Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 1986

c) the distance D is measured along the intended track. 3. En route 3.1 All power-units operating At each point along the route and planned diversion therefrom, the all power-units operating performance ceiling appropriate to the aeroplane mass at that point, taking into account the amount of fuel and oil expected to be consumed, is not less than the minimum altitude (see Chapter 4, 4.2.6) or, if greater, the planned altitude which it is intended to maintain with all power-units operating, in order to ensure compliance with 3.2 and 3.3. 3.2 One power-unit inoperative From each point along the route and planned diversions therefrom, it is possible in the event of one power-unit becoming inoperative to continue the flight to an en-route alternate aerodrome where a landing can be made in accordance with 4.2 and, on arrival at the aerodrome, the net gradient of climb is not less than zero at a height of 450 m (1 500 ft) above the elevation of the aerodrome. 3.3 Two power-units inoperative (applicable only to aeroplanes with four power-units) For each point along the route or planned diversions therefrom, at which the aeroplane is more than 90 minutes’ flying time at all power-units operating cruising speed from an en-route alternate aerodrome, the two power-units inoperative net flight path is such that a height of at least 300 m (1 000 ft) above terrain can be maintained until arrival at such an aerodrome. Note.— The net flight path is that attainable from the expected gradient of climb or descent diminished by 0.2 per cent. 3.4 Conditions The ability to comply with 3.1, 3.2 and 3.3 is assessed:

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