[Seppel]

hier der Zweite Teil,

[Flaps.2] //Inboard Flap
type= 1
span-outboard= 0.200
extending-time= 25.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 270.000
lift_scalar= 0.4950
drag_scalar= 0.250
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.1000, 255.000
flaps-position.2= 5.0000, 235.000
flaps-position.3= 15.000, 215.000
flaps-position.4= 20.000, 195.000
flaps-position.5= 25.000, 185.000
flaps-position.6= 30.000, 170.000

[Flaps.3] //Outboard Flap
type= 1
span-outboard= 0.600
extending-time= 25.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 270.000
lift_scalar= 0.4950
drag_scalar= 0.300
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.10, 235.000
flaps-position.2= 5.000, 215.000
flaps-position.3= 15.000, 196.000
flaps-position.4= 20.000, 195.000
flaps-position.5= 25.000, 185.000
flaps-position.6= 30.000, 170.000

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=0.8143
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[fuel]
Center1 = 0.0, 0.0, -4.0, 26100.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -7.0, -35.0, 0.0, 9300.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -7.0, 35.0, 0.0, 9300.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required= 1
autothrottle_max_rpm = 108.5
autothrottle_takeoff_ga= 1
pitch_takeoff_ga=8 ;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=0.7
max_pitch_velocity_hi_alt=0.4
max_pitch_velocity_lo_alt_breakpoint=11000.0
max_pitch_velocity_hi_alt_breakpoint=25000.0
max_bank=25.0
max_bank_acceleration=1.4
max_bank_velocity=2.8
max_throttle_rate=0.08
nav_proportional_control=11.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=22.0
gs_integrator_control=0.530
gs_derivative_control=0.02
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 10.5, -32.6, -8.4 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 10.5, 32.6, -8.4 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 0.80 //Scalar for fuel flow efficiency
min_throttle_limit=-0.299927

[TurbineEngineData]
fuel_flow_gain = 0.002 //Gain on fuel flow
inlet_area = 113.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 95000 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?

[jet_engine]
thrust_scalar = 1.0

[Views]
eyepoint = 90.0, -2.65, 2.25

[contact_points]
static_pitch = 0.1
static_cg_height = 17.56
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 17

point.0 = 1, 85.43, 0.00, -17.10, 1181.1, 0, 4.521, 68, 0.70, 2.5, 0.723, 13, 14, 0, 270, 270
point.1 = 1, -4.76, -20.0, -18.40, 1574.8, 1, 4.521, 0, 1.91, 2.5, 0.747, 13, 14, 2, 270, 270
point.2 = 1, -4.76, 20.0, -18.40, 1574.8, 2, 4.521, 0, 1.91, 2.5, 0.747, 12.9, 13.9, 3, 270, 270
point.3 = 2, 30.86, -31.6, -14.14, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.4 = 2, 30.86, 31.5, -14.14, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.5 = 2, -102, -36, 9, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.6 = 2, -38.4, -105, 12.5, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.7 = 2, -102, 36, 9, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.8 = 2, -38.4, 105, 12.5, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.9 = 2, -102, 0, 44.12, 2787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.10 = 2, -88.3844, 0, 0.0661, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.11 = 2, -57.091, 0, -6.708, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.12 = 2, -44.38, 0, -8.6234, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.13 = 2, -102.1003, 0, 3.9805, 2787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.14 = 2, 50.4709, 0, 13.0267, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.15 = 2, 105.0852, 0, 0.4276, 2787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.16 = 5, 0.0, 0.0, -10.0, 1600, 0.0, 0.0, 50.0, 0.0, 0.0, 1.00, 1.0, 1.0, 0, 0.0, 0.0