Appendix 1 to JAR-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
JAR–OPS 1 Subpart K SECTION 1
01.09.04 1–K–20 Amendment 7
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
Appendix 1 to JAR-OPS 1.715 (continued)
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
Appendix 1 to JAR-OPS 1.720
Flight data recorders - 2 - List of parameters to be recorded
Table A - Aeroplanes with a maximum certificated take-off mass of over 5 700 Kg
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 unless an alternate means to synchronise FDR and CVR recordings is
provided
9 Power on each engine
10 Trailing edge flap or cockpit control selection
11 Leading edge flap or cockpit control selection
12 Thrust reverse position (for turbojet aeroplanes only)
13 Ground spoiler position and/or speed brake selection
14 Outside air temperature or Total Air Temperature
15a
15b
Autopilot engagement status
Autopilot operating modes, autothrottle and AFCS systems engagement status and operating modes.
Table B - Additional parameters for aeroplanes with a maximum certificated take-off mass over 27 000 kg
No Parameter
16 Longitudinal acceleration
17 Lateral acceleration
18 Primary flight controls - Control surface position and/or pilot input (pitch, roll and yaw)
19 Pitch trim position
20 Radio altitude
21 Glide path deviation
22 Localiser deviation
23 Marker beacon passage
24 Master warning
25 NAV 1 and NAV 2 frequency selection
26 DME 1 and DME 2 distance
SECTION 1 JAR–OPS 1 Subpart K
Amendment 7 1–K–23 01.09.04
27 Landing gear squat switch status
28 Ground proximity warning system
29 Angle of attack
30 Hydraulics, each system (low pressure)
31 Navigation data
32 Landing gear or gear selector position
Appendix 1 to JAR-OPS 1.725
Flight data recorders - 3 - List of parameters to be recorded
Table A - Aeroplanes with a maximum certificated take-off mass of over 5 700 Kg
No Parameter
1 Time or relative time count
2 Pressure altitude
3 Indicated Airspeed
4 Heading
5 Normal Acceleration
Table B – Additional parameters for aeroplanes with a maximum certificated take-off mass of over 27 000 kg
No Parameter
6 Pitch attitude
7 Roll attitude
8 Manual radio transmission keying unless an alternate means to synchronise the FDR and CVR recordings is
provided
9 Power on each engine
10 Trailing edge flap or cockpit control selection
11 Leading edge flap or cockpit control selection
12 Thrust reverse position (for turbojet aeroplanes only)
13 Ground spoiler position and/or speed brake selection
14 Outside air temperature or Total air temperature
15a
15b
Autopilot engagement status
Autopilot operating modes, autothrottle and AFCS, systems engagement status and operating modes.
16 Longitudinal acceleration
17 Lateral acceleration
18 Primary flight controls – Control surface position and/or pilot input (pitch, roll and yaw)
19 Pitch trim position
20 Radio altitude
21 Glide path deviation
22 Localiser deviation
23 Marker beacon passage
24 Master warning
25 NAV 1 and NAV 2 frequency selection
26 DME 1 and DME 2 distance
27 Landing gear squat switch status
28 Ground proximity warning system
29 Angle of attack
30 Hydraulics, each system (low pressure)
31 Navigation data ( latitude, longitude, ground speed and drift angle)
32 Landing gear or gear selector position
Appendix 1 to JAR–OPS 1.770
Oxygen – Minimum Requirements for Supplemental Oxygen for Pressurised Aeroplanes (Note 1)
(a) (b)
SUPPLY FOR: DURATION AND CABIN PRESSURE ALTITUDE
1. All occupants of flight deck seats
on flight deck duty
Entire flight time when the cabin pressure altitude exceeds 13 000 ft and
entire flight time when the cabin pressure altitude exceeds 10 000 ft but
does not exceed 13 000 ft after the first 30 minutes at those altitudes, but
in no case less than:
(i) 30 minutes for aeroplanes certificated to fly at altitudes not exceeding
25 000 ft (Note 2)
(ii) 2 hours for aeroplanes certificated to fly at altitudes more than
25 000 ft (Note 3).
2. All required cabin crew members Entire flight time when cabin pressure altitude exceeds 13 000 ft but not
less than 30 minutes (Note 2), and entire flight time when cabin pressure
altitude is greater than 10 000 ft but does not exceed 13 000 ft after the
first 30 minutes at these altitudes.
3. 100% of passengers (Note 5) Entire flight time when the cabin pressure altitude exceeds 15 000 ft but in
no case less than 10 minutes.(Note 4)
4. 30% of passengers (Note 5) Entire flight time when the cabin pressure altitude exceeds 14 000 ft but
does not exceed 15 000 ft.
5. 10% of passengers (Note 5) Entire flight time when the cabin pressure altitude exceeds 10 000 ft but
does not exceed 14 000 ft after the first 30 minutes at these altitudes.
Note 1: The supply provided must take account of the cabin pressure altitude and descent profile for the routes concerned.
Note 2: The required minimum supply is that quantity of oxygen necessary for a constant rate of descent from the aeroplane’s
maximum certificated operating altitude to 10 000 ft in 10 minutes and followed by 20 minutes at 10 000 ft.
Note 3: The required minimum supply is that quantity of oxygen necessary for a constant rate of descent from the aeroplane’s
maximum certificated operating altitude to 10 000 ft in 10 minutes and followed by 110 minutes at 10 000 ft. The oxygen
required in JAR–OPS 1.780(a)(1) may be included in determining the supply required.
Note 4: The required minimum supply is that quantity of oxygen necessary for a constant rate of descent from the aeroplane’s maximum certificated operating altitude to 15 000 ft in 10 minutes.
Note 5: For the purpose of this table ‘passengers’ means passengers actually carried and includes infants
Appendix 1 to JAR–OPS 1.775
Supplemental Oxygen for non-pressurised Aeroplanes
Table 1
(a) (b)
SUPPLY FOR: DURATION AND PRESSURE ALTITUDE
1. All occupants of flight deck
seats on flight deck duty
Entire flight time at pressure altitudes above 10 000 ft
2. All required cabin crew
members
Entire flight time at pressure altitudes above 13 000 ft and for any period exceeding
30 minutes at pressure altitudes above 10 000 ft but not exceeding 13 000 ft
3. 100% of passengers
(See Note)
Entire flight time at pressure altitudes above 13 000 ft.
4. 10% of passengers
(See Note)
Entire flight time after 30 minutes at pressure altitudes greater than 10 000 ft
but not exceeding 13 000 ft.
Note: For the purpose of this table ‘passengers’ means passengers actually carried and includes infants under the age of 2.
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