Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 1928

e) not more than 50 per cent of the reported wind component opposite to the direction of take-off, and not less than 150 per cent of the reported wind component in the direction of take-off. In certain cases of operation of seaplanes, it has been found necessary to take account of the reported wind component normal to the direction of take-off. 3.4 Critical point In applying 3.2 the critical point chosen for establishing compliance with 3.2 a) is not nearer to the starting point than that used for establishing compliance with 3.2 b) and 3.2 c). 3.5 Turns In case the flight path includes a turn with bank greater than 15 degrees, the clearances specified in 3.2 c) are increased by an adequate amount during the turn, and the distance D is measured along the intended track. 4. En route 4.1 One power-unit inoperative 4.1.1 At all points along the route or planned diversion therefrom, the aeroplane is capable, at the minimum flight altitudes en route, of a steady rate of climb with one powerunit inoperative, as determined from the flight manual, of at least 1) K m/s, being expressed in km/h; 2) K m/s, being expressed in kt; 3) K ft/min, being expressed in kt; and K having the following value: K = 4.04 – in the case of 1) and 2); and K = 797 – in the case of 3) where N is the number of power-units installed. VS0 185.2 ------------      2 VS0 VS0 --------      2 VS0 VS0 --------      2 VS0 5.40 N --------- 1 060 N --------------- 2007/70/II. szám Annex 6 — Operation of Aircraft Part I 1/11/01 ATT C-4 It should be noted that minimum flight altitudes are usually considered to be not less than 300 m (1 000 ft) above terrain along and adjacent to the flight path. 4.1.2 As an alternative to 4.1.1 the aeroplane is operated at an all power-unit operating altitude such that, in the event of a power-unit failure, it is possible to continue the flight to an aerodrome where a landing can be made in accordance with 5.3, the flight path clearing all terrain and obstructions along the route within 8 km (4.3 NM) on either side of the intended track by at least 600 m (2 000 ft). In addition, if such a procedure is utilized, the following provisions are complied with:

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