<?xml version="1.0"?>
<!-- CFM56 turbofan engine model
     Version 0.9, 31 Jan 2003, David Culp, davidculp2@attbi.com
_______________________________________________________________
-->
<FG_TURBINE NAME="CFM56">
<!-- max static thrust at S.L. (installed), lbs -->
  MAXMILTHRUST 19000
<!-- augmentation not installed -->
  MAXAUGTHRUST 19000
<!-- Idle Thrust -->
  <TABLE NAME="IdleThrust" TYPE="TABLE">
    Idle_power_thrust_factor
    6
    6
    velocities/mach-norm
    position/h-sl-ft
    none
                0   10000   20000   30000   40000  50000
    0.0    0.0836  0.0528  0.0694  0.0899  0.1183  0.1467
    0.2    0.0501  0.0335  0.0544  0.0797  0.1049  0.1341
    0.4    0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
    0.6   -0.0804 -0.0560 -0.0237  0.0276  0.0718  0.1073
    0.8   -0.2129 -0.1498 -0.1025 -0.0195  0.0473  0.0868
    1.0   -0.2839 -0.1104 -0.0469 -0.0270 -0.0158  0.0552
  </TABLE>

  <TABLE NAME="MilThrust" TYPE="TABLE">
    Effects_of_altitude_and_mach_on_thrust
    7
    6
    velocities/mach-norm
    position/h-sl-ft
    none
               0    10000   20000     30000    40000    50000
    0.0   1.0000   0.7216   0.4890   0.3115   0.1932   0.1104
    0.2   1.0000   0.7216   0.4979   0.3186   0.1948   0.1104
    0.4   0.9945   0.7344   0.5213   0.3383   0.2050   0.1230
    0.6   0.9968   0.7759   0.5591   0.3675   0.2240   0.1309
    0.8   0.9771   0.8025   0.6112   0.4196   0.2563   0.1522
    0.9   0.9300   0.7900   0.6000   0.3900   0.2300   0.1300
    1.0   0.5000   0.5000   0.4000   0.2000   0.1500   0.0900
  </TABLE>

</FG_TURBINE>