BS ISO 8829-2:2006
Current
The latest, up-to-date edition.
Aerospace. Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Non-metallic braid
Hardcopy , PDF
English
10-31-2006
Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Test temperature
5 Tests on PTFE inner tubes
5.1 Density and relative density
5.2 Tensile tests
5.3 Rolling and proof-pressure tests
5.4 Electrical conductivity test
6 Test on hoses and hose assemblies
6.1 Stress degradation test
6.2 Pneumatic effusion test
6.3 Electrical conductivity test
6.4 Visual and dimensional inspection
6.5 Determination of elongation or contraction
6.6 Volumetric expansion test
6.7 Leakage test
6.8 Proof-pressure test
6.9 Burst-pressure tests
6.10 Impulse test
6.11 Flexure test
6.12 Fuel resistance test
6.13 Low-temperature flexure testing
6.14 Pneumatic leakage test
6.15 Vacuum test
6.16 Pneumatic surge test
6.17 Thermal shock test
6.18 Light-radiation aging
6.19 Push-pull test
6.20 Fire test
Annex A (informative) Test fluids
Bibliography
Describes test methods for flexible polytetrafluoroethylene (PTFE) inner tubes with non-metallic 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.
Committee |
ACE/69
|
DevelopmentNote |
Supersedes 04/30115718 DC (10/2006) Reviewed and confirmed by BSI, January 2015. (12/2014)
|
DocumentType |
Standard
|
Pages |
30
|
PublisherName |
British Standards Institution
|
Status |
Current
|
Supersedes |
This part of ISO8829 specifies test methods for flexible polytetrafluoroethylene (PTFE) inner tubes with non-metallic 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 ISO6771.
This part of ISO8829 applies to the hose and the hose coupling. The tests and assembly requirements for the connecting end fittings are covered in the procurement specification.
This part of ISO8829 is applicable when reference is made to it in a procurement specification or other definition document.
NOTE Fluids used for the tests are listed in AnnexA.
Standards | Relationship |
ISO 8829-2:2006 | Identical |
MIL L 7808 : K (1) | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
BS 1595(1965) : LATEST | PROPAN-2-OL (ISOPROPYL ALCOHOL) FOR INDUSTRIAL USE |
NFM 15 006 : 1976 FD | LIQUID MINERAL FUELS - PROPERTIES OF WHITE SPIRIT |
ISO 2685:1998 | Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
ISO 6771:2007 | Aerospace — Fluid systems and components — Pressure and temperature classifications |
MIL T 5624 : R | TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
AIR 319660/A : 1966 | |
AIR 3407/B : 1972 | CARBURANT TYPE "LARGE COUPE" POUR TURBOMACHINES D'AVIATION |
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 |
TT-S-735 Revision A:1988 | STANDARD TEST FLUIDS, HYDROCARBON |
ISO 7258:1984 | Polytetrafluoroethylene (PTFE) tubing for aerospace applications Methods for the determination of the density and relative density |
TT-I-735 Revision A:1963 | ISOPROPYL ALCOHOL |
MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
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 |
MIL H 8446 : LATEST | HYDRAULIC FLUID, NONPETROLEUM BASE, AIRCRAFT |
ISO 6773:1994 | Aerospace Fluid systems Thermal shock testing of piping and fittings |
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