/////////////////////////////////////////////////////////
//
//			VERSION 1.03 Pinhas
//		 
//21DEC10
///////////////////////////////////////////////////////

[fltsim.0]
title=PMDG Beech 1900C	
sim=beech_1900C P13
model=
panel=
sound=
texture=
kb_checklists=beech_1900C_check
kb_reference=beech_1900C_check_ref
atc_id_color=0xffffffffff
atc_id=N1900C
ui_manufacturer=Beechcraft-PMDG Express
ui_type=1900C 2D Cockpit
ui_variation=PMDG Passenger
description="PMDG Beechcraft 1900C. \nwww.precisionmanuals.com \nFor support contact [email protected]"

[fltsim.1]
title=PMDG  Beech 1900C - VC	
sim=beech_1900C P13
model=vc
panel=vc
sound=
texture=
kb_checklists=beech_1900C_check
kb_reference=beech_1900C_check_ref
atc_id_color=0xffffffffff
atc_id=N190C
ui_manufacturer=Beechcraft-PMDG Express
ui_type=1900C with VC
ui_variation=PMDG Passenger
description="PMDG Beechcraft 1900C. \nwww.precisionmanuals.com \nFor support contact [email protected]"

[General]
atc_type=BEECH
atc_model=B190
editable=0
performance="Cruise Speed\t\n263 kts            302 mph          486 kmph\/h\n\nEngines\t\nPratt & Whitney PT6A-65B 1,100 shp\n\nMaximum Range Passenger Payload\t\n629nm          \t   1,165km\n\nService Ceiling\t\n25,000 ft         7,620 m\n\nFuel Capacity\t\n667 U.S. gal      4,464Lb\n\nMaximum Takeoff Weight \n16,600 lb\t          7,530 kg\n\nLength\t\n57.9 ft\t           17.64 m\n\nWingspan\t\n54.5 ft\t           16.61 m\n\nSeating (Crew + Pax)\t\n2 + 19\n"

[EXITS]
number_of_exits = 2

[WEIGHT_AND_BALANCE]
reference_datum_position     =  23.711, 0.0, 1.40
empty_weight_CG_position     = -21.358, 0.0, 0.25
max_gross_weight = 16710.0
empty_weight = 9750.0     
CG_forward_limit=0.150
CG_aft_limit=0.390

max_number_of_stations = 50 // This is a MAXIMUM load for each station. Check fuel and weight before takeoff !!!

station_load.0 = "200.0,   -9.24, -1.2, 2.0, Pilot"      
station_load.1 = "200.0,   -9.24,  1.2, 2.0, Co-Pilot"
station_load.2 = "150.0, -5.41,  0.0, 0.0, Nose Baggage"
station_load.3 = "250.0, -13.58,  0.0, 0.0, Fwd Cab Bagg"
station_load.4 = "820.0, -17.92,  0.0, 0.0, Fwd Cabin"
station_load.5 = "2870.0, -29.17,  0.0, 0.0, Aft Cabin"
station_load.6 = "880.0, -40.29,  0.0, 0.0, Aft Cargo Fwd"
station_load.7 = "530.0, -44.41,  0.0, 0.0, Aft Cargo Aft"
station_load.8 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.9 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.10 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.11 = "0.0, 0.0, 0.0, 0.0, FsStation"
 

;Moments of Inertia
empty_weight_pitch_MOI  = 41622.0
empty_weight_roll_MOI   = 39529.0
empty_weight_yaw_MOI    = 40899.0
empty_weight_coupled_MOI= 140.0

[fuel]
LeftMain  = -22.21, -14.43, -1.0, 241.9, 0.6     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux   = -21.70,  -1.44, -1.7,  92.7, 0.4     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -22.21,  14.43, -1.0, 241.9, 0.6     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux  = -21.70,   1.44, -1.7,  92.7, 0.4     //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=1

[propeller]
thrust_scalar           = 1.0                   //Propeller thrust scalar
propeller_type          = 0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter      = 9.125                 //Propeller Diameter, (feet)
propeller_blades        = 4                     //Number of propeller blades
propeller_moi           = 44.8                  //Propeller moment of inertia
beta_max                = 45.0                  //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min                = 6.2                   //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm             = 31345.6               //Miminum governed RPM (1400 RPM)
prop_tc                 = 0.008                 //Prop time-constant
gear_reduction_ratio    = 22.39                 //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     = 700.0                 //Minimum RPM for prop feathering
beta_feather            = 79.0                  //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  = 7.0                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta    = -14.0                 //Minimum pitch angle in reverse, (degrees)
rotation=1,1

[TurbineEngineData]
fuel_flow_gain          = 0.018                 //Gain on fuel flow
inlet_area              = 1.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm            = 38062.5               //RPM, second stage compressor rated value
static_thrust           = 183.23                //Lbs, max rated static thrust at Sea Level (1700 RPM)

[turboprop_engine]
power_scalar            = 1.0                   //Scalar on Turboprop power
maximum_torque          = 3536.0                //Maximum torque available (ft-lbs)
max_rpm_mechanical_efficiency_scalar=0.960
idle_rpm_mechanical_efficiency_scalar=0.975

[GeneralEngineData]
engine_type = 5                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -16.79, -8.52, 1.7                   //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -16.79,  8.52, 1.7                   //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar   = 1.0                      //Scalar for fuel flow efficiency. Was 0.802.
min_throttle_limit = -0.25;                     //Minimum percent throttle.  Generally negative for turbine reverser

[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

[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 = 1.0  //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 = -9.539, -1.600, 3.0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 5=landing 9=logo
light.0 = 3,  -22.902, -27.500,  1.500, fx_navred_pmdg1900 ,                	//Nav Left
light.1 = 3,  -22.702, -27.250,  1.472, fx_navred_pmdg1900 ,                	//Nav Left
light.2 = 3,  -22.902,  27.500,  1.500, fx_navgre_pmdg1900 ,              	//Nav Right
light.3 = 3,  -22.702,  27.250,  1.472, fx_navgre_pmdg1900 ,                	//Nav Right
light.4 = 1,  -28.900,   0.000, -1.800, fx_beacon_pmdg_b1900,               	//Beacon Bottom
light.5 = 1,  -28.900,   0.000, -1.800, fx_navwhi,					//Beacon Bottom
light.6 = 7,  -55.750,   0.000,  9.048, fx_navwhi ,                         	//Position Rear
light.7 = 1,  -51.750,   0.000,  9.300, fx_navwhi ,                         	//Beacon Rear Top
light.8 = 1,  -51.750,   0.000,  9.300, fx_beacon_pmdg_b1900,                //Beacon Rear Top
light.9 = 9,  -54.000,  -2.500,  6.648, fx_pmdglogo1900,                    	//Logo Light Tail
light.10= 9,  -54.000,   2.500,  6.648, fx_pmdglogo1900,                 	//Logo Light Tail
light.11= 2,  -22.500, -27.000,  1.485, fx_strobe_pmdg1900,                	//Strobe White Left
light.12= 2,  -22.500,  27.000,  1.485, fx_strobe_pmdg1900,                	//Strobe White Right
light.13= 8,  -18.902, -18.500,  1.500, fx_pmdglogo1900,                	//Wing Left
light.14= 8,  -18.902,  18.500,  1.500, fx_pmdglogo1900,                	//Wing Right

[SMOKESYSTEM]
smoke.0=0.00, -10.00, 0.00, fx_pmdg1900ccabin

[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 = 130, 200
aileron  = 180, 200
rudder   = 130, 200

[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

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

[stall_warning]
type=2

[airplane_geometry]
wing_area               = 303.0                 //Square feet
wing_span               = 54.50                 //Feet
wing_root_chord         = 9.29                  //Feet
wing_dihedral           = 6.0                   //Degrees
wing_incidence          = 0.5                   //Degrees [inop]
wing_twist              = -2.0	                //Degrees [inop]
oswald_efficiency_factor= 0.65              //Measure of lift effeciency of wing. Was 0.791.
wing_winglets_flag      = 0                     //Are winglets available?  Was 1.
wing_sweep              = 1.0                   //Degrees, wing leading edge
wing_pos_apex_lon       = -19.607               //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = -0.38                 //Feet, vertical distance from reference point, positive going up
htail_area              = 132.0                 //Square feet	[85.38 + 31.68 + 15.00 effective increased by fixed fins and stabs]
htail_span              = 18.48                 //Feet
htail_pos_lon           = -51.61                //Feet, longitudinal distance from reference point, negative going aft [effective]
htail_pos_vert          = 5.832                 //Feet, vertical distance from reference point, positive going up [effective]
htail_incidence         = 0.0                   //Degrees
htail_sweep             = 22.5                  //Degrees, horizontal tail leading edge [effective]
vtail_area              = 86.29                 //Square feet
vtail_span              = 6.93                  //Feet, tip to body
vtail_sweep             = 40.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -52.08                //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 9.33                  //Feet, vertical distance from reference point, positive going up
elevator_area           = 30.0                  //Square feet
aileron_area            = 25.34                 //Square feet
rudder_area             = 25.68                 //Square feet
elevator_up_limit       = 17.0                  //Degrees
elevator_down_limit     = 15.5                  //Degrees
aileron_up_limit        = 18.0                  //Degrees
aileron_down_limit      = 18.0                  //Degrees
rudder_limit            = 30.0                  //Degrees
elevator_trim_limit     = 15.0                  //Degrees
spoiler_limit           = 0.0                   //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0.0               //Degrees
min_flaps_for_spoilerons = 0.0                  //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed    = 104.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 88.0                  //Knots True (KTAS)
cruise_speed            = 240.0                 //Knots True (KTAS)
max_mach                = 0.48
max_indicated_speed     = 247                   //Red line (KIAS)

[flaps.0]
type             = 1                            // 1 - tail, 2 - lead
span-outboard    = 0.62                         // 0.0 .. 1.0
extending-time   = 14.5                         // seconds
lift_scalar = 1.00                              // Normalised
drag_scalar = 1.00                              // Normalised
pitch_scalar = 1.00                             // Normalised
flaps-position.0 = 0.0                          // degrees
flaps-position.1 = 10.0,198.0                   // degrees
flaps-position.2 = 20.0,168.0                   // degrees
flaps-position.3 = 35.0,153.0                   // degrees

[flaps.1]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.62                                 // 0.0 .. 1.0
extending-time   = 14.5                                 // seconds
lift_scalar = -0.10                                     // Normalised
drag_scalar =  0.80                                     // Normalised
pitch_scalar = 0.00                                     // Normalised
flaps-position.0 = 0.0                                  // degrees
flaps-position.1 = 0.0                                  // degrees
flaps-position.2 = 1.0                                  // degrees
flaps-position.3 = 12.5                                 // degrees

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed=100.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
max_pitch=25.0
max_pitch_acceleration=0.85
max_pitch_velocity_lo_alt=2.00
max_pitch_velocity_hi_alt=1.65
max_pitch_velocity_lo_alt_breakpoint=7000
max_pitch_velocity_hi_alt_breakpoint=12000
max_bank=25.0
max_bank_acceleration=2.8
max_bank_velocity=3.10
max_throttle_rate=0.0
nav_proportional_control=15.0
nav_integrator_control=0.125
nav_derivative_control=9.0
nav_integrator_boundary=0.5
nav_derivative_boundary=5.0
gs_proportional_control=9.55
gs_integrator_control=0.55
gs_derivative_control= 2.0
gs_integrator_boundary=0.70
gs_derivative_boundary=0.70
yaw_damper_gain = 0.1

[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

        //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,  -1.137,   0.000, -5.445, 1200, 0, 0.677, 26.6, 0.371, 2.0242, 0.8016,  4.5,  4.2, 0, 180.0, 180.0
point.1=1, -24.633,  -8.580, -5.438, 1600, 1, 1.000,  0.0, 0.315, 2.3841, 0.8152,  5.1,  5.2, 2, 180.0, 180.0
point.2=1, -24.633,   8.580, -5.438, 1600, 2, 1.000,  0.0, 0.315, 2.3841, 0.8152,  4.8,  4.9, 3, 180.0, 180.0
point.3=2, -21.945, -28.990,  2.310,  750, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 5, 0.0, 0.0
point.4=2, -21.945,  28.990,  2.310,  750, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 6, 0.0, 0.0
point.5=2, -43.893,   0.000, -1.567,  750, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 9, 0.0, 0.0
point.6=2,   0.000,   0.000,  0.000,  750, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 4, 0.0, 0.0

static_pitch = -0.15
static_cg_height = 3.805
gear_system_type=1      //Hydraulic