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6.5.1 All aeroplanes intended to be operated at high h) means of indicating whether the supply of power to the
altitudes shall be equipped with oxygen storage and dispensing gyroscopic instruments is adequate;
apparatus capable of storing and dispensing the oxygen
supplies required in 4.9. i) a means of indicating in the flight crew compartment the
outside air temperature;
6.5.2 Aeroplanes for which the individual
certificate of airworthiness is first
issued on or after 1 January 1990
j) a rate-of-climb and descent indicator; and
k) such additional instruments or equipment as may be
prescribed by the appropriate authority.
Pressurized aeroplanes intended to be operated at flight
altitudes at which the atmospheric pressure is less than
376 hPa shall be equipped with a device to provide positive 6.7 All aeroplanes when operated st night
warning to the flight crew of any dangerous loss of
pressurization. All aeroplanes, when operated at night, shall be equipped with:
Annex 6 - Operation of Aircraft Pard I1
a) all the equipment specified in 6.6; 2) excessive terrain closure rate;
b) the lights required by Annex 2 for aircraft in flight or
operating on the movement area of an aerodrome;
Note.- Specifications for lights meeting the requirements
of Annex 2 for navigation lights are contained in
the Appendix. The general characteristics of lights are
specified in Annex 8. Detailed specifications for lights
meeting the requirements of Annex 2 for aircraft in flight
or operating on the movement area of an aerodrome are
contained in the Airworthiness Technical Manual
(Doc 9051).
c) a landing light;
d) illumination for all flight instruments and equipment that
are essential for the safe operation of the aeroplane;
e) lights in all passenger compartments; and
f) an electric torch for each crew member station.
6.8 All aeroplanes complying with the
noise certification Standards in Annex 16, Volume I
An aeroplane shall carry a document attesting noise
certification.
Note.- The attestation m y be contained in any document,
carried on board, approved by the State of Registry.
6.9 Aeroplanes required to be equipped with
ground proximity warning systems (GPWS)
6.9.1 Recommendation.- All turbine-engined aeroplanes
of a maximum certifcnted take-oflmass in excess of I5 000 kg
or authorized to carry more than 30 passengers should be
equipped with a ground proximity warning system.
6.9.2 All turbine-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 warning system from 1 January 1999.
6.9.3 A ground proximity warning system shall provide
automatically a timely and distinctive warning to the flight
crew when the aeroplane is in potentidly hazardous proximity
to the earth's surface.
6.9.4 From 1 January 1999 a ground proximity warning
system shall. provide, as a minimum, warnings of the following
circumstances;
1) excessive descent rate;
3) excessive altitude loss after take-off or go-around;
4) unsafe terrain clearance while not in landing configuration;
a) gear not locked down;
b) flaps not in a landing position; and
5) excessive descent below the instrument glide path.
6.9.5 Recommendation.- All piston-engimd aeroplanes
of a mimum certificated take-of mass in excess of 5 700 kg
or authorized to carry more than nine passengers should be
equipped with a ground proximity warning system.
6.10 Flight recorders
Note I.- Flight recorders comprise trvo systems, a flight
data recorder and a cockpit voice recorder:
Note 2.- Combination recorders (FDWCVR) can only be
used to meet the flight recorder equipage requirements as
specifically indicated in this Annex.
Note 3.- Detailed guidance on flight recorders is
contained in Attachment A.
6.10.1 Flight data recorders - types
6.10.1.1 A Type I flight data recorder shall record the
parameters required to determine accurately the aeroplane flight
path, speed, attitude, engine power, configuration and operation.
6.10.1.2 A Type LI flight data recorder shall record the
parameters required to determine accurately the aeroplane
flight path, speed, attitude, engine power and configuration of
lift and drag devices.
6.10.1.3 The use of engraving metal foil flight data
recorders shall be discontinued by 1 January 1995.
6.10.1.4 Recommendation.- The use of photographic
film data recorders and analogue data recorders using
frequency modulation (FM) should be discontinued by
5 November 1998.
6.1 0.1.5 All aeroplanes equipped to utilize digital
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