ISO 6772:2012
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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
09-24-2012
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.
| Committee |
ISO/TC 20/SC 10
|
| DevelopmentNote |
Supersedes ISO/DIS 6772. (09/2012)
|
| DocumentType |
Standard
|
| Pages |
6
|
| PublisherName |
International Organization for Standardization
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| BS ISO 6772:2012 | Identical |
| GOST R ISO 6772 : 2011 | Identical |
| DIN ISO 6772:1996-01 | Identical |
| BS M 52:1983 | Identical |
| PN 92/L-01468 : 1992 | Identical |
| UNE 28586:1986 | Identical |
| 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 |
| 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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Hardcopy - English
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PDF 3 Users - English
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Hardcopy - English
PDF - English
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