Taurus ELECTRO manual 472 ENG.pdf - Pipistrel
Taurus ELECTRO manual 472 ENG.pdf - Pipistrel
Taurus ELECTRO manual 472 ENG.pdf - Pipistrel
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TAURUS <strong>ELECTRO</strong> 15<br />
Limitations<br />
REV. 0<br />
Indicated airspeed (IAS) to true airspeed (TAS) relation<br />
Airspeed indicator measures the difference between total and static pressure (also called dynamic<br />
pressure), which does not only change as speed increases, but is also linked with altitude. Flying at<br />
high altitudes, where the air is getting thinner, results in misinterpreting airspeed which is being<br />
indicated. The indicated airspeed value is actually lower than the true airspeed to which the aircraft<br />
is exposed. The higher you fly, the bigger the difference between IAS and TAS. Be aware of this effect<br />
especially when flying at high altitude at high speeds, not to exceed VNE unawarely. Bear in mind<br />
this can happen even with the indicator still pointing within the yellow arc!<br />
VNE at altitude (standard ICAO atmosphere)<br />
The tables below indicate IAS to TAS relation for an altitude span of 0 - 5000m (0 - FL165) in different<br />
atmospheres (variable is temperature). TAS is a constant of 225 km/h (122 kts) - VNE for the entire tables.<br />
ISA-20 (-5°C at sea level):<br />
Altitude (meters) 0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000<br />
Altitude (flight level) 0 FL16 FL33 FL50 FL66 FL82 FL98 FL115 FL131 FL148 FL165<br />
VNE IAS (km/h) 225 225 223 218 213 209 203 198 194 189 185<br />
VNE IAS (kts) 121 121 120 118 115 113 110 107 105 102 100<br />
ISA-10 (5°C at sea level):<br />
Altitude (meters) 0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000<br />
Altitude (flight level) 0 FL16 FL33 FL50 FL66 FL82 FL98 FL115 FL131 FL148 FL165<br />
VNE IAS (km/h) 225 224 219 214 209 205 199 195 191 186 182<br />
VNE IAS (kts) 121 121 118 116 113 111 108 105 103 100 98<br />
ISA (15°C at sea level):<br />
Altitude (meters) 0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000<br />
Altitude (flight level) 0 FL16 FL33 FL50 FL66 FL82 FL98 FL115 FL131 FL148 FL165<br />
VNE IAS (km/h) 225 220 215 210 205 201 196 191 187 182 178<br />
VNE IAS (kts) 121 119 116 113 111 109 106 103 101 98 96<br />
ISA+10 (25°C at sea level):<br />
Altitude (meters) 0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000<br />
Altitude (flight level) 0 FL16 FL33 FL50 FL66 FL82 FL98 FL115 FL131 FL148 FL165<br />
VNE IAS (km/h) 220 215 211 206 202 197 192 188 184 179 175<br />
VNE IAS (kts) 119 116 114 111 109 106 104 102 99 97 94<br />
ISA+20 (35°C at sea level) :<br />
Altitude (meters) 0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000<br />
Altitude (flight level) 0 FL16 FL33 FL50 FL66 FL82 FL98 FL115 FL131 FL148 FL165<br />
VNE IAS (km/h) 216 211 207 202 197 193 189 184 180 175 171<br />
VNE IAS (kts) 117 114 112 109 106 104 102 99 97 94 92<br />
Note how VNE decreases at higher altitudes!<br />
WARNING! Respect the Listed values at all times, not to exceed flutter critical<br />
speed.