[fltsim.0]
title=Snowed Inn Air Charter Service
sim=DHC-2a
model=1
panel=
sound=beaver
texture=
kb_checklists=DHC2_check
kb_reference=DHC2_ref
atc_id_enable=1
atc_id=A95-202
editable=0
ui_manufacturer=Snowed Inn Charter
ui_type=THE EAGER BEAVER!
ui_variation=ALASKA SCENIC / FISHING TOURS
atc_flight_number=A95-202
description=Designed For Fly Alaska Bush Scenery

[WEIGHT_AND_BALANCE]

max_gross_weight=5100                  // (pounds)
empty_weight=3550                     // (pounds)

reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=-0.250000,0.000000,0.000000

max_number_of_stations=50
station_load.0=154.00,  2.25, -1.20, 1.75  //Pilot
station_load.1=000.00,  2.25,  1.20, 1.75  //CoPilot
station_load.2=000.00, -2.25, -1.20, 1.75  //Passenger1
station_load.3=000.00, -2.25,  1.20, 1.75  //Passenger2
station_load.4=000.00, -5.00, -1.20, 1.75  //Passenger3
station_load.5=000.00, -5.00,  1.20, 1.75  //Passenger4
station_load.6=000.00, -6.80,  0.00, 0.70  //Baggage

empty_weight_roll_MOI=5343.00000
empty_weight_pitch_MOI=5767.00000
empty_weight_yaw_MOI=9367.00000
empty_weight_coupled_MOI=0.00000

[fuel]
Center1=-1.50, 0.00, -0.75, 35.00, 0.00   //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=0.30, 0.00, -0.75, 35.00, 0.00   //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-3.00, 0.00, -0.75, 26.00, 0.00   //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=1.00
number_of_tank_selectors=1
electric_pump=1

[flight_tuning]
cruise_lift_scalar=0.6
parasite_drag_scalar=1.47
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
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

[airplane_geometry]
wing_area=250.00
wing_span=48.00
wing_root_chord=5.25
wing_dihedral=1.999512
wing_incidence=1.499634
wing_twist=0.000000
oswald_efficiency_factor=0.750294
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.00
wing_pos_apex_vert=4.00
htail_area=65.00
htail_span=15.83
htail_pos_lon=-21.00
htail_pos_vert=2.00
htail_incidence=0.417480
htail_sweep=0.00
vtail_area=30.00
vtail_span=6.244998
vtail_sweep=0.00
vtail_pos_lon=-20.00
vtail_pos_vert=4.00
elevator_area=27.95
aileron_area=25.00
rudder_area=10.50
elevator_up_limit=28.00
elevator_down_limit=20.00
aileron_up_limit=18.00
aileron_down_limit=11.00
rudder_limit=25.00
elevator_trim_limit=19.480565
spoiler_limit=90.0000
spoilerons_available=0
aileron_to_spoileron_gain=0.00
min_ailerons_for_spoilerons=0.00
min_flaps_for_spoilerons=0.00

//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=1.00,  -2.10,  -5.00, -7.90, 1574.80, 1.00, 0.74,  0.00, 0.35, 2.50, 1.16, 5.00, 5.00, 0.00
point.1=1.00,  -2.10,   5.00, -7.90, 1574.80, 2.00, 0.74,  0.00, 0.35, 2.50, 1.16, 5.00, 5.00, 0.00
point.2=1.00,  10.25,  -5.00, -7.80, 1574.80, 0.00, 0.64, 40.00, 0.26, 2.50, 0.78, 5.00, 5.00, 2.00
point.3=1.00,  10.25,   5.00, -7.80, 1574.80, 0.00, 0.64, 40.00, 0.26, 2.50, 0.78, 5.00, 5.00, 3.00
point.4=4.00, -12.00,  -5.08, -4.80, 1574.80, 0.00, 0.00,  0.00, 0.34, 2.50, 1.70, 0.00, 0.00, 2.00
point.5=4.00, -12.00,   5.08, -4.80, 1574.80, 0.00, 0.00,  0.00, 0.34, 2.50, 1.70, 0.00, 0.00, 2.00
point.6=4.00,   2.00,  -5.08, -6.00, 1574.80, 0.00, 0.00,  0.00, 0.52, 2.50, 0.73, 0.00, 0.00, 2.00
point.7=4.00,   2.00,   5.08, -6.00, 1574.80, 0.00, 0.00,  0.00, 0.52, 2.50, 0.73, 0.00, 0.00, 2.00
point.8=2.00,   0.00, -24.00,  4.00,  308.47, 0.00, 0.00,  0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00
point.9=2.00,   0.00,  24.00,  4.00,  308.47, 0.00, 0.00,  0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00
point.10=2.00, -21.83,   0.00,  0.33,  916.56, 0.00, 0.00,  0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00
point.11=2.00,   6.50,   0.00, -2.16, 1274.43, 0.00, 0.00,  0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00
point.12=2.00,   0.00, -24.00,  4.00,  308.47, 0.00, 0.00,  0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 7.00
point.13=2.00, -19.58,   0.00,  7.50,   30.03, 0.00, 0.00,  0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 8.00
point.14=5.00, -12.00,  -5.08, -4.60, 1600.00, 0.00, 0.00, 50.00, 0.00, 0.00, 1.00, 1.00, 1.20, 0.00
point.15=5.00, -12.00,   5.08, -4.60, 1600.00, 0.00, 0.00, 50.00, 0.00, 0.00, 1.00, 1.00, 1.20, 0.00

static_pitch=0.00
static_cg_height=7.75
gear_system_type=0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0=3,    1.00, -24.90, 4.45, fx_navred
light.1=3,    1.00,  24.90, 4.45, fx_navgre
light.2=3,  -23.00,   0.00, 1.95, fx_navwhi
light.3=2,    0.85, -24.90, 4.45, fx_strobe
light.4=2,    0.85,  24.90, 4.45, fx_strobe
light.5=1,   -5.95,   0.00, 4.50, fx_beacon

[SMOKESYSTEM]


[EFFECTS]
wake=fx_wake
water=fx_AI_floatplane_spray-and-wake
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[Flaps.0]
type=1
span-outboard=0.50
extending-time=7.00
system_type=0
flaps-position.0=00.00
flaps-position.1=08.25
flaps-position.2=16.50
flaps-position.3=25.00
flaps-position.4=33.00
flaps-position.5=41.00
flaps-position.6=49.00
flaps-position.7=58.00
damaging-speed=100                                 // KIAS
blowout-speed=120                                  // KIAS
lift_scalar=1.8                                     
drag_scalar=0.6
pitch_scalar=0.2

[GeneralEngineData]
engine_type=0
Engine.0=6.00, 0.00, 0.75
fuel_flow_scalar=0.92
min_throttle_limit=0.000000

[piston_engine]
cylinder_displacement=109.440000
compression_ratio=6.700000
number_of_cylinders=9
max_rated_rpm=2300.000000
max_rated_hp=450.000000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.18
turbocharged=2
max_design_mp=37.000000
min_design_mp=8.000000
critical_altitude=5000.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
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

[propeller]
propeller_type=0
propeller_diameter=9.00
propeller_blades=3
propeller_moi=8.00
beta_max=24.00
beta_min=10.50
min_gov_rpm=1400.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000

[Reference Speeds]
flaps_up_stall_speed=52.00
full_flaps_stall_speed=38.00
cruise_speed=112.00
max_indicated_speed=180.000000

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

[Views]
eyepoint=1.5, -1.0, 3.35

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
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

[direction_indicators]
direction_indicator.0=1,0

[General]
atc_type=DeHavilland
atc_model=DHC2
performance=-Dimensions \nSpan : 48'0 ft \nLength : 30'4 ft \nHeight : 9'0 ft \n-Weight \nempty : 2,850 lb \nmax : 5,100 lb \n-Power Plant : 450hp P&W R-985-AN Wasp Junior \n-Performance : \nmax speed : 140 mph \nceiling : 18.000ft\nrange : 778 miles \n\nAircraft by: Steven Grant - August 2002

[brakes]
toe_brakes_scale=0.465407
parking_brake=1

[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

[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

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0