//Copyright 2001 - Barry Blaisdell
//Premier Aircraft Design
[fltsim.0]
title=CC-138 CAF Twin Otter_13805
sim=dhc6t_22
model=
panel=
sound=
texture=
kb_checklists=DHC6_CHECK
kb_reference=DHC6_REF
atc_id_enable=1
atc_id=13805
ui_manufacturer=DeHavilland
ui_type=DHC6 Twin Otter
ui_variation=Canadian Forces 13805
description=FS2002 PRO\nDeHavilland\nDHC6-300S\nTwin Otter \nAll files Copyright 2002\nPremier Aircraft Design\nhttp:\/\/www.flightsimnetwork.com\/premaircraft\/\n\n\n
atc_heavy=0
atc_airline=
atc_flight_number=

[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\nDesigner: © Barry Blaisdell 3\/2002\nFlight Dynamics © Steve Small 8\/2001\n
atc_type=TWINOTTER
atc_model=

[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
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3,  -1.4, -33.55,  5.15, fx_navred ,
light.1=3,  -1.4,  33.55,  5.15, fx_navgre ,
light.2=3,  -31.9,   0.00,  0.28, fx_navwhi ,
light.3=2,   -1.7, -33.85,  5.2, fx_strobe ,
light.4=2,   -1.7,  33.85,  5.2, fx_strobe ,
light.5=1,  -29.0,   0.00,  13.8, fx_beacon ,
light.6=1,  -13.3,   0.00, -3.0, fx_beacon ,
light.7=4,   5.91,   0.00,  1.64, fx_vclight,
light.8=5, 1.1, -12.45,  4.30,  fx_landing ,
light.9=5, 1.1,  12.45,  4.30,  fx_landing,
light.10=5, 1.1, -13.05, 4.30,  fx_landing ,
light.11=5, 1.1,  13.05, 4.30,  fx_landing,
light.12=5, 12.5,  -0.85, -3.50,  fx_landing,

[WEIGHT_AND_BALANCE]
empty_weight= 7415.000

reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.900, 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, 0
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, -4.250, 0.000, 144.000, 0.000
LeftAux=0.000, -6.000, 0.000, 38.000, 0.000
RightMain=0.000, 4.250, 0.000, 144.000, 0.000
RightAux=0.000, 6.000, 0.000, 38.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.000000
autothrottle_available=1
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

[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=1.00,12.916667,0.00,-7.00,1574.803150,0.00,1.589497,39.300000,0.290695,4.500000,0.657370,5.00,5.00,0.00,0.00,0.00
point.1=1.00,-1.666667,-6.666667,-6.833333,1574.803150,1.00,1.589497,0.00,0.329056,2.500000,0.520396,5.00,5.00,2.00,0.00,0.00
point.2=1.00,-1.666667,6.666667,-6.833333,1574.803150,2.00,1.589497,0.00,0.329056,2.500000,0.520396,5.00,5.00,3.00,0.00,0.00
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= 0.000
static_cg_height= 6.085

[airplane_geometry]
wing_area= 375.000
wing_span= 76.667
wing_root_chord= 6.167
wing_dihedral= 2.499
wing_incidence= 0.000
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= 1.000

[TurbineEngineData]
fuel_flow_gain= 0.025
inlet_area=.300
rated_N2_rpm= 29920.000
static_thrust= 100.000
afterburner_available= 0

[propeller]
propeller_type= 0
propeller_diameter= 8.50
propeller_blades= 4
propeller_moi= 120.000
beta_max= 62.000
beta_min= 15.000
min_gov_rpm= 25520.000
prop_tc= 0.004
gear_reduction_ratio= 17.600
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= 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

[turboprop_engine]
maximum_torque= 1897.000

[Reference Speeds]
flaps_up_stall_speed= 74.000
full_flaps_stall_speed= 59.200
cruise_speed= 163.641

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

[Views]
eyepoint=8.740363,0.0000,2.742577

[direction_indicators]
direction_indicator.0=3,0

[flight_tuning]
cruise_lift_scalar=1.2999
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.4999
aileron_effectiveness=1.4999
rudder_effectiveness=1.4999
pitch_stability=1.2999
roll_stability=1.2999
yaw_stability=1.2999
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=9.000
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=25.000, 0.000
flaps-position.4=30.000, 0.000
flaps-position.5=37.500, 0.000