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15 March 2000
17 July 2000
2 November 2000
9 March 2001
16 July 2001
1 November 200 1
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28 November 2002
28/11/02
No. 22
Chapter 6 Annex 6 - Operation of Aircraft
a) when the aeroplane may be over water at a distance of
more than 93 km (50 NM) away from land suitable for
making an emergency landing:
- one life jacket or equivalent individual floatation
device for each person on board, stowed in a position
easily accessible from the seat or berth of the person
for whose use it is provided;
b) when over water away from land suitable for making an
emergency landing at a distance of more than 185 km
(100 NM), in the case of single-engined aeroplanes, and
more than 370 km (200 NM), in the case of multi-engined
aeroplanes capable of continuing flight with one engine
inoperative:
6.5.3 Aeroplanes for which the individual
certificate of airworthiness is first
issued before I January 1990
Recommendation.- Pressurized aeroplanes intended to
be operated at flight altitudes at which the atnlospheric
pressure is less than 376 hPa should be equipped with a
device to provide positive warning to the jlight crew of any
dangerous loss of pressurization.
6.6 All aeroplanes operated in accordance
with the instrument flight rules
All aeroplanes when operated in accordance with the
instrument flight rules & when the aeroplane cannot be
life-saving rafts in sufficient numbers to carry maintairled in a desired attitude without reference to one or
persons on board, stowed so as to facilitate their more flight instruments, shall be equipped with:
ready use in emergency, provided with such lifesaving
equipment including means of sustaining a) a magnetic compass;
life as is appropriate to the flight to be undertaken;
and b) an accurate timepiece indicating the time in hours,
minutes and seconds;
2) equipment for making the pyrotechnical distress
signals described in Annex 2. c) a sensitive pressure altimeter;
Note.- Due to the long history of misreadings, the use
of drum-pointer altimeters is not recommended.
6.4 All aeroplanes on flights over
designated land areas
d) an airspeed indicating system with a means of preventing
malfunctioning due to either condensation or icing;
Aeroplanes when operated across land areas which have been e) a turn and slip indicator;
designated by the State concerned as areas in which search and
rescue would be especially difficult shall be equipped with f) an attitude indicator (artificial horizon);
such signalling devices and life-saving equipment (including
means of sustaining life) as may be appropriate to the area g) a heading indicator (directional gyroscope);
overflown.
Note.- The requirements of e), f) and g), may be met
by combinations of instruments or by integrated jlight
director systems provided that the safeguards against
total failure, inherent in the three separate instruments,
6.5 All aeroplanes on high altitude flights are retained.
6.5.1 All aeroplanes intended to be operated at high h) means of indicating whether the supply of power to the
altitudes shall be equipped with oxygen storage and dispensing gyroscopic instruments is adequate;
apparatus capable of storing and dispensing the oxygen
supplies required in 4.9. i) a means of indicating in the flight crew compartment the
outside air temperature;
6.5.2 Aeroplanes for which the individual
certificate of airworthiness is first
issued on or after 1 January 1990
j) a rate-of-climb and descent indicator: and
k) such additional instruments or equipment as may be
prescribed by the appropriate authority.
Pressurized aeroplanes intended to be operated at flight
altitudes at which the atmospheric pressure is less than
-
376 hPa shall be equipped with a device to provide positive 6.7 All aeroplanes when operated at night
warning to the flight crew of any dangerous loss of
pressurization. All aeroplanes, when operated at night, shall be equipped with:
1111/01
No. 21
Annex 6 - Operation of Aircraft Part I1
a) all the equipment specified in 6.6;
b) the lights required by Annex 2 for aircraft in flight or
operating on the movement area of an aerodrome;
N o t e . Specifications for lights meeting the requirements
of Annex 2 for navigation lights are contained in
the Appendix. The general characteristics of lights are
spec~ped in Annex 8. Detailed specifications for lights
meeting the requirements of Annex 2 for aircraft injlight
　
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