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State of Registry, and are properly rated and of current
validity, and shall be satisfied that flight crew members have
maintained competence.
9.2 Composition of the flight crew
The number and composition of the flight crew shall not be
less than that specified in the flight manual or other documents
associated with the certificate of airworthiness.
ANNEX 6 - PART II
APPENDIX. LIGHTS TO BE DISPLAYED BY AEROPLANES
(Note.- See Chapter 6)
1. Terminology
When the following terms are used in ths Appendix, they
have the following meanings:
Angles of coverage.
a) Angle of coverage A is formed by two intersecting
vertical planes making angles of 70 degrees to the right
and 70 degrees to the left respectively, looking aft along
the longitudinal axis to a vertical plane passing through
the longitudinal axis.
b) Angle of coverage F is formed by two intersecting
vertical planes maktng angles of 1 10 degrees to the right
and 1 10 degrees to the left respectively, looking forward
along the longitudinal axis to a vertical plane passing
through the longitudinal axis.
c) Angle of coverage L is formed by two intersecting
vertical planes, one parallel to the longitudinal axis of
the aeroplane. and the other 110 degrees to the left of
the first. when loohng forward along the longitudinal
axis.
d) Angle of coverage R is formed by two intersecting
vertical planes, one parallel to the longitudinal axis of
the aeroplane, and the other 110 degrees to the right of
the first, when looking forward along the longitudinal
axis.
Horizontal plane. The plane containing the longitudinal axis
and perpendicular to the plane of symmetry of the
aeroplane.
Longitudinal axis ofthe aeroplane. A selected axis parallel to
the direction of flight at a normal cruising speed, and
passing through the centre of gravity of the aeroplane.
Making way. An aeroplane on the surface of the water is
"making way" when it is under way and has a velocity
relative to the water.
Under command. An aeroplane on the surface of the water is
"under command" when it is able to execute manoeuvres
as required by the International Regulations for Preventing
Collisions at Sea for the purpose of avoiding other vessels.
Under way. An aeroplane on the surface of the water is
"under way" when it is not aground or moored to the
ground or to any fixed object on the land or in the water.
Verfical planes. Planes perpendicular to the horizontal plane.
ViXble. Visible on a dark night with a clear atmosphere.
2. Navigation lights to be displayed in the air
Note.- The lights specrfied herein are intended to meet the
requirements of Annex 2 for navigation lights.
As illustrated in Figure 1, the following unobstructed
navigation lights shall be displayed:
140
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Figure 1
a) a red light projected above and below the horizontal
plane through angle of coverage L;
b) a green light projected above and below the horizontal
plane through angle of coverage R;
c) a white light projected above and below the horizontal
plane rearward through angle of coverage A.
3. Lights to be displayed on the water
3.1 General
Note.- The lights specified herein are intended to meet the
requirements of Annex 2 for lights to be displayed by
aeroplanes on the water.
The International Regulations for Preventing Collisions at Sea
require different lights to be displayed in each of the following
circumstances:
a) when under way;
ANNEX 6 - PART 11 2 1
Annex 6 - Operation of Aircraft Part II
b) when towing another vessel or aeroplane;
c) when being towed;
d) when not under command and not making way;
e) when making way but not under command;
f) when at anchor;
g) when aground.
The lights required by aeroplanes in each case are described
below.
3.2 When under way
As illustrated in Figure 2, the following appearing as steady
unobstructed lights:
a) a red light projected above and below the horizontal
through angle of coverage L;
b) a green light projected above and below the horizontal
through angle of coverage R;
C) a white light projected above and below the horizontal
through angle of coverage A; and
d) a white light projected through angle of coverage F.
The lights described in a), b) and c) should be visible at a
distance of at least 3.7 krn (2 NM). The light described in d)
should be visible at a distance of 9.3 krn (5 NM) when fitted
to an aeroplane of 20 m or more in length or visible at a
distance of 5.6 km (3 NM) when fitted to an aeroplane of less
　
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