Resumen
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.
Informaciones generales
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Estado: RetiradaFecha de publicación: 1992-06Etapa: Retirada de la Norma Internacional [95.99]
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Edición: 1Número de páginas: 14
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Comité Técnico :ISO/TC 20/SC 10
- RSS actualizaciones
Ciclo de vida
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Ahora
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Revisada por
PublicadoISO 10502:2012