[fltsim.0]
title=SAT Dash8-300
model=
texture=sat
sim=TFS_Dash8-300
atc_airline=LIAT
atc_id=SATAIR
atc_heavy=
ui_manufacturer=The Fruit Stand
ui_type=Dash 8-300
ui_variation=Sat RA67251
description=Repaint by Maksim Rudakov  www.unitedtrafficteam.net
atc_parking_types=GATE
atc_parking_codes=SHU

//The Fruit Stand TFS Dash8 Q300 (Standard) FDE v1.1 Mar/5/2009

[General]
atc_type=BOMBARDIER 
atc_model=DH8C 
editable=0 
performance=For AI pilots only! Do not attemp to fly it as UI.You've been warned! 

[weight_and_balance]

// ACM V2.5
max_gross_weight = 48000
empty_weight = 27800   
reference_datum_position = 3, 0, -5
empty_weight_CG_position = 5.8, 0, 0
empty_weight_pitch_MOI = 261232    
empty_weight_roll_MOI = 129080  
empty_weight_yaw_MOI = 293823  
empty_weight_coupled_MOI = 0
max_number_of_stations = 6

station_load.0 = "170,  30.0, -2.0, 0.0, Pilot"
station_load.1 = "170,  30.0,  2.0, 0.0, Co-Pilot"
station_load.2 = "170, 0.0, -2.0, 0.0, Passenger"
station_load.3 = "170, 0.0,  2.0, 0.0, Passenger"
station_load.4 = "170, -30.3, -2.0, 0.0, Passenger"
station_load.5 = "170, -30.3,  2.0, 0.0, Passenger"


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2.25, -44.84, 5.55, fx_navred
light.1 = 3, 2.25, 44.84, 5.55, fx_navgre
light.2 = 2, 2.55, -44.75, 5.55, fx_strobe
light.3 = 2, 2.55, 44.75, 5.55, fx_strobe
light.4 = 1, -38.3, 0, 17.9, fx_beacon
light.5 = 2, -40.4, 0.06, 1.45, fx_strobe
light.6 = 2, -40.4, -0.06, 1.45, fx_strobe

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.0
min_throttle_limit = -0.35
engine.0 = 8.3, -13.3, 3, 
engine.1 = 8.3, 13.3, 3, 

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1


[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 1

LeftMain = 6, -13.3, 4, 900, 0
RightMain =6, 13.3, 4, 900, 0


[contact_points]
static_pitch = -0.7
static_cg_height = 12.2
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 7

point.0 = 1, 33, 0, -7.65, 1200, 0, 0.8, 55, 0.496, 2.5, 0.93, 4.8, 4.8, 0, 195, 195
point.1 = 1, 0, -14.2, -7.72, 1600, 1, 1.3, 0, 0.642, 2.6, 0.95, 5.2, 5.2, 2, 195, 195
point.2 = 1, 0, 14.2, -7.72, 1600, 2, 1.3, 0, 0.642, 2.6, 0.95, 4.9, 4.9, 3, 195, 195
point.3 = 2, 2.6, -44.5, 5.5, 790, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 2.6, 44.5, 5.5, 790, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -38.55, 0, 0.8, 790, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 38, 0, -4.55, 790, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0


[keyboard_response]
elevator = 150.0, 250.0
aileron = 150.0, 250.0
rudder = 150.0, 250.0


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 9000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0,0,0,1.6459,0.7990,0.7990,0.0137,1.5772,1.5985,1.5985
//ACM_AREAW2// 0.0274,1.5089,2.3977,2.3977,0.0417,1.4407,3.1970,3.1970,0.0557,1.3724
//ACM_AREAW3// 3.9962,3.9962,0.0697,1.3041,4.7954,4.7954,0.0837,1.2358,5.5946,5.5946
//ACM_AREAW4// 0.0974,1.1675,6.3940,6.3940,0.1115,1.0987,7.1932,7.1932,0.1254,1.0305
//ACM_AREAH1// 0,0,0,1.7474,0.2912,0.2912,0.1058,1.7661,0.5824,0.5824
//ACM_AREAH2// 0.2117,1.7847,0.8737,0.8737,0.3179,1.8034,1.1648,1.1648,0.4239,1.8220
//ACM_AREAH3// 1.4562,1.4562,0.5299,1.8406,1.7474,1.7474,0.6359,1.8593,2.0387,2.0387
//ACM_AREAH4// 0.7419,1.8779,2.3299,2.3299,0.8478,1.8961,2.6212,2.6212,0.9538,1.9148
//ACM_AREAV1// 0,0,0,2.2555,0.2506,0.2506,0.2099,2.2853,0.5012,0.5012
//ACM_AREAV2// 0.4205,2.3152,0.7518,0.7518,0.6308,2.3450,1.0024,1.0024,0.8410,2.3749
//ACM_AREAV3// 1.2530,1.2530,1.0513,2.4047,1.5036,1.5036,1.2617,2.4346,1.7539,1.7539
//ACM_AREAV4// 1.4720,2.4644,2.0048,2.0048,1.6821,2.4941,2.2555,2.2555,1.8926,2.5241
//ACM_CAREAW1// 3.5966,3.5966,0.8855,1.2149,3.9962,3.9962,0.8927,1.2051,4.3958,4.3958
//ACM_CAREAW2// 0.8996,1.1957,4.7954,4.7954,0.9064,1.1864,5.1950,5.1950,0.9136,1.1769
//ACM_CAREAW3// 5.5946,5.5946,0.9204,1.1675,5.9944,5.9944,0.9275,1.1576,6.3940,6.3940
//ACM_CAREAW4// 0.9344,1.1483,6.7936,6.7936,0.9415,1.1390,7.1932,7.1932,0.9484,1.1295
//ACM_CAREAH1// 0,0,0.8737,1.7474,0.2912,0.2912,0.9797,1.8098,0.5824,0.5824
//ACM_CAREAH2// 1.0857,1.8717,0.8737,0.8737,1.1914,1.9342,1.1648,1.1648,1.2977,1.9967
//ACM_CAREAH3// 1.4562,1.4562,1.4033,2.0590,1.7474,1.7474,1.5096,2.1214,2.0387,2.0387
//ACM_CAREAH4// 1.6158,2.1837,2.3299,2.3299,1.7216,2.2460,2.6212,2.6212,1.8278,2.3083
//ACM_CAREAV1// 0,0,0.5637,1.6914,0.2506,0.2506,0.7741,1.8114,0.5012,0.5012
//ACM_CAREAV2// 0.9843,1.9313,0.7518,0.7518,1.1947,2.0518,1.0024,1.0024,1.4048,2.1719
//ACM_CAREAV3// 1.2530,1.2530,1.6153,2.2918,1.5036,1.5036,1.8256,2.4119,1.7539,1.7539
//ACM_CAREAV4// 2.0359,2.5320,2.0048,2.0048,2.2460,2.6521,2.2555,2.2555,2.4563,2.7722
wing_area = 605.0
wing_span = 90
wing_root_chord = 10.5
wing_dihedral = 2.0
wing_incidence = 0.8
wing_twist = -1.5
oswald_efficiency_factor = 0.7
wing_winglets_flag = 0
wing_sweep = 4.0
wing_pos_apex_lon = 6.8
wing_pos_apex_vert = 3.5
htail_area = 200.0
htail_span = 29.3
htail_pos_lon = -36.8
htail_pos_vert = 17.0
htail_incidence = 0.0
htail_sweep = 8.0
vtail_area = 152.0
vtail_span = 14.9
vtail_sweep = 30.0
vtail_pos_lon = -27.5
vtail_pos_vert = 3.1
elevator_area = 17.0
aileron_area = 13.5
rudder_area = 7.3
elevator_up_limit = 13.0
elevator_down_limit = 19
aileron_up_limit = 16.0
aileron_down_limit = 19.0
rudder_limit = 30.0
elevator_trim_limit = 15.0
spoiler_limit = 50.0
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[TurbineEngineData]
fuel_flow_gain=0.011                 //Gain on fuel flow
inlet_area=4.6                   //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                 //RPM, second stage compressor rated value
static_thrust=580                   //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar=1.35                   //Scalar on Turboprop power
maximum_torque=5878                  //Maximum torque available (ft-lbs)

[flight_tuning]
cruise_lift_scalar=0.80 
parasite_drag_scalar=0.9 
induced_drag_scalar=0.9 
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 

[propeller]
thrust_scalar=1.0                   //Propeller thrust scalar
propeller_type=0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=13.0                  //Propeller Diameter, (feet)
propeller_blades=4                     //Number of propeller blades
propeller_moi=54                    //Propeller moment of inertia
beta_max=45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=12                    //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520                 //Miminum governed RPM
prop_tc=0.004                 //Prop time-constant
gear_reduction_ratio=17.0                  //Propeller gear reduction ratio
fixed_pitch_beta=0                     //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80                    //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1                     //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1                     //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=1               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=700                   //Minimum RPM for prop feathering
beta_feather=79.3                  //Feathering pitch angle (degrees)
power_absorbed_cf=0.9                   //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available=1                     //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0                 //Minimum pitch angle in reverse, (degrees)

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    = 15.0     //Flap angle that activates warning at idle
flap_limit_power   = 30.0     //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 0.16  //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2
[Views]
eyepoint=-5.0, -1.45, -7.0      //(feet) longitudinal, lateral, vertical distance from reference datum

[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 8                                    // seconds
flaps-position.0 = 0                                    // degrees, KIAS
flaps-position.1 = 5                                    // degrees, KIAS
flaps-position.2 = 10                                   // degrees, KIAS
flaps-position.3 = 15                                   // degrees, KIAS
flaps-position.4 = 20                                   // degrees, KIAS
flaps-position.5 = 25                                   // degrees, KIAS
flaps-position.6 = 30                                   // degrees, KIAS
flaps-position.7 = 35                                   // degrees, KIAS
flaps-position.8 = 40                                   // degrees, KIAS

lift_scalar = 0.2

damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,0
[Reference Speeds]
flaps_up_stall_speed=110.0                  //Knots True (KTAS)
full_flaps_stall_speed=125.0                  //Knots True (KTAS)
cruise_speed=360.0                 //Knots True (KTAS)
max_mach                = 0.58
max_indicated_speed     = 285                   //Red line (KIAS)

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1500.0 
autothrottle_available=0 
pitch_takeoff_ga=5.0 
max_pitch=8.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0 
max_pitch_velocity_hi_alt=1.8
max_pitch_velocity_lo_alt_breakpoint=25000.0  
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=1ґ
[direction_indicators]
direction_indicator.0=3,0