[fltsim.0]
title=DHC5 "Buffalo"
sim=dhc5
model=
panel=
sound=
texture=
panel_alias = 
sound_alias = beech_king_air_350\sound
kb_checklists=
kb_reference=
atc_id_color=
atc_id=442
ui_manufacturer=De Havilland
ui_type=DHC5
ui_variation=Canadian Air Force
description=One of the most powerful turboprops ever made (engine vs. size), used primarily for transport of cargo and military personel. Still in use today in several countries. Has remarkable STOL capabilities.
atc_heavy=0
atc_airline=
atc_flight_number=

[General]
atc_type=Dehavilland
atc_model=DHC5
performance=Engine:	2x GE Turboprops 3133shp each \nCeiling:	30000ft  \nRange:	~3100km  \nMax Speed:	467kmh/280mph  \n
Weight:	11000kg (Empty), ~20000kg (Max)\n	

[WEIGHT_AND_BALANCE]
max_gross_weight = 41000.000
empty_weight = 22486.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, 0.000

max_number_of_stations =50


;Moments of Inertia
empty_weight_pitch_MOI  = 30000.000
empty_weight_roll_MOI   = 18200.000
empty_weight_yaw_MOI    = 36500.000
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     =1.000
parasite_drag_scalar   =1.000
induced_drag_scalar    =1.000
elevator_effectiveness =1.000
aileron_effectiveness  =1.000
rudder_effectiveness   =1.000
pitch_stability        =1.000
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[GeneralEngineData]
engine_type = 5
Engine.0 = 19.000, -15.000, 1.400
Engine.1 = 19.000, 15.000, 1.400
fuel_flow_scalar        = 1.000

[propeller]
thrust_scalar           =1.000
propeller_type          = 0
propeller_diameter      = 14.500
propeller_blades        = 3
propeller_moi           = 24.000
beta_max                = 45.000
beta_min                = 15.200
min_gov_rpm             = 25000.000
prop_tc                 = 0.004
gear_reduction_ratio    = 17.600
fixed_pitch_beta        = 0.000
low_speed_theory_limit  = 80.000
prop_sync_available     = 1
prop_deice_available    = 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather     = 700.000
beta_feather            = 79.300
power_absorbed_cf       = 0.900
defeathering_accumulators_available= 0 
prop_reverse_available  = 1
minimum_on_ground_beta  = 1.000
minimum_reverse_beta    = -14.000

[TurbineEngineData]
fuel_flow_gain          = 0.011
inlet_area              = 1.000
rated_N2_rpm            = 30000.000
static_thrust           = 300.000
afterburner_available= 0

[turboprop_engine]
power_scalar            =1.000
maximum_torque          = 5000.000
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


[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

        //0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
        //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)

[contact_points]
point.0= 1.000, 16.250, 0.000, -4.200, 1181.000, 0.000, 0.596, 39.900, 0.296, 2.500, 0.952, 4.800, 4.800, 0.000, 0.000, 0.000
point.1= 1.000, -1.250, -8.580, -4.450, 1574.000, 1.000, 0.596, 0.000, 0.642, 2.500, 0.815, 4.500, 5.200, 2.000, 0.000, 0.000
point.2= 1.000, -1.250, 8.580, -4.450, 1574.000, 2.000, 0.596, 0.000, 0.642, 2.500, 0.815, 4.800, 4.900, 3.000, 0.000, 0.000
point.3= 2.000, -3.330, -23.900, 0.160, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -3.330, 23.900, 0.160, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -22.600, 0.000, 3.160, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 23.080, 0.000, -2.660, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch = -0.300
static_cg_height = 4.050

[Views]
eyepoint = -2.54, -1.20, 3.0



[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1, 0
Com.2         = 1, 0
Nav.1         = 1, 0, 1
Nav.2         = 1, 0, 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 = 150, 250
aileron  = 150, 250
rudder   = 150, 250

[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=3,0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3,   0.56, -28.41,  1.97, fx_navred ,
light.1 = 3,   0.56,  28.41,  1.97, fx_navgre ,
light.2 = 3, -31.20,   0.00,  9.09, fx_navwhi ,
light.3 = 2,   0.89, -27.89,  1.77, fx_strobe ,
light.4 = 2,   0.89,  27.89,  1.77, fx_strobe ,
light.5 = 1, -25.49,   0.00,  9.74, fx_beacon ,
light.6 = 2,  -4.55,   0.00, -1.85, fx_strobe ,
light.7 = 4,   5.91,   0.00,  1.64, fx_vclight,

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

[fuel]
LeftMain  = 0.000, -14.500, -1.000, 500.000, 0.000
LeftAux   = 0.000, -6.000, -1.500, 79.500, 0.000
RightMain = 0.000, 14.500, -1.000, 500.000, 0.000
RightAux  = 0.000, 6.000, -1.500, 79.500, 0.000
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    


[airplane_geometry]
wing_area               = 944.000
wing_span               = 96.000
wing_root_chord         = 9.800
wing_dihedral           = 3.000
wing_incidence          = 0.000
wing_twist              = 3.000
oswald_efficiency_factor= 0.700
wing_winglets_flag      = 0
wing_sweep              = 0.000
wing_pos_apex_lon       = 0.000
wing_pos_apex_vert      = 0.000
htail_area              = 210.000
htail_span              = 32.000
htail_pos_lon           = -30.500
htail_pos_vert          = 0.000
htail_incidence         = 0.500
htail_sweep             = 0.000
vtail_area              = 150.000
vtail_span              = 14.100
vtail_sweep             = 0.000
vtail_pos_lon           = -27.000
vtail_pos_vert          = 11.000
elevator_area           = 60.000
aileron_area            = 25.000
rudder_area             = 40.000
elevator_up_limit       = 13.000
elevator_down_limit     = 10.000
aileron_up_limit        = 15.000
aileron_down_limit      = 15.000
rudder_limit            = 30.000
elevator_trim_limit     = 7.000
spoiler_limit           = 60.000
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    = 96.000
full_flaps_stall_speed  = 76.800
cruise_speed            = 240.000

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 0
pitch_takeoff_ga= 8.000

[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
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=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 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
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 1
damaging-speed= 200.000
blowout-speed= 250.000
lift_scalar= 1.000
drag_scalar= 1.400
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000
flaps-position.4= 40.000, 0.000