; AeroTech J540R
; provided by ThrustCurve.org (www.thrustcurve.org)
J540R 54 314 0 0.61376 1.08416 AT
   0.044 498.757
   0.134 639.617
   0.224 649.317
   0.314 657.966
   0.404 664.020
   0.494 666.924
   0.584 663.699
   0.675 658.398
   0.765 651.232
   0.855 638.505
   0.945 626.396
   1.035 612.557
   1.126 590.090
   1.216 562.391
   1.306 536.875
   1.396 511.607
   1.486 490.354
   1.576 468.978
   1.667 451.342
   1.758 430.180
   1.847 414.549
   1.937 398.116
   2.027 305.877
   2.118 55.541
   2.208 1.523
   2.299 0.000
;