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operating minima approved for the operation.
4.7.4 Recommendation.- The State of the Operator of
an aeroplane type with two turbine power-units which, prior to
25 March 1986 was authorized and operating on a route where
theflight time at single-engine cruise speed to an adequate enroute
alternate aerodmme exceeded the threshold time
established for such operations in accordance with 4.7.1
should give consideration to permitting such an operation to
continue on that mute after that date.
4.8 Carry-on baggage
The operator shall ensure that all baggage carried onto an
aeroplane and taken into the passenger cabin is adequately and
securely stowed.
CHAPTER 5. AEROPLANE PERFORMANCE
OPERATING LIMITATIONS
5.1 General
5.1.1 Aeroplanes shall be operated in accordance with a
comprehensive and detailed code of performance established
by the State of Registry in compliance with the applicable
Standards of this chapter.
5.1.2 Single-engined aeroplanes shall only be operated in
conditions of weather and light, and over such routes and
diversions therefrom, that permit a safe forced landing to be
executed in the event of engine failure.
5.1.3 Recommendation.- For aeroplanes for which
Parts IIIA and lllB of Annex 8 is not applicable because of the
exemption provided for in Article 41 of the Convention, the
State of Registry should ensure that the level of performance
specijied in 5.2 should be met as far as practicable.
5.2 Applicable to aeroplanes certificated
in accordance with Parts IIIA and IIIB of Annex 8
5.2.1 The Standards contained in 5.2.2 to 5.2.1 1 inclusive
are applicable to the aeroplanes to which Parts IIIA and IIIB
of Annex 8 is applicable.
Note.- The following Standards do not include quantitative
specijications comparable to those found in national
airworthiness codes. In accordance with 5.1.1, they are to be
supplemented by national requirements prepared by Contracting
States.
5.2.2 The level of performance defined by the appropriate
parts of the comprehensive and detailed national code referred
to in 5.1.1 for the aeroplanes designated in 5.2.1 shall be at
least substantially equivalent to the overall level embodied in
the Standards of this chapter.
Note.- Attachment C contains guidance material which
indicates by examples the level of performance intended by the
Standards and Recommended Practices of this chapter.
5.2.3 An aeroplane shall be operated in compliance with
the terms of its certificate of airworthiness and within the
approved operating limitations contained in its flight manual.
5.2.4 The State of Registry shall take such precautions as
are reasonably possible to ensure 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.
5.2.5 A flight shall not be commenced unless the
performance information provided in the flight manual
indicates that the Standards of 5.2.6 to 5.2.1 1 can be complied
with for the flight to be undertaken.
5.2.6 In applying the Standards of this chapter, account
shall be taken of all factors that significantly affect the
performance of the aeroplane (such as: mass, operating
procedures, the pressure-altitude appropriate to the elevation of
the aerodrome, temperature, wind, runway gradient and
condition of runway, i.e. presence of slush, water andfor ice,
for landplanes, water surface condition for seaplanes). 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 aeroplane is being operated.
5.2.7 Mass limitations
a) The mass of the aeroplane at the start of take-off shall
not exceed the mass at which 5.2.8 is complied with, nor
the mass at which 5.2.9, 5.2.10 and 5.2.11 are complied
with, allowing for expected reductions in mass as the
flight proceeds, and for such fuel jettisoning as is
envisaged in applying 5.2.9 and 5.2.10 and, in respect of
alternate aerodromes, 5.2.7 c) and 5.2.1 1.
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 appropriate to the
elevation of the aerodrome, 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 aerodrome of intended landing and at
　
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