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or operating on the movement area of an aerodrome are
contained in the Airworthiness Manual (Doc 9760).
c) a landing light;
6.9.4 Recommendation.- All piston-engined aeroplanes
of a ma.rimutn cert~j5cated 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
forward looking terrain avoidance function.
6.9.5 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.
6.9.6 A ground proximity warning system shall provide, as
a minimum, warnings of at least the following circumstances:
d) illumination for all flight instruments and equipment that a) excessive descent rate;
are essential for the safe operation of the aeroplane;
b) excessive altitude loss after take-off or go-around; and
e) lights in all passenger compartments; and
c) unsafe terrain clearance.
f) an electric torch for each crew member station.
6.9.7 Recommendation.- A11 turbine-engined aeroplanes
of a maximum cert~jicated take-off mass in excess of 5 700 kg
or authorized to carry more than nine passengers, should be
6.8 All aeroplanes complying with the equipped with a ground proximity ~varning system which has a
noise certification Standards in forward looking terrain avoidance function.
Annex 16, Volume I
An aeroplane shall carry a document attesting noise
certification. 6.10 Flight recorders
Note.- The attestation may be contained in any document, Note 1.- Flight recorders comprise two systems, a flight
carried on board, approved by the State of Registry. data recorder and a cockpit voice recorde,:
6.9 Aeroplanes required to be equipped
with ground proximity warning
systems (GPWS)
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, for which the individual
certificate of airworthiness is first issued on or after
1 January 2004, shall be equipped with a ground proximity
warning system which has a forward looking terrain
avoidance function.
6.9.2 From 1 January 2007, 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 which has
a forward looking terrain avoidance function.
6.9.3 Recommendation.- All turbine-engined aeroplanes
of a maximum certijicated take-off mass of 5 700 kg or less and
authorized to carp more than jive but not more than nine
passetzgers shocrld be equipped with a groutdproximit~ ~.c.>arning
systern which has a forward looking terrain avoidance function.
Note 2.- Combination recorders (FDR/CVR) can only be
used to meet the jlight recorder equipage requirements as
speczj5cally 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 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.
6.10.1.3 The use of engraving metal foil flight data
recorders shall be discontinued by 1 January 1995.
6.10.1.4 Recommendation.- The use of analogue flight
data recorders using frequency modulatior~ (FM) shorrld be
disco~ztitluedb y 5 Nouember 1998.
Chapter 6 Annex 6 - Operation of Aircraft
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,
which utilize data link communications and are required to
carry a cockpit voice recorder (CVR), shall record on a flight
recorder, all data link communications to and from the aeroplane.
The minimum recording duration shall be equal to the
duration of the CVR, and shall be correlated to the recorded
cockpit audio.
6.10.1.5.1 From 1 January 2007, all aeroplanes which
- Time or relative time count
- Navigation data*: drift angle, wind speed, wind direction,
latitudellongitude
- Groundspeed*
- Radio altitude*
6.10.1.7.2 The following parameters satisfy the requirements
for attitude:
　
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