Résumé
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.
Informations générales
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État actuel: AnnuléeDate de publication: 1992-06Stade: Annulation de la Norme internationale [95.99]
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Edition: 1Nombre de pages: 15
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Comité technique :ISO/TC 20/SC 10
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Cycle de vie
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Actuellement
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Révisée par
PubliéeISO 10502:2012