Honeywell Mark III manual Certification

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2.4 Certification

Honeywell received the 1st FAA certification in December 2001. This initial certification was for Embraer aircraft. The Mark III CMU has since also been type certified by Boeing. Contact Honeywell for up-to-date information on other certifications completed or in work.

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 ProcessingBite System PagesDMT and DLT Growth Functionality VDL ModeAPM Data LoadingArinc 761 Satcom Pcmcia Data LoadingMil-STD Weather GraphicsRRI 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 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 Section2 28 Vdc Input Power Requirements Power Requirements1 115 Vac Input Power Requirements Power Interrupt Requirements 3 28 Vdc Backup Input Power RequirementsTechnical Summary