Aerospace. List of equivalent terms - Environmental and operating conditions for aircraft equipment Ingestion-build-54371 This standard may also apply

This standard may also apply to metallic materials for test durations exceeding 10 000 h and/or for test temperatures exceeding 1 100 °C providing that previous agreement has been reached between the manufacturer and the purchaser

Part 6: Tests for local effects after implantation

ISO 6508-1 has been developed with a laboratory temperature requirement of 10 °C to 35 °C

as part of the Thermal Joining Process Specification

Even if methods described in this document might be applicable for feasibility and safety issues the scope of this document is design for comfort

Aerospace. List of equivalent terms - Environmental and operating conditions for aircraft equipment Ingestion-build-54371 This standard may also apply