GM1 CAT.IDE.H.125 & CAT.IDE.H.130 Operations under VFR by day & Operations under IFR or at night - flight and navigational instruments and associated equipment

• ED Decision 2014/015/R found in: Air Operations (965/2012) Part-ARO Part-ORO Part-CAT Part-SPA Part-NCC Part-NCO Part-SPO (Feb 2025)

GM1 CAT.IDE.H.125 & CAT.IDE.H.130 Operations under VFR by day & Operations under IFR or at night – flight and navigational instruments and associated equipment ED Decision 2014/015/R SUMMARY TABLE Table 1 Flight and navigational instruments and associated equipment <table border="1" cellpadding="0" cellspacing="0" width="608"><thead><tr><td colspan="2" width="196"><p>SERIAL</p></td><td colspan="2" width="202"><p>FLIGHTS UNDER VFR</p></td><td colspan="2" width="209"><p>FLIGHTS UNDER IFR OR AT NIGHT</p></td></tr><tr><td colspan="2" width="196"><p><b>INSTRUMENT</b></p></td><td width="101"><p><b>SINGLE-PILOT</b></p></td><td width="101"><p><b>TWO PILOTS REQUIRED</b></p></td><td width="105"><p><b>SINGLE-PILOT</b></p></td><td width="105"><p><b>TWO PILOTS REQUIRED</b></p></td></tr></thead><tr><td colspan="2" valign="top" width="196"><p>(a)</p></td><td valign="top" width="101"><p>(b)</p></td><td valign="top" width="101"><p>(c)</p></td><td valign="top" width="105"><p>(d)</p></td><td valign="top" width="105"><p>(e)</p></td></tr><tr><td valign="top" width="38"><p>1</p></td><td valign="top" width="158"><p>Magnetic direction</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>1</p></td></tr><tr><td valign="top" width="38"><p>2</p></td><td valign="top" width="158"><p>time</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>1</p></td></tr><tr><td valign="top" width="38"><p>3</p></td><td valign="top" width="158"><p>Pressure altitude</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>2</p><p>Note (1)</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>4</p></td><td valign="top" width="158"><p>Indicated airspeed</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>5</p></td><td valign="top" width="158"><p>Vertical speed</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>6</p></td><td valign="top" width="158"><p>Slip</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>7</p></td><td valign="top" width="158"><p>Attitude</p></td><td valign="top" width="101"><p>1</p><p>Note (2)</p></td><td valign="top" width="101"><p>2</p><p>Note(2)</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>8</p></td><td valign="top" width="158"><p>Stabilised direction</p></td><td valign="top" width="101"><p>1</p><p>Note (2)</p></td><td valign="top" width="101"><p>2</p><p>Note(2)</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>9</p></td><td valign="top" width="158"><p>Outside air temperature</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>1</p></td></tr><tr><td valign="top" width="38"><p>10</p></td><td valign="top" width="158"><p>Airspeed icing protection</p></td><td valign="top" width="101"><p>1</p><p>Note (3)</p></td><td valign="top" width="101"><p>2</p><p>Note (3)</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>11</p></td><td valign="top" width="158"><p>Airspeed icing protection failure indicating</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>1</p><p>Note (4)</p></td><td valign="top" width="105"><p>2</p><p>Note (4)</p></td></tr><tr><td valign="top" width="38"><p>12</p></td><td valign="top" width="158"><p>Static pressure source</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>2</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>13</p></td><td valign="top" width="158"><p>Standby attitude</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>1</p><p>Note (5)</p></td><td valign="top" width="105"><p>1</p><p>Note (5)</p></td></tr><tr><td valign="top" width="38"><p>14</p></td><td valign="top" width="158"><p>Chart holder</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>1</p><p>Note (6)</p></td><td valign="top" width="105"><p>1</p><p>Note (6)</p></td></tr></table> Note (1) For single-pilot night operation under VFR, one means of measuring and displaying pressure altitude may be substituted by a means of measuring and displaying radio altitude. Note (2) Applicable only to helicopters with a maximum certified take-off mass (MCTOM) of more than 3 175 kg; or helicopters operated over water when out of sight of land or when the visibility is less than 1 500 m. Note (3) Applicable only to helicopters with an MCTOM of more than 3 175 kg, or with an MOPSC of more than 9. Note (4) The pitot heater failure annunciation applies to any helicopter issued with an individual CofA on or after 1 August 1999. It also applies before that date when: the helicopter has a MCTOM of more than 3 175 kg and an MOPSC of more than 9. Note (5) For helicopters with an MCTOM of more than 3 175 kg, CS 29.1303(g) may require either a gyroscopic rate-of-turn indicator combined with a slip-skid indicator (turn and bank indicator) or a standby attitude indicator satisfying the requirements. In any case, the original type certification standard should be referred to determine the exact requirement. Note (6) Applicable only to helicopters operating under IFR. GM1 CAT.IDE.H.125 & CAT.IDE.H.130 Operations under VFR by day & Operations under IFR or at night – flight and navigational instruments and associated equipment ED Decision 2014/015/R SUMMARY TABLE Table 1 Flight and navigational instruments and associated equipment <table border="1" cellpadding="0" cellspacing="0" width="608"><thead><tr><td colspan="2" width="196"><p>SERIAL</p></td><td colspan="2" width="202"><p>FLIGHTS UNDER VFR</p></td><td colspan="2" width="209"><p>FLIGHTS UNDER IFR OR AT NIGHT</p></td></tr><tr><td colspan="2" width="196"><p><b>INSTRUMENT</b></p></td><td width="101"><p><b>SINGLE-PILOT</b></p></td><td width="101"><p><b>TWO PILOTS REQUIRED</b></p></td><td width="105"><p><b>SINGLE-PILOT</b></p></td><td width="105"><p><b>TWO PILOTS REQUIRED</b></p></td></tr></thead><tr><td colspan="2" valign="top" width="196"><p>(a)</p></td><td valign="top" width="101"><p>(b)</p></td><td valign="top" width="101"><p>(c)</p></td><td valign="top" width="105"><p>(d)</p></td><td valign="top" width="105"><p>(e)</p></td></tr><tr><td valign="top" width="38"><p>1</p></td><td valign="top" width="158"><p>Magnetic direction</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>1</p></td></tr><tr><td valign="top" width="38"><p>2</p></td><td valign="top" width="158"><p>time</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>1</p></td></tr><tr><td valign="top" width="38"><p>3</p></td><td valign="top" width="158"><p>Pressure altitude</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>2</p><p>Note (1)</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>4</p></td><td valign="top" width="158"><p>Indicated airspeed</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>5</p></td><td valign="top" width="158"><p>Vertical speed</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>6</p></td><td valign="top" width="158"><p>Slip</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>7</p></td><td valign="top" width="158"><p>Attitude</p></td><td valign="top" width="101"><p>1</p><p>Note (2)</p></td><td valign="top" width="101"><p>2</p><p>Note(2)</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>8</p></td><td valign="top" width="158"><p>Stabilised direction</p></td><td valign="top" width="101"><p>1</p><p>Note (2)</p></td><td valign="top" width="101"><p>2</p><p>Note(2)</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>9</p></td><td valign="top" width="158"><p>Outside air temperature</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>1</p></td></tr><tr><td valign="top" width="38"><p>10</p></td><td valign="top" width="158"><p>Airspeed icing protection</p></td><td valign="top" width="101"><p>1</p><p>Note (3)</p></td><td valign="top" width="101"><p>2</p><p>Note (3)</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>11</p></td><td valign="top" width="158"><p>Airspeed icing protection failure indicating</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>1</p><p>Note (4)</p></td><td valign="top" width="105"><p>2</p><p>Note (4)</p></td></tr><tr><td valign="top" width="38"><p>12</p></td><td valign="top" width="158"><p>Static pressure source</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>2</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>13</p></td><td valign="top" width="158"><p>Standby attitude</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>1</p><p>Note (5)</p></td><td valign="top" width="105"><p>1</p><p>Note (5)</p></td></tr><tr><td valign="top" width="38"><p>14</p></td><td valign="top" width="158"><p>Chart holder</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>1</p><p>Note (6)</p></td><td valign="top" width="105"><p>1</p><p>Note (6)</p></td></tr></table> Note (1) For single-pilot night operation under VFR, one means of measuring and displaying pressure altitude may be substituted by a means of measuring and displaying radio altitude. Note (2) Applicable only to helicopters with a maximum certified take-off mass (MCTOM) of more than 3 175 kg; or helicopters operated over water when out of sight of land or when the visibility is less than 1 500 m. Note (3) Applicable only to helicopters with an MCTOM of more than 3 175 kg, or with an MOPSC of more than 9. Note (4) The pitot heater failure annunciation applies to any helicopter issued with an individual CofA on or after 1 August 1999. It also applies before that date when: the helicopter has a MCTOM of more than 3 175 kg and an MOPSC of more than 9. Note (5) For helicopters with an MCTOM of more than 3 175 kg, CS 29.1303(g) may require either a gyroscopic rate-of-turn indicator combined with a slip-skid indicator (turn and bank indicator) or a standby attitude indicator satisfying the requirements. In any case, the original type certification standard should be referred to determine the exact requirement. Note (6) Applicable only to helicopters operating under IFR. GM1 CAT.IDE.H.125 & CAT.IDE.H.130 Operations under VFR by day & Operations under IFR or at night – flight and navigational instruments and associated equipment ED Decision 2014/015/R SUMMARY TABLE Table 1 Flight and navigational instruments and associated equipment <table border="1" cellpadding="0" cellspacing="0" width="608"><thead><tr><td colspan="2" width="196"><p>SERIAL</p></td><td colspan="2" width="202"><p>FLIGHTS UNDER VFR</p></td><td colspan="2" width="209"><p>FLIGHTS UNDER IFR OR AT NIGHT</p></td></tr><tr><td colspan="2" width="196"><p><b>INSTRUMENT</b></p></td><td width="101"><p><b>SINGLE-PILOT</b></p></td><td width="101"><p><b>TWO PILOTS REQUIRED</b></p></td><td width="105"><p><b>SINGLE-PILOT</b></p></td><td width="105"><p><b>TWO PILOTS REQUIRED</b></p></td></tr></thead><tr><td colspan="2" valign="top" width="196"><p>(a)</p></td><td valign="top" width="101"><p>(b)</p></td><td valign="top" width="101"><p>(c)</p></td><td valign="top" width="105"><p>(d)</p></td><td valign="top" width="105"><p>(e)</p></td></tr><tr><td valign="top" width="38"><p>1</p></td><td valign="top" width="158"><p>Magnetic direction</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>1</p></td></tr><tr><td valign="top" width="38"><p>2</p></td><td valign="top" width="158"><p>time</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>1</p></td></tr><tr><td valign="top" width="38"><p>3</p></td><td valign="top" width="158"><p>Pressure altitude</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>2</p><p>Note (1)</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>4</p></td><td valign="top" width="158"><p>Indicated airspeed</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>5</p></td><td valign="top" width="158"><p>Vertical speed</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>6</p></td><td valign="top" width="158"><p>Slip</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>7</p></td><td valign="top" width="158"><p>Attitude</p></td><td valign="top" width="101"><p>1</p><p>Note (2)</p></td><td valign="top" width="101"><p>2</p><p>Note(2)</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>8</p></td><td valign="top" width="158"><p>Stabilised direction</p></td><td valign="top" width="101"><p>1</p><p>Note (2)</p></td><td valign="top" width="101"><p>2</p><p>Note(2)</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>9</p></td><td valign="top" width="158"><p>Outside air temperature</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>1</p></td></tr><tr><td valign="top" width="38"><p>10</p></td><td valign="top" width="158"><p>Airspeed icing protection</p></td><td valign="top" width="101"><p>1</p><p>Note (3)</p></td><td valign="top" width="101"><p>2</p><p>Note (3)</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>11</p></td><td valign="top" width="158"><p>Airspeed icing protection failure indicating</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>1</p><p>Note (4)</p></td><td valign="top" width="105"><p>2</p><p>Note (4)</p></td></tr><tr><td valign="top" width="38"><p>12</p></td><td valign="top" width="158"><p>Static pressure source</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>2</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>13</p></td><td valign="top" width="158"><p>Standby attitude</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>1</p><p>Note (5)</p></td><td valign="top" width="105"><p>1</p><p>Note (5)</p></td></tr><tr><td valign="top" width="38"><p>14</p></td><td valign="top" width="158"><p>Chart holder</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>1</p><p>Note (6)</p></td><td valign="top" width="105"><p>1</p><p>Note (6)</p></td></tr></table> Note (1) For single-pilot night operation under VFR, one means of measuring and displaying pressure altitude may be substituted by a means of measuring and displaying radio altitude. Note (2) Applicable only to helicopters with a maximum certified take-off mass (MCTOM) of more than 3 175 kg; or helicopters operated over water when out of sight of land or when the visibility is less than 1 500 m. Note (3) Applicable only to helicopters with an MCTOM of more than 3 175 kg, or with an MOPSC of more than 9. Note (4) The pitot heater failure annunciation applies to any helicopter issued with an individual CofA on or after 1 August 1999. It also applies before that date when: the helicopter has a MCTOM of more than 3 175 kg and an MOPSC of more than 9. Note (5) For helicopters with an MCTOM of more than 3 175 kg, CS 29.1303(g) may require either a gyroscopic rate-of-turn indicator combined with a slip-skid indicator (turn and bank indicator) or a standby attitude indicator satisfying the requirements. In any case, the original type certification standard should be referred to determine the exact requirement. Note (6) Applicable only to helicopters operating under IFR. GM1 CAT.IDE.H.125 & CAT.IDE.H.130 Operations under VFR by day & Operations under IFR or at night – flight and navigational instruments and associated equipment ED Decision 2014/015/R SUMMARY TABLE Table 1 Flight and navigational instruments and associated equipment <table border="1" cellpadding="0" cellspacing="0" width="608"><thead><tr><td colspan="2" width="196"><p>SERIAL</p></td><td colspan="2" width="202"><p>FLIGHTS UNDER VFR</p></td><td colspan="2" width="209"><p>FLIGHTS UNDER IFR OR AT NIGHT</p></td></tr><tr><td colspan="2" width="196"><p><b>INSTRUMENT</b></p></td><td width="101"><p><b>SINGLE-PILOT</b></p></td><td width="101"><p><b>TWO PILOTS REQUIRED</b></p></td><td width="105"><p><b>SINGLE-PILOT</b></p></td><td width="105"><p><b>TWO PILOTS REQUIRED</b></p></td></tr></thead><tr><td colspan="2" valign="top" width="196"><p>(a)</p></td><td valign="top" width="101"><p>(b)</p></td><td valign="top" width="101"><p>(c)</p></td><td valign="top" width="105"><p>(d)</p></td><td valign="top" width="105"><p>(e)</p></td></tr><tr><td valign="top" width="38"><p>1</p></td><td valign="top" width="158"><p>Magnetic direction</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>1</p></td></tr><tr><td valign="top" width="38"><p>2</p></td><td valign="top" width="158"><p>time</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>1</p></td></tr><tr><td valign="top" width="38"><p>3</p></td><td valign="top" width="158"><p>Pressure altitude</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>2</p><p>Note (1)</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>4</p></td><td valign="top" width="158"><p>Indicated airspeed</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>5</p></td><td valign="top" width="158"><p>Vertical speed</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>6</p></td><td valign="top" width="158"><p>Slip</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>2</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>7</p></td><td valign="top" width="158"><p>Attitude</p></td><td valign="top" width="101"><p>1</p><p>Note (2)</p></td><td valign="top" width="101"><p>2</p><p>Note(2)</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>8</p></td><td valign="top" width="158"><p>Stabilised direction</p></td><td valign="top" width="101"><p>1</p><p>Note (2)</p></td><td valign="top" width="101"><p>2</p><p>Note(2)</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>9</p></td><td valign="top" width="158"><p>Outside air temperature</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="101"><p>1</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>1</p></td></tr><tr><td valign="top" width="38"><p>10</p></td><td valign="top" width="158"><p>Airspeed icing protection</p></td><td valign="top" width="101"><p>1</p><p>Note (3)</p></td><td valign="top" width="101"><p>2</p><p>Note (3)</p></td><td valign="top" width="105"><p>1</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>11</p></td><td valign="top" width="158"><p>Airspeed icing protection failure indicating</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>1</p><p>Note (4)</p></td><td valign="top" width="105"><p>2</p><p>Note (4)</p></td></tr><tr><td valign="top" width="38"><p>12</p></td><td valign="top" width="158"><p>Static pressure source</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>2</p></td><td valign="top" width="105"><p>2</p></td></tr><tr><td valign="top" width="38"><p>13</p></td><td valign="top" width="158"><p>Standby attitude</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>1</p><p>Note (5)</p></td><td valign="top" width="105"><p>1</p><p>Note (5)</p></td></tr><tr><td valign="top" width="38"><p>14</p></td><td valign="top" width="158"><p>Chart holder</p></td><td valign="top" width="101"></td><td valign="top" width="101"></td><td valign="top" width="105"><p>1</p><p>Note (6)</p></td><td valign="top" width="105"><p>1</p><p>Note (6)</p></td></tr></table> Note (1) For single-pilot night operation under VFR, one means of measuring and displaying pressure altitude may be substituted by a means of measuring and displaying radio altitude. Note (2) Applicable only to helicopters with a maximum certified take-off mass (MCTOM) of more than 3 175 kg; or helicopters operated over water when out of sight of land or when the visibility is less than 1 500 m. Note (3) Applicable only to helicopters with an MCTOM of more than 3 175 kg, or with an MOPSC of more than 9. Note (4) The pitot heater failure annunciation applies to any helicopter issued with an individual CofA on or after 1 August 1999. It also applies before that date when: the helicopter has a MCTOM of more than 3 175 kg and an MOPSC of more than 9. Note (5) For helicopters with an MCTOM of more than 3 175 kg, CS 29.1303(g) may require either a gyroscopic rate-of-turn indicator combined with a slip-skid indicator (turn and bank indicator) or a standby attitude indicator satisfying the requirements. In any case, the original type certification standard should be referred to determine the exact requirement. Note (6) Applicable only to helicopters operating under IFR. ##### GM1 CAT.IDE.H.125 & CAT.IDE.H.130 Operations under VFR by day & Operations under IFR or at night – flight and navigational instruments and associated equipment *ED Decision 2014/015/R* **SUMMARY TABLE** ***Table 1*** Flight and navigational instruments and associated equipment <table bgcolor="#d9d9d9" cellpadding="7" cellspacing="0"> <col/> <col/> <col/> <col/> <col/> <col/> <thead> <tr> <td bgcolor="#808080" colspan="2"><p align="center"> <b>SERIAL</b></p> </td> <td bgcolor="#808080" colspan="2"><p align="center"> <b>FLIGHTS UNDER VFR</b></p> </td> <td bgcolor="#808080" colspan="2"><p align="center"> <b>FLIGHTS UNDER IFR OR AT NIGHT</b></p> </td> </tr> <tr> <td bgcolor="#808080" colspan="2"><p align="center"> <b>INSTRUMENT</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>SINGLE-PILOT</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>TWO PILOTS REQUIRED</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>SINGLE-PILOT</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>TWO PILOTS REQUIRED</b></p> </td> </tr> </thead> <tbody> <tr valign="top"> <td bgcolor="#d9d9d9" colspan="2"><p align="center"> <b>(a)</b></p> </td> <td bgcolor="#d9d9d9"><p align="center"> <b>(b)</b></p> </td> <td bgcolor="#d9d9d9"><p align="center"> <b>(c)</b></p> </td> <td bgcolor="#d9d9d9"><p align="center"> <b>(d)</b></p> </td> <td bgcolor="#d9d9d9"><p align="center"> <b>(e)</b></p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Magnetic direction</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> time</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 3</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Pressure altitude</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> <p align="left">Note (1)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 4</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Indicated airspeed</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 5</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Vertical speed</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 6</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Slip</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 7</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Attitude</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (2)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> <p align="left">Note(2)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 8</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Stabilised direction</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (2)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> <p align="left">Note(2)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 9</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Outside air temperature</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 10</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Airspeed icing protection</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (3)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> <p align="left">Note (3)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 11</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Airspeed icing protection failure indicating</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (4)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> <p align="left">Note (4)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 12</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Static pressure source</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 13</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Standby attitude</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (5)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (5)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 14</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Chart holder</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (6)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (6)</p> </td> </tr> </tbody> </table> Note (1) For single-pilot night operation under VFR, one means of measuring and displaying pressure altitude may be substituted by a means of measuring and displaying radio altitude. Note (2) Applicable only to helicopters with a maximum certified take-off mass (MCTOM) of more than 3 175 kg; or helicopters operated over water when out of sight of land or when the visibility is less than 1 500 m. Note (3) Applicable only to helicopters with an MCTOM of more than 3 175 kg, or with an MOPSC of more than 9. Note (4) The pitot heater failure annunciation applies to any helicopter issued with an individual CofA on or after 1 August 1999. It also applies before that date when: the helicopter has a MCTOM of more than 3 175 kg and an MOPSC of more than 9. Note (5) For helicopters with an MCTOM of more than 3 175 kg, CS 29.1303(g) may require either a gyroscopic rate-of-turn indicator combined with a slip-skid indicator (turn and bank indicator) or a standby attitude indicator satisfying the requirements. In any case, the original type certification standard should be referred to determine the exact requirement. Note (6) Applicable only to helicopters operating under IFR. ##### GM1 CAT.IDE.H.125 & CAT.IDE.H.130 Operations under VFR by day & Operations under IFR or at night – flight and navigational instruments and associated equipment *ED Decision 2014/015/R* **SUMMARY TABLE** ***Table 1*** Flight and navigational instruments and associated equipment <table bgcolor="#d9d9d9" cellpadding="7" cellspacing="0"> <col/> <col/> <col/> <col/> <col/> <col/> <thead> <tr> <td bgcolor="#808080" colspan="2"><p align="center"> <b>SERIAL</b></p> </td> <td bgcolor="#808080" colspan="2"><p align="center"> <b>FLIGHTS UNDER VFR</b></p> </td> <td bgcolor="#808080" colspan="2"><p align="center"> <b>FLIGHTS UNDER IFR OR AT NIGHT</b></p> </td> </tr> <tr> <td bgcolor="#808080" colspan="2"><p align="center"> <b>INSTRUMENT</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>SINGLE-PILOT</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>TWO PILOTS REQUIRED</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>SINGLE-PILOT</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>TWO PILOTS REQUIRED</b></p> </td> </tr> </thead> <tbody> <tr valign="top"> <td bgcolor="#d9d9d9" colspan="2"><p align="center"> <b>(a)</b></p> </td> <td bgcolor="#d9d9d9"><p align="center"> <b>(b)</b></p> </td> <td bgcolor="#d9d9d9"><p align="center"> <b>(c)</b></p> </td> <td bgcolor="#d9d9d9"><p align="center"> <b>(d)</b></p> </td> <td bgcolor="#d9d9d9"><p align="center"> <b>(e)</b></p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Magnetic direction</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> time</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 3</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Pressure altitude</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> <p align="left">Note (1)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 4</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Indicated airspeed</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 5</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Vertical speed</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 6</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Slip</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 7</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Attitude</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (2)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> <p align="left">Note(2)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 8</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Stabilised direction</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (2)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> <p align="left">Note(2)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 9</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Outside air temperature</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 10</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Airspeed icing protection</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (3)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> <p align="left">Note (3)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 11</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Airspeed icing protection failure indicating</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (4)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> <p align="left">Note (4)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 12</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Static pressure source</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 13</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Standby attitude</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (5)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (5)</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 14</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Chart holder</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (6)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> <p align="left">Note (6)</p> </td> </tr> </tbody> </table> Note (1) For single-pilot night operation under VFR, one means of measuring and displaying pressure altitude may be substituted by a means of measuring and displaying radio altitude. Note (2) Applicable only to helicopters with a maximum certified take-off mass (MCTOM) of more than 3 175 kg; or helicopters operated over water when out of sight of land or when the visibility is less than 1 500 m. Note (3) Applicable only to helicopters with an MCTOM of more than 3 175 kg, or with an MOPSC of more than 9. Note (4) The pitot heater failure annunciation applies to any helicopter issued with an individual CofA on or after 1 August 1999. It also applies before that date when: the helicopter has a MCTOM of more than 3 175 kg and an MOPSC of more than 9. Note (5) For helicopters with an MCTOM of more than 3 175 kg, CS 29.1303(g) may require either a gyroscopic rate-of-turn indicator combined with a slip-skid indicator (turn and bank indicator) or a standby attitude indicator satisfying the requirements. In any case, the original type certification standard should be referred to determine the exact requirement. Note (6) Applicable only to helicopters operating under IFR.