[fltsim.0]
title=Beech D18S N412K
sim=D18S
model=
panel=
sound=
texture=
kb_checklists=Beech_18_checklist
kb_reference=Beech18_ref
atc_id=N412K
atc_id_color = 0xffffffff
atc_parking_types = RAMP
atc_parking_code = 1
ui_manufacturer=Beechcraft MSA
ui_type="D18S passenger"
ui_variation=N412K "Touch O'Texas"
atc_heavy=0
atc_airline=
atc_flight_number=
description=A post-War D18S modification (c/n A-263), now a part of Flight of the Phoenix Aviation Museum, Gilmer (TX) and business air transport for Dean Lumber Company.




[General]
atc_type=Beechcraft
atc_model=D18S
editable = 0

performance = + Empty Weight: 6887 lbs + Max Power: 450 Hp + Maneuver speed: 157 mph @ 5.0 g + Max speed: 235 mph @ 8000 ft + Max speed at sea-level: 234 mph + Climb rate: 1250 ft/min @ 119 mph Flight Dynamics By: Jerry Beckwith's Workbook, and Shupe FD Build 10 - 3/26/05 05:59 AM Flight Dynamics Workbook V2.84.65
Category=airplane

[pitot_static]
vertical_speed_time_constant = 2
pitot_heat=1.000000


[WEIGHT_AND_BALANCE]
max_gross_weight = 8750
empty_weight = 5527


reference_datum_position = 0, 0, 0
empty_weight_CG_position  = 0, 0, 0
CG_forward_limit = .21
CG_aft_limit = .33

max_number_of_stations = 13
station_load.0 = 170, 2.9, -1, 1, Pilot
station_load.1 = 170, 2.9, 1, 1, co-pilot
station_load.2 = 170, 1.5, -1.3, 1, p1
station_load.3 = 170, 1.5, 1.3, 1, p2
station_load.4 = 170, -2, -1.3, 1, p5
station_load.5 = 170, -2, 1.3, 1, p6
station_load.6 = 150, -5, -1.3, 1, p7
station_load.7 = 150, -5, 1.3, 1, p8
station_load.8 = 0, 0, 0, 0
station_load.9 = 0, 0, 0, 0
station_load.10 = 0, 0, 0, 0
station_load.11 = 0, 0, 0, 0
station_load.12 = 0, 0, 0, 0

;Moments of Inertia
empty_weight_pitch_MOI = 6776
empty_weight_roll_MOI = 7623
empty_weight_yaw_MOI = 13700
empty_weight_coupled_MOI = 0

[fuel]
Center1 = 5.0, 0, -0.1, 80,  0
LeftMain = -.5, -5.1, 0, 76,  0
RightMain = -.5, 5.1, 0, 76,  0
LeftAux = -2.1, -5.1, 0, 25,  0
RightAux = -2.1, 5.1, 0, 25,  0
fuel_type =  1
number_of_tank_selectors = 2
electric_pump=1


[flight_tuning]
cruise_lift_scalar = 1
parasite_drag_scalar = 1
induced_drag_scalar = 1
elevator_effectiveness = 1
aileron_effectiveness = 1
rudder_effectiveness = 1
pitch_stability = 1
roll_stability = 1
yaw_stability = 1
elevator_trim_effectiveness = 1
aileron_trim_effectiveness = 1
rudder_trim_effectiveness = 1
hi_alpha_on_roll = 1
hi_alpha_on_yaw = 1
p_factor_on_yaw = .5
torque_on_roll = .5


[GeneralEngineData]
engine_type = 0
Engine.0 = 7.5, -6.5, 0.036
Engine.1 = 7.5, 6.5, 0.036
fuel_flow_scalar = 1
min_throttle_limit = 0
master_ignition_switch = 1

[SMOKESYSTEM] 
//            (Z Axis) (X Axis) (Y Axis) 
smoke.0 = -0.036,  -2.5,   -6.5,   fx_smoke_ys11 
smoke.1 = 0.036,  2.5,    6.5,   fx_smoke_ys11


[piston_engine]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement= 109.4                    //Cubic inches per cylinder
compression_ratio= 6.0                          //Compression ratio
number_of_cylinders= 9                          //Number of cylinders
max_rated_rpm= 2300.0                           //Max rated RPM
max_rated_hp= 450.0                             //Max rated HP
fuel_metering_type= 1                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3                  //Starter torque factor
turbocharged= 1                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 36.5                             //Max design manifold pressure, (inHg)
min_design_mp= 1.0                              //Min design manifold pressure, (inHg)
critical_altitude= 5000.0                       //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0.0                  //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0.0                //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0

[propeller]
thrust_scalar = 1
propeller_type = 0
propeller_diameter = 8.25
propeller_blades = 2
propeller_moi = 10.4
beta_max = 65
beta_min = 15
min_gov_rpm = 345
prop_tc = 0.01
gear_reduction_ratio = 1
fixed_pitch_beta = 25
low_speed_theory_limit = 80
prop_sync_available = 1
prop_deice_available = 1
prop_feathering_available = 1
prop_auto_feathering_available = 1
min_rpm_for_feather = 700
beta_feather = 88.5
power_absorbed_cf = 0.9
defeathering_accumulators_available = 0
prop_reverse_available = 0
minimum_on_ground_beta = 1
minimum_reverse_beta = -14
rotation = 1, 1


[contact_points]
max_number_of_points = 10

//point.0 = 1, -19.904,  0.000, -0.637, 2200, 0, 0.33, 45, 0.51,  2.0, 0.50, 3, 5, 0, 139, 175.2
//Replace contact_point.0 below with the one above if you want a steerable tailwheel.  You may comment out the one below with //, and activate the one above by removing the //

point.0 = 1, -19.904,  0.000, -0.637, 2200, 0, 0.33, 180, 0.51,  2.0, 0.50, 3, 5, 0, 139, 175.2
point.1 = 1,   2.890, -6.417, -5.987, 2200, 1, 0.8,    0, 1.15,  1.1, 0.50, 5, 5, 2, 139, 175.2
point.2 = 1,   2.890,  6.417, -5.987, 2200, 2, 0.8,    0, 1.15,  1.1, 0.50, 5, 5, 3, 139, 175.2
point.3 = 2, 	8,     0,     -3,     1000, 0, 0,      0, 0,       0,    0, 0, 0, 4
point.4 = 2,   -1,     0,     -1.4,   3000, 0, 0,      0, 0,       0,    0, 0, 0, 4
point.5 = 2,    0,-23.495,     0.42,  1200, 0, 0,      0, 0,       0,    0, 0, 0, 5
point.6 = 2,    0, 23.495,     0.42,  1200, 0, 0,      0, 0,       0,    0, 0, 0, 6
point.7 = 2, -21.904,  0,      3,     1200, 0, 0,      0, 0,       0,    0, 0, 0, 9
point.8 = 2, -16.6,    0,      6.4,   1200, 0, 0,      0, 0,       0,    0, 0, 0, 9
point.9 = 2,   8.2,    0,      1,     1200, 0, 0,      0, 0,       0,    0, 0, 0, 4

static_pitch = 12.2
static_cg_height = 4.18
gear_system_type = 1
tailwheel_lock = 1

[Views]
eyepoint = 2.912, -1.245, 3.333


[flaps.0]       //Trailing Edge Flaps
type = 1
span-outboard = 0.5
extending-time = 5
flaps-position.0 = 0
flaps-position.1 = 15, 121
flaps-position.2 = 30, 116
flaps-position.3 = 45, 111
damaging-speed = 121
blowout-speed = 131
system_type = 0
lift_scalar = 1
drag_scalar = 1
pitch_scalar = 1


[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 160
electric_always_available = 0

flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
starter3 = 0, 20, 17
starter4 = 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
light_cockpit = 0, 5, 17
prop_sync = 0, 15, 17
auto_feather = 0, 15, 17
auto_brakes = 0, 15, 17
standby_vacuum = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17

[LIGHTS]
// types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//        6=Taxi, 7=Recognition, 8=Wing, 9=Logo, 10=Cabin
light.0 =   3,   -0.7,  -23.495,  1.796, fx_navred ,
light.1 =   3,   -0.7,   23.495,  1.696, fx_navgre ,
light.2 =   2,   -1.0,  -23.495,  1.796, fx_strobe.fx
light.3 =   2,   -1.0,   23.495,  1.696, fx_strobe.fx,
light.4 =  4,   2.70,     0.00,  1.050, fx_vclight,
light.5 =  10,  -3.70,     0.00,  3.250, fx_vclight,
light.6 =   1, -17.68,     0.00,  3.999, fx_beacon.fx//fx_beacon_commander.fx ,
//light.7 =   8,   -0.6,  -23.495,  1.796, fx_wing ,
light.7 =   1,   -0.1,     0.00, -1.700, fx_beacon.fx ,
light.8 =   5,    8.3,    -14.0,   -2.9, Newll ,//wing lite reflections
light.9 =   5,    8.3,     14.0,   -2.9, Newll ,//wing

[Radios] // available, 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
Adf.2 = 1
Transponder.1 = 1
Marker.1 = 1

[keyboard_response]
elevator = 350, 500
aileron  = 450, 1000
rudder   = 200, 1000

[direction_indicators]
direction_indicator.0 = 1, 0

[exits]
number_of_exits = 1
exit_rate.0 = 0.4

[EFFECTS]
wake = 	fx_wake
water = 	fx_spray
dirt = 	fx_tchdrt
concrete = 	fx_sparks
touchdown=	fx_tchdwn_s, 1
startup=	fx_msd18s

[autopilot]
autopilot_available = 1
flight_director_available = 0
default_vertical_speed = 1000
autothrottle_available = 0
autothrottle_arming_required = 0
autothrottle_max_rpm =  90
autothrottle_takeoff_ga = 1
pitch_takeoff_ga = 8
max_pitch_velocity_hi_alt = 1.5
max_pitch_velocity_lo_alt_breakpoint = 20000
max_pitch_velocity_hi_alt_breakpoint = 28000
max_pitch = 10
max_pitch_acceleration = 1
max_pitch_velocity_lo_alt = 2
max_bank= 25
max_bank_acceleration = 1.8
max_bank_velocity = 3
max_throttle_rate = 0.1
nav_proportional_control = 9
nav_integrator_control = 0.25
nav_derivative_control = 0
nav_integrator_boundary = 2.5
nav_derivative_boundary = 0
gs_proportional_control = 9.52
gs_integrator_control = 0.26
gs_derivative_control = 0
gs_integrator_boundary = 0.7
gs_derivative_boundary = 0
yaw_damper_gain = 0
default_bank_mode=2


[airplane_geometry]
wing_area = 347.5
wing_span = 47.6666666666667
wing_root_chord = 7.29020979020979
wing_dihedral = 4
wing_incidence = 0
wing_twist = 0
oswald_efficiency_factor = 0.908883252293779
wing_winglets_flag = 0
wing_sweep  = 0
wing_pos_apex_lon = 1.82255244755245
wing_pos_apex_vert = 0

htail_area = 67.5
htail_span = 18.3
htail_pos_lon = -19.4
htail_pos_vert = 0
htail_incidence = 0
htail_sweep = 0

vtail_area = 23
vtail_span = 6
vtail_sweep = 0
vtail_pos_lon  = -19.1
vtail_pos_vert = 0

elevator_area = 28.9
aileron_area = 25
rudder_area = 23
elevator_up_limit = 35
elevator_down_limit = 25
aileron_up_limit = 38.5
aileron_down_limit = 21
rudder_limit = 25
elevator_trim_limit = 18
spoiler_limit = 0
spoilerons_available = 0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
auto_spoiler_available=0
positive_g_limit_flaps_up=5.000000
positive_g_limit_flaps_down=4.000000
negative_g_limit_flaps_up=-4.000000
negative_g_limit_flaps_down=-4.000000

[Reference Speeds]
flaps_up_stall_speed    = 60.8
full_flaps_stall_speed  = 52.1
cruise_speed            = 183
max_indicated_speed 	= 183
max_mach = 0.3325

[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[gear_warning_system]
gear_warning_available = 1
pct_throttle_limit = 0.1
flap_limit_idle = 33.75
flap_limit_power = 16.875

[brakes]
toe_brakes_scale = 0.640888698995941
parking_brake = 1
differential_braking_scale = 1.0

[stall_warning] //  0 = None, 1 = Suction, 2 = Electric.
type = 1
stick_shaker=1

[hydraulic_system]
electric_pumps = 0
engine_map = 1, 1, 0, 0
normal_pressure = 1000

[attitude_indicators] // 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1

[turn_indicators] // 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0 = 1, 0

[direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind
direction_indicator.0 = 1, 0

[airspeed_indicators]
airspeed_indicator.0 = 1, 0

[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=4.900000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[deice_system]
structural_deice_type=2