M.A.301 Continuing airworthiness tasks

• Regulation (EU) 2019/1383 found in: Continuing Airworthiness (1321/2014) Part-M Part-145 Part-66 Part-147 Part-T Part-ML Part-CAMO Part-CAO (Jul 2024)

M.A.301 Continuing airworthiness tasks Regulation (EU) 2019/1383 The aircraft continuing airworthiness and the serviceability of operational and emergency equipment shall be ensured by: (a) the accomplishment of pre-flight inspections; (b) the rectification of any defect and damage affecting safe operation in accordance with data specified in points [M.A.304](#_DxCrossRefBm1518544953) and [M.A.401](#_DxCrossRefBm1518544954), as applicable, while taking into account the minimum equipment list (‘MEL’) and configuration deviation list, when they exist; (c) the accomplishment of all maintenance in accordance with the AMP referred to in point [M.A.302](#_DxCrossRefBm1518544873); (d) the release of all maintenance in accordance with Subpart H; (e) for all complex motor-powered aircraft or aircraft used by air carriers licensed in accordance with Regulation (EC) No 1008/2008, the analysis of the effectiveness of the approved AMP referred to in point [M.A.302](#_DxCrossRefBm1518544873); (f) the accomplishment of any applicable: (1) airworthiness directive (AD); (2) operational directive with a continuing airworthiness impact; (3) continuing airworthiness requirement established by the Agency; (4) measures required by the competent authority in immediate reaction to a safety problem; (g) the accomplishment of modifications and repairs in accordance with point [M.A.304](#_DxCrossRefBm1518544953); (h) delivering to the pilot-in-command, or to the operator in the case of air carriers licensed in accordance with Regulation (EC) No 1008/2008, the mass and balance statement reflecting the current configuration of the aircraft; (i) maintenance check flights, when necessary. #### M.A.301 Continuing airworthiness tasks *Regulation (EU) 2019/1383* The aircraft continuing airworthiness and the serviceability of operational and emergency equipment shall be ensured by: (a) the accomplishment of pre-flight inspections; (b) the rectification of any defect and damage affecting safe operation in accordance with data specified in points [M.A.304](#_DxCrossRefBm1203439840) and [M.A.401](#_DxCrossRefBm1203439841), as applicable, while taking into account the minimum equipment list (‘MEL’) and configuration deviation list, when they exist; (c) the accomplishment of all maintenance in accordance with the AMP referred to in point [M.A.302](#_DxCrossRefBm1203439760); (d) the release of all maintenance in accordance with Subpart H; (e) for all complex motor-powered aircraft or aircraft used by air carriers licensed in accordance with Regulation (EC) No 1008/2008, the analysis of the effectiveness of the approved AMP referred to in point [M.A.302](#_DxCrossRefBm1203439760); (f) the accomplishment of any applicable: (1) airworthiness directive (AD); (2) operational directive with a continuing airworthiness impact; (3) continuing airworthiness requirement established by the Agency; (4) measures required by the competent authority in immediate reaction to a safety problem; (g) the accomplishment of modifications and repairs in accordance with point [M.A.304](#_DxCrossRefBm1203439840); (h) delivering to the pilot-in-command, or to the operator in the case of air carriers licensed in accordance with Regulation (EC) No 1008/2008, the mass and balance statement reflecting the current configuration of the aircraft; (i) maintenance check flights, when necessary.