[fltsim.0]
title=C-1-402
sim=C-1_EC-1
model=C-1
panel=
sound=
texture=SQ-402
kb_checklists=
kb_reference=
atc_id=78-1022
atc_airline=JASDF
atc_flight_number=1123
ui_manufacturer=Kawasaki
ui_type=C-1
ui_variation=SQ-402
description=Transport kawasaki C-1
atc_heavy=0
atc_parking_codes=M003,C1
atc_parking_types=MIL_CARGO

[fltsim.1]
title=C-1-403
sim=C-1_EC-1
model=C-1
panel=
sound=
texture=SQ-403
kb_checklists=
kb_reference=
atc_id=78-1026
atc_airline=JASDF
atc_flight_number=1123
ui_manufacturer=kawasaki
ui_type=C-1
ui_variation=SQ-403
description=Transport kawasaki C-1
atc_heavy=0
atc_parking_codes=M003,C1
atc_parking_types=MIL_CARGO
 
[fltsim.2]
title=EC-1
sim=C-1_EC-1
model=EC-1
panel=
sound=
texture=EC-1
kb_checklists=
kb_reference=
atc_id=78-1021
atc_airline=JASDF
atc_flight_number=1123
ui_manufacturer=kawasaki
ui_type=EC-1
ui_variation=SQ-402
description=ECM Trainer Kawasaki EC-1
atc_heavy=0
atc_parking_codes=M003,C1
atc_parking_types=MIL_CARGO
 


[General]
atc_type=KAWASAKI
atc_model=C-1
editable=1
performance=Max Speed : 425 kts\nPower Plant : P&W JT8D-9 . 14,500 lb  \nMax Gross Weight : 99,225 lb\n


[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI

[WEIGHT_AND_BALANCE]
max_gross_weight= 99225.000
empty_weight= 53000.000

reference_datum_position=0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=0.000000,0.000000,0.000000,0.000000
//station_load.0=170.000000, 41.000000, -1.500000, 0.000000, ѓpѓCѓЌѓbѓg                         
//station_load.1=170.000000, 41.000000, 1.500000, 0.000000, •›‘ЂЏcЋm                                   

;Moments of Inertia
empty_weight_pitch_MOI=3172439
empty_weight_roll_MOI=2262183
empty_weight_yaw_MOI=3337024
empty_weight_coupled_MOI=0

[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

[GeneralEngineData]
engine_type= 1
Engine.0= 6.000, -16.100, -0.500
Engine.1= 6.000, 16.100, -0.500
fuel_flow_scalar= 1.000
min_throttle_limit=-0.25                      //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature=-30                  //Temperature (deg C) below which contrails may appear

[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 19.600
rated_N2_rpm= 29920.000
static_thrust= 14500.000
afterburner_available= 0
reverser_available= 1.000

[jet_engine]
thrust_scalar=1.0

[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, 26.000, 0.000, -8.200, 1000.000, 0.000, 1.500, 40.000, 0.300, 2.500, 0.600, 9.000, 8.000, 0.000, 200.000, 235.000
point.1= 1.000, -4.000, -4.000, -8.200, 2000.000, 1.000, 2.500, 0.000, 0.300, 2.500, 0.500, 11.000, 9.000, 2.000, 200.000, 235.000
point.2= 1.000, -4.000, 4.000, -8.200, 2000.000, 2.000, 2.500, 0.000, 0.300, 2.500, 0.500, 11.000, 9.000, 3.000, 200.000, 235.000
point.3= 2.000, -70.600, 0.000, 0.500, 700.000, 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, -21.600, 79.500, 0.500, 700.000, 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, -21.600, -79.500, 0.500, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.6= 2.000, 70.000, 0.000, 0.500, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
static_pitch= 0.000
static_cg_height= 8.000
gear_system_type=0

max_number_of_points=21

//static_pitch=0.04       //degrees, pitch when at rest on the ground (+=Up, -=Dn)
//static_cg_height=7.67   //feet, altitude of CG when at rest on the ground
//gear_system_type=1      //Hydraulic

[Views]
eyepoint=43.7, -1.31, 3.7   //(feet) longitudinal, lateral, vertical distance from reference datum
[stall_warning]
type=2


[tailhook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=1.0
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 20.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 5.000, 0.000
flaps-position.4= 10.000, 0.000
flaps-position.5= 15.000, 0.000
flaps-position.6= 25.000, 0.000
flaps-position.7= 30.000, 0.000
flaps-position.8= 40.000, 0.000
[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 3.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.500, 0.000
flaps-position.2= 1.000, 0.000


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

[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1=2,  2.65,   0.00,  -6.00, fx_beaconb ,
light.2=4,  28.0,   0.80,  2.00, fx_vclighth ,


[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

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second

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

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
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

[fuel]
Center1= 0.000, 0.000, 0.000, 2313.000, 0.000
LeftMain= -3.000, -19.000, 0.000, 1500.000, 0.000
RightMain= -3.000, 19.000, 0.000, 1500.000, 0.000
fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area=1137.0                //Square feet
wing_span=94.75                 //Feet
wing_root_chord=18.0                  //Feet
wing_dihedral=6.2                   //Degrees
wing_incidence=1.0                   //Degrees
wing_twist=-0.5                  //Degrees
oswald_efficiency_factor=0.75                  //Measure of lift effeciency of wing
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=25.0                  //Degrees, wing leading edge
wing_pos_apex_lon=8.0                   //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0                   //Feet, vertical distance from reference point, positive going up
htail_area=338.0                 //Square feet
htail_span=41.7                  //Feet
htail_pos_lon=-35.0                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence=0.0                   //Degrees
htail_sweep=30.0                  //Degrees, horizontal tail leading edge
vtail_area=224.0                 //Square feet
vtail_span=20.0                  //Feet, tip to body
vtail_sweep=35.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-35.8                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=5.8                   //Feet, vertical distance from reference point, positive going up
elevator_area=70.5                  //Square feet
aileron_area=26.9                  //Square feet
rudder_area=56.2                  //Square feet
elevator_up_limit=22.5                  //Degrees
elevator_down_limit=19.5                  //Degrees
aileron_up_limit=20.0                  //Degrees
aileron_down_limit=20.0                  //Degrees
rudder_limit=26.0                  //Degrees
elevator_trim_limit=20.0                  //Degrees
spoiler_limit=60.0                  //Degrees
spoilerons_available=1                     //Spoilerons Available?
aileron_to_spoileron_gain=3                   //Aileron to spoileron gain
min_ailerons_for_spoilerons=10                //Degrees
min_flaps_for_spoilerons=0                    //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed=142.0                 //Knots True (KTAS)
full_flaps_stall_speed=113.0                 //Knots True (KTAS)
cruise_speed=260.0                 //Knots True (KTAS)
max_indicated_speed=341.000000
max_mach=0.839990

[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

[brakes]
toe_brakes_scale=0.885037
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=2
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0