Honeywell Mark III manual Control and Display Unit CDU, Mcdu Midu CDU

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Control and Display Unit (CDU)

In the business jet and regional aircraft market place, there is limited cockpit pedestal real estate. Often, these aircraft are equipped with a 4-line-select key CDU instead of a 6-line-select key MCDU. The Mark III CMU can be configured to interface with one or two of these CDU devices via an RS-422 interface.

MCDU

MCDU

MIDU

CDU

Figure 2.2.2-1 Datalink Display Units

Printer

The Mark III CMU can interface with a single ARINC 740 or 744 compliant printer via low speed ARINC 429. This includes Honeywell’s ARINC 740 printer, as well as all other manufacturer’s who support the ARINC 740/744 specification.

ARINC 744A defines an Ethernet printer interface. The Mark III CMU has available Ethernet ports but requires a software upgrade to support an ARINC 744A printer. Currently, there are no aircraft configurations defined using the Ethernet interface for the CMU to printer interface.

Figure 4 Cockpit Printer

Crew Alerts

The Mark III CMU provides the interfaces necessary to support aural and visual alerts as well as an indication of NO COMM.

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 Overview Interface Baseline Specificati Growth System Interfaces Mark 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 ProcessingBite System PagesDMT and DLT Data Loading VDL ModeGrowth Functionality APMWeather Graphics Pcmcia Data LoadingArinc 761 Satcom Mil-STDRRI Encryption/AuthenticationATN 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 DesignInput/Output CCA Power Supply CCAProcessor 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 Section2 28 Vdc Input Power Requirements Power Requirements1 115 Vac Input Power Requirements Power Interrupt Requirements 3 28 Vdc Backup Input Power RequirementsTechnical Summary