anx_II__cpt_1__cpt_1__cpt_2__cpt_4
Text with EEA relevance.
1.2.4. The effects of cyclic loading, environmental and operational degradation and likely subsequent part failures must not reduce the integrity of the propulsion system below acceptable levels. All necessary instructions for ensuring continued airworthiness in this regard must be promulgated.
← anx_II__cpt_1__cpt_1__cpt_2__cpt_3__text_2 · All articles · anx_II__cpt_1__cpt_1__cpt_2__cpt_4__text_1 →
Source: EUR-Lex (Cellar) · retrieved 2026-10-12 · Text as adopted (Official Journal); later amendments are not incorporated in this text.