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9 November 1998, shall be provided with automatically
deployable oxygen equipment to satisfy the requirements of
4.3.8.2. The total number of oxygen dispensing units shall
exceed the number of passenger and cabin crew seats by at
least 10 per cent.
6.7.6 Recommendation.— An aeroplane intended to be
operated at flight altitudes at which the atmospheric pressure is
less than 376 hPa, or which, if operated at flight altitudes at
which the atmospheric pressure is more than 376 hPa cannot
descend safely within four minutes to a flight altitude at which
the atmospheric pressure is equal to 620 hPa, and for
which the individual certificate of airworthiness was first
issued before 9 November 1998, should be provided with automatically
deployable oxygen equipment to satisfy the requirements
of 4.3.8.2. The total number of oxygen dispensing units
should exceed the number of passenger and cabin crew seats by
at least 10 per cent.
Annex 6 — Operation of Aircraft Part I
12/31/111//0016 6-8
No. 30
6.8 All aeroplanes in icing conditions
All aeroplanes shall be equipped with suitable de-icing and/or
anti-icing devices when operated in circumstances in which
icing conditions are reported to exist or are expected to be
encountered.
6.9 All aeroplanes operated in accordance
with instrument flight rules
6.9.1 All aeroplanes when operated in accordance with
the instrument flight rules, or when the aeroplane cannot be
maintained in a desired attitude without reference to one or
more flight instruments, shall be equipped with:
a) a magnetic compass;
b) an accurate timepiece indicating the time in hours,
minutes and seconds;
c) two sensitive pressure altimeters with counter drumpointer
or equivalent presentation;
Note.— Neither three-pointer nor drum-pointer
altimeters satisfy the requirement in 6.9.1 c).
d) an airspeed indicating system with means of preventing
malfunctioning due to either condensation or icing;
e) a turn and slip indicator;
f) an attitude indicator (artificial horizon);
g) a heading indicator (directional gyroscope);
Note.— The requirements of 6.9.1 e), f) and g) may
be met by combinations of instruments or by integrated
flight director systems provided that the safeguards
against total failure, inherent in the three separate
instruments, are retained.
h) a means of indicating whether the power supply to the
gyroscopic instrument is adequate;
i) a means of indicating in the flight crew compartment the
outside air temperature;
j) a rate-of-climb and descent indicator; and
k) such additional instruments or equipment as may be
prescribed by the appropriate authority.
6.9.2 All aeroplanes over 5 700 kg —
Emergency power supply for electrically
operated attitude indicating instruments
6.9.2.1 All aeroplanes of a maximum certificated take-off
mass of over 5 700 kg newly introduced into service after
1 January 1975 shall be fitted with an emergency power
supply, independent of the main electrical generating system,
for the purpose of operating and illuminating, for a minimum
period of 30 minutes, an attitude indicating instrument
(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.
6.10 All aeroplanes when operated at night
All aeroplanes, when operated at night shall be equipped with:
a) all equipment specified in 6.9;
b) the lights required by Annex 2 for aircraft in flight or
operating on the movement area of an aerodrome;
Note.— Specifications for lights meeting the requirements
of Annex 2 for navigation lights are contained in
Appendix 1. The general characteristics of lights are
specified in Annex 8. Detailed specifications for lights
meeting the requirements of Annex 2 for aircraft in flight
or operating on the movement area of an aerodrome are
contained in the Airworthiness Manual (Doc 9760).
c) two landing lights;
Note.— Aeroplanes not certificated in accordance
with Annex 8 which are equipped with a single landing
light having two separately energized filaments will be
　
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