communications (SATCOM)

The Mark III CMU can be configured to interface with one or two ARINC 741 compliant Satellite Data Units (SDUs) via low speed ARINC 429, or can be configured for high speed 429.

The industry is still working on the definition of the ARINC 761 specification for second generation satellite communications systems, which will include access to Low Earth Orbit (LEO) and Medium Earth Orbit (MEO) satellite constellations. When datalink communications over ARINC 761 subnetworks is fully defined, it is planned that the Mark III will be updated (software only) to accommodate both ARINC 741 and ARINC 761 satellite communications.

HF Data Radio (HFDR)

The Mark III CMU can be configured to interface with one or two ARINC 753 compliant HFDRs (or HF Data Units -- HFDU) via low speed ARINC 429. The HFDR offers a datalink user another datalink option when line- of-site VHF and satellite communications are not available (i.e., over the ocean or poles).

UHF

The Mark III CMU contains a UHF modem to support UHF datalink. Software support of this interface requires a software upgrade. Currently there are no interfaces used with datalink for UHF, but the hardware has been added into the baseline unit to support potential future capability.

Mode S Transponder

The Mark III CMU can be configured to interface with one or two Mode S Transponders via high speed ARINC 429. Currently, datalink operation over Mode S is not defined. However, the Mark III CMU has the necessary ARINC 429 receivers in place to support such future need, if ever required. It should be noted that the Mark III CMU baseline does include the interface to the Mode S in order to obtain the ICAO 24 character address (which is then used for verification of data in the APM).

Gatelink

The current ARINC 758 specification identifies an ARINC 429 interface for gatelink interfaces. This is supported by the Mark III CMU hardware. However, Ethernet 10BaseT is a more likely Gatelink interface. The Mark III CMU supports up to four 10BaseT Ethernet ports. Honeywell will be offering a future upgrade package to the Mark III CMU that supports Gatelink capability within the unit, interfacing directly with a TWLU (Gatelink - Transceiver Wireless LAN Unit).

2.2.2 Flight Deck Devices Interfaces

The Mark III CMU supports interfaces to the following flight deck devices: (See Figure 2.2.2-1 for the available Datalink display devices supported by the Mark III CMU).

Multi-purpose Control and Display Unit (MCDU) / Multi-Input Display Unit (MIDU)

The Mark III CMU can be configured to interface with up to three ARINC 739 compliant display devices. These devices could be a standard MCDU or the compact MIDU. This is the standard interface on all Boeing

/Airbus and many other types of aircraft. The Mark III CMU supports the ability to present different menus simultaneously on different displays, providing a high degree of flexibility to the flight crew.

Dedicated Display and Control Unit (DCDU)

The industry envisions that certain ATS Datalink Services will require a dedicated datalink display device mounted in the primary field of view. The Mark III CMU can be configured to interface with one or two DCDUs via high speed ARINC 429. Software support for these devices is likely to be available through a software- only upgrade once the definition of this interface is fully defined by the industry.

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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 RegionsDMT and DLT System PagesBite APM VDL ModeGrowth Functionality Data LoadingMil-STD Pcmcia Data LoadingArinc 761 Satcom 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 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 Section1 115 Vac Input Power Requirements Power Requirements2 28 Vdc Input Power Requirements 3 28 Vdc Backup Input Power Requirements Power Interrupt RequirementsTechnical Summary