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conditions at those aerodromes will be at or above the
aerodrome 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, prwr to
25 March 1986 was authorized and operating on a route
where the flight time at single-engine cruise speed to an
adequate en-route alternate aerodrome 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 route 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.
4.9 Additional requirements for
single pilot operations under the
Instrument Flight Rules (IFR) or at night
4.9.1 An aeroplane shall not be operated under the JFR or
at night by a single pilot unless approved by the State of the
Operator.
4.9.2 An aeroplane shall not be operated under the JFR or
at night by a single pilot unless:
a) the flight manual does not require a fight crew of more
than one;
b) the aeroplane is propeller-driven;
c) the maximum approved passenger seating configuration
is not more than nine;
d) the maximum certificated take-off mass does not exceed
5 700 kg;
e) the aeroplane is equipped as described in 6.22; and
f) the pilot-in-command has satisfied requirements of
experience, training, checking and recency described
in 9.4.5.
241 1105
No. 29
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.
5.12 Except as provided in 5.4, single-engine 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 llIA and ZllB 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
specijled 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
52.1 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 are applicable.
Note.- The following Standards do not include quuntitative
specifications comparable to those &und in ~ t i o n a l
airworthiness codes. In accordance with 5.1.1, they are to be
supplemented by M ~ ~ O Mre[q uirements prepared by Contracting
states.
5.2.2 The level of perforrnance 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 guidnnce 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 infonnation provided in the flight manual
indicates that the Standards of 5.2.6 to 5.2.11 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 and/or 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
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