--- /dev/null
+; AeroTech I366R\r
+; provided by ThrustCurve.org (www.thrustcurve.org)\r
+I366R 38 298 0 0.3136 0.55552 AT\r
+ 0.027 323.256\r
+ 0.088 485.393\r
+ 0.148 483.744\r
+ 0.208 479.926\r
+ 0.268 473.365\r
+ 0.327 466.192\r
+ 0.388 457.444\r
+ 0.448 448.751\r
+ 0.509 441.477\r
+ 0.570 430.236\r
+ 0.630 421.524\r
+ 0.690 411.757\r
+ 0.750 398.876\r
+ 0.810 387.496\r
+ 0.870 375.430\r
+ 0.930 361.325\r
+ 0.991 345.057\r
+ 1.053 330.392\r
+ 1.112 312.636\r
+ 1.173 293.508\r
+ 1.233 275.085\r
+ 1.292 262.408\r
+ 1.353 230.881\r
+ 1.413 118.008\r
+ 1.474 23.611\r
+ 1.535 0.000\r