AMC6 CAT.IDE.A.190 Flight data recorder

• ED Decision 2019/019/R found in: Air Operations (965/2012) Part-ARO Part-ORO Part-CAT Part-SPA Part-NCC Part-NCO Part-SPO (Feb 2025)

AMC6 CAT.IDE.A.190 Flight data recorder ED Decision 2019/019/R LIST OF PARAMETERS TO BE RECORDED FOR AEROPLANES FIRST ISSUED WITH AN INDIVIDUAL CofA BEFORE 1 JUNE 1990 (a) The FDR should, with reference to a timescale, record: (1) the parameters listed in Table 1 below; (2) the additional parameters 6 to 15b of Table 2 below, for aeroplanes with an MCTOM exceeding 5 700 kg but not exceeding 27 000 kg and first issued with an individual CofA on or after 1 January 1989, when the following conditions are met: (i) sufficient capacity is available on a flight recorder system; (ii) the sensor is readily available; and (iii) a change is not required in the equipment that generates the data; (3) the additional parameters from 6 to 15b of Table 2 below, for aeroplanes with a maximum certificated take-off mass exceeding 27 000 kg that are of a type first type certified after 30 September 1969; and (4) the additional parameters listed in Table 2 below for aeroplanes with an MCTOM exceeding 27 000 kg and first issued with an individual CofA on or after 1 January 1987, when the following conditions are met: (i) sufficient capacity is available on a flight recorder system; (ii) the sensor is readily available; and (iii) a change is not required in the equipment that generates the data. (b) The FDR of aeroplanes with an MCTOM exceeding 27 000 kg that are of a type first type certified after 30 September 1969 does not need to record the parameters 13, 14 and 15b in Table 2 below, when any of the following conditions are met: (1) sufficient capacity is not available on a flight recorder system; (2) the sensor is not readily available; and (3) a change is required in the equipment that generates the data. (c) The parameters to be recorded should meet, as far as practicable, the performance specifications (range, sampling intervals, accuracy limits, and resolution in read-out) defined in Table 1 of [AMC5 CAT.IDE.A.190](#_DxCrossRefBm927678994)). (d) When so determined by the Agency, the FDR does not need to record individual parameters that can be derived by calculation from the other recorded parameters. Table 1 Flight data recorder — aeroplanes with an MCTOM exceeding 5 700 kg <table border="1" cellpadding="0" cellspacing="0" width="606"><thead><tr><td valign="top" width="40"><p><b>No</b></p></td><td valign="top" width="565"><p><b>Parameter</b></p></td></tr></thead><tr><td valign="top" width="40"><p>1</p></td><td valign="top" width="565"><p>Time or relative time count</p></td></tr><tr><td valign="top" width="40"><p>2</p></td><td valign="top" width="565"><p>Pressure altitude</p></td></tr><tr><td valign="top" width="40"><p>3</p></td><td valign="top" width="565"><p>Indicated airspeed or calibrated airspeed</p></td></tr><tr><td valign="top" width="40"><p>4</p></td><td valign="top" width="565"><p>Heading</p></td></tr><tr><td valign="top" width="40"><p>5</p></td><td valign="top" width="565"><p>Normal acceleration</p></td></tr></table> \* The number in the left hand column reflects the serial number depicted in EUROCAE Document ED-112. Table 2 Additional parameters for aeroplanes under conditions of AMC6 CAT.IDE.A.190, 1 & 2 <table border="1" cellpadding="0" cellspacing="0" width="607"><thead><tr><td valign="top" width="40"><p><b>No</b></p></td><td valign="top" width="566"><p><b>Parameter</b></p></td></tr></thead><tr><td valign="top" width="40"><p>6</p></td><td valign="top" width="566"><p>Pitch attitude</p></td></tr><tr><td valign="top" width="40"><p>7</p></td><td valign="top" width="566"><p>Roll attitude</p></td></tr><tr><td valign="top" width="40"><p>8</p></td><td valign="top" width="566"><p>Manual radio transmission keying unless an alternate means to synchronise the FDR and CVR recordings is provided</p></td></tr><tr><td valign="top" width="40"><p>9</p></td><td valign="top" width="566"><p>Power on each engine</p></td></tr><tr><td valign="top" width="40"><p>10</p></td><td valign="top" width="566"><p>Trailing edge flap or flight crew compartment control selection</p></td></tr><tr><td valign="top" width="40"><p>11</p></td><td valign="top" width="566"><p>Leading edge flap or flight crew compartment control selection</p></td></tr><tr><td valign="top" width="40"><p>12</p></td><td valign="top" width="566"><p>Thrust reverse position (for turbojet aeroplanes only)</p></td></tr><tr><td valign="top" width="40"><p>13</p></td><td valign="top" width="566"><p>Ground spoiler position and/or speed brake selection</p></td></tr><tr><td valign="top" width="40"><p>14</p></td><td valign="top" width="566"><p>Outside air temperature (OAT) or total air temperature</p></td></tr><tr><td valign="top" width="40"><p>15a</p><p>15b</p></td><td valign="top" width="566"><p>Autopilot engagement status</p><p>Autopilot operating modes, autothrottle and AFCS, systems engagement status and operating modes.</p></td></tr><tr><td valign="top" width="40"><p>16</p></td><td valign="top" width="566"><p>Longitudinal acceleration</p></td></tr><tr><td valign="top" width="40"><p>17</p></td><td valign="top" width="566"><p>Lateral acceleration</p></td></tr><tr><td valign="top" width="40"><p>18</p></td><td valign="top" width="566"><p>Primary flight controls — control surface position and/or pilot input (pitch, roll and yaw)</p></td></tr><tr><td valign="top" width="40"><p>19</p></td><td valign="top" width="566"><p>Pitch trim position</p></td></tr><tr><td valign="top" width="40"><p>20</p></td><td valign="top" width="566"><p>Radio altitude</p></td></tr><tr><td valign="top" width="40"><p>21</p></td><td valign="top" width="566"><p>Glide path deviation</p></td></tr><tr><td valign="top" width="40"><p>22</p></td><td valign="top" width="566"><p>Localiser deviation</p></td></tr><tr><td valign="top" width="40"><p>23</p></td><td valign="top" width="566"><p>Marker beacon passage</p></td></tr><tr><td valign="top" width="40"><p>24</p></td><td valign="top" width="566"><p>Master warning</p></td></tr><tr><td valign="top" width="40"><p>25</p></td><td valign="top" width="566"><p>NAV 1 and NAV 2 frequency selection</p></td></tr><tr><td valign="top" width="40"><p>26</p></td><td valign="top" width="566"><p>DME 1 and DME 2 distance</p></td></tr><tr><td valign="top" width="40"><p>27</p></td><td valign="top" width="566"><p>Landing gear squat switch status</p></td></tr><tr><td valign="top" width="40"><p>28</p></td><td valign="top" width="566"><p>Ground proximity warning system (GPWS)</p></td></tr><tr><td valign="top" width="40"><p>29</p></td><td valign="top" width="566"><p>Angle of attack</p></td></tr><tr><td valign="top" width="40"><p>30</p></td><td valign="top" width="566"><p>Hydraulics, each system (low pressure)</p></td></tr><tr><td valign="top" width="40"><p>31</p></td><td valign="top" width="566"><p>Navigation data (latitude, longitude, ground speed and drift angle)</p></td></tr><tr><td valign="top" width="40"><p>32</p></td><td valign="top" width="566"><p>Landing gear or gear selector position</p></td></tr></table> \* The number in the left hand column reflects the serial number depicted in EUROCAE Document ED-112. AMC6 CAT.IDE.A.190 Flight data recorder ED Decision 2019/019/R LIST OF PARAMETERS TO BE RECORDED FOR AEROPLANES FIRST ISSUED WITH AN INDIVIDUAL CofA BEFORE 1 JUNE 1990 (a) The FDR should, with reference to a timescale, record: (1) the parameters listed in Table 1 below; (2) the additional parameters 6 to 15b of Table 2 below, for aeroplanes with an MCTOM exceeding 5 700 kg but not exceeding 27 000 kg and first issued with an individual CofA on or after 1 January 1989, when the following conditions are met: (i) sufficient capacity is available on a flight recorder system; (ii) the sensor is readily available; and (iii) a change is not required in the equipment that generates the data; (3) the additional parameters from 6 to 15b of Table 2 below, for aeroplanes with a maximum certificated take-off mass exceeding 27 000 kg that are of a type first type certified after 30 September 1969; and (4) the additional parameters listed in Table 2 below for aeroplanes with an MCTOM exceeding 27 000 kg and first issued with an individual CofA on or after 1 January 1987, when the following conditions are met: (i) sufficient capacity is available on a flight recorder system; (ii) the sensor is readily available; and (iii) a change is not required in the equipment that generates the data. (b) The FDR of aeroplanes with an MCTOM exceeding 27 000 kg that are of a type first type certified after 30 September 1969 does not need to record the parameters 13, 14 and 15b in Table 2 below, when any of the following conditions are met: (1) sufficient capacity is not available on a flight recorder system; (2) the sensor is not readily available; and (3) a change is required in the equipment that generates the data. (c) The parameters to be recorded should meet, as far as practicable, the performance specifications (range, sampling intervals, accuracy limits, and resolution in read-out) defined in Table 1 of [AMC5 CAT.IDE.A.190](#_DxCrossRefBm318086614)). (d) When so determined by the Agency, the FDR does not need to record individual parameters that can be derived by calculation from the other recorded parameters. Table 1 Flight data recorder — aeroplanes with an MCTOM exceeding 5 700 kg <table border="1" cellpadding="0" cellspacing="0" width="606"><thead><tr><td valign="top" width="40"><p><b>No</b></p></td><td valign="top" width="565"><p><b>Parameter</b></p></td></tr></thead><tr><td valign="top" width="40"><p>1</p></td><td valign="top" width="565"><p>Time or relative time count</p></td></tr><tr><td valign="top" width="40"><p>2</p></td><td valign="top" width="565"><p>Pressure altitude</p></td></tr><tr><td valign="top" width="40"><p>3</p></td><td valign="top" width="565"><p>Indicated airspeed or calibrated airspeed</p></td></tr><tr><td valign="top" width="40"><p>4</p></td><td valign="top" width="565"><p>Heading</p></td></tr><tr><td valign="top" width="40"><p>5</p></td><td valign="top" width="565"><p>Normal acceleration</p></td></tr></table> \* The number in the left hand column reflects the serial number depicted in EUROCAE Document ED-112. Table 2 Additional parameters for aeroplanes under conditions of AMC6 CAT.IDE.A.190, 1 & 2 <table border="1" cellpadding="0" cellspacing="0" width="607"><thead><tr><td valign="top" width="40"><p><b>No</b></p></td><td valign="top" width="566"><p><b>Parameter</b></p></td></tr></thead><tr><td valign="top" width="40"><p>6</p></td><td valign="top" width="566"><p>Pitch attitude</p></td></tr><tr><td valign="top" width="40"><p>7</p></td><td valign="top" width="566"><p>Roll attitude</p></td></tr><tr><td valign="top" width="40"><p>8</p></td><td valign="top" width="566"><p>Manual radio transmission keying unless an alternate means to synchronise the FDR and CVR recordings is provided</p></td></tr><tr><td valign="top" width="40"><p>9</p></td><td valign="top" width="566"><p>Power on each engine</p></td></tr><tr><td valign="top" width="40"><p>10</p></td><td valign="top" width="566"><p>Trailing edge flap or flight crew compartment control selection</p></td></tr><tr><td valign="top" width="40"><p>11</p></td><td valign="top" width="566"><p>Leading edge flap or flight crew compartment control selection</p></td></tr><tr><td valign="top" width="40"><p>12</p></td><td valign="top" width="566"><p>Thrust reverse position (for turbojet aeroplanes only)</p></td></tr><tr><td valign="top" width="40"><p>13</p></td><td valign="top" width="566"><p>Ground spoiler position and/or speed brake selection</p></td></tr><tr><td valign="top" width="40"><p>14</p></td><td valign="top" width="566"><p>Outside air temperature (OAT) or total air temperature</p></td></tr><tr><td valign="top" width="40"><p>15a</p><p>15b</p></td><td valign="top" width="566"><p>Autopilot engagement status</p><p>Autopilot operating modes, autothrottle and AFCS, systems engagement status and operating modes.</p></td></tr><tr><td valign="top" width="40"><p>16</p></td><td valign="top" width="566"><p>Longitudinal acceleration</p></td></tr><tr><td valign="top" width="40"><p>17</p></td><td valign="top" width="566"><p>Lateral acceleration</p></td></tr><tr><td valign="top" width="40"><p>18</p></td><td valign="top" width="566"><p>Primary flight controls — control surface position and/or pilot input (pitch, roll and yaw)</p></td></tr><tr><td valign="top" width="40"><p>19</p></td><td valign="top" width="566"><p>Pitch trim position</p></td></tr><tr><td valign="top" width="40"><p>20</p></td><td valign="top" width="566"><p>Radio altitude</p></td></tr><tr><td valign="top" width="40"><p>21</p></td><td valign="top" width="566"><p>Glide path deviation</p></td></tr><tr><td valign="top" width="40"><p>22</p></td><td valign="top" width="566"><p>Localiser deviation</p></td></tr><tr><td valign="top" width="40"><p>23</p></td><td valign="top" width="566"><p>Marker beacon passage</p></td></tr><tr><td valign="top" width="40"><p>24</p></td><td valign="top" width="566"><p>Master warning</p></td></tr><tr><td valign="top" width="40"><p>25</p></td><td valign="top" width="566"><p>NAV 1 and NAV 2 frequency selection</p></td></tr><tr><td valign="top" width="40"><p>26</p></td><td valign="top" width="566"><p>DME 1 and DME 2 distance</p></td></tr><tr><td valign="top" width="40"><p>27</p></td><td valign="top" width="566"><p>Landing gear squat switch status</p></td></tr><tr><td valign="top" width="40"><p>28</p></td><td valign="top" width="566"><p>Ground proximity warning system (GPWS)</p></td></tr><tr><td valign="top" width="40"><p>29</p></td><td valign="top" width="566"><p>Angle of attack</p></td></tr><tr><td valign="top" width="40"><p>30</p></td><td valign="top" width="566"><p>Hydraulics, each system (low pressure)</p></td></tr><tr><td valign="top" width="40"><p>31</p></td><td valign="top" width="566"><p>Navigation data (latitude, longitude, ground speed and drift angle)</p></td></tr><tr><td valign="top" width="40"><p>32</p></td><td valign="top" width="566"><p>Landing gear or gear selector position</p></td></tr></table> \* The number in the left hand column reflects the serial number depicted in EUROCAE Document ED-112. ##### AMC6 CAT.IDE.A.190 Flight data recorder *ED Decision 2019/019/R* **LIST OF PARAMETERS TO BE RECORDED FOR AEROPLANES FIRST ISSUED WITH AN INDIVIDUAL CofA BEFORE 1 JUNE 1990** (a) The FDR should, with reference to a timescale, record: (1) the parameters listed in Table 1 below; (2) the additional parameters 6 to 15b of Table 2 below, for aeroplanes with an MCTOM exceeding 5 700 kg but not exceeding 27 000 kg and first issued with an individual CofA on or after 1 January 1989, when the following conditions are met: (i) sufficient capacity is available on a flight recorder system; (ii) the sensor is readily available; and (iii) a change is not required in the equipment that generates the data; (3) the additional parameters from 6 to 15b of Table 2 below, for aeroplanes with a maximum certificated take-off mass exceeding 27 000 kg that are of a type first type certified after 30 September 1969; and (4) the additional parameters listed in Table 2 below for aeroplanes with an MCTOM exceeding 27 000 kg and first issued with an individual CofA on or after 1 January 1987, when the following conditions are met: (i) sufficient capacity is available on a flight recorder system; (ii) the sensor is readily available; and (iii) a change is not required in the equipment that generates the data. (b) The FDR of aeroplanes with an MCTOM exceeding 27 000 kg that are of a type first type certified after 30 September 1969 does not need to record the parameters 13, 14 and 15b in Table 2 below, when any of the following conditions are met: (1) sufficient capacity is not available on a flight recorder system; (2) the sensor is not readily available; and (3) a change is required in the equipment that generates the data. (c) The parameters to be recorded should meet, as far as practicable, the performance specifications (range, sampling intervals, accuracy limits, and resolution in read-out) defined in Table 1 of [AMC5 CAT.IDE.A.190](#_DxCrossRefBm523088555)). (d) When so determined by the Agency, the FDR does not need to record individual parameters that can be derived by calculation from the other recorded parameters. ***Table 1*** Flight data recorder — aeroplanes with an MCTOM exceeding 5 700 kg <table bgcolor="#d9d9d9" cellpadding="7" cellspacing="0"> <col/> <col/> <thead> <tr valign="top"> <td bgcolor="#808080"><p align="left"> <b>No</b></p> </td> <td bgcolor="#808080"><p align="left"> <b>Parameter</b></p> </td> </tr> </thead> <tbody> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Time or relative time count</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Pressure altitude</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 3</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Indicated airspeed or calibrated airspeed</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 4</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Heading</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 5</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Normal acceleration</p> </td> </tr> </tbody> </table> \* The number in the left hand column reflects the serial number depicted in EUROCAE Document ED-112. ***Table 2*** Additional parameters for aeroplanes under conditions of AMC6 CAT.IDE.A.190, 1 & 2 <table bgcolor="#d9d9d9" cellpadding="7" cellspacing="0"> <col/> <col/> <thead> <tr valign="top"> <td bgcolor="#808080"><p align="left"> <b>No</b></p> </td> <td bgcolor="#808080"><p align="left"> <b>Parameter</b></p> </td> </tr> </thead> <tbody> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 6</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Pitch attitude</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 7</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Roll attitude</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 8</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Manual radio transmission keying unless an alternate means to synchronise the FDR and CVR recordings is provided</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 9</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Power on each engine</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 10</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Trailing edge flap or flight crew compartment control selection</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 11</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Leading edge flap or flight crew compartment control selection</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 12</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Thrust reverse position (for turbojet aeroplanes only)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 13</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Ground spoiler position and/or speed brake selection</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 14</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Outside air temperature (OAT) or total air temperature</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 15a</p> <p align="left">15b</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Autopilot engagement status</p> <p align="left">Autopilot operating modes, autothrottle and AFCS, systems engagement status and operating modes.</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 16</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Longitudinal acceleration</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 17</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Lateral acceleration</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 18</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Primary flight controls — control surface position and/or pilot input (pitch, roll and yaw)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 19</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Pitch trim position</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 20</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Radio altitude</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 21</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Glide path deviation</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 22</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Localiser deviation</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 23</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Marker beacon passage</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 24</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Master warning</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 25</p> </td> <td bgcolor="#d9d9d9"><p align="left"> NAV 1 and NAV 2 frequency selection</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 26</p> </td> <td bgcolor="#d9d9d9"><p align="left"> DME 1 and DME 2 distance</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 27</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Landing gear squat switch status</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 28</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Ground proximity warning system (GPWS)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 29</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Angle of attack</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 30</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Hydraulics, each system (low pressure)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 31</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Navigation data (latitude, longitude, ground speed and drift angle)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 32</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Landing gear or gear selector position</p> </td> </tr> </tbody> </table> \* The number in the left hand column reflects the serial number depicted in EUROCAE Document ED-112.