ISO 8829-1:2009
Current
The latest, up-to-date edition.
Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 1: Metallic (stainless steel) braid
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English
23-03-2009
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ISO 8829-1:2009 specifies test methods for flexible polytetrafluoroethylene (PTFE) inner tubes with metallic (stainless steel) braided hose and hose assemblies used in aircraft fluid systems, in the pressure and temperature ranges covered by pressure classes and temperature types, as specified in ISO 6771.
If performance requirements are not defined in ISO 8829-1:2009, they are defined in the performance specification.
ISO 8829-1:2009 is applicable when reference is made to it in a procurement specification or other definition document.
| DevelopmentNote |
Supersedes ISO/DIS 8829-1. (03/2009)
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| DocumentType |
Standard
|
| Pages |
19
|
| PublisherName |
International Organization for Standardization
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| Status |
Current
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| Standards | Relationship |
| BS ISO 8829-1:2009 | Identical |
| 00/715934 DC : DRAFT OCT 2000 | ISO/CD 8913 - AEROSPACE - LIGHTWEIGHT POLYTETRAFLUOROETHYLENE (PTFE) HOSE ASSEMBLIES, CLASSIFICATION 204 DEGREE C/20 684 KPA (400 DEGREE F/ 3000 PSI), 204 DEGREE C/21 000 KPA (400 DEGREE F/ 3046 PSI) - PROCUREMENT SPECIFICATION |
| ISO 10502:2012 | Aerospace — Hose assemblies in polytetrafluoroethylene (PTFE) for use up to 232 °C and 10 500 kPa — Technical specifications and requirements |
| 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 |
| 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 1595(1965) : LATEST | PROPAN-2-OL (ISOPROPYL ALCOHOL) FOR INDUSTRIAL USE |
| MIL-DTL-5624 Revision W:2016 | TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5 |
| NFM 15 006 : 1976 FD | LIQUID MINERAL FUELS - PROPERTIES OF WHITE SPIRIT |
| MIL-PRF-7808 Revision L:1997 | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| ISO 2685:1998 | Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
| MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
| ISO 6771:2007 | Aerospace — Fluid systems and components — Pressure and temperature classifications |
| AIR 319660/A : 1966 | |
| AIR 3407/B : 1972 | CARBURANT TYPE "LARGE COUPE" POUR TURBOMACHINES D'AVIATION |
| MIL-PRF-680 Revision C:2010 | DEGREASING SOLVENT |
| AIR 3520/B : 1979 | LIQUIDE MINERAL TYPE 5 CENTISTOKES A 100 DEGRE C, POUR TRANSMISSIONS HYDRAULIQUES |
| ISO 6772:2012 | Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies |
| AIR 3514/A : 1982 | HUILE SYNTHETIQUE, TYPE 3 MM[2]/S (CENTISTOKES) A 100 DEGRE C, POUR TURBOMACHINES D'AVIATION |
| ISO 7258:1984 | Polytetrafluoroethylene (PTFE) tubing for aerospace applications Methods for the determination of the density and relative density |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
| TT-I-735 Revision A:1963 | ISOPROPYL ALCOHOL |
| BS 245:1976 | Specification for mineral solvents (white spirit and related hydrocarbon solvents) for paints and other purposes |
| DEFSTAN 91-48/2(1997) : 1997 | HYDRAULIC FLUID, PETROLEUM: SUPERCLEAN NATO CODE: H-515 JOINT SERVICE DESIGNATION: OM-15 HYDRAULIC FLUID, PETROLEUM: NORMAL NATO CODE: H-520 JOINT SERVICE DESIGNATION: OM-18 |
| ASTM D 471 : 2016-02 | TEST METHOD FOR RUBBER PROPERTY - EFFECT OF LIQUIDS |
| ISO 8829-2:2006 | Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 2: Non-metallic braid |
| ISO 6773:1994 | Aerospace Fluid systems Thermal shock testing of piping and fittings |
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