//DeHavilland DHC-2 Beaver for FS2004
//Made from FS2004 Lake Renegade 250 (originally C182) by John L. Woodward, October 2003

[fltsim.0]
title=de Havilland DHC-2 Beaver
sim=DeHavilland DHC-2 Beaver
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=Beaver_ref
atc_id=N101TC
ui_manufacturer=de Havilland
ui_type=DHC-2 Beaver
ui_variation=Floats
description=FSDS2 model by John L. Woodward, October 2003

[General]
atc_type=deHavilland
atc_model=Beaver
editable=1
performance=See Reference page on kneeboard

[WEIGHT_AND_BALANCE]
max_gross_weight=5090.000
empty_weight=1900.000

reference_datum_position=-1.500, 0.000, 0.000
empty_weight_CG_position=1.500, 0.000, 0.000

max_number_of_stations=50

//Moments of Inertia
empty_weight_pitch_MOI=2900
empty_weight_roll_MOI=1137.000
empty_weight_yaw_MOI=2360.000
empty_weight_coupled_MOI=0.000
CG_forward_limit=0.000
CG_aft_limit=1.000
station_load.0=0.000000,0.000000,0.000000,0.000000

[flight_tuning]
cruise_lift_scalar=1.00 
parasite_drag_scalar=2.600
induced_drag_scalar=1.500
elevator_effectiveness=1.000
aileron_effectiveness=.75
rudder_effectiveness=1.000
pitch_stability=1.50
roll_stability=1.00
yaw_stability=1.00
elevator_trim_effectiveness=1.50
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
p_factor_on_yaw          = 0.5
torque_on_roll           = .10
gyro_precession_on_yaw   = .10
gyro_precession_on_pitch = .10

[GeneralEngineData]
engine_type=0
Engine.0=4.500, 0.000, 0.000
fuel_flow_scalar=0.70
min_throttle_limit=0.000000

[piston_engine]
power_scalar=1.000
cylinder_displacement=109.440
compression_ratio=6.700
number_of_cylinders=9
max_rated_rpm=2300.000
max_rated_hp=450.000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.300
turbocharged=1
max_design_mp=36.500
min_design_mp=1.000
critical_altitude=15000.000
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=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[propeller]
thrust_scalar=.65
propeller_type=0
propeller_diameter=8.500
propeller_blades=2
propeller_moi=9.000
beta_max=43.000
beta_min=15.000
min_gov_rpm=1400.000
prop_tc=0.100
gear_reduction_ratio=1.000
fixed_pitch_beta=0.000
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]
//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

[contact_points]
point.0=4.000, -9.000, 6.000, -6.050, 1500.000, 0.000, 0.000, 0.000, .750, 2.000, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000
point.1=4.000, -9.000, -6.000, -6.050, 1500.000, 0.000, 0.000, 0.000, .750, 2.000, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000
point.2=4.000, 9.000, 6.000, -6.650, 1500.000, 0.000, 0.000, 30.000, .750, 2.000, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000
point.3=4.000, 9.000, -6.000, -6.650, 1500.000, 0.000, 0.000, 30.000, .750, 2.000, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000
point.4=5.000, -10.000, 0.000, -6.000, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 2.000, 2.000, 0.000, 0.000, 0.000

max_number_of_points=21
static_pitch=1.000
static_cg_height=6.00
gear_system_type=0

[fuel]
//Tanks Position and capacity: 
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1=0.000, 0.000, 0.000,35.0, 0.000
LeftMain=0.000, 0.000, 0.000, 35.000, 0.000
RightMain=0.000, 0.000, 0.000, 26.000, 0.000
//Fuel type: 1=Avgas, 2 = JetA
fuel_type=1
number_of_tank_selectors=1
electric_pump=1

[Views]
eyepoint=1.80, -1.25, 2.40
//(feet) longitudinal, lateral, vertical distance from reference datum

[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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit            
light.0=3, .75, -23.80, 3.90, fx_navred
light.1=3, .75, 23.80, 3.90, fx_navgre
light.2=3, -22.00,   0.00, .78, fx_navwhi
light.3=5, 2.6, -12.22, 3.42, fx_landing
light.4=4, 0, 1, 2.30, fx_vclight
light.5=4, 0, -1, 2.30, fx_vclight

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

[airplane_geometry]
wing_area=170.000
wing_span=38.000
wing_root_chord=4.900
wing_dihedral=2.000
wing_incidence=1.500
wing_twist=0.000
oswald_efficiency_factor=0.800
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=1.500
wing_pos_apex_vert=0.000
htail_area=39.000
htail_span=11.700
htail_pos_lon=-12.000
htail_pos_vert=4.500
htail_incidence=3.200
htail_sweep=10.000
vtail_area=18.000
vtail_span=4.800
vtail_sweep=40.000
vtail_pos_lon=-12.000
vtail_pos_vert=0.000
elevator_area=16.600
aileron_area=18.300
rudder_area=6.700
elevator_up_limit=28.000
elevator_down_limit=21.000
aileron_up_limit=20.000
aileron_down_limit=15.000
rudder_limit=24.000
elevator_trim_limit=30
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

[Reference Speeds]
flaps_up_stall_speed=54
full_flaps_stall_speed=39
cruise_speed=110
max_indicated_speed=128

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
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=0.000000

[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

[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=8.000
system_type=0
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=1.000
drag_scalar=1.25
pitch_scalar=.25
flaps-position.0= 0.0, 0.0
flaps-position.1= 15.0, 0.0
flaps-position.2= 35.0, 0.0
flaps-position.3= 50.0, 0.0
flaps-position.4= 58.0, 0.0

[brakes]
toe_brakes_scale=0.976592
parking_brake=0

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[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]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0