[fltsim.0]
title=Bv-141 B-05
sim=BV-141B05
model=
panel=
sound=
texture=
checklists=


[WEIGHT_AND_BALANCE]
max_gross_weight= 12570.000
empty_weight = 10360.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, 0.000

max_number_of_stations = 50

station_load.0 = 170.000, 0.000, 0.000, -0.700
station_load.1 = 170.000, -1.500, 0.000, -0.400
station_load.2 = 170.000, -4.200, 0.000, -1.500


;Moments of Inertia
empty_weight_pitch_MOI  = 24930.000
empty_weight_roll_MOI  = 16500.000
empty_weight_yaw_MOI  = 32047.000

[flight_tuning]
cruise_lift_scalar     =1.000
parasite_drag_scalar   =1.000
induced_drag_scalar    =1.000
elevator_effectiveness =1.000
aileron_effectiveness  =1.000
rudder_effectiveness   =1.000
pitch_stability        =1.000
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[piston_engine]
power_scalar =1.000

[propeller]
thrust_scalar =1.000

[exits]
number_of_exits = 1
exit_rate.0 = 0.4  				;Percent per second

[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0

[contact_points]
	//0  Class
	//1  Longitudinal Position        (feet)
	//2  Lateral Position             (feet)
	//3  Vertical Position            (feet)
	//4  Impact Damage Threshold      (Feet Per Minute)
	//5  Brake Map 		         (0=None, 1=Left, 2=Right)
	//6  Wheel Radius	         (feet)
	//7  Steer Angle		         (degrees)
	//8  Static Compression           (feet)  (0 if rigid)
	//9  Max/Static Compression Ratio
	//10 Damping Ratio	         (0=Undamped, 1=Critically Damped)
	//11 Extension Time	         (seconds)
	//12 Retraction Time	         (seconds)
	//13 Sound Type
	//14 Airspeed limit for retraction (KIAS)
	//15 Airspeed that gear gets damage at (KIAS)


point.0= 1.000, -33.170, 0.000, -5.593, 2500.000, 0.000, 0.820, 80.000, 0.500, 2.500, 0.900, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, 3.281, -9.550, -12.630, 2200.000, 1.000, 1.706, 0.000, 0.855, 1.300, 0.950, 3.000, 4.000, 2.000, 0.000, 0.000
point.2= 1.000, 3.281, 9.550, -12.630, 2200.000, 2.000, 1.706, 0.000, 0.855, 1.300, 0.950, 4.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, 0.000, -27.030, -1.911, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, 0.000, 31.330, -1.911, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -33.170, -4.265, -3.551, 2400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 13.190, -4.265, -3.551, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 2.000, 11.880, 4.265, -4.043, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000


static_pitch= 11.100
static_cg_height= 10.651


[fuel]
fuel_type=1.000000
number_of_tank_selectors=1
LeftMain= 10.000, 0.000, 0.000, 180.000, 0.000
RightMain= -10.000, 0.000, 0.000, 180.000, 0.000
Center1= 0.000, 0.000, 0.000, 120.000, 0.000

[airplane_geometry]
wing_area= 482.000
wing_span= 57.280
wing_root_chord= 11.480
wing_dihedral= 2.100
wing_incidence= 1.000
wing_twist= 0.000
oswald_efficiency_factor= 0.900
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 38.750
htail_span= 14.440
htail_pos_lon= -24.930
htail_pos_vert= 3.182
htail_incidence= 0.000
htail_sweep= 9.730
vtail_area= 23.680
vtail_span= 8.793
vtail_sweep= 18.000
vtail_pos_lon= -18.833
vtail_pos_vert= 1.837
elevator_area= 29.600
aileron_area= 26.500
rudder_area= 17.150
elevator_up_limit= 29.000
elevator_down_limit= 29.000
aileron_up_limit= 22.000
aileron_down_limit= 19.000
rudder_limit= 28.000
elevator_trim_limit= 20.000
spoiler_limit= 0.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[GeneralEngineData]
engine_type= 0
Engine.0= 0.000, 0.000, 0.000
fuel_flow_scalar= 1.000

[Reference Speeds]
flaps_up_stall_speed= 64.000
full_flaps_stall_speed= 53.000
cruise_speed= 210.000

[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000

[direction_indicators]
direction_indicator.0=1,0

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.0
autothrottle_available=1
pitch_takeoff_ga=8.000000
use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = bank mode. 
use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = pitch mode.


[Views]
eyepoint=0,0,0
view_forward_WINDOWS=MAIN_PANEL
VIEW_FORWARD_ZOOM=0.75 

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=4,0.8,0.9,0,fx_vclight

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=0, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[TailHook]
tailhook_length=4
tailhook_position = -32.25, 0.0, -5.8
cable_force_adjust = 1.0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1


[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5#
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1#
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[Flaps.0]
type= 1
span-outboard= 0.116
extending-time= 5
system_type= 0
damaging-speed= 180
blowout-speed= 260
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 30.000, 0.000
flaps-position.3= 60.000, 0.000