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parameters designated by an (*) are to be recorded if an information
source for the parameter is used by aeroplane systems
and/or flight crew to operate the aeroplane.
6.3.2 Flight data recorders — duration
All FDRs shall be capable of retaining the information
recorded during at least the last 25 hours of their operation,
except for the Type IIA FDR which shall be capable of
retaining the information recorded during at least the last
30 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.
Chapter 6 Annex 6 — Operation of Aircraft
6-5 12/31/111/0/016
No. 30
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 II FDR.
6.3.3.3 Recommendation.— All multi-engined turbinepowered
aeroplanes of a maximum certificated take-off mass
of 5 700 kg or less for which the individual certificate of
airworthiness is first issued on or after 1 January 1990 should
be equipped with a Type IIA FDR.
6.3.4 Flight data recorders — aeroplanes for which the
individual certificate of airworthiness was first issued
on or after 1 January 1987 but before 1 January 1989
6.3.4.1 All turbine-engined aeroplanes of a maximum
certificated take-off mass of over 5 700 kg, except those in
6.3.4.3, shall be equipped with an FDR which shall record
time, altitude, airspeed, normal acceleration and heading.
6.3.4.2 Recommendation.— All turbine-engined aeroplanes
of a maximum certificated take-off mass of over
5 700 kg, except those in 6.3.4.3, should be equipped with an
FDR which shall record time, altitude, airspeed, normal
acceleration, heading and such additional parameters as are
necessary to determine pitch attitude, roll attitude, radio
transmission keying and power on each engine.
6.3.4.3 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 Type II FDR.
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-engined 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,
normal acceleration and heading.
6.3.5.2 Recommendation.— 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 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
All aeroplanes of a maximum certificated take-off mass of
over 5 700 kg shall be equipped with a Type IA FDR.
6.3.7 Cockpit voice recorders — aeroplanes for
which the individual certificate of airworthiness is
first issued on or after 1 January 1987
6.3.7.1 All aeroplanes of a maximum certificated take-off
mass of over 5 700 kg shall be equipped with a CVR, the
objective of which is the recording of the aural environment on
the flight deck during flight time.
6.3.7.2 Recommendation.— All multi-engined turbinepowered
aeroplanes of a maximum certificated take-off mass
of 5 700 kg or less for which the individual certificate of
airworthiness is first issued on or after 1 January 1990 should
be equipped with a CVR, the objective of which is the
recording of the aural environment on the flight deck during
flight time.
6.3.8 Cockpit voice recorders — aeroplanes
for which the individual certificate of airworthiness
was first issued before 1 January 1987
Note.— CVR performance requirements are as contained in
the Minimum Operational Performance Specification (MOPS)
document for Flight Recorder Systems of the European
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