Abstract
ISO 14621-2:2003 establishes technical guidelines for developing and documenting an electrical, electronic and electromechanical (EEE) parts control program, in order to assure that the parts used in the flight hardware are acceptable and possess adequate functional, radiation and reliability characteristics to meet the system requirements. These guidelines are tailorable to the needs of each individual programme based on the project performance criteria, risk tolerance, budget, mission duration, environment, schedule and other considerations. ISO 14621-2:2003 is applicable to all customers and suppliers furnishing flight hardware and is suitable for reference in proposal instructions.
General information
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Status: WithdrawnPublication date: 2003-07Stage: Withdrawal of International Standard [95.99]
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Edition: 1Number of pages: 6
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Technical Committee :ISO/TC 20/SC 14ICS :49.140
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Life cycle
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Now
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Revised by
PublishedISO 14621-2:2019
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