ICAO Annex 8
Chapter 4 - Continuing Airworthiness
4.2.1 State of Design
4.2.1.1 The State of Design of an aircraft shall:
c) ensure that, in respect of aeroplanes over 5700 kg maximum certificated take-off mass, there exists a continuing structural integrity programme to ensure the airworthiness of the aeroplane. The programme shall include specific information concerning corrosion prevention and control.
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