Publication: Magyar Közlöny
Issue: MK-2009-104 (Year: 2009, Number: 104)
Era: 2004-2010
Section: 
Paragraph Index: 1428

d) in the event of the critical power-unit failure being recognized at the LDP or at any point before the LDP, it is possible either to land and stop within the FATO or to overshoot, meeting the conditions of 4.1.2.1 and 4.1.2.2. Note.— For elevated heliports, the airworthiness code provides appropriate clearance from the elevated heliport edge. 4.2 Operations in performance Class 2 4.2.1 Take-off (Figures A-6 and A-7) The mass of the helicopter at take-off should not exceed the maximum take-off mass specified in the flight manual for the procedures to be used and to achieve a rate of climb of 150 ft/min at 300 m (1 000 ft) above the level of the heliport with the critical power-unit inoperative and the remaining power-units operating at an appropriate power rating, taking into account the parameters specified in 2.2. 4.2.2 Take-off flight path From DPATO or, as an alternative, no later than 60 m (200 ft) above the take-off surface with the critical power-unit inoperative, the conditions of 4.1.2.1 and 4.1.2.2 should be met. 4.2.3 En route The requirements of 4.1.3 should be met. 4.2.4 Approach, landing and balked landing (Figures A-8 and A-9) The estimated landing mass at the destination or alternate should be such that:

Source: https://magyarkozlony.hu/hivatalos-lapok/bfd0d67db9f223889f627fd618725b03526630e2/dokumentumok/d5234fd7275da04023366ab8a434989962a31bdf/letoltes