[fltsim.0]
title=SAAB 2000 
sim=SAAB2000
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=VP-BPL
ui_manufacturer=Saab
ui_type=2000 
ui_variation=Polet
description=2000       
atc_heavy=0
atc_airline=
atc_flight_number=BPL


[General]
atc_type=SAAB AIRCRAFT
atc_model=S2000
performance=Max cruising speed 682km/h (368kt) at 25,000ft, long range cruising speed 594km/h (321kt). Initial rate of climb 2250ft/min. Service ceiling 31,000ft. High speed range with 50 passengers and reserves 2185km (1180nm), range at long range cruising speed 2868km (1549nm).
[WEIGHT_AND_BALANCE]
max_gross_weight = 50265.000
empty_weight = 31423.000

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 =360.000000, 10.000000, 0.000000, 2.000000, longitudinal
station_load.1 =4000.000000, -3.380000, 0.000000, 2.000000, longitudinal
station_load.2 =4000.000000, -7.000000, 0.000000, 2.000000, longitudinal
station_load.5 =0.000000, 0.000000, 0.000000, 0.000000, longitudinal
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"

;Moments of Inertia
empty_weight_pitch_MOI  = 231763.000
empty_weight_roll_MOI   = 243463.000
empty_weight_yaw_MOI    = 327461.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.3=0.000000, 0.000000, 0.000000, 0.000000, Station 4

[flight_tuning]
cruise_lift_scalar     =1.321
parasite_drag_scalar   =0.475
induced_drag_scalar    =1.000
elevator_effectiveness =1.987
aileron_effectiveness  =2.287
rudder_effectiveness   =2.000
pitch_stability        =1.301
roll_stability         =1.367
yaw_stability          =1.512
elevator_trim_effectiveness =0.900
aileron_trim_effectiveness  =0.896
rudder_trim_effectiveness   =0.896

[GeneralEngineData]
engine_type = 5
Engine.0 = 9.500, -8.500, 2.300
Engine.1 = 9.500, 8.500, 2.300
fuel_flow_scalar        = 0.800
min_throttle_limit = -0.50                      //Minimum percent throttle.  Generally negative forturbine reverser

[propeller]
thrust_scalar           =1.278
propeller_type          = 0
propeller_diameter      = 13.000
propeller_blades        = 6
propeller_moi           = 115.000
beta_max                = 35.000
beta_min                = 20.200
min_gov_rpm             = 25555.000
prop_tc                 = 0.004
gear_reduction_ratio    = 10.600
fixed_pitch_beta        = 0.000
low_speed_theory_limit  = 80.000
prop_sync_available     = 1
prop_deice_available    = 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather     = 800.000
beta_feather            = 79.300
power_absorbed_cf       = 0.900
defeathering_accumulators_available= 0 
prop_reverse_available  = 1.000
minimum_on_ground_beta  = 1.000
minimum_reverse_beta    = -14.000

[TurbineEngineData]
fuel_flow_gain          = 0.011
inlet_area              = 1.100
rated_N2_rpm            = 29920.000
static_thrust           = 2000.000
afterburner_available= 0

[turboprop_engine]
power_scalar            =1.300
maximum_torque          = 7956.865
max_rpm_mechanical_efficiency_scalar=0.990
idle_rpm_mechanical_efficiency_scalar=0.618
max_rpm_friction_scalar=0.718
idle_rpm_friction_scalar=0.718


[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2 , 17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 17.0
light_nav          = 0, 5 , 17.0
light_beacon       = 0, 5 , 17.0
light_landing      = 0, 5 , 17.0
light_taxi         = 0, 5 , 17.0
light_strobe       = 0, 5 , 17.0
light_panel        = 0, 5 , 17.0

        //0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
        //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)

[contact_points]
point.0 = 1, 28.07, 0, -6.8, 1181, 0, 0.84, 39.9, 0.6, 2, 0.952, 4.8, 4.8, 0, 0, 0
point.1 = 1, -10, -12.87, -7.14, 1574, 1, 1.22, 0, 0.642, 2.5, 0.815, 4.5, 5.2, 2, 0, 0
point.2 = 1, -10, 12.87, -7.14, 1574, 2, 1.22, 0, 0.642, 2.5, 0.815, 4.8, 4.9, 3, 0, 0
point.3 = 2.000, -3.330, -41.640, 3.153, 787.000, 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, -3.330, 41.640, 3.153, 787.000, 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, -38.060, 0.000, 0.000, 787.000, 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, 32.62, 0, -0.98, 787, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0

static_pitch = -1
static_cg_height = 6.8
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 7

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  0.0     //Flap angle that activates warning at idle
flap_limit_power   = 16.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 1.5  //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 = 22.54, -2.0, 4.2




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

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
elevator = 150, 250
aileron  = 150, 250
rudder   = 150, 250

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0

[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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
//light.0 = 3,   0.56, -28.41,  1.97, fx_bsmpnavred ,
//light.1 = 3,   0.56,  28.41,  1.97, fx_bsmpgreen ,
//light.2 = 3, -31.20,   0.00,  9.09, fx_bsmpnav ,
//light.3 = 2,   0.89, -27.89,  1.77, fx_bsmpstrobe ,
//light.4 = 2,   0.89,  27.89,  1.77, fx_bsmpstrobe ,
//light.5 = 1, -25.49,   0.00,  9.74, fx_bsmpbeacon ,
//light.6 = 2,  -4.55,   0.00, -1.85, fx_bsmpstrobe ,
//light.7 = 4,   5.91,   0.00,  1.64, fx_vclight,

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

[fuel]
LeftMain  = 0.000, -14.430, 0.000, 766.823, 0.000
LeftAux   = 0.000, 0.000, 0.000, 0.000, 0.000
RightMain = 0.000, 14.430, 0.000, 766.823, 0.000
RightAux  = 0.000, 0.000, 0.000, 0.000, 0.000
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=1


[airplane_geometry]
wing_area               = 724.000
wing_span               = 70.000
wing_root_chord         = 10.250
wing_dihedral           = 1.999
wing_incidence          = -0.494
wing_twist              = -1.000
oswald_efficiency_factor= 1.000
wing_winglets_flag      = 0
wing_sweep              = 0.000
wing_pos_apex_lon       = 0.000
wing_pos_apex_vert      = 0.000
htail_area              = 245.000
htail_span              = 26.000
htail_pos_lon           = -37.000
htail_pos_vert          = 1.000
htail_incidence         = 0.500
htail_sweep             = 9.000
vtail_area              = 253.000
vtail_span              = 18.000
vtail_sweep             = 0.000
vtail_pos_lon           = -35.960
vtail_pos_vert          = 5.840
elevator_area           = 16.985
aileron_area            = 13.400
rudder_area             = 51.930
elevator_up_limit       = 15.498
elevator_down_limit     = 15.000
aileron_up_limit        = 18.000
aileron_down_limit      = 18.000
rudder_limit            = 32.000
elevator_trim_limit     = 15.000
spoiler_limit           = 59.989
spoilerons_available    = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000

[Reference Speeds]
flaps_up_stall_speed    = 115.000
full_flaps_stall_speed  = 90.800
cruise_speed            = 350.000
max_mach                = 0.78
max_indicated_speed= 400.000

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
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
pitch_takeoff_ga= 8.000
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000

[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds

[exits]
number_of_exits = 3
exit_rate.0 = 0.1
exit_rate.0 = 0.1

[folding_wings]
wing_fold_system_type=4
fold_rates=0.12,0.11

[stall_warning]
type=1

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 280.000
blowout-speed= 320.000
lift_scalar= 1.300
drag_scalar= 2.9
pitch_scalar= 0.550
flaps-position.0= 0.000, 0.000
flaps-position.1= 6.998, 0.000
flaps-position.2= 19.997, 0.000
flaps-position.3= 29.995, 0.000
flaps-position.4= 34.994, 0.000



[TailHook] 
tailhook_length = 4 
tailhook_position = -15, 0, -1 
cable_force_adjust = 1