Applies primarily to civil and transport aircraft and specifies the test requirements and various test procedures for aerospace equipment which could be subjected to moisture ingress, frosting and condensation, resulting from the passage through atmospheric conditions of high humidity, in combination with or induced by changing temperature and pressure.
Document identifier
ISO 9662:1994
Title
Aircraft equipment - Environmental and operating conditions for airborne equipment - Humidity, temperature and pressure tests
ISO Category
TC 20: Aircraft and space vehicles
Publication date
1994-02-01
International Relationship
BS G 259:1996
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