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accordance with Part IV of Annex 8
3.2.1 The Standards contained in 3.2.2 to 3.2.7 inclusive
are applicable to the helicopters to which Part IV of Annex 8
is applicable.
Note.- The following Standards do not irxclude quantitative
specifications compamble to those found in national
ainvortlziness codes. In accordance with 3.1.1, they are to be
supplemented by national requiremerzts prepared by
Contracting States.
3.2.2 The level of perfomlance defined by the appropriate
parts of the cornprehcnsive and detailed national code referred
to jn 3.1.1 for the helicoptcrs designated in 3.2.1 shall be at
least substantially equivalent to. the overall level embodied in
the Standards of this chapter.
Note.- Artachment A conrains guidance materia/ which
indicates, by an example, the level of performance intended by
the Standards arid Reconzmended Practices of this chapter:
3.2.3 A helicopter shall bc operated in compliance with
the terms of its certihcatc of airwortl~iness and within
the approved operating limitations contained in its flight
manual.
3.2.4 The State of Registry shall take such precautions as
are reasonably possible to ensurc that the general level of
safety contemplated by these provisions is maintained under
all expected operating conditions, including those not covered
specifically by the provisions of this chapter.
3.2.5 A flight shall not be commenced unless the
performance information provided in the flight manual
indicates that the Standards ol' 3.2.6 and 3.2.7 can be complied
with for the flight to be undertaken.
3.2.6 In applying the Standards of this chapter, account
shall be taken of all factors that significantly affect the
performance of the helicopter (such as: mass, operating
procedures, the pressure-altitude appropriate to the elevation of
the operating site, temperature, wind and condition of the
surface). Such factors shall be taken into account directly as
operational parameters or indirectly by means of allowances or
margins, which may be provided in the scheduling of
performance data or in the comprehensive and detailed code of
performance in accordance with which the helicopter is being
operated.
3.2.7 Mass limitations
a) The mass of the helicopter at the start of take-off shall
not exceed the mass at which 3.2.7.1 is complied with,
nor the mass at which 3.2.7.2 and 3.2.7.3 are complied
with, allowing for expected reductions in mass as the
flight proceeds, and for such fuel jettisoning as is
envisaged in applying 3.2.7.2 and in respect of alternates
3.2.7 c) and 3.2.7.3.
b) In no case shall the mass at the start of take-off exceed
the maximum take-off mass specified in the flight
manual for the pressure-altitude and temperature
appropriate to the elevation of the operating site, and, if
used as a parameter to determine the maximum take-off
mass, any other local atmospheric condition.
c) In no case shall the estimated mass for the expected
time of landing at the destination and at any alternate,
exceed the maximum landing mass specified in
thc llight manual for the pressure-altitude and
temperature appropriate lo the elevation of those
operating sites, and, if used as a parameter to
ANNEX 6 - PART I11 11-3-1 1/11/01
Annex 6 - Operatiofz of Airera3 Part III
determine the maximum landing mass, any other local
atmospheric condition.
d) In no case shall the mass at the start of take-off, or at
the expected time of landing at the destination and at
any alternate, exceed the relevant maximum mass at
which compliance has been demonstrated with the
applicable noise certification Standards in Annex 16,
Volume I. unless otherwise authorized in exceptional
circumstances for a certain operating site where there is
no noise disturbance problem, by the ' competent
authorily of the State in which the operating site is
situated.
3.2.7.1 Take-off and initial climb phase
3.2.7.1.1 For pe$orrnance Class I helicopters. The helicopter
shall be ahle, in the event of the critical power-unit
failing at or before the take-off decision point, to discontinue
the take-off and stop within the rejected take-off area
available, or, in the event of the failure occurring at or past the
take-off decision point, to continue the take-off and then
climb, clearing all obstacles along the flight path by an
adequate margin until the helicopter is in a position to comply
with 3.2.7.2.1.
3.2.7. I .2 For pedorrnance Class 2 helicopters. The helicopter
shall. be ahle, with all engines operating, to clear all
obstacles along its flight path by an adequate margin until it is
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