Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 2583

b) it is possible to continue the flight if the critical powerunit failure occurs at or after the TDP. In this case, the flight path of the helicopter may descend below the height of the FATO in order to achieve VTOSS if the following conditions are satisfied: 1) A clearance margin is established in relation to the elevated heliport or helideck itself and to all obstacles located on the elevated heliport or helideck. 4.5 m (15 ft) has been found appropriate to a wide range of helicopters. 2) The vertical clearance above all obstacles not located on the elevated heliport or helideck is at least equal to 10.7 m (35 ft). An obstacle is considered if its distance from the flight path does not exceed 30 m or 1.5 times the maximum dimension of the helicopter, whichever is greater. 4.1.2 Initial climb 4.1.2.1 The take-off mass is such that the climb path provides a vertical clearance of not less than 10.7 m (35 ft) for VFR operations and 10.7 m (35 ft) + 0.01 DR for IFR operations above all obstacles located in the climb path, the critical power-unit failure occurring at the TDP. 4.1.2.2 An obstacle is considered if its lateral distance from the nearest point on the surface below the intended flight path does not exceed 30 m or 1.5 times the over-all length of the helicopter, whichever is greater, plus: 2007/70/II. szám Attachment A Annex 6 — Operation of Aircraft ATT A-3 1/11/01 0.10 DR for VFR day operations 0.15 DR for VFR night operations 0.30 DR for IFR operations without electronic guidance 0.15 DR for IFR operations with electronic guidance 0.10 DR for IFR operations with ILS or MLS guidance except obstacles may be disregarded if they are situated beyond:

Source: https://magyarkozlony.hu/hivatalos-lapok/4c6310a937d14bac566ee9c9d944896656c292dd/dokumentumok/5a6ac3c6db12e692ae41096677ad5f072d2cc9f3/letoltes