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than 20 m in length.
b) a second light having the same characteristics as the
light described in 3.2 d) and mounted in a vertical line
at least 2 m above or below it; and
c) a yellow light having otherwise the same characteristics
as the light described in 3.2 c) and mounted in a vertical
line at least 2 m above it.
Ftgure 3
3.4 When being towed
The lights described in 3.2 a), b) and c) appearing as steady,
unobstructed lights.
3.5 When not under command and not making way
As illustrated in Figure 4, two steady red lights placed where
they can best be seen, one vertically over the other and not less
than 1 m apart, and of such a character as to be visible all
around the horizon at a distance of at least 3.7 krn (2 NM).
Red
1 metre at least
A - -
Figure 4
3.6 When making way but not under command
As illustrated in Figure 5, the lights described in 3.5 plus the
lights described in 3.2 a), b) and c).
3.3 When towing another vessel or aeroplane
Nore.- The display of lights prescribed in 3.5 and 3.6
As illustrated in Figure 3, the following appearing as steady, above is to be taken by other aircrafi as signals that the
unobstructed Lights: aeroplane showing them is nut under command md cunnut
therefore get out of the way. They are not ~ignuls of aeroa)
the lights described in 3.2 above; pjanes irz distress and requiring assistance.
Appendix Annex 6 - Operahbn of Aircraft
Green 140°
- --le R; L
-1 1 oo
Flgure 5
3.7 When at anchor
a) If less than 50 rn in length, where it can best be seen, a
steady white light (Figure 6), visible all around the
horizon at a distance of at least 3.7 krn (2 NM).
b) If SO m or more in length, where they can best be seen,
a steady white forward light and a steady white rear
light (Figure 7) both visible all around the horizon at a
distance of at least 5.6 km (3 NM).
c) If SO rn or more in span a steady white light on each side
(Figures 8 and 9) to indicate the maximum span and
visible, so far as practicable, all around the horizon at a
distance of at least 1.9 km (1 NM).
&f*-L
- - - - 7L-C
A - -------Ah
- - - - --- A
Figure 6
I Figure 7 I
Less than 50 metres in length; 50 metres or more in span
Figure 8
--
50 metres or more In length; 50 metres or more in span
Figure 9
3.8 When aground
The lights prescribed in 3.7 and in addition two steady red
lights in vertical line. at least 1 m apart so placed as to be
visible all around the horizon.
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ATTACHMENT A. FLIGHT RECORDERS
Supplementary to 6.10
Int reduction
The material in this Attachment concerns flight recorders
intended for installation in aeroplanes engaged in international
air navigation. Flight recorders comprise two systems - a
flight data recorder and a cockpit voice recorder. Flight data
recorders are classified as Type I and Type I1 depending upon
the number of parameters to be recorded.
1. Flight data recorder (FDR)
1. I General requirements
1. I. 1 The recorder is to record continuously during flight
time.
1.1.2 The recorder container is to:
a) be painted a distinctive orange or yellow colour;
b) carry reflective material to facilitate its location; and
c) have securely attached an automatically activated
underwater locating device.
1.1.3 The recorder is to be installed so that:
a) the probability of damage to the recording is minimized.
To meet this requirement it should be located as far aft
as practicable. In the case of pressurized aeroplanes it
should be located in the vicinity of the rear pressure
bulkhead;
b) it receives its electrical power from a bus that provides
the maximum reliability for operation of the recorder
without jeopardizing service to essential or emergency
loads; and
C) there is an aural or visual means for pre-flight checking
that the recorder is operating properly.
1.2 Parameters to be recorded
1.2.1 Type I flight data recorder. This recorder will be
capable of recording, as appropriate to the aeroplane, at least
the 32 parameters in Table A-1. However, other parameters
may be substituted with due regard to the aeroplane type and
the characteristics of the recording equipment.
1.2.2 Type [Iflight data recorder. This recorder will be
capable of recording, as appropriate to the aeroplane, at least
the first 15 parameters in Table A-I. However, other
parameters may be substituted with due regard to the
aeroplane type and the characteristics of the recording
equipment.
　
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