[fltsim.0]
title=BT-13 Malden2
sim=BT-13
model=
panel=
sound=
texture=malden2
kb_checklists=
prop_anim_ratio=1.76
ui_manufacturer=Vultee
ui_type=BT-13
ui_variation=Malden AAF_2
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
description=World War 2 basic trainer, over 13,000 built. This paint scheme represents a plane my dad, cadet Robert Lawsen, flew during his training at Malden Army Airfield in Missouri during the summer of 1943; textures by Chuck Lawsen.
atc_id=243120
[fltsim.1]
title=BT-13 1941 Yellow Blue
sim=BT-13
model=
panel=
sound=
texture=1941
kb_checklists=
prop_anim_ratio=1.76
ui_manufacturer=Vultee
ui_type=BT-13
ui_variation=1941 Yellow Blue
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
description=World War 2 basic trainer, over 13,000 built. This represents the pre-war paint scheme used through 1941; textures by Chuck Lawsen.
atc_id=1244
[fltsim.2]
title=BT-13 Factory Fresh
sim=BT-13
model=
panel=
sound=
texture=factoryfresh
kb_checklists=
prop_anim_ratio=1.76
ui_manufacturer=Vultee
ui_type=BT-13
ui_variation=Factory Fresh
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
description=World War 2 basic trainer, over 13,000 built. After the U.S. entered the war in early 1942 an order came down from the Army Air Corp to have future trainers manufactured unpainted. This paint scheme represents a new bare metal aircraft as it was looked when delivered to it's destination, any number of training fields throughout the country; textures by Chuck Lawsen.
atc_id=242300
[fltsim.3]
title=BT-13 Navy
sim=BT-13
model=
panel=
sound=
texture=navy
kb_checklists=
prop_anim_ratio=1.76
ui_manufacturer=Vultee
ui_type=BT-13
ui_variation=Navy
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
description=World War 2 basic trainer, over 13,000 built. This paint scheme represents a Navy paint scheme of a restored and flyable plane owned an operated by Mid Atlantic Air Museum in Reading, PA. Textures by Chuck Lawsen.
atc_id=22441
[fltsim.4]
title=BT-13 Malden
sim=BT-13
model=
panel=
sound=
texture=malden
kb_checklists=
prop_anim_ratio=1.76
ui_manufacturer=Vultee
ui_type=BT-13
ui_variation=Malden AAF
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
description=World War 2 basic trainer, over 13,000 built. This represents a model from Malden Army Airfield circa 1943.
atc_id=42300
[CameraDefinition.0]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0, 2.0, -5
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Nose"
Guid = {8A1987D0-09B6-7E48-B4E1-62C5DBE2A720}
Description =Looking back from the nose of the engine toward the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0, 1.5, 5.0
InitialPbh = 20, 0, 180
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[CameraDefinition.2]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 7, 1, 0
InitialPbh = 0, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[CameraDefinition.3]
Title = "Left Wing"
Guid = {7a91803e-898b-435a-8391-725be6a48203}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -7, 1, 0
InitialPbh = 0, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[CameraDefinition.4]
Title = "Rear Cockpit"
Guid = {b1c13530-89ca-11db-b606-0800200c9a66}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.55
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=30
HeadingPanRate=75
PanAcceleratorTime=0
HotKeySelect=1
InitialXyz=0.0, 0, -1.125
InitialPbh=0, 0, 0
[General]
atc_type=Vibrator
atc_model=
editable=0
performance=Length: 28' 7"\nWing span: 42'\nWeight: 2976# empty, 3991# gross\nPower:P&W Wasp Jr. rated @ 450hp.\nMax Speed:182 mph\nCruise:170 mph\nCeiling:21,000 ft.\nRange:1050 miles\nDesigner: P. Clawson\nDate: 12\/2005\n\n
Category=airplane
[weight_and_balance]
// ACM V2.5
max_gross_weight = 3991
empty_weight = 2976
reference_datum_position = 7.24, 0, 0
empty_weight_CG_position = -7.76, 0, -1
empty_weight_pitch_MOI = 1788.8
empty_weight_roll_MOI = 1606.8
empty_weight_yaw_MOI = 5000
empty_weight_coupled_MOI = 0
max_number_of_stations = 2
station_load.0 = 170, -6.32, 0, 0.56
station_load.1 = "0.0, -9.0, 0.0, -0.5, Navigator"
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, -6.00, 0.00, 2.20, fx_vclight,
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.0
min_throttle_limit = 0.1
engine.0 = 0.34, -0.06, -0.05,
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup = fx_engstrt_vega
windshield_rain_effect_available = 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 1
electric_pump = 0
LeftMain = -6.2, -4.2, 2.7, 96, 0
RightMain = -6.2, 4.2, 2.7, 96, 0
[contact_points]
static_pitch = 11.5
static_cg_height = 4.6
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 7
point.0 = 1, -24.8071, 0, -2.4605, 1200, 0, 0.4, 30, 0.4, 2.5, 0.595, 0, 0, 0, 0, 0
point.1 = 1, -5.7684, -5.2872, -6.4, 1600, 1, 1.2, 0, 0.6, 2.5, 0.756, 0, 0, 2, 0, 0
point.2 = 1, -5.8336, 5.2872, -6.4, 1600, 2, 1.2, 0, 0.6, 2.5, 0.752, 0, 0, 3, 0, 0
point.3 = 2, -8, -21.09, -0.9722, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -8, 21.221, -0.7753, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -27.4812, 0, 0.1054, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.4908, 0, -2.4281, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
[keyboard_response]
elevator = 200, 1000
aileron = 200, 1000
rudder = 200, 1000
[forcefeedback]
ground_bumps_magnitude1 = 2600
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 3500000
[airplane_geometry]
wing_area = 238.0
wing_span = 42
wing_root_chord = 7.40
wing_dihedral = 4
wing_incidence = 1.0
wing_twist = 0.0
oswald_efficiency_factor = 0.6
wing_winglets_flag = 0
wing_sweep = 2.5
wing_pos_apex_lon = -4.83
wing_pos_apex_vert = -1.99
htail_area = 51.0
htail_span = 14.09
htail_pos_lon = -21.79
htail_pos_vert = 0.18
htail_incidence = -1.0
htail_sweep = 12
vtail_area = 10.0
vtail_span = 5.59
vtail_sweep = 18
vtail_pos_lon = -20.80
vtail_pos_vert = 1.5
elevator_area = 16.3
aileron_area = 25.6
rudder_area = 18
elevator_up_limit = 22.0
elevator_down_limit = 22.0
aileron_up_limit = 22.0
aileron_down_limit = 22.0
rudder_limit = 22.0
elevator_trim_limit = 20.0
spoiler_limit = 0.0
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
auto_spoiler_available=0
positive_g_limit_flaps_up=6.000000
positive_g_limit_flaps_down=4.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 25
max_generator_alternator_amps = 60
engine_generator_map = 1
electric_always_available = 0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=2.5
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[Flaps.0]
type= 1
span-outboard= 0.5
extending-time= 4.0
flaps-position.0= 0.0, 0.0
flaps-position.1= 12.00, 0.0
flaps-position.2= 25.0, 0.0
flaps-position.3= 40.0, 0.0
damaging-speed=110 // KIAS
blowout-speed=130 // KIAS
lift_scalar=1.5
drag_scalar=2.8
pitch_scalar=1.8
system_type= 1
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=149.3 //Cubic inches per cylinder
compression_ratio=6.0 //Compression ratio
number_of_cylinders=9 //Number of cylinders
max_rated_rpm=2200 //Max rated RPM
max_rated_hp=450 //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=34 //Max design manifold pressure, (inHg)
min_design_mp=10 //Min design manifold pressure, (inHg)
critical_altitude=9000 //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 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=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 //Scalar on idle RPM friction
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=9 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi=8.0 //Propeller moment of inertia
beta_max=24.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=14.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1400 //Miminum governed RPM
prop_tc=0.1 //Prop time-constant
gear_reduction_ratio=1.0 //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=0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=0 //Minimum RPM for prop feathering
beta_feather=0 //Feathering pitch angle (degrees)
power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees)
//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 (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 3000.0 //PSI
engine_map=1,0,0,0
[Views]
eyepoint=-7.25, 0, 2.75
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Nav.1=0, 0, 0
Adf.1=1
Transponder.1=0
Marker.1=0
[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=1,0
direction_indicator.1=2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=2,0
[Reference Speeds]
flaps_up_stall_speed=62.5 //Knots True (KTAS)
full_flaps_stall_speed=56.0 //Knots True (KTAS)
cruise_speed=139.0 //Knots True (KTAS)
max_indicated_speed = 200 //Red line (KIAS)
[autopilot]
autopilot_available=0
flight_director_available=0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain = 0.0
default_bank_mode=2 //Default to Heading Hold
[stall_warning]
type=1
stick_shaker=1
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
