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minutes of its operation.
6.3.3 Flight data recorders - aeroplanes for which
the individual certificate of airworthiness is first
issued on or after 1 January 1989
6.3.3.1 All aeroplanes of a maximum certificated take-off
mass of over 27 000 kg shall be equipped with a Type I FDR.
6.3.3.2 All aeroplanes of a maximum certificated take-off
mass of over 5 700 kg, up to and including 27 000 kg, shall be
equipped with a Type 11 FDR.
6.3.3.3 Recommendation.- All multi-engined turbinepowered
aeroplanes of a maximum certijicated take-off mass
Chapter 6 Annex 6 - Operetion of Aircmfl
of 5 700 kg or less for which the individual certificate of 6.3.7 Cockpit voice recorders - aeroplanes for
airworthiness is first issued on or after 1 January 1990 should which the individual certificate of airworthiness is
be equipped with a Type IIA FDR. first issued on or after 1 January 1987
6.3.7.1 All aeroplanes of a maximum certificated take-off
6.3.4 Flight data recorders - aeroplanes for which the mass of over 5 700 kg shall be equipped with a CVR, the
individual certificate of airworthiness was first issued objective of which is the recording of the aural environment on
on or after 1 January 1987 but before 1 January 1989 the flight deck during flight time.
6.3.4.1 -All turbine-engined aeroplanes of a maximum 6.3.7.2 Recornmendation.- All multi-engined turbinecertificated
take-off mass of Over 5 700 kg, except those in powered aeroplanes of a mimum certiJ;cated mass
6.3.4.37 shall be equipped with an FDR which record of 5 700 kg or less for which the individual certificate of
time, altitude, airspeed, normal acceleration and heading. airworthiness is fist issued on or afier 1 January 1990 should
6.3.4.2 Recommendation- All turbine-engined aero- be equipped with a CVR, the objective of which is the
planes of a mimum cert8cated take-off mass of over
recording of the aural environment on the flight deck during
5 700 kg, except those in 6.3.4.3, should be equipped with an
jlight time.
FDR which shall record time, altitude, airs-p eed-. normal
acceleration, heading and such additional parameters as are
6.3.8 Cockpit voice recorders - aeroplanes necessary to determine pitch attitude, roll attitude, radio
transmission keying and power on each engine. for which the individual certificate of airworthiness
was first issued before 1 January 1987
63.4.3 All turbine-eugined aeroplanes of a maximum
certificated take-off mass of over 27 000 kg that are of types Note.- CVR performance requirements are as contained in
of which the prototype was certificated by the appropriate the Minimum Operational Performance Speci&ations (MOPS)
national authority after 30 September 1969 shall be equipped d o c ~ ~ ~feonr tF light Recorder Systems of the European
with a Type II FDR. Organization for Civil Aviation Equipment (EUROCAE) or
equivalent documents.
6.3.5 Flight data recorders - aeroplanes for which
the individual certificate of airworthiness was first
issued before 1 January 1987
6.3.5.1 All turbine-eugined aeroplanes of a maximum
certificated take-off mass of over 5 700 kg shall be equipped
with an FDR which shall record time, altitude, airspeed,
nonnal acceleration and heading.
6.3.5.2 Reconunendation- All turbine-engined aeroplanes
of a maximum certificated take-off mass of over
27000 kg that are of types of which the prototype was
cerhficated by the appropriate national authority afer
30 September 1969 should be equipped with an FDR which
should record, in addition to time, altitude, airspeed normal
acceleration and heading, such additional parameters as are
necessary to meet the objectives of determining:
a) the attitude of the aeroplane in achieving its flight path;
and
b) the basic forces acting upon the aeroplane resulting in
the achieved flight path and the origin of such basic
forces.
6.3.6 Flight data recorders - aeroplanes for which
the individual certificate of airworthiness
is first issued after 1 January 2005
6.3.8.1 All turbine-engined aeroplanes of a maximum
certificated take-off mass of over 27 000 kg that are of types
of which the prototype was certificated by the appropriate
national authority after 30 September 1969 shall be equipped
with a CVR, the objective of which is the recording of the
aural environment on the flight deck during flight time.
6.3.82 Recommendation- All turbine-engined aeroplanes
of a maximum certificated take-off mass of over 5 700
kg up to and including 27 000 kg that are of rypes of which tk
prototype was certijlcated by the appropriate national
authority after 30 September 1%9 should be equipped with a
CVR, the objective of which is the recording of the aural
　
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