ISO 6773:1994
Current
Current
The latest, up-to-date edition.
Aerospace Fluid systems Thermal shock testing of piping and fittings
Available format(s)
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
Language(s)
English, French
Published date
29-09-1994
Important note : Users cannot be edited or removed once added to your Multi user PDF.
Cancels and replaces the first edition (1982). Provides an environmental test method for thermal shock testing of fluid system piping and fittings, excluding hose and hose assemblies.
| DevelopmentNote |
Supersedes 91/77455 DC. (02/2002) Also numbered as BS 2M53(1997) (07/2005)
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| DocumentType |
Standard
|
| Pages |
2
|
| PublisherName |
International Organization for Standardization
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| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| SAE MA2004A | Identical |
| DIN ISO 6773:1996-01 | Identical |
| 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 |
| 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 |
| BS ISO 19631:2015 | Aerospace series. Tube fittings for fluid systems, 5 080 psi (35 000 kPa). Qualification specification |
| 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 |
| 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) |
| BS ISO 8829-2:2006 | Aerospace. Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Non-metallic braid |
| SAE AIR 2000 : 2000 | AEROSPACE FLUID SYSTEM STANDARDS, METRIC, NATIONAL AND INTERNATIONAL |
| ISO 8829-2:2006 | Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 2: Non-metallic braid |
| BS ISO 8829-1:2009 | Aerospace. Test methods for polytetraflouroethylene (PTFE) inner-tube hose assemblies Metallic (stainless steel) braid |
| ISO 8829-1:2009 | Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 1: Metallic (stainless steel) braid |
| 96/702228 DC : 0 | PREN 4231 - AEROSPACE SERIES - PIPE COUPLINGS 60 DEGREES UP TO 1000 KPA; METRIC SERIES - TECHNICAL SPECIFICATION |
| 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 |
| ISO 8829:1990 | Aerospace Polytetrafluoroethylene (PTFE) hose assemblies Test methods |
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