Article 3 Continuing airworthiness requirements

• Regulation (EU) 2021/700 found in: Continuing Airworthiness (1321/2014) Part-M Part-145 Part-66 Part-147 Part-T Part-ML Part-CAMO Part-CAO (Jul 2024)

Article 3 Continuing airworthiness requirements Regulation (EU) 2021/700 1. The continuing airworthiness of aircraft referred to in point (a) of Article 1 and components for installation thereon shall be ensured in accordance with the requirements of Annex I (Part-M), except for aircraft listed in the first subparagraph of paragraph 2 to which the requirements of Annex Vb (Part-ML) shall apply. 2. The requirements of Annex Vb (Part-ML) shall apply to the following other than complex motor-powered aircraft: (a) aeroplanes of 2 730 kg maximum take-off mass or less; (b) rotorcraft of 1 200 kg maximum take-off mass or less, certified for a maximum of up to 4 occupants; (c) other ELA2 aircraft. Where aircraft referred to points (a), (b) and (c) of the first subparagraph is listed in the air operator certificate of an air carrier licensed in accordance with Regulation (EC) No 1008/2008, the requirements of Annex I (Part-M) shall apply. 3. In order to be listed in the air operator certificate of an air carrier licensed in accordance with Regulation (EC) No 1008/2008, aircraft referred to in points (a), (b) and (c) of the first subparagraph of paragraph 2 shall comply with all of the following requirements: (a) its aircraft maintenance programme has been approved by the competent authority in accordance with point [M.A.302](#_DxCrossRefBm1518544873) of Annex I (Part-M); (b) due maintenance required by the maintenance programme referred to in point (a) has been performed and certified in accordance with point [145.A.48](#_DxCrossRefBm1518544879) and [145.A.50](#_DxCrossRefBm1518544878) of Annex II (Part-145); (c) an airworthiness review has been performed and a new airworthiness review certificate has been issued in accordance with point [M.A.901](#_DxCrossRefBm1518544877) of Annex I (Part-M). 4. By way of derogation from paragraph 1 of this Article, the continuing airworthiness of aircraft referred to in point (a) of Article 1, for which a permit to fly has been issued, shall be ensured on the basis of the specific continuing airworthiness arrangements defined in the permit to fly issued in accordance with Annex I (Part-21) to Commission Regulation (EU) No 748/2012[[13]](#_ftn13). 5. Aircraft maintenance programmes for aircraft referred to in point (a) of Article 1 that comply with the requirements specified in point [M.A.302](#_DxCrossRefBm1518544873) of Annex I (Part-M) applicable before 24 March 2020 shall be deemed to comply with the requirements specified in point [M.A.302](#_DxCrossRefBm1518544873) of Annex I (Part-M) or point [ML.A.302](#_DxCrossRefBm1518544876) of Annex Vb (Part-ML), as applicable, in accordance with paragraphs 1 and 2. 6. Operators shall ensure the continuing airworthiness of aircraft referred to in point (b) of Article 1 and components for installation thereon in accordance with the requirements of Annex Va (Part-T). 7. The continuing airworthiness of aeroplanes with a maximum certificated take-off mass at or below 5 700 kg which are equipped with multiple turboprop engines shall be ensured in accordance with the requirements applicable to other than complex motor-powered aircraft as set out in points [M.A.201](#_DxCrossRefBm1518544875), [M.A.301](#_DxCrossRefBm1518544874), [M.A.302](#_DxCrossRefBm1518544873), [M.A.601](#_DxCrossRefBm1518544872) and [M.A.803](#_DxCrossRefBm1518544871) of Annex I (Part-M), point [145.A.30](#_DxCrossRefBm1518544859) of Annex II (Part-145), points [66.A.5](#_DxCrossRefBm1518544870), [66.A.30](#_DxCrossRefBm1518544869), [66.A.70](#_DxCrossRefBm1518544868), Appendix V and VI of Annex III (Part-66), point [CAMO.A.315](#_DxCrossRefBm1518544867) of Annex Vc (Part-CAMO), point [CAO.A.010](#_DxCrossRefBm1518544866) and Appendix I of Annex Vd (Part-CAO) to the extent that they apply to other than complex motor-powered aircraft. --- [[13]](#_ftnref13) Commission Regulation (EU) No 748/2012 of 3 August 2012 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations (OJ L 224, 21.8.2012, p. 1) ## Article 3 Continuing airworthiness requirements *Regulation (EU) 2021/700* 1. The continuing airworthiness of aircraft referred to in point (a) of Article 1 and components for installation thereon shall be ensured in accordance with the requirements of Annex I (Part-M), except for aircraft listed in the first subparagraph of paragraph 2 to which the requirements of Annex Vb (Part-ML) shall apply. 2. The requirements of Annex Vb (Part-ML) shall apply to the following other than complex motor-powered aircraft: (a) aeroplanes of 2 730 kg maximum take-off mass or less; (b) rotorcraft of 1 200 kg maximum take-off mass or less, certified for a maximum of up to 4 occupants; (c) other ELA2 aircraft. Where aircraft referred to points (a), (b) and (c) of the first subparagraph is listed in the air operator certificate of an air carrier licensed in accordance with Regulation (EC) No 1008/2008, the requirements of Annex I (Part-M) shall apply. 3. In order to be listed in the air operator certificate of an air carrier licensed in accordance with Regulation (EC) No 1008/2008, aircraft referred to in points (a), (b) and (c) of the first subparagraph of paragraph 2 shall comply with all of the following requirements: (a) its aircraft maintenance programme has been approved by the competent authority in accordance with point [M.A.302](#_DxCrossRefBm1203439760) of Annex I (Part-M); (b) due maintenance required by the maintenance programme referred to in point (a) has been performed and certified in accordance with point [145.A.48](#_DxCrossRefBm1203439766) and [145.A.50](#_DxCrossRefBm1203439765) of Annex II (Part-145); (c) an airworthiness review has been performed and a new airworthiness review certificate has been issued in accordance with point [M.A.901](#_DxCrossRefBm1203439764) of Annex I (Part-M). 4. By way of derogation from paragraph 1 of this Article, the continuing airworthiness of aircraft referred to in point (a) of Article 1, for which a permit to fly has been issued, shall be ensured on the basis of the specific continuing airworthiness arrangements defined in the permit to fly issued in accordance with Annex I (Part-21) to Commission Regulation (EU) No 748/2012[[13]](#_ftn13). 5. Aircraft maintenance programmes for aircraft referred to in point (a) of Article 1 that comply with the requirements specified in point [M.A.302](#_DxCrossRefBm1203439760) of Annex I (Part-M) applicable before 24 March 2020 shall be deemed to comply with the requirements specified in point [M.A.302](#_DxCrossRefBm1203439760) of Annex I (Part-M) or point [ML.A.302](#_DxCrossRefBm1203439763) of Annex Vb (Part-ML), as applicable, in accordance with paragraphs 1 and 2. 6. Operators shall ensure the continuing airworthiness of aircraft referred to in point (b) of Article 1 and components for installation thereon in accordance with the requirements of Annex Va (Part-T). 7. The continuing airworthiness of aeroplanes with a maximum certificated take-off mass at or below 5 700 kg which are equipped with multiple turboprop engines shall be ensured in accordance with the requirements applicable to other than complex motor-powered aircraft as set out in points [M.A.201](#_DxCrossRefBm1203439762), [M.A.301](#_DxCrossRefBm1203439761), [M.A.302](#_DxCrossRefBm1203439760), [M.A.601](#_DxCrossRefBm1203439759) and [M.A.803](#_DxCrossRefBm1203439758) of Annex I (Part-M), point [145.A.30](#_DxCrossRefBm1203439746) of Annex II (Part-145), points [66.A.5](#_DxCrossRefBm1203439757), [66.A.30](#_DxCrossRefBm1203439756), [66.A.70](#_DxCrossRefBm1203439755), Appendix V and VI of Annex III (Part-66), point [CAMO.A.315](#_DxCrossRefBm1203439754) of Annex Vc (Part-CAMO), point [CAO.A.010](#_DxCrossRefBm1203439753) and Appendix I of Annex Vd (Part-CAO) to the extent that they apply to other than complex motor-powered aircraft. --- [[13]](#_ftnref13) Commission Regulation (EU) No 748/2012 of 3 August 2012 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations (OJ L 224, 21.8.2012, p. 1)