Honeywell manual System Interfaces, Mark III CMU Interfaces Device, Arinc

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Figure 1 Mark III CMU Front Panel

ARINC 607 defines the Aircraft Personality Module (APM) which contains all aircraft and system configuration information. The APM is external to the MARK III CMU and is a permanent fixture in the aircraft. Only one APM is required per MARK III CMU installation (one APM for each MARK III CMU mounting tray). The same APM part number is used on all aircraft in the fleet.

2.2 System Interfaces

The Mark III CMU supports an extensive set of interfaces. Many of these interfaces are specifically defined by ARINC 758. There are also a number of spare ARINC 429 ports available for additional devices as needed by the user. The Mark III CMU supports all of today’s ACARS interfaces used on today’s aircraft, with extensive capability for future growth.

 

 

PCMCIA

 

 

 

Table 1

Mark III CMU Interfaces

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Device

 

 

ARINC

 

Interface

#

Baseline /

 

 

 

 

 

 

Specificati

 

 

 

Growth

 

 

 

 

 

 

on

 

 

 

 

 

 

VHF Radio

716

 

Audio

1

Baseline

 

VDR: Mode 0

750

 

Audio

1

Baseline

 

 

Mode A

 

 

High speed ARINC 429

3

Baseline

 

 

Mode 2

 

 

High speed ARINC 429

3

Option

 

Satellite Data Unit (SDU)

741

 

High speed ARINC 429

2

Baseline

 

 

 

 

 

 

761

 

High speed ARINC 429

2 (note 1)

Growth

 

HF Data Radio (HFDR)

753

 

Low speed ARINC 429

2

Baseline

 

UHF

---

 

Audio

1

Growth

 

Mode S Transponder

718A

 

High speed ARINC 429

2 (note 7)

Baseline

 

Gatelink

751

 

High speed ARINC 429

1

Growth

 

 

 

 

 

 

undefined

 

Ethernet 10BaseT

note 2

Growth

 

MCDU/MIDU

739

 

High speed ARINC 429

3

Baseline

 

DCDU

undefined

 

High speed ARINC 429

1/2 (note 5)

Growth

 

CDU

----

 

RS-422

2

Baseline

 

Printer

740/744

 

Low speed ARINC 429

1 (note 3)

Baseline (note 3)

 

 

 

 

 

 

744A

 

Ethernet 10BaseT

note 2

Growth

 

FMC

702

 

Low speed ARINC 429

2/3 (note 4)

Baseline

 

 

 

 

 

 

702A

 

High speed ARINC 429

2/3 (note 4)

Growth

 

Performance Computer (PZ)

-----

 

RS-422

1

Growth

 

ACMS/DFDAU

619/429

 

Low speed ARINC 429

1

Baseline

 

CMC/CFDS/CFDIU

604/624

 

Low speed ARINC 429

1

Baseline

 

Cabin Terminal

---

 

Low speed ARINC 429

2

Baseline

 

Electronic Library (ELS)

---

 

High speed ARINC 429

1

Growth

 

Cockpit Voice Recorder

757

 

Low speed ARINC 429

1

Growth

 

(CVR)

 

 

 

 

 

 

 

GPSSU

743

 

High speed ARINC 429

1

Baseline

 

APM

607

 

---

1

Baseline

 

Dual CMU

758

 

High speed ARINC 429

1

note 6

 

Mil-Std-1553B

---

 

Mil-Std-1553B

1

Growth

 

DMT

---

 

RS-232

1

Baseline

 

DLT

---

 

RS-232

1

Baseline

 

Airborne Data Loader

615

 

High speed ARINC 429

1

Baseline

 

 

 

 

 

 

 

 

 

 

 

 

 

 

HONEYWELL Aerospace Electronic Systems

 

 

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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 ArincSystem Interfaces Mark III CMU Interfaces DeviceArinc Interface Baseline Specificati GrowthSubnetwork Interfaces Arinc VDR SDU HfdrCMU Arinc 750 VHF Data Radio VDRFlight Deck Devices Interfaces UHFControl and Display Unit CDU Mcdu Midu CDULRU Interfaces Flight Management Computer FMCPerformance Computer PZ Aircraft Condition Monitoring System AcmsOther Interfaces Software Overview MIL-STD-1553BPcmcia OooiCMF VIACMU AOC HGI AMI Fidb Gbst Database DesignCertification Baseline Functionality AOA VDLM2Operations Uplink ProcessingDownlink Processing World RegionsBite System PagesDMT and DLT VDL Mode Growth FunctionalityAPM Data LoadingPcmcia Data Loading Arinc 761 SatcomMil-STD Weather GraphicsRRI Encryption/AuthenticationATN 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 CCAInput/Output CCA Power Supply CCAProcessor CCA Spare CCAs Growth Detailed Interface DefinitionMcdu PrntrCMC ADLSDI PGM VHF PGM OooiVOICE/DATA MON SEL CMUMechanical Packaging Unit Weight Unit Connectors and MountsUnit Size Cooling RequirementsEnvironmental Specifications Power Input DO-160D Section Induced Signal Susceptibility DO-160D SectionWaterproofness DO-160D Section Fluids Susceptibility DO-160D Section2 28 Vdc Input Power Requirements Power Requirements1 115 Vac Input Power Requirements 3 28 Vdc Backup Input Power Requirements Power Interrupt RequirementsTechnical Summary