[fltsim.0]
title=ATC DHC-2 Beaver green
sim=F33An
model=
panel=
sound=
texture=
atc_id=CG-DVY
atc_heavy=0
ui_manufacturer=ATC
ui_type=de Havilland DHC-2 Beaver 
ui_variation=Wheel CG-DVY
description=de Havilland Canada DHC-2 Beaver MkI. The world's greatest bush plane.

[General]
atc_type=DEHAVILLAND
atc_model=DH2T
performance=Length: 35 ft 3 in\nWing span: 48 ft\nWeight: 2996 \/ 5370 lb\nPower: 550 hp P&W PT6A-20 Turbine\nDesigner: Fred Banting\nDate: Nov 2001\n

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=1800.000
empty_weight_roll_MOI=2400.000
empty_weight_pitch_MOI=5200.000
empty_weight_yaw_MOI=4400.000
empty_weight_coupled_MOI=0.000
max_gross_weight=2244.000
CG_forward_limit=0.000
CG_aft_limit=1.000

[Reference Speeds]
flaps_up_stall_speed=52.000000
full_flaps_stall_speed=41.600000
cruise_speed=135.0

[flight_tuning]
cruise_lift_scalar=0.800
parasite_drag_scalar=0.800
induced_drag_scalar=0.800
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.500
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000

[airplane_geometry]
wing_area=182.000
wing_span=33.500
wing_root_chord=4.917
wing_dihedral=5.999
wing_incidence=0.000
wing_twist=-0.994
oswald_efficiency_factor=1.208  //was 1.508
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=1.229
wing_pos_apex_vert=0.000
htail_area=38.000
htail_span=10.500
htail_pos_lon=-13.917
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=0.000
vtail_area=15.000
vtail_span=4.416
vtail_sweep=0.000
vtail_pos_lon=-14.583
vtail_pos_vert=1.500
elevator_area=16.610
aileron_area=18.300
rudder_area=6.650
elevator_up_limit=28.000
elevator_down_limit=20.999
aileron_up_limit=19.996
aileron_down_limit=15.000
rudder_limit=23.995
elevator_trim_limit=19.498
spoiler_limit=0.000
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000

[ground_reaction]
main_gear_static_compression=0.3		// (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=0.3            // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=1.0		// Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=1.0		// Center gear strut damping, 0 = undamped osciallations, 1 = critically damped

[pitot_static]
vertical_speed_time_constant=1.0

[propeller]
thrust_scalar=1.500
propeller_type=0
propeller_diameter=6.833
propeller_blades=2
propeller_moi=5.000
beta_max=43.000
beta_min=15.000
min_gov_rpm=1100.000
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

[piston_engine]
power_scalar=1.000
cylinder_displacement=86.667
compression_ratio=8.500
number_of_cylinders=6
max_rated_rpm=2700.000
max_rated_hp=285.000
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.300
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=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[fuel]
LeftMain=0.000, -13.333, 0.000, 37.000, 0.000
RightMain=0.000, 13.333, 0.000, 37.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1

[contact_points]
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
// vertical positions were -2.2 -6.49
point.0=1, -20.42,  0.0,  -1.8,   1600,  0, 0.66, 45.0,  0.3,  2.5, 0.82, 0.0, 0.0, 0, 0.0,  0.0
point.1=1,   2.0,  -5.08, -6.10,  1600,  1, 0.83, 0.0,   0.46, 2.5, 0.79, 0.0, 0.0, 2, 0.0,  0.0
point.2=1,   2.0,   5.08, -6.10,  1600,  2, 0.83, 0.0,   0.46, 2.5, 0.79, 0.0, 0.0, 3, 0.0,  0.0
point.3=2,   0.0, -24.0,   4.0,   308.5, 0, 0.0,  0.0,   0.0,  0.0, 0.0,  0.0, 0.0, 5, 0.0,  0.0
point.4=2,   0.0,  24.0,   4.0,   308.5, 0, 0.0,  0.0,   0.0,  0.0, 0.0,  0.0, 0.0, 6, 0.0,  0.0
point.5=2, -21.83,  0.0,   0.33,  916.5, 0, 0.0,  0.0,   0.0,  0.0, 0.0,  0.0, 0.0, 9, 0.0,  0.0
point.6=2,   6.5,   0.0,  -2.17, 1274.5, 0, 0.0,  0.0,   0.0,  0.0, 0.0,  0.0, 0.0, 4, 0.0,  0.0
point.7=2, -19.58,  0.0,   6.5,   308.5, 0, 0.0,  0.0,   0.0,  0.0, 0.0,  0.0, 0.0, 7, 0.0,  0.0
static_pitch=10.991821
static_cg_height=5.057427 // was 5.557427

[Views]
eyepoint=0.884289,-1.320025,2.665682


[GeneralEngineData]
engine_type=0
Engine.0=8.333, 0.000, 1.250
fuel_flow_scalar=1.000

[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit            
light.0=3, 0.4, -24.4, 3.85,  fx_navred ,
light.1=3, 0.4,  24.4, 3.85,  fx_navgre ,
light.2=3, -22.7,   0.00, 0.85,  fx_navwhi ,
light.3=2, -6.35, 0.0, 3.3,  fx_strobe ,

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0



[direction_indicators]
direction_indicator.0=1,0

[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, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 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

[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

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

[exits]
number_of_exits=2
exit_rate.0=0.4                             
exit_rate.1=0.4                             

[Flaps.0]
type=1
span-outboard=0.500
extending-time=5.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=16., 0.000
flaps-position.2=37.999, 0.000

[forcefeedback]
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=35500		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=2700		; 0 - 10000
gear_bump_right_direction=00500		; 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


[fltsim.0]
title=ATC DHC-2 Turbo Beaver
sim=F33An
model=
panel=
sound=
texture=
atc_id=C-FBKB
atc_heavy=0
ui_manufacturer=ATC
ui_type=de Havilland DHC-2 Turbo Beaver Mklll
ui_variation=C-FBKB
description=de Havilland DHC-2T Turbo Beaver Mk III

[General]
atc_type=DEHAVILLAND
atc_model=DH2T
performance=Length: 35 ft 3 in\nWing span: 48 ft\nWeight: 2996 \/ 5370 lb\nPower: 550 hp P&W PT6A-20 Turbine\nDesigner: Fred Banting\nDate: Nov 2001\n

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=1800.000
empty_weight_roll_MOI=2400.000
empty_weight_pitch_MOI=5200.000
empty_weight_yaw_MOI=4400.000
empty_weight_coupled_MOI=0.000
max_gross_weight=2244.000
CG_forward_limit=0.000
CG_aft_limit=1.000

[Reference Speeds]
flaps_up_stall_speed=52.0
full_flaps_stall_speed=41.0
cruise_speed=125.0

[flight_tuning]
cruise_lift_scalar=0.900
parasite_drag_scalar=0.900
induced_drag_scalar=0.900
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.500
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000

[airplane_geometry]
wing_area=182.000
wing_span=33.500
wing_root_chord=4.917
wing_dihedral=5.999
wing_incidence=0.000
wing_twist=-0.994
oswald_efficiency_factor=1.008  //was 1.508
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=1.229
wing_pos_apex_vert=0.000
htail_area=38.000
htail_span=10.500
htail_pos_lon=-13.917
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=0.000
vtail_area=15.000
vtail_span=4.416
vtail_sweep=0.000
vtail_pos_lon=-14.583
vtail_pos_vert=1.500
elevator_area=16.610
aileron_area=18.300
rudder_area=6.650
elevator_up_limit=28.000
elevator_down_limit=20.999
aileron_up_limit=19.996
aileron_down_limit=15.000
rudder_limit=23.995
elevator_trim_limit=19.498
spoiler_limit=0.000
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000

[ground_reaction]
main_gear_static_compression=0.3		// (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=0.3            // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=1.0		// Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=1.0		// Center gear strut damping, 0 = undamped osciallations, 1 = critically damped

[pitot_static]
vertical_speed_time_constant=1.0

[propeller]
thrust_scalar=1.500
propeller_type=0
propeller_diameter=6.833
propeller_blades=2
propeller_moi=5.000
beta_max=43.000
beta_min=15.000
min_gov_rpm=1100.000
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

[piston_engine]
power_scalar=1.000
cylinder_displacement=86.667
compression_ratio=8.500
number_of_cylinders=6
max_rated_rpm=2700.000
max_rated_hp=285.000
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.300
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=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[fuel]
LeftMain=0.000, -13.333, 0.000, 37.000, 0.000
RightMain=0.000, 13.333, 0.000, 37.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1

[contact_points]
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
// vertical positions were -2.35 -6.85
point.0=1, -20.4,   0.0, -1.95, 1600, 0, 0.66, 90.0, 0.46, 2.5, 0.79, 0.0, 0.0, 0,  0.0, 0.0
point.1=1,   2.58, -5.1, -6.18, 1600, 1, 0.83, 0.0,  0.54, 2.5, 0.79, 0.0, 0.0, 2,  0.0, 0.0
point.2=1,   2.58,  5.1, -6.18, 1600, 2, 0.83, 0.0,  0.54, 2.5, 0.79, 0.0, 0.0, 3,  0.0, 0.0
// Scrapes 
point.3=2,   0.0, -24.0,  4.0,  308.5, 0, 0.00, 0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 5,  0.0, 0.0	//left wing
point.4=2,   0.0,  24.0,  4.0,  308.5, 0, 0.00, 0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 6,  0.0, 0.0	//right wing
point.5=2, -22.0,   0.0,  0.3,  916.5, 0, 0.00, 0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 9,  0.0, 0.0	//tail cone
point.6=2,  11.0,   0.0, -1.0, 1274.5, 0, 0.00, 0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 4,  0.0, 0.0	//nose
point.7=2, -19.6,   0.0,  7.5,  308.5, 0, 0.00, 0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 7,  0.0, 0.0	//tail
static_pitch=10.795
static_cg_height=5.05 //was 5.5

[Views]
eyepoint=3.203945,-1.320025,2.665682


[GeneralEngineData]
engine_type=0
Engine.0=8.333, 0.000, 1.250
fuel_flow_scalar=1.000

[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit            
light.0=3, -0.2, -24.45, 3.85,  fx_navred ,
light.1=3, -0.2,  24.45, 3.85,  fx_navgre ,
light.2=3, -22.7,   0.00, 0.85,  fx_navwhi ,
light.3=2, -6.35, 0.0, 3.3,  fx_strobe ,

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0


[direction_indicators]
direction_indicator.0=1,0

[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, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 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

[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

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

[exits]
number_of_exits=2
exit_rate.0=0.4                             
exit_rate.1=0.4                             

[Flaps.0]
type=1
span-outboard=0.500
extending-time=5.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=16., 0.000
flaps-position.2=37.999, 0.000

[forcefeedback]
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=35500		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=2700		; 0 - 10000
gear_bump_right_direction=00500		; 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