Time; or

Relative time count

Global navigation satellite system (GNSS) time synchronisation

Pressure altitude

Indicated airspeed; or Calibrated airspeed

Heading (primary flight crew reference) — when true or magnetic heading can be selected, the primary heading reference, a discrete indicating selection, should be recorded

Normal acceleration

Pitch attitude

Roll attitude

Manual radio transmission keying and CVR/FDR synchronisation reference

Engine thrust/power

Parameters required to determine propulsive thrust/power on each engine

Flight crew compartment thrust/power lever position for aeroplanes with non-mechanically linked flight crew compartment — engine control

Total or outside air temperature

Longitudinal acceleration (body axis)

Lateral acceleration

Primary flight control surface and/or primary flight control pilot input (for aeroplanes with control systems in which movement of a control surface will back drive the pilot’s control, ‘or’ applies. For aeroplanes with control systems in which movement of a control surface will not back drive the pilot’s control, ‘and’ applies. For multiple or split surfaces, a suitable combination of inputs is acceptable in lieu of recording each surface separately. For aeroplanes that have a flight control break-away capability that allows either pilot to operate the controls independently, record both inputs):

Pitch axis

Roll axis

Yaw axis

Pitch trim surface position

Marker beacon passage

Warnings — in addition to the master warning, each ‘red’ warning (including smoke warnings from other compartments) should be recorded when the warning condition cannot be determined from other parameters or from the CVR

Each navigation receiver frequency selection

Flaps

Trailing edge flap position

Flight crew compartment control selection

Slats

Leading edge flap (slat) position

Flight crew compartment control selection

Thrust reverse status

Ground spoiler and speed brake

Ground spoiler position

Ground spoiler selection

Speed brake position

Speed brake selection

Autopilot, autothrottle and automatic flight control system (AFCS) mode and engagement status

Radio altitude. For auto-land/Category III operations, each radio altimeter should be recorded.

Vertical deviation — the approach aid in use should be recorded. For auto-land/Category III operations, each system should be recorded.

ILS/GPS/GLS glide path

MLS elevation

Integrated approach navigation (IAN)/integrated area navigation (IRNAV), vertical deviation

Horizontal deviation — the approach aid in use should be recorded. For auto land/Category III operations, each system should be recorded.

ILS/GPS/GLS localiser

MLS azimuth

GNSS approach path/IRNAV lateral deviation

Distance measuring equipment (DME) 1 and 2 distances

Distance to runway threshold (GLS)

Distance to missed approach point (IRNAV/IAN)

Ground proximity warning system (GPWS)/terrain awareness warning system (TAWS)/ground collision avoidance system (GCAS) status:

Selection of terrain display mode, including pop-up display status

Terrain alerts, including cautions and warnings and advisories

On/off switch position

Angle of attack

Low pressure warning (each system ):

Hydraulic pressure

Pneumatic pressure

Ground speed

Landing gear:

Landing gear position

Gear selector position

Navigation data:

Drift angle

Wind speed

Wind direction

Latitude

Longitude

GNSS augmentation in use

Brakes:

Left and right brake pressure

Left and right brake pedal position

Additional engine parameters (if not already recorded in parameter 9 of Table 1 of AMC1 CAT.IDE.190.A, and if the aeroplane is equipped with a suitable data source):

Engine pressure ratio (EPR)

N1

Indicated vibration level

N2

Exhaust gas temperature (EGT)

Fuel flow

Fuel cut-off lever position

N3

Traffic alert and collision avoidance system (TCAS)/airborne collision avoidance system (ACAS) — a suitable combination of discretes should be recorded to determine the status of the system:

Combined control

Vertical control

Up advisory

Down advisory

Sensitivity level

Wind shear warning

Selected barometric setting

Pilot selected barometric setting

Co-pilot selected barometric setting

Selected altitude (all pilot selectable modes of operation) — to be recorded for the aeroplane where the parameter is displayed electronically

Selected speed (all pilot selectable modes of operation) — to be recorded for the aeroplane where the parameter is displayed electronically

Selected Mach (all pilot selectable modes of operation) — to be recorded for the aeroplane where the parameter is displayed electronically

Selected vertical speed (all pilot selectable modes of operation) — to be recorded for the aeroplane where the parameter is displayed electronically

Selected heading (all pilot selectable modes of operation) — to be recorded for the aeroplane where the parameter is displayed electronically

Selected flight path (All pilot selectable modes of operation) — to be recorded for the aeroplane where the parameter is displayed electronically

Course/desired track

(DSTRK) Path angle

Coordinates of final approach path (IRNAV/IAN)

Selected decision height — to be recorded for the aeroplane where the parameter is displayed electronically

Electronic flight instrument system (EFIS) display format:

Pilot

Co-pilot

Multi-function/engine/alerts display format

Alternating current (AC) electrical bus status — each bus

Direct current (DC) electrical bus status — each bus

Engine bleed valve position

Auxiliary power unit (APU) bleed valve position

Computer failure — (all critical flight and engine control systems)

Engine thrust command

Engine thrust target

Computed centre of gravity (CG)

Fuel quantity in CG trim tank

Head up display in use

Para visual display on

Operational stall protection, stick shaker and pusher activation

Primary navigation system reference:

GNSS

Inertial navigational system (INS)

VHF omnidirectional radio range

(VOR)/distance measuring equipment

(DME) MLS

Loran C ILS

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

Yaw trim surface position

Roll trim surface position

Yaw or sideslip angle

De-icing and/or anti-icing systems selection

Hydraulic pressure — each system

Loss of cabin pressure

Trim control input position in the flight crew compartment, pitch — when mechanical means for control inputs are not available, displayed trim position or trim command should be recorded.

Trim control input position in the flight crew compartment, roll — when mechanical means for control inputs are not available, displayed trim position or trim command should be recorded.

Trim control input position in the flight crew compartment, yaw — when mechanical means for control inputs are not available, displayed trim position or trim command should be recorded.

All flight control input forces (for fly-by-wire flight control systems, where control surface position is a function of the displacement of the control input device only, it is not necessary to record this parameter):

Control wheel

Control column

Rudder pedal

Event marker

Date