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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 verticl
line at least 2 m above it.
3.2 When under way
As illustrated in Figure 2, the following appearing as steady
unobsuucted 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 3.2 a), b) and c) should be visible at a
distance of at least 3.7 km (2 NM). The light described in 3.2
d) should be visible at a distance of 9.3 km (5 NM) when fitted
to an aeroplane of 20 m or more in length or visible at a
distance of 5.6 krn (3 NM) when fitted to an aeroplane of less
than 20 m in length.
o0
Green
Figure 2
Figure 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 whe~e
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 km (2 NM).
Red
1 metre at least -
-
Figure 4
111 1/01 APP 1-2
Appendix 1 Annex 6 - Operation of Aircrafl
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).
Note.- The display of lights prescribed in 3.5 and 3.6 is to
be taken by other aircraft as signals that the aeroplane
showing them is not under command and cannot therefore get
out of the way. They are not signals of aeroplanes in distress
and requiring assistance.
Green 140°
Figure 5
3.7 When at anchor
a) If less than 50 m 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 km (2 NM).
Z- h- - - --- - - A &
- A h
A
Figure 6
h - - - - h -C- As- - - - - - &
A
- A h Z
Figure 7
C) If 50 m 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).
\ -
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
b) If 50 m or more in length, where they can best be seen,
a steady white forward light and a steady white rear The lights prescribed in 3.7 and in addition two steady red
light (Figure 7) both visible all around the horizon at a lights in vertical line, at least 1 m apart so placed as to be
distance of at least 5.6 km (3 NM). visible all around the horizon.
APP 1-3
APPENDIX 2. CONTENTS OF AN OPERATIONS MANUAL
(See Chapter 4, 4.2.2.1)
An operations manual, which may be issued in separate parts
corresponding to specific aspects of operations, provided in
accordance with Chapter 4, 4.2.2.1, shall contain at least the
following:
5. Flight operations
5.1 The flight crew for each type of operation including
the designation of the succession of command.
5.2 The in-flight and the emergency duties assigned to
each crew member.
1. Operations administration and supervision
1.1 Instructions outlining the responsibilities of operations
personnel pertaining to the conduct of flight operations.
1.2 Checklist of emergency and safety equipment and
instructions for its use.
1.3 The minimum equipment list for the aeroplane types
operated and specific operations authorized, including any
requirements relating to operations in RNP airspace.
1.4 Safety precautions during refuelling with passengers
on board.
2. Accident prevention and flight
safety programme
Details of the accident prevention and flight safety programme
provided in accordance with Chapter 3, 3.2, including a statement
of safety policy and the responsibility of personnel.
3. Personnel training
3.1 Details of the flight crew training programme and
requirements.
3.2 Details of the cabin crew duties training programme
as required by Chapter 12, 12.4.
4. Fatigue and
flight time limitations
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