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equipped with at least one automatic ELT.
6.17.6 From 1 January 2005, aeroplanes on flights over
designated land areas as described in 6.6 shall be equipped
with at least one automatic ELT.
6.17.7 Recommendation.- All aeroplanes should carry
an automatic ELT
6.17.8 ELT equipment canied to satisfy the requirements
of 6.17.1, 6.17.2, 6.17.3, 6.17.4, 6.17.5, 6.17.6 and 6.17.7
shall operate in accordance with the relevant provisions of
Annex 10, Volume 111.
6.18 Aeroplanes required to be equipped with an
airborne collision avoidance system (ACAS 11)
6.18.1 From 1 January 2003, all turbine-engined aeroplanes
of a maximum certificated take-off mass in excess of 15 000 kg
or authorized to cany more than 30 passengers shall be
equipped with an airborne collision avoidance system
(ACAS 11).
6.18.2 From 1 January 2005, all turbine-engined
aeroplanes of a maximum certificated take-off mass in excess
of 5 700 kg or authorized to carry more than 19 passengers
shall be equipped with an airborne collision avoidance system
(ACAS 11).
6.18.3 Recommendation.- All aeroplanes should be
equipped with an airborne collision avoidance system
(ACAS II).
6.18.4 An airborne collision avoidance system shall
operate in accordance with the relevant provisions of
Annex 10, Volume IV.
6.19 Aeroplanes required to be equipped
with a pressure-altitude reporting transponder
All aeroplanes shall be equipped with a pressure-altitude
reporting transponder which operates in accordance with the
relevant provisions of Annex 10, Volume IV.
Note.- This pmvision is intended to improve the
effectiveness of air trafic services as well as airborne collision
avoidance systems.
6.20 Microphones
All flight crew members required to be on flight deck duty
shall communicate through boom or throat microphones below
the transition level/altitude.
6.21 Turbo-jet aeroplanes -
forward-looking wind shear
warning system
6.21.1 Recommendation.- All turbo-jet aeroplanes of
a maximum certijicated take-off mass in excess of 5 700 kg
Chapter 6 Annex 6 - Operation of Aircraft
or authorized to carry more than nine passengers should be aircrafr, and the information required to permit the pilot to
equipped with a forward-looking wind shear warning system. safely commence and continue a missed approach or go-around
or to execute an escape manoeuvre if necessary. The system
6.21.2 Recorninendation.- A forward-looking wind shear should also provide an indication to the pilot when the limits
warning system should be capable of providing the pilot with a specijied for the certification of automatic landing equipment
timely aural and visual warning of wind shear ahead of the are being approached, when such equipment is in use.
CHAPTER 7. AEROPLANE COMMUNICATION AND
NAVIGATION EQUIPMENT
7.1 Communication equipment navigation performance specifications (MNPS) are prescribed,
an aeroplane shall be provided with navigation equipment
7.1.1 An aeroplane shall be provided with radio which:
communication equipment capable of:
a) continuously provides indications to the flight crew of
a) conducting two-way communication for aerodrome adherence to or departure from track to the required
control purposes; degree of accuracy at any point along that track; and
b) receiving meteorological information at any time during b) has been authorized by the State of the Operator for
flight; and MNPS operations concerned.
C) conducting two-way communication at any time during Note.- The prescribed minimum navigation perjormance
flight with at least one aeronautical station and with specifications and the procedures governing their application
such other aeronautical stations and on such frequencies are published in the Regi0na1 Procedures
as may be prescribed by the appropriate authority. (Doc 7030).
Note.- The requirements of 7.1.1 are considered fulfilled 7.2.3 For flights in defined portions of airspace where,
if the ability to conduct the communications specified therein based On Regiona1 Air Navigation Agreement, a vertical
is established during radio propagation conditions which are separation minimum (VSM) of 300 m (1 000 ft) is applied
nonnal for the route. above FL 290, an aeroplane:
7.1.2 The radio communication equipment required in a) shall be provided with equipment which is capable of:
accordance with 7.1.1 shall provide for communications on the
aeronautical emergency frequency 121.5 MHz. 1) indicating to the flight crew the flight level being
flown;
2) automatically maintaining a selected flight level;
7.2 Navigation equipment 3) providing an alert to the flight crew when a deviation
　
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