//Copyright 2004 - Barry Blaisdell, Udo Lemmob, Bob May
//Premier Aircraft Design
//New ski model updated Feb 2004

[fltsim.0]
title=DHC6-300 Twin Otter - British Antarctic Survey
sim=DHC6W_24
model=
panel=
sound=
texture=
kb_checklists=DHC6_CHECK
kb_reference=DHC6_REF
atc_id_enable=1
atc_id=VP-FBB
ui_manufacturer=DeHavilland
ui_type=DHC6 Twin Otter
ui_variation=British Antarctic Survey VP-FBB Ski
atc_heavy=0
atc_airline=
atc_flight_number=
description=FS2004\nDeHavilland\nDHC6-300 Twin Otter \FDE and CFG files Copyright 2004\nPremier Aircraft Design\nhttp:www.flightsimnetwork.com\/premaircraft\nModel by Udo Lemmob

[General]
performance=Height 18 feet - 7 inches\nRate of Climb: 1200 fpm\nCeiling 21,000 feet\nEmpty Weight:7,415 lb\nMax T\/O wt. 12,500 lb\nPower: 2 x 652 SHP P&W PT6A-27\nStall: 74 kts Clean \/ 58 kts full flaps\nFlight Dynamics: Barry Blaisdell\nDesign: Udo Lemmob\nMaster Textures & livery: Bob May
atc_type=DEHAVILLAND
atc_model=DHC6

prop_anim_ratio=1.76

[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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit

light.0=3,  0.0, -33.00,  2.69, fx_navred ,
light.1=3,  0.0,  33.00,  2.69, fx_navgre ,

light.3=2,  -.70, -32.5,  2.69, fx_strobe ,
light.4=2,  -.70,  32.5,  2.69, fx_strobe ,

light.5=1,  -28.85,    0.00,  11.85, fx_beacon ,
light.6=1,  -20.00,   0.00, -3.30, fx_beacon ,

light.7=4,   9.97,  0.00,   0.47 , fx_vclight,
light.8=4,   0.00,  0.00,   0.47 , fx_vclighth,

[WEIGHT_AND_BALANCE]
empty_weight=7415.000

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

max_number_of_stations=20

station_load.0=170.000, 5.000, -2.000, 0.000
station_load.1=170.000, 5.000, 2.000, 0.000
station_load.2=170.000, -2.100, -2.000, 0.000
station_load.3=170.000, -2.100, 2.000, 0.000
empty_weight_roll_MOI=110000.000
empty_weight_pitch_MOI=150000.000
empty_weight_yaw_MOI=147500.000
empty_weight_coupled_MOI=0.000
max_gross_weight=10775.000
CG_forward_limit=0.000
CG_aft_limit=1.000

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

[SMOKESYSTEM]
smoke.0=0.00, 2.00,  9.40, fx_engsmoke

[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, 0,1
Adf.1=1
Transponder.1=1
Marker.1=1

[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 , 1

[fuel]
LeftMain=0.000, -14.500, -1.000, 150.000, 0.000
LeftAux=0.000, -6.000, -1.500, 50.000, 0.000
RightMain=0.000, 14.500, -1.000, 150.000, 0.000
RightAux=0.000, 6.000, -1.500, 50.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=800.000000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=150.000000
pitch_takeoff_ga=8.000000
autoland_available=0
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
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

[contact_points]
//Classes...What type of point    0=Unused or Ignore
//                                                      1=Wheel
//                                                      2=Scrape point
//                                                      4=Float
//                                                      5=Float Rudder
//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 / Water Rudder Effectiveness  (0=Undamped, 1=Critically Damped) / 1.0 = normal
//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)

point.0=1.000, 12.877, 0.000, -7.480, 2360.907, 0.000, 0.568,100.000,0.270, 2.237, 0.895, 0.000, 0.000, 1.000, 0.000, 0.000
point.1=1.000, -3.000,-6.417, -7.747, 2360.907, 1.000, 0.568, 0.000, 0.400, 2.400, 0.709, 0.000, 0.000, 2.000, 0.000, 0.000
point.2=1.000, -3.000, 6.417, -7.747, 2360.907, 2.000, 0.568, 0.000, 0.400, 2.400, 0.709, 0.000, 0.000, 3.000, 0.000, 0.000
point.3=2.000, 0.000, -33.417, 5.000, 2360.907, 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, 0.000, 33.417, 5.000, 2360.907, 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, -34.750, 0.000, -0.833, 2360.907, 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, 19.167, 0.000, -0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch=-0.500
static_cg_height=7.820

[airplane_geometry]
wing_area=375.000
wing_span=76.667
wing_root_chord=6.167
wing_dihedral=2.5
wing_incidence=1.000
wing_twist=-1.500
oswald_efficiency_factor=0.325
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=0.000
wing_pos_apex_vert=0.000
htail_area=67.000
htail_span=17.167
htail_pos_lon=-24.583
htail_pos_vert=0.000
htail_incidence=0.500
htail_sweep=0.000
vtail_area=42.000
vtail_span=7.389
vtail_sweep=0.000
vtail_pos_lon=-20.500
vtail_pos_vert=4.083
elevator_area=36.000
aileron_area=32.000
rudder_area=21.000
elevator_up_limit=25.000
elevator_down_limit=16.000
aileron_up_limit=17.500
aileron_down_limit=16.000
rudder_limit=19.000
elevator_trim_limit=19.500
spoiler_limit=59.000
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000

[GeneralEngineData]
engine_type=5
Engine.0=5.833, -9.167, 0.000
Engine.1=5.833, 9.167, 0.000
fuel_flow_scalar=1.005
min_throttle_limit=-0.599915

[TurbineEngineData]
fuel_flow_gain=0.090
inlet_area=.300
rated_N2_rpm=25920.000
static_thrust=100.000
afterburner_available=0

[propeller]
propeller_type=0
propeller_diameter=8.750
propeller_blades=3
propeller_moi=18.000
beta_max=62.000
beta_min=15.000
min_gov_rpm=21520.000
prop_tc=0.004
gear_reduction_ratio=14.600
fixed_pitch_beta=20.000
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=84.300
power_absorbed_cf=0.900
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=1.000
minimum_reverse_beta=-12.000

[turboprop_engine]
maximum_torque=1897.000

[Reference Speeds]
flaps_up_stall_speed=74.000
full_flaps_stall_speed=59.000
cruise_speed=170.000
max_indicated_speed=190.000000
max_mach=0.350000

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=0.000,0.000,0.000

[direction_indicators]
direction_indicator.0=3,0

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.5
aileron_effectiveness=1.5
rudder_effectiveness=1.5
pitch_stability=1.3
roll_stability=1.3
yaw_stability=1.3
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[Flaps.0]
type=1
span-outboard=0.500
extending-time=10.000
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=10.000, 0.000
flaps-position.2=15.000, 0.000
flaps-position.3=20.000, 0.000
flaps-position.4=25.000, 0.000
flaps-position.5=35.000, 0.000

[exits]
number_of_exits=3
exit_rate.0=0.3                               ;Percent per second
exit_rate.1=0.3                               ;Percent per second
exit_rate.2=0.3

[brakes]
toe_brakes_scale=1.000000
parking_brake=1

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0