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- Roll attitude
- Yaw or sideslip angle*
- Angle of attack*
6.3.1.8.3 The following parameters satisfy the requirements
for engine power:
- Engine thrust/power: propulsive thrusr/power on each
engine, cockpit thrust/power lever position
- 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
6.3.1.8.4 The following parameters satisfy the requirements
for configuration:
241 1/05
No. 29
Annex 6 - Operation of Aircrafi Part I
- 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*
6.3.1.8.5 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 CVRIFDR
synchronization reference
- Autopilof/autothrottle/AFCS mode and engagement
status*
- Selected barometric setting*: pilot, first officer
- Selected altitude (all pilot selectable modes of operation)*
- Selected speed (all pilot selectable modes of operation)*
- Selected Mach (all pilot selectable modes of operation)*
- Selected vertical speed (all pilot selectable modes of
operation) *
- Selected heading (all pilot selectable modes of operation)*
- Selected flight path (all pilot selectable modes of
operation)*: course/DSTRK, path angle
- Selected decision height*
- EFIS display format*: pilot, first officer
- Multi-function/engine/alerts display format*
- GPWS/TAWS/GCAS status*: selection of terrain
display mode including pop-up display status, terrain
alerts, both cautions and warnings, and advisories,
onloff switch position - Low pressure warning*: hydraulic pressure, pneumatic
pressure
- Computer failure*
- Loss of cabin pressure*
- TCASIACAS (traffic alert and collision avoidance
systemlairborne collision avoidance system)*
- Ice detection* - Engine warning each engine vibration*
- Engine warning each engine over temperature*
- Engine warning each engine oil pressure low*
- Engine warning each engine over speed*
- W~nd shear warning*
- Operational stall protection, stick shaker and pusher
activation*
- All cockpit flight control input forces*: control wheel,
control column, rudder pedal cockpit input forces
- Vertical deviation*: ILS glide path, MLS elevation,
GNSS approach path
- Horizontal deviation*: ILS localizer, MLS azimuth,
GNSS approach path
- DME 1 and 2 distances*
- Primary navigation system reference*: GNSS, INS,
VORIDME, MLS, Loran C, ILS
- Brakes*: left and right brake pressure, left and right
brake pedal position
- Date*
- Event marker*
- Head up display in use*
- Para visual display on*
Note 1.- Parameter requirements, including range,
sampling, accuracy and resolution, as contained in the
Minimum Operational Performance Spec$cation (MOPS)
document for Flight Recorder Systems of the European
Organization for Civil Aviation Equipment (EUROCAE) or
equivalent documents.
Note 2.- The number of parameters to be recorded will
depend on aeroplane complexity. Rzrameters without an (*)
are to be recorded regardless of aeroplane complexity. Those
parameters designated by an (*) are to be recorded if an
information source for the parameter is used by aeroplane
systems anaYorpight 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
　
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