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Commission Regulation (EC) No 8/2008Show full title
Commission Regulation (EC) No 8/2008 of 11 December 2007 amending Council Regulation (EEC) No 3922/91 as regards common technical requirements and administrative procedures applicable to commercial transportation by aeroplane (Text with EEA relevance)
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- Regulations originating from the EU
- 2008 No. 8
- ANNEX
- Division Appendix 1 to OPS 1.715
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“Appendix 1 to OPS 1.715Flight data recorders — 1 — List of parameters to be recorded
Table A1 — Aeroplanes with a maximum certificated take-off mass of over 5 700 kgU.K.
Note: The number in the left hand column reflect the Serial Numbers depicted in EUROCAE document ED55U.K.
| 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 belowU.K.
Note: The number in the left hand column reflect the Serial Numbers depicted in EUROCAE document ED55U.K.
| 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 kgU.K.
Note: The number in the left hand column reflect the Serial Numbers depicted in EUROCAE document ED55U.K.
| 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 systemsU.K.
Note: The number in the centre column reflect the Serial Numbers depicted in EUROCAE document ED55 table A1.5U.K.
| 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 |
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