Honeywell Mark III manual Spare CCAs Growth, Detailed Interface Definition

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Patented multi-layer microstrip/fiberglass high reliability printed wiring board (PWB

Analog Output Discretes

PCI BUS-based Connector

5.1.5 Spare CCAs (Growth)

The MARK III provides two CCA growth slots for expansion. The growth slots may be used to provide an integrated VHF Data Radio (VDR) into the MARK III, memory expansion to allow the CMU to act as an aircraft file server, or other product variants.

Minimum features of the Spare CCAs are:

PCI BUS-based Connector.

BITE Circuitry.

5.2 Detailed Interface Definition

Figure 32 and Figure 33 show the default external system interfaces supported by the MARK III CMU. The default external system interfaces, including the bus speeds, are modifiable using the APM.

The rear connector is a standard unit connector as defined in ARINC 758. The function and type of circuitry connected to the pin is listed in the table. All pins named ‘Spare’ are Honeywell reserved for future growth.

The front panel PDL circular connector is a standard 53-pin connector that is defined in ARINC 615. The function and type of circuitry connected to the pin is listed in the table. All function input and outputs are referenced to the CMU (DLT Input is input into the CMU and output from the terminal).

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 ProcessingDMT and DLT System PagesBite Growth Functionality VDL ModeAPM Data LoadingArinc 761 Satcom Pcmcia Data LoadingMil-STD Weather GraphicsATN Encryption/AuthenticationRRI 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 DesignProcessor CCA Power Supply 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 Section1 115 Vac Input Power Requirements Power Requirements2 28 Vdc Input Power Requirements Power Interrupt Requirements 3 28 Vdc Backup Input Power RequirementsTechnical Summary