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a) excessive descent rate;
b) excessive terrain closure rate;
c) excessive altitude loss after take-off or go-around;
Note.- The equipment is calibrated on the basis of
assumptions acceptable to the appropriate national d) unsafe terrain clearance while not in landing
authorities. configuration;
I) gear not locked down;
6.13 All aeroplanes complying with
the noise certification Standards
in Annex 16, Volume I
An aeroplane shall carry a document attesting noise
certification. When the document, or a suitable statement
attesting noise certification as contained in another document
approved by the State of Registry, is issued in a language other
than English, it shall include an English translation.
Note.- The attestation may be contained in any document,
carried on board, approved by the State of Registry.
6.14 Mach number indicator
2) flaps not in a landing position; and
e) excessive descent below the instrument glide path.
6.15.5 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, for which the
individual certificate of airworthiness is first issued on or
after 1 January 2001, shall be equipped with a ground
proximity warning system which has a predictive terrain
hazard warning function.
6.15.6 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 a ground proximity warning system which
has a predictive terrain hazard warning function.
All aeroplanes with speed limitations expressed in terms of
Mach number, shall be equipped with a Mach number 6.15.7 Recommendation.- All turbine-engined aeroplanes
indicator. of a maximum certificated take-off mass in excess of 5 700 kg or
authorized to carry more than nine passengers should be
equipped with a ground proximity warning system which has a
Note.- This does not preclude the use of the airspeed predictive terrain hazard warningfunction.
indicator to derive Mach number for ATS purposes.
6.16 Aeroplanes carrying passengers -
cabin crew seats
6.15 Aeroplanes required to be
equipped with ground proximity
warning systems (GPWS) 6.16.1 Aeroplanes for which the individual
certificate of airworthiness is first
6.15.1 All turbine-engined aeroplanes of a maximum issued on or after 1 January 1981
certificated take-off mass in excess of 5 700 kg or authorized
to carry more than nine passengers shall be equipped with a All aeroplanes shall be equipped with a forward or rearward
ground proximity warning system. facing (within 15 degrees of the longitudinal axis of the
Annex 6 - Operation of Aircraft Part I
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
　
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