Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 1910

d) Landing distance available (LDA). The length of runway which is declared available and suitable for the ground run of an aeroplane landing. Note.— The calculation of declared distances is described in Annex 14, Volume I, Attachment A. Height. The vertical distance of a level, a point, or an object considered as a point, measured from a specified datum. Note.— For the purposes of this example, the point referred to above is the lowest part of the aeroplane and the specified datum is the take-off or landing surface, whichever is applicable. Landing surface. That part of the surface of an aerodrome which the aerodrome authority has declared available for the normal ground or water run of aircraft landing in a particular direction. Take-off surface. That part of the surface of an aerodrome which the aerodrome authority has declared available for the normal ground or water run of aircraft taking off in a particular direction. VS0. A stalling speed or minimum steady flight speed in the landing configuration. (Note.— See 2.4.) VS1. A stalling speed or minimum steady flight speed. (Note.— See 2.5.) 2007/70/II. szám Annex 6 — Operation of Aircraft Part I 1/11/01 ATT C-2 Note.— See Chapter 1 and Annexes 8 and 14, Volume I, for other definitions. 2. Stalling speed — minimum steady flight speed 2.1 For the purpose of this example, the stalling speed is the speed at which an angle of attack greater than that of maximum lift is reached, or, if greater, the speed at which a large amplitude pitching or rolling motion, not immediately controllable, is encountered, when the manoeuvre described in 2.3 is executed. Note.— It should be noted that an uncontrollable pitching motion of small amplitude associated with pre-stall buffeting does not necessarily indicate that the stalling speed has been reached. 2.2 The minimum steady flight speed is that obtained while maintaining the elevator control in the most rearward possible position when the manoeuvre described in 2.3 is executed. This speed would not apply when the stalling speed defined in 2.1 occurs before the elevator control reaches its stops. 2.3 Determination of stalling speed — Minimum steady flight speed 2.3.1 The aeroplane is trimmed for a speed of approximately 1.4VS1 . From a value sufficiently above the stalling speed to ensure that a steady rate of decrease is obtainable, the speed is reduced in straight flight at a rate not exceeding 0.5 m/s2 (1 kt/s) until the stalling speed or the minimum steady flight speed, defined in 2.1 and 2.2, is reached. 2.3.2 For the purpose of measuring stalling speed and minimum steady flight speed, the instrumentation is such that the probable error of measurement is known. 2.4 VS0 VS0 denotes the stalling speed if obtained in flight tests conducted in accordance with 2.3, or the minimum steady flight speed, CAS, as defined in 2.2, with:

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