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less and authorized to carry more thanJive but not more than
nine passengers should be equipped with a ground proximity
warning system which provides the warnings of 6.15.9 a) and
c), warning of unsafe terrain clearance and a forward looking
terrain avoidance function.
6.15.7 From 1 January 2007 all piston-engined aeroplanes
of a maximum certificated take-off mass in excess of 5 700 kg
or authorized to carry more than nine passengers shall be
equipped with a ground proximity waming system which
provides the warnings in 6.15.9 a) and c), warning of unsafe
terrain clearance and a forward looking terrain avoidance
function.
6.15.8 A ground proximity warning system shall provide
automatically a timely and distinctive warning to the flight
crew when the aeroplane is in potentially hazardous proximity
to the earth's surface.
6.15.9 A ground proximity warning system shall provide,
6.15 Aeroplanes required to be unless otherwise specified herein, warnings of the following
equipped with ground proximity circumstances:
warning systems (GPWS)
a) excessive descent rate;
6.15.1 All turbine-engined aeroplanes of a maximum
certificated take-off mass in excess of 5 700 kg or authorized b) excessive terrain closure rate;
to carry more than nine passengers shall be equipped with a
ground proximity warning system. c) excessive altitude loss after take-off or go-around;
6.15.2 All turbine-engined aeroplanes of a maximum d) unsafe terrain clearance while not in landing
certificated take-off mass in excess of 15 000 kg or authorized configuration;
28/11/02
No. 27
Annex 6 - Operation of Aircraft Part I
1) gear not locked down;
2) flaps not in a landing position; and
e) excessive descent below the instrument glide path.
6.16 Aeroplanes carrying passengers -
cabin crew seats
6.16.1 Aeroplanes for which the individual
certificate of airworthiness is first
issued on or after 1 January 1981
All aeroplanes shall be equipped with a forward or rearward
facing (within 15 degrees of the longitudinal axis of the
aeroplane) seat, fitted with a safety harness for the use of each
cabin crew member required to satisfy the intent of 12.1 in
respect of emergency evacuation.
6.16.2 Aeroplanes for which the individual
certificate of airworthiness was first
issued before 1 January 198 1
6.17.4 Except as provided for in 6.17.5, until 1 January
2005 aeroplanes on flights over designated land areas as
described in 6.6 shall be equipped with at least one ELT(S).
6.17.5 All aeroplanes for which the individual certificate
of airworthiness is first issued after 1 January 2002, on flights
over designated land areas as described in 6.6, shall be
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 ELC
6.17.8 ELT equipment carried 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)
Recommendation.- All aeroplanes should be equipped 6.18.1 From 1 January 2003, all turbine-engined aeroplanes
with a fornard or rearward facing (within 15 degrees of the of a maximum certificated take-off mass in excess of 15 000 kg
longitudinal axis of the aeroplane) seat, fitted with a safe& or authorized to carry more than 30 passengers shall be
harness for the use of each cabin crew member required to equipped with an airborne collision avoidance system
satisfy the intent of 12.1 in respect of emergency evacuation. (ACAS 11).
Note.- Safety harness includes shoulder straps and a seat
belt which may be used independently.
6.16.3 Cabin crew seats provided in accordance with
6.16.1 and 6.16.2 shall be located near floor level and other
emergency exits as required by the State of Registry for
emergency evacuation.
6.17 Emergency locator transmitter (ELT)
6.17.1 Except as provided for in 6.17.2, until 1 January
2005 all aeroplanes operated on long-range over-water flights
as described in 6.5.3 shall be equipped with at least two
ELT(S).
6.17.2 All aeroplanes for which the individual certificate
of airworthiness is first issued after 1 January 2002, operated
on long-range over-water flights as described in 6.5.3, shall be
equipped with at least two ELTs, one of which shall be
automatic.
6.17.3 From 1 January 2005, all aeroplanes operated on
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