Honeywell Mark III manual Technical Summary

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6 SUMMARY

The Mark III CMU is a high-end system which provides the latest in both hardware and software technology, unequalled in the industry. In addition to the Mark III CMU, Honeywell also manufactures a Mark II CMU, which is provided for both 724B wiring or 758 wiring, as well as other datalink related products including cockpit printers, Multi-Input Interactive Display Units (MIDUs); and VHF, HF and SATCOM systems. The following provides a summary of the Mark III CMU.

Technical Summary

The Mark III CMU is a high end CMU with significant

 

advancement over all other ACARS / CMU products in the

 

market today. The Mark III CMU hardware platform has

 

been designed as a modular avionics platform which can

 

not only be used as a CMU, but adapted to other future

 

potential uses. It is a 4 MCU unit, which complies to the

 

new ARINC 758 CMU characteristic, while providing

 

flexibility to add in additional functionality in the future to

 

expand it’s capability to our airline customers. Today’s

 

ACARS and CMU systems provide processor performance

 

capabilities in the range of 5 to 50 MIPS (Millions of

 

Instructions Per Second) and from 1 to 6 Mbytes of Memory.

Mark III CMU has Over 400 MIPs of

The Mark III CMU is a much higher end system, and has

Processing Power and Over 100 Mbytes

greater than 400 MIPs of processing capability and over a

of Memory – Designed to Support Long

100 Mbytes of memory. Although only a fraction of this

Term Growth without Hardware

processor and memory capability is used today, this

Changes

unprecedented growth capability has been designed into the

 

unit to ensure the lowest life cycle cost and long term growth capability to our customers. This will be a significant factor over the next ten to fifteen years, as the use of datalink, such as for Air Traffic Control communication continues to evolve. Such future processing as the addition of the Aeronautical Telecommunication Network (ATN)3, ATC unique applications, and the addition of new communication protocols will require more and more processor and memory capabilities within the CMU. Much of this new technology is just now being defined within the industry and will continue to be evolving over the next ten years. It is because of this evolution, that we have developed this high end platform with such significant growth capability, providing the lowest risk hardware platform for ensuring such upgrades can be supported in the unit you purchase today.

The Mark III CMU hardware has also been designed to not only meet the required interfaces as identified in the new ARINC 758 characteristic, but contains additional interfaces to support potential future growth options. As an example, The Mark III CMU comes standard with four (4) Ethernet ports. These ports provide growth capability to support future interfaces, without the need to perform hardware modifications, requiring software only modifications. The Mark III CMU also includes a UHF modem for future use. Thus, we are well positioned for such future changes such as the use of Ethernet links for dataloading, or other high speed interfaces that may be defined by the industry in the future.

3The ATN software is the next generation CMU air to ground and ground-to-ground protocols. The ATN is the ICAO defined protocols that will be used in the future as ATC communication transitions from voice to datalink. Honeywell has a unique position relative to the ATN, in that as program manager and one of the primary developers of the ATN router software (under contract to ATNSI), Honeywell is the only CMU manufacturer involved in the actual development of this future technology. Thus although the ATN will not be in operational use for at least several years, Honeywell has the technical expertise to assist our customers as such transition occurs in the future.

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 OverviewMark III CMU Interfaces Device System InterfacesArinc Interface Baseline Specificati GrowthArinc VDR SDU Hfdr Subnetwork InterfacesCMU Arinc 750 VHF Data Radio VDRUHF Flight Deck Devices InterfacesMcdu Midu CDU Control and Display Unit CDUFlight Management Computer FMC LRU InterfacesPerformance Computer PZ Aircraft Condition Monitoring System AcmsOther Interfaces MIL-STD-1553B Software OverviewPcmcia OooiVIA CMFDatabase Design CMU AOC HGI AMI Fidb GbstCertification AOA VDLM2 Baseline FunctionalityUplink Processing OperationsWorld Regions Downlink ProcessingSystem Pages DMT and DLTBite Growth Functionality VDL ModeAPM Data LoadingArinc 761 Satcom Pcmcia Data LoadingMil-STD Weather GraphicsEncryption/Authentication ATNRRI 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 DesignPower Supply CCA Processor CCAInput/Output CCA Detailed Interface Definition Spare CCAs GrowthPrntr McduCMC ADLOooi SDI PGM VHF PGMVOICE/DATA MON SEL CMUUnit Connectors and Mounts Mechanical Packaging Unit WeightUnit Size Cooling RequirementsEnvironmental Specifications Induced Signal Susceptibility DO-160D Section Power Input DO-160D SectionWaterproofness DO-160D Section Fluids Susceptibility DO-160D SectionPower Requirements 1 115 Vac Input Power Requirements2 28 Vdc Input Power Requirements Power Interrupt Requirements 3 28 Vdc Backup Input Power RequirementsTechnical Summary