• BS ISO 8278:2016

    Current The latest, up-to-date edition.

    Aerospace series. Hydraulic, pressure compensated, variable delivery pumps. General requirements

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  31-03-2016

    Publisher:  British Standards Institution

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

    Foreword
    1 Scope
    2 Normative references
    3 Terms and definitions
    4 General requirements
    5 Functional requirements
    6 Detail design requirements
    7 Strength requirements
    8 Construction requirements
    9 Installation requirements
    10 Maintenance requirements
    11 Reliability requirements
    12 Quality assurance provisions
    13 Acceptance tests
    14 Qualification tests
    Bibliography

    Abstract - (Show below) - (Hide below)

    Describes the general requirements for pressure compensated, variable delivery hydraulic pumps, suitable for use in aircraft hydraulic systems at pressures up to 35000 kPa (5000 psi).

    Scope - (Show below) - (Hide below)

    This International Standard establishes the general requirements for pressure compensated, variable delivery hydraulic pumps, suitable for use in aircraft hydraulic systems at pressures up to 35000kPa (5000 psi).

    This International Standard is to be used in conjunction with detail specifications that is particular to each application.

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

    Committee ACE/69
    Development Note Supersedes BS M65(1987), BS ISO 12334 & 13/30280221 DC. (03/2016)
    Document Type Standard
    Publisher British Standards Institution
    Status Current
    Supersedes

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

    ISO 7320:1992 Aerospace Couplings, threaded and sealed, for fluid systems Dimensions
    ISO 8078:1984 Aerospace process Anodic treatment of aluminium alloys Sulfuric acid process, undyed coating
    ISO 8625-2:1991 Aerospace Fluid systems Vocabulary Part 2: General terms and definitions relating to flow
    ISO 3323:1987 Aircraft — Hydraulic components — Marking to indicate fluid for which component is approved
    ISO 2685:1998 Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones
    ISO 8399-2:1998 Aerospace — Accessory drives and mounting flanges (Metric series) — Part 2: Dimensions
    ISO 6771:2007 Aerospace Fluid systems and components Pressure and temperature classifications
    ISO 8399-1:1998 Aerospace — Accessory drives and mounting flanges (Metric series) — Part 1: Design criteria
    ISO 8625-1:1993 Aerospace Fluid systems Vocabulary Part 1: General terms and definitions related to pressure
    ISO 11218:2017 Aerospace Cleanliness classification for hydraulic fluids
    ISO 8079:1984 Aerospace process Anodic treatment of aluminium alloys Sulfuric acid process, dyed coating
    ISO 2093:1986 Electroplated coatings of tin — Specification and test methods
    ISO 7137:1995 Aircraft — Environmental conditions and test procedures for airborne equipment
    ISO 3601-1:2012 Fluid power systems — O-rings — Part 1: Inside diameters, cross-sections, tolerances and designation codes
    ISO 2669:1995 Environmental tests for aircraft equipment — Steady-state acceleration
    ISO 8081:1985 Aerospace process Chemical conversion coating for aluminium alloys General purpose
    ISO 2671:1982 Environmental tests for aircraft equipment — Part 3.4 : Acoustic vibration
    ISO 8625-3:1991 Aerospace Fluid systems Vocabulary Part 3: General terms and definitions relating to temperature
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