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(artificial horizon), clearly visible to the pilot-in-command.
The emergency power supply shall be automatically operative
after the total failure of the main electrical generating system
and clear indication shall be given on the instrument panel that
the attitude indicator(s) is being operated by emergency
power.
6.9.2.2 Those instruments that are used by any one pilot
shall be so arranged as to permit the pilot to see their
indications readily from his or her station, with the minimum
practicable deviation from the position and line of vision
normally assumed when looking forward along the flight path.
c) two sensitive pressure altimeters with counter drumpointer
or equivalent presentation; 6.10 All aeroplanes when operated at night
Note.- Neither three-pointer nor drum-pointer All aeroplanes, when operated at night shall be equipped with:
altimeters satisfy the requirement in 6.9.1 c).
a) all equipment specified in 6.9;
d) an airspeed indicating system with means of preventing
malfunctioning due to either condensation or icing; b) the lights required by Annex 2 for aircraft in flight or
operating on the movement area of an aerodrome;
e) a turn and slip indicator;
Note.- Specifications for lights meeting the
requirements of Annex 2 for navigation lights are
f) an attitude indicator (artificial horizon); contained in Appendix I. The general characteristics of
lights are specified in Annex 8. Detailed specifications
g) a heading indicator (directional gyroscope); for lights meeting the requirements of Annex 2 for
aircraft in flight or operating on the movement area of
Note.- The requirements of 6.9.1 e), f) and g) may an aerodrome are contained in the Airworthiness
be met by combinations of instruments or by integrated Manual (Doc 9760).
flight director systems provided that the safeguards
against total failure, inherent in the three separate C) two landing lights;
instruments, are retained.
Note.- Aeroplanes not certificated in accordance
h) a means of indicating whether the power supply to the with Annex 8 which are equipped with a single landing
gyroscopic instrument is adequate; light having two separately energized filaments will be
considered to have complied with 6.10 c).
i) a means of indicating in the flight crew compartment the
outside air temperature; d) illumination for all instruments and equipment that are
essential for the safe operation of the aeroplane that are
j) a rate-of-climb and descent indicator; and used by the flight crew;
k) such additional instruments or equipment as may be e) lights in all passenger compartments; and
prescribed by the appropriate authority.
f) an electric torch for each crew member station
6.9.2 All aeroplanes over 5 700 kg -
Emergency power supply for electrically
operated attitude indicating instruments 6.11 Pressurized aeroplanes when carrying
passengers - weather radar
6.9.2.1 All aeroplanes of a maximum certificated take-off
mass of over 5 700 kg newly introduced into service after Recommendation.- Pressurized aeroplanes when
1 January 1975 shall be fitted with an emergency power carving passengers should be equipped with operative
supply, independent of the main electrical generating system, weather radar whenever such aeroplanes are being operated
for the purpose of operating and illuminating, for a minimum in areas where thunderstorms or other potentially hazardous
period of 30 minutes, an attitude indicating instrument weather conditions, regarded as detectable with airborne
Chapter 6 Annex 6 - Operation of Aircraft
weather radar, may be expected to exist along the route either 6.15.2 Recommendation.- All piston-engined aeroplanes
at night or under instrument meteorological conditions. of a maximum certijicated take-off mass in excess of 5 700 kg or
authorized to carry more than nine passengers should be
equipped with a ground proximity warning system.
6.12 All aeroplanes operated
above 15 000 m (49 000 ft) -
radiation indicator
All aeroplanes intended to be operated above 15 000 m
(49 000 ft) shall carry equipment 'to measure and indicate
continuously the dose rate of total cosmic radiation being
received (i.e. the total of ionizing and neutron radiation of
galactic and solar origin) and the cumulative dose on each
flight. The display unit of the equipment shall be readily
visible to a flight crew member.
6.15.3 A ground proximity warning system shall provide
automatically a timely and distinctive warning to the flight
crew when the aeroplane is in potentially hazardous proximity
to the earth's surface.
6.15.4 A ground proximity warning system shall provide,
as a minimum, warnings of the following circumstances:
　
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