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preventive measures and techniques in relation to passengers,
baggage, cargo, mail, equipment, stores and supplies intended
Following an act of unlawful interference, the pilot-incommand
shall submit, without delay, a report of such an act
to the designated local authority.
13.5 Miscellaneous
13.5.1 Recommendation.- Specialized means of
attenuating and directing the blast should be provided for use
at the least-risk bomb location.
13.5.2 Recommendation.- Where an operator accepts
the carriage of weapons removed from passengers, the
aeroplane should have provision for stowing such weapons in
a place so that they are inaccessible to any person during
flight time.
* In the context of this Chapter, the word "security" is used in the
sense of prevention of illicit acts against civil aviation.
ANNEX 6 - PART I
APPENDIX 1. LIGHTS TO BE DISPLAYED BY AEROPLANES
1. Terminology
(Note.- See Chapter 6, 6.10)
Visible. Visible on a dark night with a clear atmosphere.
When the following terms are used in this Appendix, they
have the following meanings:
2. Navigation lights to be displayed in the air
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 making angles of 110 degrees to the right
and 110 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 looking 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 of the 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.
Vertical planes. Planes perpendicular to the horizontal plane.
Note.- The lights specified 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:
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.
Red l l O # ~ O oGreen
1 4 0
White
Figure 1
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;
b) when towing another vessel or aeroplane;
ANNEX 6 - PART I APP 1-1 1/11/01
Annex 6 - Operation of Aircraft
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.
Part I
3.3 When towing another
vessel or aeroplane
As illustrated in Figure 3, the following appearing as steady,
unobstructed lights:
a) the lights described in 3.2;
b) a second light having the same characteristics as the
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