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of drum-pointer altimeters is not recommended.
d) an airspeed indicating system with a means of preventing
malfunctioning due to either condensation or icing;
e) a turn and slip indicator;
f) an attitude indicator (artificial horizon);
g) a heading indicator (directional gyroscope);
Note.- The requirements of e), f) and g), may be met
by combinations of instruments or by integrated flight
director systems provided that the safeguards against
total failure, inherent in the three separate instruments,
are retained.
h) means of indicating whether the supply of power to the
gyroscopic instruments is adequate;
i) a means of indicating in the flight crew compartment the
outside air temperature;
j) a rate-of-climb and descent indicator; and
k) such additional instruments or equipment as may be
prescribed by the appropriate authority.
6.7 All aeroplanes when operated at night
All aeroplanes, when operated at night, shall be equipped with:
1/11/01
No. 21
Annex 6 - Operation of Aircraft Part II
a) all the equipment specified in 6.6; b) excessive terrain closure rate;
b) the lights required by Annex 2 for aircraft in flight or
operating on the movement area of an aerodrome;
c) excessive altitude loss after take-off or go-around;
d) unsafe terrain clearance while not in landing configur-
Note.- Specifications for lights meeting the require- ation;
ments 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 requirenients of Annex 2 for aircraft in flight
or operating on the movement area of an aerodrome are
contained in the Airworthiness Manual (Doc 9760).
1) gear not locked down;
2) flaps not in a landing position; and
e) excessive descent below the instrument glide path
6.9.5 Recommendation.- 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, should be
equipped with a ground proximity warning system which has a
predictive terrain hazard warning function.
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. 6.10 Flight recorders
Note I.- Flight recorders comprise two systems, a flight
data reconier and a cockpit voice reconier:
6.8 All aeroplanes complying with the
noise certification Standards in
Annex 16, Volume I
Note 2.- Combination reconiers (FDWCVR) can only be
used to meet the flight reconier equipage requirements as
specifically indicated in this Annex.
An aeroplane shall cany a document attesting noise
certification. Note 3.- Detailed guidance on flight reconiers is contained
in Attachment A.
Note.- The attestation may be contained in any document,
carried on board, approved by the State of Registry.
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.
6.9 Aeroplanes required to be equipped
with ground proximity warning
systems (GPWS)
6.10.1.2 A Type I1 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.
6.9.1 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.
6.10.1.3 The use of engraving metal foil flight data
6.9.2 Recommendation.- All piston-engined aeroplanes recorders shall be discontinued by 1 January 1995.
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 pmximit;v warning system.
6.10.1.4 Recommendation.- The use of analogue flight
data recorders using frequency modulation (FM) sholilcl be
discontinued by 5 November 1998.
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 potentially hazardous proximity
to the earth's surface.
6.10.1.4.1 The use of photographic film flight data
recorders shall be discontinued from 1 January 2003.
6.10.1.5 All aeroplanes for which the individual
certificate of airworthiness is first issued after 1 January 2005,
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