ARINC 739A : 1996 SUPP 1
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
MULTI-PURPOSE CONTROL AND DISPLAY UNIT
12-01-2022
12-01-2013
1.0 INTRODUCTION AND DESCRIPTION
1.1 Purpose of This Document
1.2 Functions
1.3 System Description
1.4 Interchangeability
1.4.1 General
1.4.2 Interchangeability Desired for the
ARINC 739A MCDU
1.4.3 "Generation Interchangeability" Consideration
1.5 Regulatory Approval
1.6 Relationship to ARINC 739
2.0 INTERCHANGEABILITY STANDARDS
2.1 Introduction
2.2 Form Factor
2.3 Environmental Conditions
2.4 Interwiring
2.5 Thermal Interface and Design
2.6 Power Circuitry
2.6.1 Primary Power Input
2.6.2 Power Control Circuitry
2.6.3 The Common Ground
2.6.4 The AC Common Cold
2.7 Weights
2.8 Grounding and Bonding
3.0 MCDU DESCRIPTION
3.1 General
3.2 Display
3.3 Keyboard
3.3.1 Basic Function Keys
3.3.2 Specific Function Keys
3.3.3 Alpha-Numeric Keys
3.3.4 Panel Illumination and Annunciator Lights
3.4 MCDU Operation and Display
3.4.1 Typical MCDU Initiation
3.4.2 MCDU Menu
3.4.3 Subsystem Specific Menu
3.4.4 Non-Menu Operation
3.4.5 Scratchpad and Data Field Entry
3.4.6 Clearing Data Fields
3.4.7 Exiting
3.4.8 Proposed Philosophy to Menu Stepping
3.5 MCDU Outputs
3.6 MCDU Inputs
3.7 System Communication
3.7.1 Subsystem and MCDU Identification
3.7.2 Menu Generation
3.7.2.1 Initial Menu
3.7.2.1.1 Addressing and Responses
3.7.2.1.2 Protocol Timing and Responses
3.7.2.2 Menu Changes
3.7.2.3 Alternate Menu Display
3.7.3 Data Communication
3.7.3.1 Subsystem Initiated Messages
3.7.3.1.1 Subsystems Not Currently Active
3.7.3.1.2 Active Subsystems
3.7.3.2 MCDU Communication with Inactive Subsystem
and Data Request
3.7.3.3 Message Transfer
3.7.3.4 Control (CNTRL) Word
3.7.3.5 Data Word
3.7.3.6 Background/Vector Words
3.7.3.7 Discrete Word
3.7.3.8 Button Push Word
3.8 Built-In Test Equipment (BITE)
3.8.1 BITE Considerations
3.8.2 BITE Display
3.8.3 Self-Test
3.9 Electronic Flight Instrument System Interface
3.9.1 MCDU Outputs to EFI
3.9.2 MCDU Inputs from EFI
3.9.3 MCDU Map Inputs from FMC
3.9.4 Flight Plans and Guidance
3.9.5 Map Display Edit Area
3.9.6 Background Data Prioritizing
3.9.7 Data Type Word Formats
3.9.8 Flight Plan Retention
4.0 NAVIGATION AND DISPLAY CONTROL
4.1 Introduction
4.2 Functional Requirements
4.2.1 System Selection and Control
4.2.2 Navigation Radio Tuning
4.2.2.1 Mode Selection
4.2.2.2 General Operation
4.2.2.3 Navigation Tuning Page Functions
4.2.2.3.1 Tuning Inhibit
4.2.2.4 Interface Requirements
4.2.3 Standby Navigation
4.2.3.1 Mode Selection
4.2.3.2 Operation
4.2.3.2.1 General
4.2.3.2.2 Navigation and Guidance
4.2.3.2.3 CDU Page Access
4.2.3.2.4 Navigation Computations
4.2.3.2.5 Map Display
4.2.3.3 Interface Requirement
4.2.4 Alternate EFIS Control
4.2.4.1 General
4.2.4.2 Page Access
4.2.4.3 Interface
4.2.5 Alternate EICAS Control
4.2.5.1 General
4.2.5.2 Page Access
4.2.5.3 Interface
4.2.6 System Communication
4.2.6.1 Inter-system
4.3 Hardware Requirements
4.3.1 General
4.3.2 Interwiring Definition
4.4 Standby Navigation Lateral Guidance
ATTACHMENTS
1 Standard Interwiring
2 Address Labels
3 Digital Word Formats
4 Character Code Assignments
(Derived from ISO No. 5)
5 Environmental Test Categories
6 Typical System Configuration
7 Typical Front Panel Layout
8 Glossary
9 Optional MCDU Functions
10 MCDU Display Considerations
Consists of the original ARINC 739 definition with enhancements to allow it to be logged on to up to two systems at one time. Alternate form factors are included to allow the MCDU to be introduced into a wide variety of airframes candidate for CNS/ATM upgrade.
DocumentType |
Standard
|
PublisherName |
Aeronautical Radio Inc.
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
ARINC 756-3 : 2004 | GNSS NAVIGATION AND LANDING UNIT (GNLU) |
ARINC 658 : 2017 | INTERNET PROTOCOL SUITE (IPS) FOR AERONAUTICAL SAFETY SERVICES - ROADMAP DOCUMENT |
ARINC 760-1 : 2000 | GNSS NAVIGATION UNIT (GNU) |
ARINC 660A : 2001 | CNS/ATM AVIONICS, FUNCTIONAL ALLOCATION AND RECOMMENDED ARCHITECTURES |
ARINC 660B : 2014 | CNS/ATM AVIONICS ARCHITECTURES SUPPORTING NEXTGEN/SESAR CONCEPTS |
ARINC 764 : 2005 | HEAD-UP DISPLAY (HUD) SYSTEM |
ARINC 758-3:2011 | COMMUNICATIONS MANAGEMENT UNIT (CMU) MARK 2 |
ARINC 771 : 2016 | LOW-EARTH ORBITING AVIATION SATELLITE COMMUNICATION SYSTEM |
ARINC 702A : 2014 | ADVANCED FLIGHT MANAGEMENT COMPUTER SYSTEM |
ARINC 738A : 1999 | AIR DATA AND INERTIAL REFERENCE SYSTEM (ADIRS) |
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