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the rotation of the engine in flight or to reduce it to a safe
level.
7.1.4 Engine restarting
Means shall be provided for restarting an engine in flight at
altitudes up to a declared maximum altitude.
7.2 Arrangement and functioning
7.2.1 Independence of power-units
The powerplant shall be arranged and installed so that each
power-unit together with its associated systems is capable of
being controlled and operated independently from the others
and so that there is at least one arrangement of the powerplant
and systems in which any failure, unless the probability
of its occurrence is extremely remote, cannot result in a loss
of more power than that resulting from complete failure of
the critical power-unit.
The cooling system shall be capable of maintaining powerplant
temperatures within the established limits (see 7.1.2) at
ambient air temperatures up to the maximum air temperature
appropriate to the intended operation of the aeroplane. The
maximum and, if necessary, minimum ambient air temperature
for which the powerplant has been established as being
suitable shall be scheduled in the aeroplane flight manual.
7.2.4 Associated systems
The fuel, oil, air induction, and other systems associated with
the powerplant shall be capable of supplying each engine in
accordance with its established requirements, under all
conditions affecting the functioning of the systems (e.g. engine
power, aeroplane attitudes and accelerations, atmospheric
conditions, fluid temperatures) within the anticipated operating
conditions.
7.2.5 Fire protection
For regions of the powerplant where the potential fire hazards
are particularly serious because of the proximity of ignition
sources to combustible materials, the following shall apply in
addition to the general Standard of 4.1.6 e).
a) Isolation. Such regions shall be isolated by fire-resisting
material from other regions of the aeroplane where the
presence of fire would jeopardize continued flight,
taking into account the probable points of origin and
paths of propagation of fire.
b) Flammable fluids. Flammable fluid system components
located in such regions shall be capable of containing
the fluid when exposed to fire conditions. Means shall
be provided for the crew to shut off the flow of
flammable fluids into such regions if a fire occurs.
C) Fire detection. A sufficient number of fire detectors
shall be provided and located to ensure rapid detection
of any fire that might occur in such regions.
ANNEX 8 IIIA-7-1 13/12/07
Annex 8 -Airworthiness of Aircraft
d) Fire extinguishment. Such regions shall be provided
with a fire extinguisher system capable of extinguishing
any fire likely to occur therein, unless the degree of
isolation, quantity of combustibles, fire resistance of the
structure, and other factors are such that any fire likely
to occur in the region would not jeopardize the safety of
the aeroplane.
Part ZZZA
CHAPTER 8. INSTRUMENTS AND EQUIPMENT
8.1 Required instruments
and equipment
The aeroplane shall be provided with approved instruments
and equipment necessary for the safe operation of the
aeroplane in the anticipated operating conditions. These shall
include the instruments and equipment necessary to enable the
crew to operate the aeroplane within its operating limitations.
Note 1.- Instruments and equipment additional to the
minimum necessary for the issuance of a Certificate of Airworthiness
are prescribed in Annex 6, Parts I and IZ, for
particular circumstances or on particular kinds of routes.
Note 2.- Instruments and equipment design shall observe
Human Factors principles.
Note 3.- Guidance material on Human Factors principles
can be found in the Human Factors Training Manual
(Doc 9683) and in the Human Factors Guidelines for Air
Traffic Management (ATM) Systems (Doc 9758).
8.2 Installation
Instrument and equipment installations shall comply with the
Standards of Chapter 4.
8.3 Safety and
survival equipment
Prescribed safety and survival equipment that the crew or
passengers are expected to use or operate at the time of an
emergency shall be reliable, readily accessible and easily
identified, and its method of operation shall be plainly marked.
*8.4 Navigation lights
and anti-collision lights
8.4.1 The lights required by Annex 2 -Rules of the Air
to be displayed by aeroplanes in flight or operating on the
movement area of an aerodrome shall have intensities,
colours, fields of coverage and other characteristics such that
they furnish the pilot of another aircraft or personnel on the
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附件8--航空器适航性 Airworthiness of Aircraft(27)
