SAE MA2078B
Current
The latest, up-to-date edition.
Test Methods, Hose Assemblies, Polytetrafluoroethylene (PTFE), Metric
Hardcopy , PDF
English
24-04-2009
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1 SCOPE AND FIELD OF APPLICATION
2 REFERENCES
3 TEST ON PTFE INNER TUBES
4 HOSE AND HOSE ASSEMBLY TESTS
APPENDIX A TEST FLUIDS AND MATERIALS
Defines the test methods for flexible PTFE hose and hose assemblies used in aircraft fluid systems in the pressure and temperature ranges defined in MA2001.
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
SAE International
|
| Status |
Current
|
| SupersededBy | |
| Supersedes |
This SAE Aerospace Standard describes the test methods for flexible PTFE hose and hose assemblies used in aircraft fluid systems in the pressure and temperature ranges defined in MA2001 (ISO 6771). It applies to the hose and the hose coupling. The tests and assembly requirements for the connecting end fitting are covered in the procurement specifiction. The document applies each time that it is referred to in a procurement specification or other definition document.
| Standards | Relationship |
| ISO 8829:1990 | Identical |
| SAE MA2126B | Hose Assembly, Polytetrafluoroethylene (PTFE), up to 232 °C and 10 500 kPa Procurement Specification, Metric (ISO/DIS 10502) |
| SAE MA4098 | Hose Assembly, Polytetrafluoroethylene, Heavy Duty, Metallic Reinforced, 204 °C, 35 000 kPa Hydraulic and Pneumatic, Metric |
| SAE MA1339 | Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 21,000 kPa, 204 °C, Lightweight, Hydraulic and Pneumatic, Metric |
| SAE MA1975 | Hose Assemblies, Polytetrafluoroethylene, Aramid Reinforced, 135 °C, Standard Duty, 28 000/21 000 kPa, Hydraulic, Aircraft Systems |
| SAE MA620 | Hose Assemblies, Convoluted Polytetrafluoroethylene Metallic Reinforced, High Temperature, Medium Pressure, Aircraft Metric |
| SAE MA614A | Hose Assembly, Polytetrafluoroethylene (PTFE), Metallic Reinforced, 28,000 kPa, 204 °C, Hydraulic, Metric |
| SAE MA4623 | Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced Heavy-Duty, 21 000 kPa, 135 °C, Aircraft Hydraulic Systems, Metric |
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