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include the particular airfrarndengine combinations, including
the current type design standard for such operations, the
specific aeroplanes approved, and the areas or routes of such
operations.
5.2 The operator's maintenance control manual should
include a statement of certification of the additional equipment
required, and of the maintenance and reliability programme for
such equipment, including the engine.
6. Route limitations over water
6.1 Operators of single-engine turbine-powered aeroplanes
carrying out operations at night and/or in IMC should
make an assessment of route limitations over water. The distance
that the aeroplane may be operated from a land mass
suitable for a safe forced landing should be determined. This
equates to the ghde distance from the cruise altitude to the safe
forced landing area following engine failure, assuming still air
conditions. States may add to this an additional distance taking
into account the likely prevailing conditions and type of operation.
This should take into account the likely sea conditions,
the survival equipment carried, the achieved engine reliability
and the search and rescue services available.
6.2 Any additional distance allowed beyond the glide
distance should not exceed a distance equivalent to 15 minutes
at the aeroplane's normal cruise speed.
- END -
2411 1705
No. 29
ATT 1-2
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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