曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
with as much time as possible for interpretation and for subsequent
manoeuvre necessary to avoid a collision. In the design
of such lights, due account shall be taken of the conditions
under which they may reasonably be expected to perform
these functions.
Note 1.- It is likely that lights will be viewed against a
variety of backgrounds, such as typical city lighting, clear
starry sky, moonlit water and daytime conditions of low
background luminance. Furthermore, collision risk situations
are most likely to arise in terminal control areas in which
aircrafr are manoeuvring in the intermediate and lower jlight
levels at closing speeds that are unlikely to exceed 900 km/h
(500 kt).
Note 2.- See the Airworthiness Manual (Doc 9760) for
detailed technical specifications for exterior lights for
aeroplanes.
F.4.2 Lights shall be installed in aeroplanes so as to
minimize the possibility that they will:
a) adversely affect the satisfactory performance of the
flight crews' duties; or
b) subject a person outside the aeroplane to harmful dazzle.
ANNEX 8
Annex 8 - Airworthiness of Aircraft
Note.- In order to avoid the effects mentioned in R4.2, it
will be necessary in some cases to provide means whereby the
pilot can switch off or reduce the intensity of the flashing
lights.
F.5 Electromagnetic interference protection
Aeroplane electronic systems, particularly flight-critical and
flight-essential systems, shall be protected against electromagnetic
interference from both internal and external sources.
F.6 Ice protection
If certification for flight in icing conditions is requested, the
aeroplane shall be shown to be able to operate safely in icing
conditions likely to be encountered in all expected operating
environments.
Part ZZZB
SUB-PART G. OPERATING LIMITATIONS AND INFORMATION
G.l General G2.6 Miscellaneous limitations
The operating limitations within which compliance with the
Standards of this Annex is determined, together with any other
information necessary to the safe operation of the aeroplane,
shall be made available by means of a flight manual, markings
and placards, and such other means as may effectively
accomplish the purpose. The limitations and information shall
include at least those prescribed in this sub-part.
G.2 Operating limitations
G2.1 Limitations which there is a risk of exceeding in
flight and which are defined quantitatively shall be expressed
in suitable units and corrected if necessary for errors in
measurements so that the flight crew can, by reference to the
instruments available to them, readily determine when the
limitations are reached.
G.2.2 Loading limitations
Miscellaneous limitations shall include any necessary limitations
with respect to conditions found to be prejudicial to the
safety of the aeroplane (see A.2.1).
G.2.7 Flight crew limitations
The flight crew limitations shall include the minimum number
of flight crew personnel necessary to operate the aeroplane,
having regard, among other things, to the accessibility to the
appropriate crew members of all necessary controls and instruments
and to the execution of the established emergency
procedures.
Note.- See Annex 6 - Operation of Aircraft, Parts I and
11, for the circumstances in which the flight crew shall include
members in addition to the minimumflight crew defined in this
Annex.
G.2.8 Flying time limitation after system
or power-unit failure
The loading limitations shall include all limiting masses, The systems limitations shall include the maximum flying time
centres of gravity positions, mass distributions and floor for which system reliability has been established in relation to
loadings (see A.2.2). the approval of operations by aeroplanes with two turbine
powei-"nits beyond the threshold time established in accordance
with 4.7 of Annex 6, Part I.
G2.3 Airspeed limitations
Note.- The maximum time established in accordance with
The airspeed limitations shall include all speeds (see C.5) that 4.7 of Annex 6, Part I, for a particular route may be less than
are limiting from the standpoint of structural integrity or flying that detemined in accordance with G2.8 because of the
qualities of the aeroplane, or from other considerations. These operational considerations involved.
speeds shall be identified with respect to the appropriate
aeroplane configurations and other pertinent factors.
G.2.4 Powerplant limitations
6 3 Operating information and procedures
The powerplant limitations shall include all those established G.3.1 Types of eligible operations
for the various powerplant components as installed in the
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
附件8--航空器适航性 Airworthiness of Aircraft(39)
