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  • ISO 6772:2012

    Current The latest, up-to-date edition.

    Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies

    Available format(s):  Hardcopy, PDF, PDF 3 Users, PDF 5 Users, PDF 9 Users

    Language(s):  English

    Published date:  24-09-2012

    Publisher:  International Organization for Standardization

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    Abstract - (Show below) - (Hide below)

    This International Standard specifies the requirements and the procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace hydraulic systems. Requirements may apply, when appropriate, to components used in other aerospace fluid systems.

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

    Committee ISO/TC 20/SC 10
    Development Note Supersedes ISO/DIS 6772. (09/2012)
    Document Type Standard
    Publisher International Organization for Standardization
    Status Current
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    11/30254515 DC : 0 BS EN 4560 - AEROSPACE SERIES - PIPE COUPLING 37 DEGREES, SPHERICAL, UP TO 21000 KPA - INCH SERIES - TECHNICAL SPECIFICATION
    SAE MA 2005 : 2015 TUBE FITTINGS, AEROSPACE FLUID SYSTEMS, SEPARABLE, FOR 24 DEGREE CONE, GENERAL SPECIFICATION, METRIC
    BS ISO 7169:2014 Aerospace. Separable tube fittings for fluid systems, for 24° cones, for pressures up to 3 000 psi or 21 000 kPa. Procurement specification, inch/metric
    BS ISO 8913:2006 Aerospace. Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 400°F/3000 psi (204°C/20684 kPa) and 204°C/21000 kPa (400°F/3046 psi). Procurement specification
    BS 2M 53:1997 Aircraft. Fluid systems. Thermal shock testing of piping and fittings
    16/30282721 DC : 0 BS ISO 18487-1 - AEROSPACE SERIES - TITANIUM TUBE FOR 35MPA OPERATING PRESSURE - PART 1: INCH SERIES
    04/30112507 DC : DRAFT APR 2004 ISO 7169 - AEROSPACE - SEPARABLE TUBE FITTINGS FOR FLUID SYSTEMS, FOR 24 CONES, FOR PRESSURES UP TO 3000 PSI OR 21 KPA - PROCUREMENT SPECIFICATION INCH/METRIC
    PREN 4560 : 200P2 AEROSPACE SERIES - PIPE COUPLING, 37 DEGREES, SPHERICAL, UP TO 21000 KPA - INCH SERIES - TECHNICAL SPECIFICATION
    PREN 2624 : 200P1 AEROSPACE SERIES - PRESSURE IMPULSE TESTING OF HYDRAULIC SYSTEM COMPONENTS
    PREN 4832 : DRAFT 2017 AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING AND RING-LOCKED FITTING-REDUCER - INCH SERIES - TECHNICAL SPECIFICATION
    PREN 4800-003 : 200P2 AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 3: TUBE
    ISO 9528:1994 Aerospace Standard-weight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/21 000 kPa Procurement specification
    ISO 8574:2004 Aerospace Hydraulic system tubing Qualification tests for bent tubes
    BS EN 4560:2015 Aerospace series. Pipe coupling 37°, spherical up to 21 000 kPa. Inch series. Technical specification
    DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/14(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F)
    DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT1)SEC6/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
    04/30115718 DC : DRAFT JUL 2004 ISO 8829-2 - AEROSPACE - TEST METHODS FOR POLYTETRAFLUOROETHYLENE (PTFE) INNERTUBE HOSE ASSEMBLIES - PART 2: NON-METALLIC BRAID
    12/30237808 DC : DRAFT JUNE 2012 BS ISO 19631 - AEROSPACE - TUBE FITTINGS FOR FLUID SYSTEMS, 5000 PSI (35000 KPA) - QUALIFICATION SPECIFICATION
    17/30358538 DC : 0 BS EN 3275 - AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30 MINUTES UP TO 28000 KPA - DYNAMIC BEAM SEAL - METRIC SERIES - TECHNICAL SPECIFICATION
    BS EN 4814:2017 Aerospace series. Flange couplings up to 21 000 kPa. Technical specification. Inch series
    NF EN 3275 : 2002 AEROSPACE SERIES - PIPE COUPLING 8 DEGREES 30 MINUTES UP TO 28 000 KPA - DYNAMIC BEAM SEAL - METRIC SERIES - TECHNICAL SPECIFICATION
    BS ISO 19631:2015 Aerospace series. Tube fittings for fluid systems, 5 080 psi (35 000 kPa). Qualification specification
    BS ISO 23933:2006 Aerospace series. Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135°C/20 684 kPa (275°F/3 000 psi) and 135°C/21 000 kPa (275°F/3 046 psi). Procurement specification
    PD ISO/TR 17784:2003 Rubber and plastic hoses and hose assemblies. Guide for use by purchasers, assemblers, installers and operating personnel
    I.S. EN 3120:2012 AEROSPACE SERIES - TITANIUM ALLOY TI-P64003 - COLD WORKED AND STRESS RELIEVED - SEAMLESS TUBE FOR PRESSURE SYSTEMS - 4 MM <= D <= 51 MM - 690 MPA <= R[M] <= 1030 MPA
    04/30115599 DC : DRAFT JUN 2004 ISO 8913 - AEROSPACE SERIES - LIGHTWEIGHT POLYTETRAFLUOROETHYLENE (PTFE) HOSE ASSEMBLIES, CLASSIFICATION 400 DEGREE F/3000 PSI, 204 DEGREE C/21000 KPA
    BS 3M 60:1998 Separable tube fittings for fluid systems, 24° cone. General specification
    BS 2M 60:1993 Specification for separable tube fittings, 24° cone, for aerospace fluid systems
    I.S. EN 3275:2002 AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30 MINUTES UP TO 28 000 KPA - DYNAMIC BEAM SEAL - METRIC SERIES - TECHNICAL SPECIFICATION
    NF EN 4800-003 : 2012 AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 003: TUBE
    PREN 3120 : 200P3 AEROSPACE SERIES - TITANIUM ALLOY TI-P64003 - COLD WORKED AND STRESS RELIEVED - SEAMLESS TUBE FOR PRESSURE SYSTEMS - 4 MM <= D <= 51 MM - 690 MPA <= R[M] <= 1030 MPA
    PREN 3275 : 200P1 AEROSPACE SERIES - PIPE COUPLING 8 DEGREES 30 MINUTES UP TO 28000 KPA DYNAMIC BEAM SEAL - METRIC SERIES - TECHNICAL SPECIFICATION
    ISO 8913:2006 Aerospace Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 400 degrees F/3 000 psi (204 degrees C/20 684 kPa) and 204 degrees C/21 000 kPa (400 degrees F/3 046 psi) Procurement specification
    BS EN 3275:2002 Aerospace series. Pipe coupling 8°30\' up to 28000 kPa. Dynamic beam seal. Metric series. Technical specification
    I.S. EN 2624:2007 AEROSPACE SERIES - PRESSURE IMPULSE TESTING OF HYDRAULIC SYSTEM COMPONENTS
    I.S. EN 4560:2015 AEROSPACE SERIES - PIPE COUPLING 37 DEGREES, SPHERICAL, UP TO 21000 KPA - INCH SERIES - TECHNICAL SPECIFICATION
    05/30128217 DC : DRAFT JAN 2005 ISO/DIS 23933 - AEROSPACE - ARAMID REINFORCED LIGHTWEIGHT POLYTETRAFLUOROETHYLENE (PTFE) HOSE ASSEMBLIES, CLASSIFICATION 135 DEGREE C/20 684 KPA (275 DEGREE F/3 000 PSI) AND 135 DEGREE C/21 000 KPA (275 DEGREE F/3 046 PSI) - PROCUREMENT SPECIFICATION
    BS ISO 18487-1:2017 Aerospace series. Titanium tube for 35 MPa operating pressure Inch series
    BS EN 2624:2007 Aerospace series. Pressure impulse testing of hydraulic system components
    06/30160259 DC : 0 BS ISO 8829-1 - TEST METHODS (PTFE) INNERTUBE HOSE ASSYS - PART 1: STAINLESS STBRAID
    14/30310862 DC : 0 BS EN 4832 - AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING AND RING-LOCKED FITTING-REDUCER - INCH SERIES - TECHNICAL SPECIFICATION
    96/712318 DC : DRAFT SEP 1996 PREN 3079 - AEROSPACE SERIES - ADAPTORS WITH LOCKING RING UP TO 2800 KPA - TECHNICAL SPECIFICATION
    ISO 23933:2006 Aerospace Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135 degrees C/20 684 kPa (275 degrees F /3 000 psi) and 135 degrees C/21 000 kPa (275 degrees F/3 046 psi) Procurement specification
    PREN 4814 : DRAFT 2015 AEROSPACE SERIES - FLANGE COUPLINGS UP TO 21000 KPA - TECHNICAL SPECIFICATION - INCH SERIES
    SAE AIR 2000 : 2000 AEROSPACE FLUID SYSTEM STANDARDS, METRIC, NATIONAL AND INTERNATIONAL
    ISO 10502:2012 Aerospace — Hose assemblies in polytetrafluoroethylene (PTFE) for use up to 232 °C and 10 500 kPa — Technical specifications and requirements
    ISO 9938:1994 Aerospace Polytetrafluoroethylene (PTFE) hose assemblies, classification 204 degrees C/28 000 kPa Procurement specification
    ISO/TR 17784:2003 Rubber and plastics hoses and hose assemblies Guide for use by purchasers, assemblers, installers and operating personnel
    DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
    DEFSTAN 00-970(PT7)SEC2/SUPP6/6(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F)
    97/719220 DC : DRAFT NOV 1997 PREN 3557 - AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T4 - DRAWN TUBE FOR PRESSURE APPLICATIONS - 0,6 MM <= A <= 3 MM
    SAE MA 2006 : 2015 HYDRAULIC TUBING - QUALIFICATION TEST REQUIREMENTS
    BS ISO 8574:2004 Aerospace. Hydraulic system tubing. Qualification tests for bent tubes
    BS ISO 8829-2:2006 Aerospace. Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Non-metallic braid
    UNI EN 4800-003 : 2011 AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 003: TUBE
    09/30208359 DC : 0 BS EN 4814 - AEROSPACE SERIES - FLANGE COUPLINGS - UP TO 21000 KPA - TECHNICAL SPECIFICATION, INCH SERIES
    DIN 65210-3:1987-11 AEROSPACE; HOSE ASSEMBLIES FOR NOMINAL PRESSURES UP TO 210 BAR; TECHNICAL SPECIFICATION FOR COMPLETE HOSE ASSEMBLIES
    BS ISO 10502:2012 Aerospace. Hose assemblies in polytetrafluoroethylene (PTFE) for use up to 232 °C and 10 500 kPa. Technical specifications and requirements
    BS EN 4800-003:2010 Aerospace series. Titanium and titanium alloys. Technical specification Tube
    BS EN 3120:2012 Aerospace series. Titanium alloy TI-P64003. Cold worked and stress relieved. Seamless tube for pressure systems. 4 mm ≤ D ≤ 51 mm. 690 MPa ≤ Rm ≤ 1 030 MPa
    ISO 8829-1:2009 Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 1: Metallic (stainless steel) braid
    SAE AS 603 : 2015 IMPULSE TESTING OF HYDRAULIC HOSE, TUBING, AND FITTING ASSEMBLIES
    ISO 8829-2:2006 Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 2: Non-metallic braid
    UNI EN 3120 : 2013 Aerospace series - Titanium alloy TI-P64003 - Cold worked and stress relieved - Seamless tube for pressure systems - 4 mm ≤ D ≤ 51 mm - 690 MPa ≤ Rm ≤ 1 030 MPa
    EN 3275:2002 Aerospace series - Pipe coupling 8°30' up to 28 000 kPa - Dynamic beam seal - Metric series - Technical specification
    ISO 7169:2014 Aerospace Separable tube fittings for fluid systems, for 24 degree cones, for pressures up to 3 000 psi or 21 000 kPa Procurement specification, inch/metric
    EN 4800-003:2010 Aerospace series - Titanium and titanium alloys - Technical specification - Part 003: Tube
    EN 3120 : 2012 Aerospace series - Titanium alloy TI-P64003 - Cold worked and stress relieved - Seamless tube for pressure systems - 4 mm ≤ D ≤ 51 mm - 690 MPa ≤ Rm ≤ 1 030 MPa
    EN 4814:2017 Aerospace series - Flange couplings up to 21 000 kPa - Technical specification - Inch series
    EN 4560:2015 Aerospace series - Pipe coupling 37°, spherical up to 21 000 kPa - Inch series - Technical specification
    EN 3079:2006 Aerospace series - Pipe coupling 8°30' up to 28 000 kPa - Adaptors - Metric series - Technical specification
    EN 2624 : 2007 AEROSPACE SERIES - PRESSURE IMPULSE TESTING OF HYDRAULIC SYSTEM COMPONENTS
    BS ISO 8829-1:2009 Aerospace. Test methods for polytetraflouroethylene (PTFE) inner-tube hose assemblies Metallic (stainless steel) braid
    DIN ISO 6773:1996-01 AEROSPACE - FLUID SYSTEMS - THERMAL SHOCK TESTING OF PIPING AND FITTINGS
    I.S. EN 4800-003:2010 AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 003: TUBE
    BS M 60:1986 Specification for separable tube fittings for fluid systems
    ISO 19631:2015 Aerospace series Tube fittings for fluid systems, 5 080 psi (35 000 kPa) Qualification specification
    10/30212765 DC : 0 BS ISO 10502 - AEROSPACE - HOSE ASSEMBLIES IN POLYTETRAFLUOROETHYLENE (PTFE) FOR USE UP TO 232 DEGREES C AND 10500 KPA - TECHNICAL SPECIFICATION
    ISO 18487-1:2017 Aerospace series — Titanium tube for 35 MPa operating pressure — Part 1: Inch series
    PREN 3079 : 200P1 AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30 MINUTES UP TO 28000 KPA - ADAPTORS - METRIC SERIES - TECHNICAL SPECIFICATION
    PREN 3557 : 200P1 AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T4 - DRAWN TUBE FOR PRESSURE APPLICATIONS - 0,6 MM <= A <= 3,0 MM
    I.S. EN 4814:2017 AEROSPACE SERIES - FLANGE COUPLINGS UP TO 21000 KPA - TECHNICAL SPECIFICATION - INCH SERIES
    ISO 8829:1990 Aerospace Polytetrafluoroethylene (PTFE) hose assemblies Test methods
    BS EN 3079:2006 Pipe coupling 8°30\' up to 28000 kPa. Adaptors. Metric series. Technical specification

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

    ISO 6771:2007 Aerospace Fluid systems and components Pressure and temperature classifications
    ISO 8625-1:1993 Aerospace Fluid systems Vocabulary Part 1: General terms and definitions related to pressure
    SAE AIR 1228 : 2009 STANDARD IMPULSE MACHINE EQUIPMENT AND OPERATION
    ISO 8575:2016 Aerospace — Fluid systems — Hydraulic system tubing
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