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- Pitch attitude
- Roll attitude
- Yaw or sideslip angle*
- Angle of attack*
utilize data link communications and are required to carry a
CVR, shall record on a flight recorder, all data link com- 6.10.1.7.3 The following parameters satisfy the requiremunications
to and from the aeroplane. The minimum ments for engine power:
recording duration shall be equal to the duration of the CVR,
and shall be correlated to the recorded cockpit audio. - Engine thrustlpower: propulsive thrustlpower on each
engine, cockpit thrustlpower lever position
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 linkflight
information services (D-FIS) and aeronautical
operational control (AOC) messages.
- Thrust reverse status*
- Engine thrust command*
- Engine thrust target*
- Engine bleed valve position*
- Additional engine parameters*: EPR, Nl, indicated
vibration level, N2, EGT, TLA, fuel flow, fuel cut-off
lever position, N3
6.10.1.7.4 The following parameters satisfy the requirements
for configuration:
6.10.1.6 Recommendation.- All aeroplanes of a - Pitch trim surface position
maximum certijicated take-off mass over 5 700 kg, required to - Flaps*: trailing edge flap position, cockpit control
be equipped with a flight 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
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*
- Indicated airspeed or calibrated airspeed
- Air - ground status and each landing gear air-ground 6.10.1.7.5 The following parameters satisfy the requiresensor
when practicable ments for operation:
- Total or outside air temperature
- Heading (primary flight crew reference)
- Normal acceleration
- Lateral acceleration
- Longitudinal acceleration (body axis)
- Warnings
- Primary flight control surface and primary flight control
pilot input: pitch axis, roll axis, yaw axis
- Marker beacon passage
Annex 6 - Operation of Aircraft Part I1
- Each navigation receiver frequency selection Note 2.- The number of parameters to be recorded will
- Manual radio transmission keying and CVRlFDR depend on aeroplane complexity. Parameters without an (*)
synchronization reference are to be recorded regardless of aeroplane complexity. Those
- Autopilot/autothrottle/AFCS mode and engagement parameters designated by an (*) are to be recorded if an instatus*
formation source for the parameter is used by aeroplane
- Selected barometric setting*: pilot, first officer systems and/orflight crew to operate the aeroplane.
- Selected altitude (all pilot selectable modes of
operation)*
- Selected speed (all pilot selectable modes of operation)* 6.10.2 Flight data recorders - duration
- Selected mach (all pilot selectable modes of operation)*
- selected vertical speed (all pilot selectable modes of OPer- Types I and I1 flight data recorders shall be capable of
ation)* retaining the information recorded during at least the last
　
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