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testing.
B.1.2 Compliance with each Standard shall be established
for all applicable combinations of aeroplane mass and centre
of gravity position, within the range of loading conditions for
which certification is sought.
B.1.3 Where necessary, appropriate aeroplane configurations
shall be established for the determination of performance
in the various stages of flight and for the investigation of
the aeroplane's flying qualities.
pressure-altitude either in the standard atmosphere or in
specified still air atmospheric conditions, and, for seaplanes, in
specified conditions of smooth water, the aeroplane shall be
capable of accomplishing the minimum performances specified
in B.2.5 and B.2.6, respectively, not considering obstacles,
or runway or water run length.
Note.- This Standard permits the maximum take-off mass
and maximum landing mass to be scheduled in the aeroplane
flight manual against, for example:
- aerodrome elevation, or
-pressure-altitude at aerodrome level, or
-pressure-altitude and atmospheric temperature at aerodrome
level,
so as to be readily usable when applying the national code on
aeroplane performance operating limitations.
B.2 Performance design parameters
B.2.1 Sufficient data on the performance of the aeroplane
shall be determined and scheduled in the flight manual to
provide operators with the necessary information for the
purpose of determining the total mass of the aeroplane on the
basis of the values, peculiar to the proposed flight, of the
relevant operational parameters, in order that the flight may be
made with reasonable assurance that a safe minimum
performance for that flight will be achieved.
B.2.2 Achieving the performance scheduled for the aeroplane
shall take into consideration human performance and in
particular shall not require exceptional skill or alertness on the
part of the flight crew.
Note.- Guidance material on human performance can be
found in the Human Factors Training Manual (Doc 9683).
B.2.3 The scheduled performance of the aeroplane shall
be consistent with compliance with A.2.1 and with the
operation in logical combinations of those of the aeroplane's
systems and equipment, the operation of which may affect
performance.
a) The aeroplane shall be capable of taking off assuming the
critical power-unit to fail (see B.2.7), the remaining
power-units being operated within their take-off power or
thrust limitations.
b) After the end of the period during which the take-off power
or thrust may be used, the aeroplane shall be capable of
continuing to climb, with the critical power-unit inoperative
and the remaining power-units operated within their
maximum continuous power or thrust limitations, up to a
height that it can maintain and at which it can continue safe
flight and landing.
C) The minimum performance at all stages of take-off and
climb shall be sufficient to ensure that under conditions of
operation departing slightly from the idealized conditions
for which data are scheduled (see B.2.7), the departure from
the scheduled values is not disproportionate.
B.2.4 Minimum performance B.2.6 Landing
At the maximum mass scheduled (see B.2.7) for take-off and a) Starting from the approach configuration and with the
for landing as functions of the aerodrome elevation or critical power-unit inoperative, the aeroplane shall be
ANNEX 8 IIIB-B-1 13/12/07
Annex 8 - Airworthiness of Aircrafl Part ZZZB
capable, in the event of a missed approach, of continuing e) Landing. The landing distance shall be the horizontal
the flight to a point from which another approach can be distance traversed by the aeroplane from a point on the
made. approach flight path at a selected height above the
landing surface to the point on the landing surface at
b) Starting from the landing configuration, the aeroplane shall which the aeroplane comes to a complete stop, or, for a
be capable, in the event of a balked landing, of making a seaplane, comes to a satisfactorily low speed. The
climb-out, with all power-units operating. selected height above the landing surface and the
approach speed shall be appropriately related to operating
practices. This distance may be supplemented by
B .2.7 Scheduling of performance
Performance data shall be determined and scheduled in the
flight manual so that their application by means of the operating
rules to which the aeroplane is to be operated in accordance
with 5.2 of Annex 6, Part I, will provide a safe
relationship between the performance of the aeroplane and the
aerodromes and routes on which it is capable of being operated.
　
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