Covers Class I fitting assemblies of corrosion-resistant steel or titanium parts (- 55 °C to + 232 °C) and Class II fitting assemblies of corrosion-resistant steel and aluminium parts, DN 12 and larger (- 55 °C to + 135 °C) for use in aircraft hydraulic, fuel and lubricating oil systems and in aerospace pneumatic systems where some gaseous diffusion through the wall may be tolerated. Annex A gives equivalent materials and components for information only.
Status: WithdrawnPublication date: 1992-06
Edition: 1Number of pages: 14
Technical Committee: ISO/TC 20/SC 10 Aerospace fluid systems and components
ISO 10502:1992Stage: 95.99
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