Commission Regulation (EC) No 8/2008Show full title

“Appendix 1 to OPS 1.715 Flight data recorders — 1 — List of parameters to be recorded

Table A1 — Aeroplanes with a maximum certificated take-off mass of over 5 700 kg

Note: The number in the left hand column reflect the Serial Numbers depicted in EUROCAE document ED55

No	Parameter
1	TIME OR RELATIVE TIME COUNT
2	PRESSURE ALTITUDE
3	INDICATED AIRSPEED
4	HEADING
5	NORMAL ACCELERATION
6	PITCH ATTITUDE
7	ROLL ATTITUDE
8	MANUAL RADIO TRANSMISSION KEYING
9	PROPULSIVE THRUST/POWER ON EACH ENGINE AND COCKPIT THRUST/POWER LEVER POSITION IF APPLICABLE
10	TRAILING EDGE FLAP OR COCKPIT CONTROL SELECTION
11	LEADING EDGE FLAP OR COCKPIT CONTROL SELECTION
12	THRUST REVERSE STATUS
13	GROUND SPOILER POSITION AND/OR SPEED BRAKE SELECTION
14	TOTAL OR OUTSIDE AIR TEMPERATURE
15	AUTOPILOT, AUTOTHROTTLE AND AFCS MODE AND ENGAGEMENT STATUS
16	LONGITUDINAL ACCELERATION (BODY AXIS)
17	LATERAL ACCELERATION

Table A2 — Aeroplanes with a maximum certificated take-off mass of 5 700 kg or below

Note: The number in the left hand column reflect the Serial Numbers depicted in EUROCAE document ED55

No	Parameter
1	TIME OR RELATIVE TIME COUNT
2	PRESSURE ALTITUDE
3	INDICATED AIRSPEED
4	HEADING
5	NORMAL ACCELERATION
6	PITCH ATTITUDE
7	ROLL ATTITUDE
8	MANUAL RADIO TRANSMISSION KEYING
9	PROPULSIVE THRUST/POWER ON EACH ENGINE AND COCKPIT THRUST/POWER LEVER POSITION IF APPLICABLE
10	TRAILING EDGE FLAP OR COCKPIT CONTROL SELECTION
11	LEADING EDGE FLAP OR COCKPIT CONTROL SELECTION
12	THRUST REVERSE STATUS
13	GROUND SPOILER POSITION AND/OR SPEED BRAKE SELECTION
14	TOTAL OR OUTSIDE AIR TEMPERATURE.
15	AUTOPILOT/AUTOTHROTTLE ENGAGEMENT STATUS
16	ANGLE OF ATTACK (IF A SUITABLE SENSOR IS AVAILABLE)
17	LONGITUDINAL ACCELERATION (BODY AXIS)

Table B — Additional parameters for aeroplanes with a maximum certificated take-off mass of over 27 000 kg

Note: The number in the left hand column reflect the Serial Numbers depicted in EUROCAE document ED55

No	Parameter
18	PRIMARY FLIGHT CONTROLS — CONTROL SURFACE POSITION AND/OR PILOT INPUT (PITCH, ROLL, YAW)
19	PITCH TRIM POSITION
20	RADIO ALTITUDE
21	VERTICAL BEAM DEVIATION (ILS GLIDE PATH OR MLS ELEVATION)
22	HORIZONTAL BEAM DEVIATION (ILS LOCALISER OR MLS AZIMUTH)
23	MARKER BEACON PASSAGE
24	WARNINGS
25	RESERVED (NAVIGATION RECEIVER FREQUENCY SELECTION IS RECOMMENDED)
26	RESERVED (DME DISTANCE IS RECOMMENDED)
27	LANDING GEAR SQUAT SWITCH STATUS OR AIR/GROUND STATUS
28	GROUND PROXIMITY WARNING SYSTEM
29	ANGLE OF ATTACK
30	LOW PRESSURE WARNING (HYDRAULIC AND PNEUMATIC POWER)
31	GROUNDSPEED
32	LANDING GEAR OR GEAR SELECTOR POSITION

Table C — Aeroplanes equipped with electronic display systems

Note: The number in the centre column reflect the Serial Numbers depicted in EUROCAE document ED55 table A1.5

No	No	Parameter
33	6	SELECTED BAROMETRIC SETTING (EACH PILOT STATION)
34	7	SELECTED ALTITUDE
35	8	SELECTED SPEED
36	9	SELECTED MACH
37	10	SELECTED VERTICAL SPEED
38	11	SELECTED HEADING
39	12	SELECTED FLIGHT PATH
40	13	SELECTED DECISION HEIGHT
41	14	EFIS DISPLAY FORMAT
42	15	MULTI FUNCTION/ENGINE/ALERTS DISPLAY FORMAT