[fltsim.0]
title=B1900D Air Labrador
sim=Beech_B1900
model=
panel=b1909
sound=
texture=AirLab
kb_checklists=Beech_B1900_check
kb_reference=Beech_B1900_ref
atc_id=C-GTMB
ui_manufacturer=Beechcraft
ui_type=B1900D
ui_variation=Air Labrador 
description=The Beechcraft 1900 Airliner is a 19 passenger, pressurized twin-engine turboprop airplane manufactured by the Beechcraft Division of the Raytheon Company (now Hawker Beechcraft). It was designed as, and is primarily used as, a regional airliner. It is also used commercially as a freight aircraft, corporate transport, and by the United States military and other governments.
The B1900D is designed to carry passengers in all weather conditions from airports with relatively short runways for distances of less than 600 miles. In terms of the number of aircraft built and its continued use by many passenger airlines and other users, it is the most successful 19-passenger airliner in history

[General]
atc_type=BEECH
atc_model=B190
editable=1
performance=Max speed: 330 mph\nCruising Speed at 15,000 ft 300mph true air speed\nRange: 1720 nm\nService Ceiling: 25,000\nMax weight: 16,949\nPassenger: 19
Category=airplane

[WEIGHT_AND_BALANCE]
max_gross_weight = 20000.00
empty_weight = 10593.00
reference_datum_position     = 0.00, 0.00, 0.00
empty_weight_CG_position     = 0.00, 0.00, 0.00
max_number_of_stations =20

station_load.0 = "170,  13.0 -1.75, 0.0, Pilot"                  //Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170,  13.0  1.75, 0.0, Front Passenger"        //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "4500, -3.0,  0.0, 0.0, Payload"                //Payload  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)



;Moments of Inertia
empty_weight_pitch_MOI  = 80000.00
empty_weight_roll_MOI   = 36000.00
empty_weight_yaw_MOI    = 75000.00
empty_weight_coupled_MOI= 0.00
CG_forward_limit= 0.00
CG_aft_limit= 1.00


[flight_tuning]
cruise_lift_scalar     =1.00
parasite_drag_scalar   =0.90
induced_drag_scalar    =0.90
elevator_effectiveness =1.00
aileron_effectiveness  =1.00
rudder_effectiveness   =1.00
pitch_stability        =1.00
roll_stability         =1.00
yaw_stability          =1.00
elevator_trim_effectiveness =1.00
aileron_trim_effectiveness  =1.00
rudder_trim_effectiveness   =1.00

[GeneralEngineData]
engine_type = 5
Engine.0 = 6.50, -8.60, 0.60
Engine.1 = 6.50,  8.60, 0.60
fuel_flow_scalar        = 0.75
min_throttle_limit=-0.250

[propeller]
thrust_scalar           =1.00
propeller_type          = 0
propeller_diameter      = 8.60
propeller_blades        = 4
propeller_moi           = 22.00
beta_max                = 45.00
beta_min                = 15.20
min_gov_rpm             = 25520.00
prop_tc                 = 0.004
gear_reduction_ratio    =17.6  // 11.60
fixed_pitch_beta        = 0.00
low_speed_theory_limit  = 80.00
prop_sync_available     = 1
prop_deice_available    = 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather     = 700.00
beta_feather            = 79.30
power_absorbed_cf       = 0.90
defeathering_accumulators_available= 0 
prop_reverse_available  = 1
minimum_on_ground_beta  = 1.00
minimum_reverse_beta    = -14.00

[TurbineEngineData]
fuel_flow_gain          = 0.011
inlet_area              = 1.00
rated_N2_rpm            = 29920.00
static_thrust           = 150   // 250.00
afterburner_available= 0

[turboprop_engine]
power_scalar            =1.45
maximum_torque          =3270.0 // 4270.00
max_rpm_mechanical_efficiency_scalar=1.00
idle_rpm_mechanical_efficiency_scalar=1.00
max_rpm_friction_scalar=1.00
idle_rpm_friction_scalar=1.00

[Reference Speeds]
flaps_up_stall_speed    = 101.00
full_flaps_stall_speed  = 84.00
cruise_speed            = 280.00	//knots over the ground speed at 20,000 ft.
normal_cruise_speed	= 260.00
max_indicated_speed=359.00
max_mach=0.579980
max_level_speed=300

[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, 10, 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 20, 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

[contact_points]
//Classes...What type of point    0=Unused or Ignore
//                                                      1=Wheel
//                                                      2=Scrape point
//                                                      4=Float
//                                                      5=Float Rudder
//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 / Water Rudder Effectiveness  (0=Undamped, 1=Critically Damped) / 1.0 = normal
//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=1.000,21.830,0.000,-5.700,1181, 0, 0.75, 39.9, 0.296, 2.5, 0.9516,  4.8,  4.8, 0, 184.0, 184.0
point.1=1.000,-2.000,-8.600,-5.400,1574, 1, 0.75,  0.0, 0.642, 2.5, 0.8152,  4.5,  5.2, 2, 184.0, 184.0
point.2=1.000,-2.000,8.600,-5.400,1574, 2, 0.75,  0.0, 0.642, 2.5, 0.8152,  4.8,  4.9, 3, 184.0, 184.0
point.3=2.000,-2.200,-29.300,3.200,2360.907127,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,5.000,0.000,0.000
point.4=2.000,-2.200,29.300,3.200,2360.907127,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,6.000,0.000,0.000
point.5=2.000,-35.000,0.000,11.000,2360.907127,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,9.000,0.000,0.000
point.6=2.000,23.600,-0.000,-0.500,1574.803150,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,4.000,0.000,0.000
static_pitch = 1.9
static_cg_height = 5.10
gear_system_type=1      //Hydraulic

[Views]
//eyepoint=13.267,-0.619,2.607
//eyepoint=13.104,-0.815,2.77
eyepoint=13.267,-1.100,2.607

[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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3,  0.28, -28.40,  1.60, fx_navred ,
light.1 = 3,  0.30,  28.40,  1.60, fx_navgre ,
light.2 = 3, -35.00,   0.00,  11.00, fx_navwhi ,
light.3 = 2,  -1.80, -29.05,  2.10, fx_strobe ,
light.4 = 2,  -1.80,  29.05,  2.10, fx_strobe ,
light.5 = 1, -29.20,   0.00, 11.6,fx_PADbeaconh ,
light.6 = 1,  -4.80,   0.00, -2.30, fx_PADbeaconh ,
light.7 = 4,  12.70,   -1.10,2.0,  fx_vclighth,
light.8 = 4,  12.70, 1.10, 2.0,  fx_vclighth,
light.9 = 4, 12.00, 1.00, 2.10,  fx_vclightwhite ,
light.10 = 4, 10.00, 1.00, 2.10,  fx_vclightwhite ,
light.11 = 4,  6.00, 1.00, 2.10,  fx_vclightwhite,
light.12 = 4, 0.00, 1.00, 2.10,  fx_vclightwhite,


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

[fuel]
LeftMain  = 0.00,-14.50, -1.00, 300.00, 0.00  // 253.00
'LeftAux   = 0.00, -6.00, -1.50,  79.50, 0.00
RightMain = 0.00, 14.50, -1.00, 300.00, 0.00
'RightAux  = 0.00,  6.00, -1.50,  79.50, 0.00
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=0

[airplane_geometry]
wing_area               = 310.00
wing_span               = 58.00
wing_root_chord         = 6.60
wing_dihedral           = 6.00
wing_incidence          = 1.00
wing_twist              = -1.50
oswald_efficiency_factor= 0.70
wing_winglets_flag      = 1
wing_sweep              = 3.00
wing_pos_apex_lon       = 2.00
wing_pos_apex_vert      = -1.00
htail_area              = 76.00
htail_span              = 18.20
htail_pos_lon           = -27.50
htail_pos_vert          = 11.00
htail_incidence         = 0.00
htail_sweep             = 20.00
vtail_area              = 50.00
vtail_span              = 6.50
vtail_sweep             = 35.00
vtail_pos_lon           = -23.50
vtail_pos_vert          = 4.50
elevator_area           = 14.00
aileron_area            = 13.00
rudder_area             = 17.00
elevator_up_limit       = 17.00
elevator_down_limit     = 15.50
aileron_up_limit        = 18.00
aileron_down_limit      = 18.00
rudder_limit            = 30.00
elevator_trim_limit     = 15.00
spoiler_limit           = 60.00
spoilerons_available    = 0
aileron_to_spoileron_gain = 0.00
min_ailerons_for_spoilerons = 0.00
min_flaps_for_spoilerons = 0.00
auto_spoiler_available=0
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000

[autopilot]
autopilot_available= 1
use_no_default_pitch=1
use_no_default_bank=1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 0
pitch_takeoff_ga=8.00
max_pitch=10.00
max_pitch_acceleration=1.00
max_pitch_velocity_lo_alt=2.00
max_pitch_velocity_hi_alt=1.50
max_pitch_velocity_lo_alt_breakpoint=20000.00
max_pitch_velocity_hi_alt_breakpoint=28000.00
max_bank=25.00
max_bank_acceleration=1.80
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.250
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.520
gs_integrator_control=0.260
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.00
default_pitch_mode=0
default_bank_mode=0

[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

[Flaps.0]
type= 1
span-outboard= 0.30
extending-time= 5.00
system_type= 0
damaging-speed= 250.00
blowout-speed= 300.00
flaps-position.0= 0.00, 0.00
flaps-position.1= 5.00, 0.00
flaps-position.2=17.00, 0.00
flaps-position.3=28.00, 0.00
flaps-position.4=35.00, 0.00

[Flaps.1]
type= 1
span-outboard= 0.30
extending-time= 5.00
system_type= 0
damaging-speed= 250.00
blowout-speed= 300.00
flaps-position.0= 0.00, 0.00
flaps-position.1= 5.00, 0.00
flaps-position.2=17.00, 0.00
flaps-position.3=28.00, 0.00
flaps-position.4=35.00, 0.00

[brakes]
toe_brakes_scale=1.00
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.00

[stall_warning]
type=1
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[exits]
number_of_exits=2
exit_rate.0=0.5                             ;Percent per second
exit_rate.1=0.5              

[pitot_static]
pitot_heat=1.000000
[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