CAT.POL.A.415 En-route - OEI

• Regulation (EU) 2023/217 found in: Air Operations (965/2012) Part-ARO Part-ORO Part-CAT Part-SPA Part-NCC Part-NCO Part-SPO (Sep 2023)

CAT.POL.A.415 En-route – OEI Regulation (EU) 2023/217 (a) In the meteorological conditions expected for the flight, in the event of any one engine becoming inoperative at any point on its route or on any planned diversion therefrom and with the other engine(s) operating within the maximum continuous power conditions specified, the aeroplane shall be capable of continuing the flight from the cruising altitude to an aerodrome where a landing can be made in accordance with [CAT.POL.A.430](#_DxCrossRefBm318086299) or [CAT.POL.A.435](#_DxCrossRefBm318086298), as appropriate. The aeroplane shall clear obstacles within 9,3 km (5 NM) either side of the intended track by a vertical interval of at least: (1) 1 000 ft, when the rate of climb is zero or greater; or (2) 2 000 ft, when the rate of climb is less than zero. (b) The flight path shall have a positive slope at an altitude of 450 m (1 500 ft) above the aerodrome where the landing is assumed to be made after the failure of one engine. (c) The available rate of climb of the aeroplane shall be taken to be 150 ft per minute less than the gross rate of climb specified. (d) The width margins provided for in point (a) shall be increased to 18,5 km (10 NM) if the navigational accuracy does not meet at least navigation specification RNAV 5. (e) Fuel jettisoning is permitted to an extent consistent with reaching the aerodrome where the aeroplane is assumed to land after engine failure with the required fuel reserves in accordance with point [CAT.OP.MPA.181](#_DxCrossRefBm318085139), appropriate for an alternate aerodrome, if a safe procedure is used. CAT.POL.A.415 En-route – OEI Regulation (EU) 2023/217 (a) In the meteorological conditions expected for the flight, in the event of any one engine becoming inoperative at any point on its route or on any planned diversion therefrom and with the other engine(s) operating within the maximum continuous power conditions specified, the aeroplane shall be capable of continuing the flight from the cruising altitude to an aerodrome where a landing can be made in accordance with [CAT.POL.A.430](#_DxCrossRefBm927678679) or [CAT.POL.A.435](#_DxCrossRefBm927678678), as appropriate. The aeroplane shall clear obstacles within 9,3 km (5 NM) either side of the intended track by a vertical interval of at least: (1) 1 000 ft, when the rate of climb is zero or greater; or (2) 2 000 ft, when the rate of climb is less than zero. (b) The flight path shall have a positive slope at an altitude of 450 m (1 500 ft) above the aerodrome where the landing is assumed to be made after the failure of one engine. (c) The available rate of climb of the aeroplane shall be taken to be 150 ft per minute less than the gross rate of climb specified. (d) The width margins provided for in point (a) shall be increased to 18,5 km (10 NM) if the navigational accuracy does not meet at least navigation specification RNAV 5. (e) Fuel jettisoning is permitted to an extent consistent with reaching the aerodrome where the aeroplane is assumed to land after engine failure with the required fuel reserves in accordance with point [CAT.OP.MPA.181](#_DxCrossRefBm927677501), appropriate for an alternate aerodrome, if a safe procedure is used. #### CAT.POL.A.415 En-route – OEI *Regulation (EU) 2023/217* (a) In the meteorological conditions expected for the flight, in the event of any one engine becoming inoperative at any point on its route or on any planned diversion therefrom and with the other engine(s) operating within the maximum continuous power conditions specified, the aeroplane shall be capable of continuing the flight from the cruising altitude to an aerodrome where a landing can be made in accordance with [CAT.POL.A.430](#_DxCrossRefBm523088235) or [CAT.POL.A.435](#_DxCrossRefBm523088234), as appropriate. The aeroplane shall clear obstacles within 9,3 km (5 NM) either side of the intended track by a vertical interval of at least: (1) 1 000 ft, when the rate of climb is zero or greater; or (2) 2 000 ft, when the rate of climb is less than zero. (b) The flight path shall have a positive slope at an altitude of 450 m (1 500 ft) above the aerodrome where the landing is assumed to be made after the failure of one engine. (c) The available rate of climb of the aeroplane shall be taken to be 150 ft per minute less than the gross rate of climb specified. (d) The width margins provided for in point (a) shall be increased to 18,5 km (10 NM) if the navigational accuracy does not meet at least navigation specification RNAV 5. (e) Fuel jettisoning is permitted to an extent consistent with reaching the aerodrome where the aeroplane is assumed to land after engine failure with the required fuel reserves in accordance with point [CAT.OP.MPA.181](#_DxCrossRefBm523087007), appropriate for an alternate aerodrome, if a safe procedure is used.