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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
6.9.4 A ground proximity warning system shall provide,
as a minimum, warnings of the following circumstances:
a) excessive descent rate;
1/11/01
No. 21
Chapter 6 Annex 6 - Operation ofAircraft
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
utilize data link communications and are required to carry a
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 .5.2 Sufficient information to derive the content of
the data link communications message, and, whenever
practical, the time the message was displayed to or generated
by the crew shall be recorded.
Note.- Data link communications include, but are not
limited to, automatic dependent surveillance (ADS),
controller-pilot data link communications (CPDLC), data linkjlight
information services (D-FIS) and aeronautical
operational control (AOC) messages.
6.10.1.6 Recommendation.- All aeroplanes of a
maximum certificated take-off mass over 5 700 kg, required to
be equipped with a jlight data recorder and a cockpit voice
recordel; may alternatively be equipped with two combination
recorders (FDWCVR).
6.10.1.7 A Type IA flight data recorder shall record the
parameters required to determine accurately the aeroplane
flight path, speed, attitude, engine power, configuration and
operation. The parameters that satisfy the requirements for a
Type IA flight data recorder are listed in the paragraphs below.
The parameters without an asterisk (*) are mandatory
parameters which shall be recorded. In addition, the
parameters designated by an asterisk (*) shall be recorded if an
information data source for the parameter is used by aeroplane
systems or the flight crew to operate the aeroplane.
6.10.1.7.1 The following parameters satisfy the requirements
for flight path and speed:
- Pressure altitude
- Indicated airspeed or calibrated airspeed
- Air - ground status and each landing gear air-ground
sensor when practicable
- Total or outside air temperature
- Heading (primary flight crew reference)
- Normal acceleration
- Lateral acceleration
- Longitudinal acceleration (body axis)
- 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:
- Pitch attitude
- Roll attitude
- Yaw or sideslip angle*
- Angle of attack*
6.10.1.7.3 The following parameters satisfy the requirements
for engine power:
- Engine thrustlpower: propulsive thrustlpower on each
engine, cockpit thrustlpower lever position
- Thrust reverse status*
- Engine thrust command*
- Engine thrust target*
- Engine bleed valve position*
- Additional engine parameters*: EPR, N,, indicated
vibration level, NZ, EGT, TLA, fuel flow, fuel cut-off
lever position, N3
6.10.1.7.4 The following parameters satisfy the requirements
for configuration:
- Pitch trim surface position
- Flaps*: trailing edge flap position, cockpit control
selection
- Slats*: leading edge flap (slat) position, cockpit control
selection
- Landing gear*: landing gear, gear selector position
- Yaw trim surface position*
- Roll trim surface position*
- Cockpit trim control input position pitch*
- Cockpit trim control input position roll*
- Cockpit trim control input position yaw *
- Ground spoiler and speed brake*: ground spoiler
position, ground spoiler selection, speed brake position,
speed brake selection
- De-icing andlor anti-icing systems selection*
- Hydraulic pressure (each system)*
- Fuel quantity *
- AC electrical bus status*
- DC electrical bus status*
- APU bleed valve position*
- Computed centre of gravity*
6.10.1.7.5 The following parameters satisfy the requirements
for operation:
- Warnings
- Primary flight control surface and primary flight control
pilot input: pitch axis, roll axis, yaw axis
- Marker beacon passage
- Each navigation receiver frequency selection
- Manual radio transmission keying and CVRlFDR
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