//This file uses standard lights. To use change name to AIRCRAFT.CFG
[fltsim.0]
title=Seabird-camo
sim=Seeker
model=
panel=
sound=
texture=camo
kb_checklists=SB7L_Seeker_Check
kb_reference=SB7L_Seeker_Ref
atc_id=N72163
ui_manufacturer=Seabird Aviation
ui_type=Seeker SB7L-360A
ui_variation="N72163 Camo"
description= Designed & developed in Australia, and now operating in Australia, the USA, Middle-East and Africa, the SEEKER is a purpose built, rugged utility aircraft for private, commercial and security operations. At a third of the operating cost of rotary-wing equivalents, the SEEKER provides an efficient alternative for powerline and pipeline inspection, coast watch, environmental and stock monitoring, aerial photography and security - where VTOL (vertical take-off and landing) is not mission essential. Crew visibility is unrivalled by any other fixed-wing aircraft and is superior to many helicopters.
[FLTSIM.1]
title=Seabird-Country Energy
sim=Seeker
model=
panel=
sound=
texture=VH-OPT
kb_checklists=SB7L_Seeker_Check
kb_reference=SB7L_Seeker_Ref
atc_id=VH-OPT
atc_parking_types=RAMP
atc_airline=
ui_manufacturer=Seabird Aviation
ui_type=Seeker SB7L-360A
ui_variation="VH-OPT Country Energy"
ui_createdby=Marty
description=Designed & developed in Australia, and now
operating in Australia, the USA, Middle-East and Africa,
the SEEKER is a purpose built, rugged utility aircraft for
private, commercial and security operations.
At a third of the operating cost of rotary-wing equivalents,
the SEEKER provides an efficient alternative for powerline
and pipeline inspection, coast watch, environmental and
stock monitoring, aerial photography and security - where
VTOL (vertical take-off and landing) is not mission
essential. Crew visibility is unrivalled by any other
fixed-wing aircraft and is superior to many helicopters.
The Seeker provides an efficient alternative to Country
Energy for powerline inspection. Country Energy manages Australia's largest energy supply network across 95 per
cent of New South Wales.
[fltsim.2]
title=Seabird VH-SEE
sim=Seeker
model=
panel=
sound=
texture=VH-SEE
kb_checklists=SB7L_Seeker_Check
kb_reference=SB7L_Seeker_Ref
atc_id=VH-SEE
ui_manufacturer=Seabird Aviation
ui_type=Seeker SB7L-360A
ui_variation="VH-SEE "Spirit of Hervey Bay""
description=Designed & developed in Australia, and now
operating in Australia, the USA, Middle-East and Africa,
the SEEKER is a purpose built, rugged utility aircraft for
private, commercial and security operations.
At a third of the operating cost of rotary-wing equivalents,
the SEEKER provides an efficient alternative for powerline
and pipeline inspection, coast watch, environmental and
stock monitoring, aerial photography and security - where
VTOL (vertical take-off and landing) is not mission
essential. Crew visibility is unrivalled by any other
fixed-wing aircraft and is superior to many helicopters.
[fltsim.3]
title=Seabird VH-SUA
sim=Seeker
model=
panel=
sound=
texture=VH-SUA
kb_checklists=SB7L_Seeker_Check
kb_reference=SB7L_Seeker_Ref
atc_id=VH-SUA
ui_manufacturer=Seabird Aviation
ui_type=Seeker SB7L-360A
ui_variation="VH-SUA"
description=Designed & developed in Australia, and now
operating in Australia, the USA, Middle-East and Africa,
the SEEKER is a purpose built, rugged utility aircraft for
private, commercial and security operations.
At a third of the operating cost of rotary-wing equivalents,
the SEEKER provides an efficient alternative for powerline
and pipeline inspection, coast watch, environmental and
stock monitoring, aerial photography and security - where
VTOL (vertical take-off and landing) is not mission
essential. Crew visibility is unrivalled by any other
fixed-wing aircraft and is superior to many helicopters.
[FLTSIM.4]
title=Seabird VH-SBO
sim=Seeker
model=
panel=
sound=
texture=VH-SBO
kb_checklists=SB7L_Seeker_Check
kb_reference=SB7L_Seeker_Ref
atc_id=VH-SBO
atc_parking_types=RAMP
atc_airline=Firespotter 377
ui_manufacturer=Seabird Aviation
ui_type=Seeker SB7L-360A
ui_variation="VH-SBO Firespotter"
description=Designed & developed in Australia, and now
operating in Australia, the USA, Middle-East and Africa,
the SEEKER is a purpose built, rugged utility aircraft for
private, commercial and security operations.\nAt a third of the operating cost of rotary-wing equivalents, the SEEKER provides an efficient alternative for powerline and pipeline inspection, coast watch, environmental and stock monitoring, aerial photography and security - where VTOL (vertical take-off and landing) is not mission essential. Crew visibility is unrivalled by any other
fixed-wing aircraft and is superior to many helicopters.
[General]
atc_type=Seabird
atc_model=seeker
editable=0
performance="Cruise Speed\n164 mph 129 kts 264 km\/h\nEngine\nLycoming O-360-B2C four-cylinder liquid-cooled, 168 hp\nPropeller\n2-blade Bishton-Seabird fixed pitch 1.77m dia\n\nMaximum Range\n476 nm 888 km\n\nService Ceiling\n15,000 ft 6,096 m\nFuel Capacity (Usable)\n47.5 gal 180 L\nEmpty Weight\n1,342 lb 610 kg\nMaximum Gross Weight\n2,040 lb 925 kg\nLength\n23 ft, 6 in 7.2 m\nWingspan\n36 ft, 4 in 11.07 m\nnHeight\n6 ft, 7 in 2.03 m\nSeating\n2\nUseful Load\n829 lb 377 kg"
category = Airplane
[CameraDefinition.0]
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 = 1.0
ShowWeather = Yes
InitialXyz = 10.5, 0.2, 0.3
InitialPbh = 9, 0, 270
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.1]
Title = "Left Wing"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
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 = 1.00
ShowWeather = Yes
InitialXyz = -10.5, 0.2, 0.3
InitialPbh = 9, 0, 90
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.2]
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 = 0.75
ShowWeather = Yes
InitialXyz = 0, 2.2, -13.0
InitialPbh = 11, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.001]
Title = "Right Seat"
Guid = {195EAB58-9E4A-1E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=40
HeadingPanRate=60
InitialXyz=0.45, 0.0, 0.0
InitialPbh=-2, 0, 0
[WEIGHT_AND_BALANCE]
max_gross_weight = 2040 // (pounds)
empty_weight = 1342 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -2.5, 0, 0 // was -1.07,0,0(feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, 2.6, -1.5, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, 2.6, 1.5, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 85, -6.0, 0.0, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_name.1 = "Front Passenger"
station_name.2 = "Baggage"
;Moments of Inertia
empty_weight_pitch_MOI = 1083.0
empty_weight_roll_MOI = 907.0
empty_weight_yaw_MOI = 1630.0
empty_weight_coupled_MOI= 0.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = .60
rudder_effectiveness =1.0
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
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -1, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= .70 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
//Lycoming 0-360-B2C Engine 169HP @ 2500RPM
power_scalar=1.00000
cylinder_displacement= 90.252
compression_ratio= 8.5000
number_of_cylinders= 4
max_rated_rpm= 2500.000
max_rated_hp= 168.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque=5.500000
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
critical_altitude= 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.00000
idle_rpm_mechanical_efficiency_scalar=1.0000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
[propeller]
thrust_scalar=1.000
propeller_type= 1
propeller_diameter= 6.7 //6.833
propeller_blades= 2
propeller_moi= 5.700
beta_max= 31.800
beta_min= 17.000
min_gov_rpm=0
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 20.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[electrical]
max_battery_voltage=28.0
generator_alternator_voltage=30.0
max_generator_alternator_amps=100.0
electric_always_available = 0
;BusType, MaxAmpLoad, MinVoltage
;BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 5, 17.0
avionics = 1, 5, 17.0
autopilot = 1, 2, 17.0
pitot_heat = 0, 2, 17.0
additional_system = 0, 1, 16.0
marker_beacon = 1, 2, 9.0
fuel_pump = 0, 5, 17.0
starter1 = 0, 20, 15.0
light_nav = 0, 5, 17.0
light_landing = 0, 5, 17.0
light_strobe = 0, 1.5 , 17.0
light_panel = 0, 2, 17.0
light_taxi = 0, 3, 17.0
light_recognition = 0, 2, 17.0
light_logo = 0, 2, 17.0
light_wing = 0, 2, 17.0
flap_motor = 0, 5 , 17.0
//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
[contact_points]
point.0 = 1, -14.7, 0.00, -3.60, 1500, 0, 0.36, 45.0, 0.3, 2.5, 0.7, 0.0, 0.0, 0
point.1 = 1, 1.30, -3.90, -6.60, 2500, 1, 0.67, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 2
point.2 = 1, 1.30, 3.90, -6.60, 2500, 2, 0.67, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 3
point.3 = 2, -1.00, -16.3, 2.15, 1600, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5,
point.4 = 2, -1.00, 16.3, 2.15, 1600, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6,
point.5 = 2, 5.40, 0.0, -2.80, 1600, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4,
point.6 = 2,-17.00, 0.0, 4.50, 1600, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7,
max_number_of_points = 21
static_pitch=11.0 //8.9 degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=6.0 //feet, altitude of CG when at rest on the ground
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.68 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
auto_brakes = 0
[hydraulic_system]
normal_pressure = 0.0 //PSI
[airspeed_indicators]
airspeed_scalar=1
airspeed_offset=0
[fuel]
//Tanks Position and capacity:
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -2.24, -5.4, 2.40, 23.75, 1.25
RightMain= -2.24, 5.4, 2.40, 23.75, 1.25
//Fuel type: 1 = Avgas, 2 = JetA
fuel_type=1
number_of_tank_selectors = 1
electric_pump=1
engine_driven_pump=0
fuel_dump_rate=.0167
[Views]
eyepoint= 2.8, -.6, -1.6 // (feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 3 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 10 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 40 // degrees
damaging-speed = 105 // KIAS
blowout-speed = 150 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 3 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 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 = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[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
[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=1,1 //Turn AND Bank
[airspeed_indicators]
airspeed_indicator.0 = 1.3, -24.0
[vacuum_system]
max_pressure=5.15 //PSI
vacuum_type=1 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
engine_map=1
[pneumatic_system]
max_pressure=0.000000
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available
[LIGHTS]
//-----THIS SECTION USES STANDARD LIGHTS
Types: 1=beacon, 2=strobe, 3=navigation, 4=panel, 5=landing, 6=taxi, 7=cabin, 8=wing, 9=logo,
//longditudinal dist, lateral dist, vertical dist,
light.0 = 3, -1.600, -18.25, -0.100, fx_navred, //left
light.1 = 3, -1.600, 18.25, -0.100, fx_navgre, //right
light.2 = 3, -14.200, -0.10, -1.006, fx_navwhi, //tail
light.3 = 2, -1.703, -18.25, -0.100, fx_strobe, //left
light.4 = 2, -1.703, 18.25, -0.100, fx_strobe, //right
light.5 = 1, -13.111, 0.00, 3.100, fx_beaconh, //tail
light.6 = 1, -2.111, 0.00, -4.350, fx_beaconb, //underbody
light.7 = 7, 3.5, 0.00, -0.911, fx_vclight,
light.8 = 7, 0.0, 0.00, -0.750, fx_navwhi, //Display only for cabin light
light.9 = 5, 8.0, 0.25, -3.7, fx_landing,
light.10 = 6, 8.0, -0.25, -3.7, fx_landing, //display only
light.11 = 8, -1.00, -8.0, -3.00, fx_vclight, //LH Underwing Light
light.12 = 9, -12.111, -2.00, -2.00, fx_vclight, //LH Tail
light.13 = 9, -12.111, 2.00, -2.00, fx_vclight, //RH Tail
//------------------------------------------------
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Cargo 2=Emergency)
[airplane_geometry]
wing_area = 171.0 //Square feet
wing_span = 32.97 //Feet
wing_root_chord = 5.1 //Feet
wing_dihedral = 1.5 //Degrees
wing_incidence = 1.0 //Degrees
wing_twist = 0.0 //Degrees
oswald_efficiency_factor= 0.65 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = 0.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 2.46 //Feet, vertical distance from reference point, positive going up
htail_area = 27.0 //Square feet
htail_span = 10.9 //Feet
htail_pos_lon = -12.76 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.45 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 40.0 //Degrees, horizontal tail leading edge
vtail_area = 26.5 //Square feet
vtail_span = 5.4 //Feet, tip to body
vtail_sweep = 50.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -13.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 1.6 //Feet, vertical distance from reference point, positive going up
elevator_area = 12.0 //Square feet
aileron_area = 11.5 //Square feet
rudder_area = 5.6 //Square feet
elevator_up_limit = 25.0 //Degrees
elevator_down_limit = 21.0 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 20.0 //Degrees
rudder_limit = 21.0 //Degrees
elevator_trim_limit = 16.0 //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 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available = 0
positive_g_limit_flaps_up = 4.0 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down= 2.0 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up = -1.5 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= -1.5 //Design G load tolerance (negative, flaps down)
load_safety_factor = 1.5 //Design G load safety factor
[Reference Speeds]
flaps_up_stall_speed = 54.0 //Knots True (KTAS)
full_flaps_stall_speed = 49.0 //Knots True (KTAS)
cruise_speed = 120.0 //Knots True (KTAS)
max_indicated_speed = 129 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 500.0
autothrottle_available= 1
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=35.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
[forcefeedback]
gear_bump_nose_magnitude=6000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=3250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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
[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
