• BS EN 4660-004:2011

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

    Aerospace series. Modular and open avionics architectures Packaging

    Available format(s):  Hardcopy, PDF

    Superseded date:  28-08-2019

    Language(s):  English

    Published date:  31-03-2011

    Publisher:  British Standards Institution

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    Table of Contents - (Show below) - (Hide below)

    Foreword
    0 Introduction
    1 Scope
    2 Normative references
    3 Terms, definitions and abbreviations
    4 Generic module specification
    5 Module Mechanical Tests
    6 Guidelines for a rack slot
    7 Typical modular avionics environment

    Abstract - (Show below) - (Hide below)

    Defines uniform requirements for Packaging for the Common Functional Modules (CFM) within an Integrated Modular Avionic (IMA) system, as defined per ASAAC.

    Scope - (Show below) - (Hide below)

    The purpose of this standard is to establish uniform requirements for Packaging for the Common Functional Modules (CFM) within an Integrated Modular Avionic (IMA) system, as defined per ASAAC. It comprises the module physical properties and the Module Physical Interface (MPI) definitions together with guidelines for IMA rack and the operational environment. The characteristics addressed by the Packaging Standard are: Interchangeability: ? For a given cooling method all modules conforming to the packaging standard will function correctly when inserted into any rack slot conforming to the standard for the cooling method. - All modules conforming to the Module Physical Interface (MPI) definitions for connector, IED and cooling interface will function correctly when inserted into any rack slot conforming to the same MPI definition. Maintainability: - All modules are easily removable at first line. - No special tools required at first line. - No manual adjustment is necessary when installing modules. No tool is required for installation or removal of the modules. - Mechanical keying is provided that prevents insertion of a module into a rack slot that may cause an unsafe condition. The Module Physical Interface definition, contained within this standard, does not include the properties of the signalling used in the optical interface (e.g. wavelength). These are covered in EN 4660-003.

    General Product Information - (Show below) - (Hide below)

    Committee ACE/6
    Document Type Standard
    Publisher British Standards Institution
    Status Superseded
    Superseded By

    Standards Referencing This Book - (Show below) - (Hide below)

    EN 4660-002:2011 Aerospace series - Modular and Open Avionics Architectures - Part 002: Common Functional Modules
    EN 4660-003:2011 Aerospace series - Modular and Open Avionics Architectures - Part 003: Communications/Network
    EN 2284 : 1991 AEROSPACE SERIES - SULPHURIC ACID ANODIZING OF ALUMINIUM AND WROUGHT ALUMINIUM ALLOYS
    PREN 4660-005 : 200P1 AEROSPACE SERIES - MODULAR AND OPEN AVIONICS ARCHITECTURES - PART 5: FINAL DRAFT OF PROPOSED STANDARDS FOR SOFTWARE
    EN 2437 : 2001 AEROSPACE SERIES - CHROMATE CONVERSION COATINGS (YELLOW) FOR ALUMINIUM AND ALUMINIUM ALLOYS
    BS 5599:1993 Specification for hard anodic oxidation coatings on aluminium and its alloys for engineering purposes
    EN 4660-001:2011 Aerospace series - Modular and Open Avionics Architectures - Part 001: Architecture
    MIL C 5541 : E CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS
    EN 2101 : 1991 AEROSPACE SERIES - CHROMIC ACID ANODIZING OF ALUMINIUM AND WROUGHT ALUMINIUM ALLOYS
    MIL A 8625 : F ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
    MIL C 26074 : E COATINGS, ELECTROLESS NICKEL, REQUIREMENTS FOR
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