COPY AND PASTE WHERE APPROPRIATE. [GeneralEngineData] engine_type = 1 Engine.0 = 10.200, -21.250, -3.290 Engine.1 = 10.200, 21.250, -3.290 fuel_flow_scalar = 0.6991 min_throttle_limit=-0.319946 max_contrail_temperature = -35 [TurbineEngineData] fuel_flow_gain =0.002 bypass_ratio=6.00 inlet_area =33.5757 rated_N2_rpm =29920 static_thrust =38400.000 afterburner_available =0 reverser_available =1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=110.5000 //Max N1 = 110.50% for RR RB21, 117.50% for GE CF6, 104.70% for JT9D pitch_takeoff_ga= 0.000 use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode. use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode. default_pitch_mode=0 default_bank_mode=0 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=0.300000 max_pitch_velocity_lo_alt_breakpoint= 7000.000000 max_pitch_velocity_hi_alt_breakpoint=24000.000000 max_bank=32.000000 max_bank_acceleration=1.200000 max_bank_velocity=2.000000 max_throttle_rate=0.02800 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=1.000000 [fuel] Center1 = 0.000, 0.000, 0.000, 6964.000, 0.000 LeftMain = -3.000, -12.000, 0.000, 2156.000, 0.000 RightMain = -3.000, 12.000, 0.000, 2156.000, 0.000 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 2 electric_pump=0 [brakes] toe_brakes_scale=0.496741 parking_brake=1 auto_brakes=4 hydraulic_system_scalar=1 [hydraulic_system] electric_pumps=2 engine_map=1,1,0,0 normal_pressure=3000.000000 (COPY BELOW INTO APPROPRIATE PLACES WITHIN [exits]) [exits] exit.0 = 0.4, 60.3, -4.0, 9, 0 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=2