[fltsim.0]
title=CT-114  Snowbirds
sim=CT-114  Snowbirds
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Canadair
ui_type=CT 114
ui-variation=CT 114
description=The CT-114 Tutor aircraft was designed and manufactured by Canadair Limited (now Canadair, Bombardier Inc.) to a Royal Canadian Air Force (RCAF) specification

[General]
performance=Manufacturer:  Canadair:  Crew:  2 (pilots) in ejection seats \nPower Plant:  Orenda J-85 CAN-40 Turbojet with 2,950 lbs thrust \nPerformance:  Max Speed: 486 mph (782 km\/h) \nService Ceiling: 42,200 ft (12,863 m) Range: 940 m (1,563 km) \nWeights:  Empty: 4,895 lbs (2,220 kg) Gross: 7,397 lbs (3,335 kg) \nDimensions:  Span: 36 ft 6 in (11.13 m) Length: 32 ft 0 in (9.75 m) Height 9 ft 4 in (2.84 m)  \nBy: Rey Lopez e-mail: reylopez_99@yahoo.com\nFS2002 Pro, July 29, 2002 All rights reserved\n

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000

empty_weight_roll_MOI=23506.000000
empty_weight_pitch_MOI=16188.000000
empty_weight_yaw_MOI=14958.000000
empty_weight_coupled_MOI=0.000000

empty_weight=4895.000000
max_gross_weight=7397.00

[Reference Speeds]
flaps_up_stall_speed=108.000000
full_flaps_stall_speed=88.000000
cruise_speed=345.405968               //KIAS


max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000

empty_weight=4895.000000
max_gross_weight=7397.00

[fuel]
//Parameter 1 = Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//          2 = Lateral      (feet)
//          3 = Vertical     (feet)
//          4 = Usable       (gallons)
//          5 = Unusable     (gallons)
//
//          1      2      3        4     5
//____________________________________________
Center1=   0.000, 0.000, 0.000, 400.00, 0.00
LeftMain=  0.000, 0.000, 0.000, 850.00, 0.00
RightMain= 0.000, 0.000, 0.000, 850.00, 0.00

number_of_tank_selectors=1
fuel_type=2.000000          //Fuel type: 1 = Avgas, 2 = JetA

[airplane_geometry]
wing_area=359.580000   // 
wing_span=36.0
wing_root_chord=8.00
wing_dihedral=0.000
wing_incidence=0.0
wing_twist=0.0
oswald_efficiency_factor=0.750638  // pretty good Activ
//oswald_efficiency_factor=0.800638
wing_winglets_flag=0
wing_sweep=0.0
wing_pos_apex_lon=2.550000
wing_pos_apex_vert=0.000000
htail_area=98.7200  
htail_span=13.66
htail_pos_lon=-17.4914
htail_pos_vert=5.1900
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=12.440
vtail_span=3.48
vtail_sweep=0.000000
vtail_pos_lon=-16.1400
vtail_pos_vert=2.120
elevator_area=23.000000 
aileron_area=18.20000  
rudder_area=6.9400 
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.00000
min_flaps_for_spoilerons=0.000000

[contact_points]
/Parameters as defined in Flight Simulator 2002 SDK -- AIRCRAFT CONTAINER SYSTEM --
//1  Class
//2  Longitudinal Position             (feet)
//3  Lateral Position                  (feet)
//4  Vertical Position                 (feet)
//5  Impact Damage Threshold           (Feet Per Minute)
//6  Brake Map                         (0=None, 1=Left, 2=Right)
//7  Wheel Radius                      (feet)
//8  Steer Angle                       (degrees)
//9  Static Compression                (feet)  (0 if rigid) 
//10 Max/Static Compression Ratio
//11 Damping Ratio / Water Rudder Effectiveness  (0=Undamped, 1=Critically Damped) / 1.0 = normal
//12 Extension Time                    (seconds)
//13 Retraction Time                   (seconds)
//14 Sound Type
//15 Airspeed limit for retraction     (KIAS)
//16 Airspeed that gear gets damage at (KIAS)

//     1       2       3      4       5    6      7      8      9     10   11   12   13  14  15   16
//___________________________________________________________________________________________________
point.0=1,   10.66,   0.00, -3.265, 1574, 0.00, 0.700, 57.68, 0.350, 2.5, 0.95, 5.0, 5.0, 0, 0.0, 0.0
point.1=1,   -1.00,  -6.75, -3.086, 1574, 1.00, 1.064,  0.00, 0.350, 2.5, 0.75, 5.0, 5.0, 2, 0.0, 0.0
point.2=1,   -1.00,   6.75, -3.086, 1574, 2.00, 1.064,  0.00, 0.350, 2.5, 0.75, 5.0, 5.0, 3, 0.0, 0.0

point.3=2,   -5.91, -22.16,  0.830, 1574, 0.00,  0.00,  0.00, 0.000, 0.0, 0.00, 0.0, 0.0, 5, 0.0, 0.0
point.4=2,   -5.91,  22.16,  0.830, 1574, 0.00,  0.00,  0.00, 0.000, 0.0, 0.00, 0.0, 0.0, 6, 0.0, 0.0

point.5=2,  -16.58,   0.00,  -0.16, 1574, 0.00,  0.00,  0.00, 0.000, 0.0, 0.00, 0.0, 0.0, 9, 0.0, 0.0
point.6=2,   11.66,   0.00,  -0.16, 1574, 0.00,  0.00,  0.00, 0.000, 0.0, 0.00, 0.0, 0.0, 4, 0.0, 0.0

static_pitch=0.0
static_cg_height=3.05750926

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=12.5000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=4.998114,0.000000
flaps-position.2=9.996227,0.000000
flaps-position.3=19.994341,0.000000
flaps-position.4=29.992454,0.000000

[GeneralEngineData]
engine_type=1
Engine.0=-3.5167,0.000000,0.000000
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=6.525560
rated_N2_rpm=29920.000000
//static_thrust=3245     //#1
//static_thrust=3445   //#2
static_thrust=4245
//static_thrust=2950   //Too little for Take Off
afterburner_available=0
reverser_available=0

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=0, 0
Nav.1=1, 0, 1
Nav.2=0, 0, 0
Adf.1=1
Transponder.1=0
Marker.1=0

[LIGHTS]
//Parameter 1 = Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit  
//          2 = Longitudinal      (feet)
//          3 = Lateral           (feet)
//          4 = Vertical          (feet)
//          5 = Effect file name
//____________________________________________________      
light.0 = 3,  -0.88, -18.60, 0.90, fx_navred
light.1 = 3,  -0.88,  18.401, 0.90, fx_navgre
light.2 = 2,  -1.15, -18.50, 0.90, fx_strobe
light.3 = 2,  -1.15,  18.30, 0.90, fx_strobe
light.4 = 1, -17.60,   0.00, 6.18, fx_beacon
//light.5 = 4,  -2.27,   0.00, 1.40, fx_vclight



[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0

                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus       = 0, 10, 9.5
avionics           = 1, 5 , 9.5
additional_system  = 0, 20, 9.5
marker_beacon      = 1, 2 , 9.0
fuel_pump          = 0, 5 , 9.0

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

[Views]
eyepoint=4.67,-1.250,3.299

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=3,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 0

[SMOKESYSTEM]
smoke.0=0.000, -15.00, -1.50, fx_smoke_rx
smoke.1=0.000, -15.00,  1.50, fx_smoke_rx
smoke.2=-1.0,-3.0,-10.0, fx_contrail_s.fx
smoke.3=-1.0,-3.0,10.0, fx_contrail_s.fx

[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5#
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1#
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[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