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AMC2 CAT.IDE.H.190 Flight data recorder
Available versions for ERULES-1963177438-12617
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 (Sep 2023)
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AMC2 CAT.IDE.H.190 Flight data recorder ED Decision 2019/019/R LIST OF PARAMETERS TO BE RECORDED FOR HELICOPTERS HAVING AN MCTOM OF MORE THAN 3 175 KG AND FIRST ISSUED WITH AN INDIVIDUAL COFA ON OR AFTER 1 AUGUST 1999 AND BEFORE 1 JANUARY 2016 AND HELICOPTERS HAVING AN MCTOM OF MORE THAN 7 000 KG OR AN MOPSC OF MORE THAN 9 AND FIRST ISSUED WITH AN INDIVIDUAL COFA ON OR AFTER 1 JANUARY 1989 AND BEFORE 1 AUGUST 1999 (a) The FDR should, with reference to a timescale, record: (1) for helicopters with an MCTOM between 3 175 kg and 7 000 kg the parameters listed in Table 1 below; (2) for helicopters with an MCTOM of more than 7 000 kg the parameters listed in Table 2 below; (3) for helicopters equipped with electronic display systems, the additional parameters listed in Table 3 below; and (4) any dedicated parameters relating to novel or unique design or operational characteristics of the helicopter. (b) The FDR of helicopters with an MCTOM of more than 7 000 kg does not need to record parameter 19 of Table 2 below, if any of the following conditions are met: (1) the sensor is not readily available; or (2) a change is required in the equipment that generates the data. (c) Individual parameters that can be derived by calculation from the other recorded parameters need not to be recorded, if agreed by the competent authority. (d) The parameters should meet, as far as practicable, the performance specifications (range, sampling intervals, accuracy limits and resolution in read-out) defined in [AMC3 CAT.IDE.H.190](#_DxCrossRefBm318086778). (e) If recording capacity is available, as many of the additional parameters as possible specified in table II-A.2 of EUROCAE Document ED 112 dated March 2003 should be recorded. (f) For the purpose of this AMC, a sensor is considered ‘readily available’ when it is already available or can be easily incorporated. Table 1 Helicopters with an MCTOM of 7 000 kg or less <table border="1" cellpadding="0" cellspacing="0" width="605"><thead><tr><td valign="top" width="40"><p><b>No</b></p></td><td valign="top" width="564"><p><b>Parameter</b></p></td></tr></thead><tr><td valign="top" width="40"><p>1</p></td><td valign="top" width="564"><p>Time or relative time count</p></td></tr><tr><td valign="top" width="40"><p>2</p></td><td valign="top" width="564"><p>Pressure altitude</p></td></tr><tr><td valign="top" width="40"><p>3</p></td><td valign="top" width="564"><p>Indicated airspeed or calibrated airspeed</p></td></tr><tr><td valign="top" width="40"><p>4</p></td><td valign="top" width="564"><p>Heading</p></td></tr><tr><td valign="top" width="40"><p>5</p></td><td valign="top" width="564"><p>Normal acceleration</p></td></tr><tr><td valign="top" width="40"><p>6</p></td><td valign="top" width="564"><p>Pitch attitude</p></td></tr><tr><td valign="top" width="40"><p>7</p></td><td valign="top" width="564"><p>Roll attitude</p></td></tr><tr><td valign="top" width="40"><p>8</p></td><td valign="top" width="564"><p>Manual radio transmission keying</p></td></tr><tr><td valign="top" width="40"><p>9</p></td><td valign="top" width="564"><p>Power on each engine (free power turbine speed and engine torque)/cockpit power control position (if applicable)</p></td></tr><tr><td valign="top" width="40"><p>10a</p><p>10b</p></td><td valign="top" width="564"><p>Main rotor speed</p><p>Rotor brake (if installed)</p></td></tr><tr><td valign="top" width="40"><p>11</p><p>11a</p><p>11b</p><p>11c</p><p>11d</p><p>11e</p><p>11f</p></td><td valign="top" width="564"><p>Primary flight controls — pilot input and control output position (if applicable)</p><p>Collective pitch</p><p>Longitudinal cyclic pitch</p><p>Lateral cyclic pitch</p><p>Tail rotor pedal</p><p>Controllable stabiliser</p><p>Hydraulic selection</p></td></tr><tr><td valign="top" width="40"><p>13</p></td><td valign="top" width="564"><p>Outside air temperature</p></td></tr><tr><td valign="top" width="40"><p>14</p></td><td valign="top" width="564"><p>Autopilot engagement status</p></td></tr><tr><td valign="top" width="40"><p>15</p></td><td valign="top" width="564"><p>Stability augmentation system engagement</p></td></tr><tr><td valign="top" width="40"><p>26</p></td><td valign="top" width="564"><p>Warnings</p></td></tr></table> Table 2 Helicopters with an MCTOM of more than 7 000 kg <table border="1" cellpadding="0" cellspacing="0" width="605"><thead><tr><td valign="top" width="40"><p><b>No</b></p></td><td valign="top" width="564"><p><b>Parameter</b></p></td></tr></thead><tr><td valign="top" width="40"><p>1</p></td><td valign="top" width="564"><p>Time or relative time count</p></td></tr><tr><td valign="top" width="40"><p>2</p></td><td valign="top" width="564"><p>Pressure altitude</p></td></tr><tr><td valign="top" width="40"><p>3</p></td><td valign="top" width="564"><p>Indicated airspeed or calibrated airspeed</p></td></tr><tr><td valign="top" width="40"><p>4</p></td><td valign="top" width="564"><p>Heading</p></td></tr><tr><td valign="top" width="40"><p>5</p></td><td valign="top" width="564"><p>Normal acceleration</p></td></tr><tr><td valign="top" width="40"><p>6</p></td><td valign="top" width="564"><p>Pitch attitude</p></td></tr><tr><td valign="top" width="40"><p>7</p></td><td valign="top" width="564"><p>Roll attitude</p></td></tr><tr><td valign="top" width="40"><p>8</p></td><td valign="top" width="564"><p>Manual radio transmission keying</p></td></tr><tr><td valign="top" width="40"><p>9</p></td><td valign="top" width="564"><p>Power on each engine (free power turbine speed and engine torque)/cockpit power control position (if applicable)</p></td></tr><tr><td valign="top" width="40"><p>10a</p><p>10b</p></td><td valign="top" width="564"><p>Main rotor speed</p><p>Rotor brake (if installed)</p></td></tr><tr><td valign="top" width="40"><p>11</p><p>11a</p><p>11b</p><p>11c</p><p>11d</p><p>11e</p><p>11f</p></td><td valign="top" width="564"><p>Primary flight controls — pilot input and control output position (if applicable)</p><p>Collective pitch</p><p>Longitudinal cyclic pitch</p><p>Lateral cyclic pitch</p><p>Tail rotor pedal</p><p>Controllable stabiliser</p><p>Hydraulic selection</p></td></tr><tr><td valign="top" width="40"><p>12</p></td><td valign="top" width="564"><p>Hydraulics low pressure</p></td></tr><tr><td valign="top" width="40"><p>13</p></td><td valign="top" width="564"><p>Outside air temperature</p></td></tr><tr><td valign="top" width="40"><p>14</p></td><td valign="top" width="564"><p>AFCS mode and engagement status</p></td></tr><tr><td valign="top" width="40"><p>15</p></td><td valign="top" width="564"><p>Stability augmentation system engagement</p></td></tr><tr><td valign="top" width="40"><p>16</p></td><td valign="top" width="564"><p>Main gear box oil pressure</p></td></tr><tr><td valign="top" width="40"><p>17</p></td><td valign="top" width="564"><p>Main gear box oil temperature</p></td></tr><tr><td valign="top" width="40"><p>18</p></td><td valign="top" width="564"><p>Yaw rate or yaw acceleration</p></td></tr><tr><td valign="top" width="40"><p>19</p></td><td valign="top" width="564"><p>Indicated sling load force (if installed)</p></td></tr><tr><td valign="top" width="40"><p>20</p></td><td valign="top" width="564"><p>Longitudinal acceleration (body axis)</p></td></tr><tr><td valign="top" width="40"><p>21</p></td><td valign="top" width="564"><p>Lateral acceleration</p></td></tr><tr><td valign="top" width="40"><p>22</p></td><td valign="top" width="564"><p>Radio altitude</p></td></tr><tr><td valign="top" width="40"><p>23</p></td><td valign="top" width="564"><p>Vertical beam deviation (ILS glide path or MLS elevation)</p></td></tr><tr><td valign="top" width="40"><p>24</p></td><td valign="top" width="564"><p>Horizontal beam deviation (ILS localiser or MLS azimuth)</p></td></tr><tr><td valign="top" width="40"><p>25</p></td><td valign="top" width="564"><p>Marker beacon passage</p></td></tr><tr><td valign="top" width="40"><p>26</p></td><td valign="top" width="564"><p>Warnings</p></td></tr><tr><td valign="top" width="40"><p>27</p></td><td valign="top" width="564"><p>Reserved (navigation receiver frequency selection is recommended)</p></td></tr><tr><td valign="top" width="40"><p>28</p></td><td valign="top" width="564"><p>Reserved (DME distance is recommended)</p></td></tr><tr><td valign="top" width="40"><p>29</p></td><td valign="top" width="564"><p>Reserved (navigation data are recommended)</p></td></tr><tr><td valign="top" width="40"><p>30</p></td><td valign="top" width="564"><p>Landing gear or gear selector position</p></td></tr></table> Table 3 Helicopters equipped with electronic display systems <table border="1" cellpadding="0" cellspacing="0" width="605"><tr><td valign="top" width="40"><p><b>No</b></p></td><td valign="top" width="564"><p><b>Parameter</b></p></td></tr><tr><td valign="top" width="40"><p>38</p></td><td valign="top" width="564"><p>Selected barometric setting (each pilot station)</p></td></tr><tr><td valign="top" width="40"><p>39</p></td><td valign="top" width="564"><p>Selected altitude</p></td></tr><tr><td valign="top" width="40"><p>40</p></td><td valign="top" width="564"><p>Selected speed</p></td></tr><tr><td valign="top" width="40"><p>41</p></td><td valign="top" width="564"><p>Selected Mach</p></td></tr><tr><td valign="top" width="40"><p>42</p></td><td valign="top" width="564"><p>Selected vertical speed</p></td></tr><tr><td valign="top" width="40"><p>43</p></td><td valign="top" width="564"><p>Selected heading</p></td></tr><tr><td valign="top" width="40"><p>44</p></td><td valign="top" width="564"><p>Selected flight path</p></td></tr><tr><td valign="top" width="40"><p>45</p></td><td valign="top" width="564"><p>Selected decision height</p></td></tr><tr><td valign="top" width="40"><p>46</p></td><td valign="top" width="564"><p>EFIS display format</p></td></tr><tr><td valign="top" width="40"><p>47</p></td><td valign="top" width="564"><p>Multi-function/engine/alerts display format</p></td></tr></table>
AMC2 CAT.IDE.H.190 Flight data recorder ED Decision 2019/019/R LIST OF PARAMETERS TO BE RECORDED FOR HELICOPTERS HAVING AN MCTOM OF MORE THAN 3 175 KG AND FIRST ISSUED WITH AN INDIVIDUAL COFA ON OR AFTER 1 AUGUST 1999 AND BEFORE 1 JANUARY 2016 AND HELICOPTERS HAVING AN MCTOM OF MORE THAN 7 000 KG OR AN MOPSC OF MORE THAN 9 AND FIRST ISSUED WITH AN INDIVIDUAL COFA ON OR AFTER 1 JANUARY 1989 AND BEFORE 1 AUGUST 1999 (a) The FDR should, with reference to a timescale, record: (1) for helicopters with an MCTOM between 3 175 kg and 7 000 kg the parameters listed in Table 1 below; (2) for helicopters with an MCTOM of more than 7 000 kg the parameters listed in Table 2 below; (3) for helicopters equipped with electronic display systems, the additional parameters listed in Table 3 below; and (4) any dedicated parameters relating to novel or unique design or operational characteristics of the helicopter. (b) The FDR of helicopters with an MCTOM of more than 7 000 kg does not need to record parameter 19 of Table 2 below, if any of the following conditions are met: (1) the sensor is not readily available; or (2) a change is required in the equipment that generates the data. (c) Individual parameters that can be derived by calculation from the other recorded parameters need not to be recorded, if agreed by the competent authority. (d) The parameters should meet, as far as practicable, the performance specifications (range, sampling intervals, accuracy limits and resolution in read-out) defined in [AMC3 CAT.IDE.H.190](#_DxCrossRefBm927679158). (e) If recording capacity is available, as many of the additional parameters as possible specified in table II-A.2 of EUROCAE Document ED 112 dated March 2003 should be recorded. (f) For the purpose of this AMC, a sensor is considered ‘readily available’ when it is already available or can be easily incorporated. Table 1 Helicopters with an MCTOM of 7 000 kg or less <table border="1" cellpadding="0" cellspacing="0" width="605"><thead><tr><td valign="top" width="40"><p><b>No</b></p></td><td valign="top" width="564"><p><b>Parameter</b></p></td></tr></thead><tr><td valign="top" width="40"><p>1</p></td><td valign="top" width="564"><p>Time or relative time count</p></td></tr><tr><td valign="top" width="40"><p>2</p></td><td valign="top" width="564"><p>Pressure altitude</p></td></tr><tr><td valign="top" width="40"><p>3</p></td><td valign="top" width="564"><p>Indicated airspeed or calibrated airspeed</p></td></tr><tr><td valign="top" width="40"><p>4</p></td><td valign="top" width="564"><p>Heading</p></td></tr><tr><td valign="top" width="40"><p>5</p></td><td valign="top" width="564"><p>Normal acceleration</p></td></tr><tr><td valign="top" width="40"><p>6</p></td><td valign="top" width="564"><p>Pitch attitude</p></td></tr><tr><td valign="top" width="40"><p>7</p></td><td valign="top" width="564"><p>Roll attitude</p></td></tr><tr><td valign="top" width="40"><p>8</p></td><td valign="top" width="564"><p>Manual radio transmission keying</p></td></tr><tr><td valign="top" width="40"><p>9</p></td><td valign="top" width="564"><p>Power on each engine (free power turbine speed and engine torque)/cockpit power control position (if applicable)</p></td></tr><tr><td valign="top" width="40"><p>10a</p><p>10b</p></td><td valign="top" width="564"><p>Main rotor speed</p><p>Rotor brake (if installed)</p></td></tr><tr><td valign="top" width="40"><p>11</p><p>11a</p><p>11b</p><p>11c</p><p>11d</p><p>11e</p><p>11f</p></td><td valign="top" width="564"><p>Primary flight controls — pilot input and control output position (if applicable)</p><p>Collective pitch</p><p>Longitudinal cyclic pitch</p><p>Lateral cyclic pitch</p><p>Tail rotor pedal</p><p>Controllable stabiliser</p><p>Hydraulic selection</p></td></tr><tr><td valign="top" width="40"><p>13</p></td><td valign="top" width="564"><p>Outside air temperature</p></td></tr><tr><td valign="top" width="40"><p>14</p></td><td valign="top" width="564"><p>Autopilot engagement status</p></td></tr><tr><td valign="top" width="40"><p>15</p></td><td valign="top" width="564"><p>Stability augmentation system engagement</p></td></tr><tr><td valign="top" width="40"><p>26</p></td><td valign="top" width="564"><p>Warnings</p></td></tr></table> Table 2 Helicopters with an MCTOM of more than 7 000 kg <table border="1" cellpadding="0" cellspacing="0" width="605"><thead><tr><td valign="top" width="40"><p><b>No</b></p></td><td valign="top" width="564"><p><b>Parameter</b></p></td></tr></thead><tr><td valign="top" width="40"><p>1</p></td><td valign="top" width="564"><p>Time or relative time count</p></td></tr><tr><td valign="top" width="40"><p>2</p></td><td valign="top" width="564"><p>Pressure altitude</p></td></tr><tr><td valign="top" width="40"><p>3</p></td><td valign="top" width="564"><p>Indicated airspeed or calibrated airspeed</p></td></tr><tr><td valign="top" width="40"><p>4</p></td><td valign="top" width="564"><p>Heading</p></td></tr><tr><td valign="top" width="40"><p>5</p></td><td valign="top" width="564"><p>Normal acceleration</p></td></tr><tr><td valign="top" width="40"><p>6</p></td><td valign="top" width="564"><p>Pitch attitude</p></td></tr><tr><td valign="top" width="40"><p>7</p></td><td valign="top" width="564"><p>Roll attitude</p></td></tr><tr><td valign="top" width="40"><p>8</p></td><td valign="top" width="564"><p>Manual radio transmission keying</p></td></tr><tr><td valign="top" width="40"><p>9</p></td><td valign="top" width="564"><p>Power on each engine (free power turbine speed and engine torque)/cockpit power control position (if applicable)</p></td></tr><tr><td valign="top" width="40"><p>10a</p><p>10b</p></td><td valign="top" width="564"><p>Main rotor speed</p><p>Rotor brake (if installed)</p></td></tr><tr><td valign="top" width="40"><p>11</p><p>11a</p><p>11b</p><p>11c</p><p>11d</p><p>11e</p><p>11f</p></td><td valign="top" width="564"><p>Primary flight controls — pilot input and control output position (if applicable)</p><p>Collective pitch</p><p>Longitudinal cyclic pitch</p><p>Lateral cyclic pitch</p><p>Tail rotor pedal</p><p>Controllable stabiliser</p><p>Hydraulic selection</p></td></tr><tr><td valign="top" width="40"><p>12</p></td><td valign="top" width="564"><p>Hydraulics low pressure</p></td></tr><tr><td valign="top" width="40"><p>13</p></td><td valign="top" width="564"><p>Outside air temperature</p></td></tr><tr><td valign="top" width="40"><p>14</p></td><td valign="top" width="564"><p>AFCS mode and engagement status</p></td></tr><tr><td valign="top" width="40"><p>15</p></td><td valign="top" width="564"><p>Stability augmentation system engagement</p></td></tr><tr><td valign="top" width="40"><p>16</p></td><td valign="top" width="564"><p>Main gear box oil pressure</p></td></tr><tr><td valign="top" width="40"><p>17</p></td><td valign="top" width="564"><p>Main gear box oil temperature</p></td></tr><tr><td valign="top" width="40"><p>18</p></td><td valign="top" width="564"><p>Yaw rate or yaw acceleration</p></td></tr><tr><td valign="top" width="40"><p>19</p></td><td valign="top" width="564"><p>Indicated sling load force (if installed)</p></td></tr><tr><td valign="top" width="40"><p>20</p></td><td valign="top" width="564"><p>Longitudinal acceleration (body axis)</p></td></tr><tr><td valign="top" width="40"><p>21</p></td><td valign="top" width="564"><p>Lateral acceleration</p></td></tr><tr><td valign="top" width="40"><p>22</p></td><td valign="top" width="564"><p>Radio altitude</p></td></tr><tr><td valign="top" width="40"><p>23</p></td><td valign="top" width="564"><p>Vertical beam deviation (ILS glide path or MLS elevation)</p></td></tr><tr><td valign="top" width="40"><p>24</p></td><td valign="top" width="564"><p>Horizontal beam deviation (ILS localiser or MLS azimuth)</p></td></tr><tr><td valign="top" width="40"><p>25</p></td><td valign="top" width="564"><p>Marker beacon passage</p></td></tr><tr><td valign="top" width="40"><p>26</p></td><td valign="top" width="564"><p>Warnings</p></td></tr><tr><td valign="top" width="40"><p>27</p></td><td valign="top" width="564"><p>Reserved (navigation receiver frequency selection is recommended)</p></td></tr><tr><td valign="top" width="40"><p>28</p></td><td valign="top" width="564"><p>Reserved (DME distance is recommended)</p></td></tr><tr><td valign="top" width="40"><p>29</p></td><td valign="top" width="564"><p>Reserved (navigation data are recommended)</p></td></tr><tr><td valign="top" width="40"><p>30</p></td><td valign="top" width="564"><p>Landing gear or gear selector position</p></td></tr></table> Table 3 Helicopters equipped with electronic display systems <table border="1" cellpadding="0" cellspacing="0" width="605"><tr><td valign="top" width="40"><p><b>No</b></p></td><td valign="top" width="564"><p><b>Parameter</b></p></td></tr><tr><td valign="top" width="40"><p>38</p></td><td valign="top" width="564"><p>Selected barometric setting (each pilot station)</p></td></tr><tr><td valign="top" width="40"><p>39</p></td><td valign="top" width="564"><p>Selected altitude</p></td></tr><tr><td valign="top" width="40"><p>40</p></td><td valign="top" width="564"><p>Selected speed</p></td></tr><tr><td valign="top" width="40"><p>41</p></td><td valign="top" width="564"><p>Selected Mach</p></td></tr><tr><td valign="top" width="40"><p>42</p></td><td valign="top" width="564"><p>Selected vertical speed</p></td></tr><tr><td valign="top" width="40"><p>43</p></td><td valign="top" width="564"><p>Selected heading</p></td></tr><tr><td valign="top" width="40"><p>44</p></td><td valign="top" width="564"><p>Selected flight path</p></td></tr><tr><td valign="top" width="40"><p>45</p></td><td valign="top" width="564"><p>Selected decision height</p></td></tr><tr><td valign="top" width="40"><p>46</p></td><td valign="top" width="564"><p>EFIS display format</p></td></tr><tr><td valign="top" width="40"><p>47</p></td><td valign="top" width="564"><p>Multi-function/engine/alerts display format</p></td></tr></table>
##### AMC2 CAT.IDE.H.190 Flight data recorder *ED Decision 2019/019/R* **LIST OF PARAMETERS TO BE RECORDED FOR HELICOPTERS HAVING AN MCTOM OF MORE THAN 3 175 KG AND FIRST ISSUED WITH AN INDIVIDUAL COFA ON OR AFTER 1 AUGUST 1999 AND BEFORE 1 JANUARY 2016 AND HELICOPTERS HAVING AN MCTOM OF MORE THAN 7 000 KG OR AN MOPSC OF MORE THAN 9 AND FIRST ISSUED WITH AN INDIVIDUAL COFA ON OR AFTER 1 JANUARY 1989 AND BEFORE 1 AUGUST 1999** (a) The FDR should, with reference to a timescale, record: (1) for helicopters with an MCTOM between 3 175 kg and 7 000 kg the parameters listed in Table 1 below; (2) for helicopters with an MCTOM of more than 7 000 kg the parameters listed in Table 2 below; (3) for helicopters equipped with electronic display systems, the additional parameters listed in Table 3 below; and (4) any dedicated parameters relating to novel or unique design or operational characteristics of the helicopter. (b) The FDR of helicopters with an MCTOM of more than 7 000 kg does not need to record parameter 19 of Table 2 below, if any of the following conditions are met: (1) the sensor is not readily available; or (2) a change is required in the equipment that generates the data. (c) Individual parameters that can be derived by calculation from the other recorded parameters need not to be recorded, if agreed by the competent authority. (d) The parameters should meet, as far as practicable, the performance specifications (range, sampling intervals, accuracy limits and resolution in read-out) defined in [AMC3 CAT.IDE.H.190](#_DxCrossRefBm523088719). (e) If recording capacity is available, as many of the additional parameters as possible specified in table II-A.2 of EUROCAE Document ED 112 dated March 2003 should be recorded. (f) For the purpose of this AMC, a sensor is considered ‘readily available’ when it is already available or can be easily incorporated. ***Table 1*** Helicopters with an MCTOM of 7 000 kg or less <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> <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</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 (free power turbine speed and engine torque)/cockpit power control position (if applicable)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 10a</p> <p align="left">10b</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Main rotor speed</p> <p align="left">Rotor brake (if installed)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 11</p> <p align="left"> 11a</p> <p align="left"> 11b</p> <p align="left"> 11c</p> <p align="left"> 11d</p> <p align="left"> 11e</p> <p align="left">11f</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Primary flight controls — pilot input and control output position (if applicable)</p> <p align="left"> Collective pitch</p> <p align="left"> Longitudinal cyclic pitch</p> <p align="left"> Lateral cyclic pitch</p> <p align="left"> Tail rotor pedal</p> <p align="left"> Controllable stabiliser</p> <p align="left">Hydraulic selection</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 13</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Outside air temperature</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 14</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Autopilot engagement status</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 15</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Stability augmentation system engagement</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 26</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Warnings</p> </td> </tr> </tbody> </table> ***Table 2*** Helicopters with an MCTOM of more than 7 000 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> <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</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 (free power turbine speed and engine torque)/cockpit power control position (if applicable)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 10a</p> <p align="left">10b</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Main rotor speed</p> <p align="left">Rotor brake (if installed)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 11</p> <p align="left"> 11a</p> <p align="left"> 11b</p> <p align="left"> 11c</p> <p align="left"> 11d</p> <p align="left"> 11e</p> <p align="left">11f</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Primary flight controls — pilot input and control output position (if applicable)</p> <p align="left"> Collective pitch</p> <p align="left"> Longitudinal cyclic pitch</p> <p align="left"> Lateral cyclic pitch</p> <p align="left"> Tail rotor pedal</p> <p align="left"> Controllable stabiliser</p> <p align="left">Hydraulic selection</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 12</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Hydraulics low pressure</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 13</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Outside air temperature</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 14</p> </td> <td bgcolor="#d9d9d9"><p align="left"> AFCS mode and engagement status</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 15</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Stability augmentation system engagement</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 16</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Main gear box oil pressure</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 17</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Main gear box oil temperature</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 18</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Yaw rate or yaw acceleration</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 19</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Indicated sling load force (if installed)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 20</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Longitudinal acceleration (body axis)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 21</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Lateral acceleration</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 22</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Radio altitude</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 23</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Vertical beam deviation (ILS glide path or MLS elevation)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 24</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Horizontal beam deviation (ILS localiser or MLS azimuth)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 25</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Marker beacon passage</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 26</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Warnings</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 27</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Reserved (navigation receiver frequency selection is recommended)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 28</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Reserved (DME distance is recommended)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 29</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Reserved (navigation data are recommended)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 30</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Landing gear or gear selector position</p> </td> </tr> </tbody> </table> ***Table 3*** Helicopters equipped with electronic display systems <table bgcolor="#d9d9d9" cellpadding="7" cellspacing="0"> <col/> <col/> <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> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 38</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Selected barometric setting (each pilot station)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 39</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Selected altitude</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 40</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Selected speed</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 41</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Selected Mach</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 42</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Selected vertical speed</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 43</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Selected heading</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 44</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Selected flight path</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 45</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Selected decision height</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 46</p> </td> <td bgcolor="#d9d9d9"><p align="left"> EFIS display format</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 47</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Multi-function/engine/alerts display format</p> </td> </tr> </table>