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b) excessive terrain closure rate;
c) excessive altitude loss after take-off or go-around;
d) unsafe terrain clearance while not in landing configuration;
1) gear not locked down;
2) flaps not in a landing position; and
e) excessive descent below the instrument glide path.
23/11/06
Annex 6 — Operation of Aircraft Part I
12/31/111//0016 6-10
No. 30
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 1981
Recommendation.— All aeroplanes should 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.
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
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.
6.17.4 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 ELT.
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 III.
6.18 Aeroplanes required to be equipped
with an airborne collision avoidance
system (ACAS II)
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 carry more than 30 passengers shall be
equipped with an airborne collision avoidance system
(ACAS II).
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 II).
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 provision is intended to improve the effectiveness
of air traffic 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.
Chapter 6 Annex 6 — Operation of Aircraft
6-11 12/31/111/0/016
　
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