19-09-2005, 03:22 PM
If you have time to make it
here are the config file and the pic
pic:
http://www.alexisflight.com/images/b1900c.jpg
config :
/////////////////////////////////////////////////////////
//
// VERSION 1.0
//
//29MAR05
///////////////////////////////////////////////////////
[fltsim.0]
title=Beech 1900C
sim=beech_1900C
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 support@precisionmanuals.com"
[fltsim.1]
title=Beech 1900C - VC
sim=beech_1900C
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 support@precisionmanuals.com"
[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
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 = "2070.0, -23.01, 0.0, 0.0, 19 Pax+FA/Cargo"
station_load.3 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.4 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "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 = 0.802 //Scalar for fuel flow efficiency
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= 7, -22.500, -27.000, 1.485, fx_strobe_pmdg1900, //Strobe White Left
light.12= 7, -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= 0.791 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
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
here are the config file and the pic
pic:
http://www.alexisflight.com/images/b1900c.jpg
config :
/////////////////////////////////////////////////////////
//
// VERSION 1.0
//
//29MAR05
///////////////////////////////////////////////////////
[fltsim.0]
title=Beech 1900C
sim=beech_1900C
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 support@precisionmanuals.com"
[fltsim.1]
title=Beech 1900C - VC
sim=beech_1900C
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 support@precisionmanuals.com"
[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
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 = "2070.0, -23.01, 0.0, 0.0, 19 Pax+FA/Cargo"
station_load.3 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.4 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "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 = 0.802 //Scalar for fuel flow efficiency
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= 7, -22.500, -27.000, 1.485, fx_strobe_pmdg1900, //Strobe White Left
light.12= 7, -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= 0.791 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
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