[fltsim.0]
title=Lockheed C-130
sim=c130
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=N700MS
atc_airline=USAF
atc_flight_number=1123
atc_parking_types=GATE,RAMP
ui_manufacturer=Lockheed
ui_type=C-130
ui_variation=USAF
description=
atc_heavy=0


[General]
atc_type=LOCKHEED
atc_model=C130
editable=1
performance=

[WEIGHT_AND_BALANCE]
max_gross_weight = 155000.000
empty_weight = 83000.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, 0.000
max_number_of_stations = 50

station_load.0 = 0.000, 0.000, 0.000, 0.000
station_load.1 = "170,  -9.8,  1.75, 0.0, Front Passenger"        //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "5660, -27.0,  0.0, 0.0, Payload"                //Payload  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI   = 1200000.000
empty_weight_roll_MOI    = 1800000.000
empty_weight_yaw_MOI     = 3400000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[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        =2.002
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =0.504
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[GeneralEngineData]
engine_type = 5
Engine.0 = 12.000, -31.500, 6.000
Engine.1 = 12.000, -15.000, 6.000
fuel_flow_scalar        = 1.000
min_throttle_limit = -0.25                      //Minimum percent throttle.  Generally negative for turbine reverser
Engine.2= 12.000, 15.000, 6.000
Engine.3= 12.000, 31.500, 6.000

[propeller]
thrust_scalar           =1.412
propeller_type          = 0
propeller_diameter      = 13.500
propeller_blades        = 4
propeller_moi           = 86.000
beta_max                = 45.000
beta_min                = 12.000
min_gov_rpm             = 5000.000
prop_tc                 = 0.004
gear_reduction_ratio    = 17.000
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            = 80.000
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              = 2.000
rated_N2_rpm            = 29920.000
static_thrust           = 400.000
afterburner_available= 0

[turboprop_engine]
power_scalar            =1.000
maximum_torque          = 9000.000
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, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2 , 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, 30.000, 0.000, -9.600, 3000.000, 0.000, 1.500, 40.000, 0.300, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000
point.1 = 1.000, -3.000, -7.000, -9.500, 5000.000, 1.000, 2.200, 0.000, 0.300, 2.500, 0.800, 4.000, 4.000, 2.000, 0.000, 0.000
point.2 = 1.000, -3.000, 7.000, -9.500, 5000.000, 2.000, 2.200, 0.000, 0.300, 2.500, 0.800, 4.000, 4.000, 3.000, 0.000, 0.000
point.3 = 2.000, -2.970, -65.380, 7.560, 1200.000, 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, -2.970, 65.380, 7.560, 1200.000, 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, -54.750, 0.000, 6.450, 1200.000, 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, 41.270, 0.000, -4.500, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 
 
max_number_of_points = 21


static_pitch = 0.000
static_cg_height = 9.600
gear_system_type=1              //Hydraulic

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    = 15.0     //Flap angle that activates warning at idle
flap_limit_power   = 30.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 1.06  //Brake scalar

[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[Views]
eyepoint= 32.30, -1.98, 3.1     //(feet) longitudinal, lateral, vertical distance from reference datum


[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,0

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

[fuel]
LeftMain  = 0.000, -10.000, 6.000, 4500.000, 0.000
RightMain = 0.000, 10.000, 6.000, 4500.000, 0.000
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=1

[airplane_geometry]
wing_area               = 1800.000
wing_span               = 132.000
wing_root_chord         = 16.000
wing_dihedral           = 3.000
wing_incidence          = 1.500
wing_twist              = -1.000
oswald_efficiency_factor= 0.800
wing_winglets_flag      = 0
wing_sweep              = 3.000
wing_pos_apex_lon       = 1.000
wing_pos_apex_vert      = 6.000
htail_area              = 399.000
htail_span              = 34.000
htail_pos_lon           = -50.000
htail_pos_vert          = 3.000
htail_incidence         = 0.000
htail_sweep             = 10.000
vtail_area              = 286.000
vtail_span              = 22.000
vtail_sweep             = 30.000
vtail_pos_lon           = -50.000
vtail_pos_vert          = 7.000
elevator_area           = 150.000
aileron_area            = 45.000
rudder_area             = 66.000
elevator_up_limit       = 18.000
elevator_down_limit     = 15.000
aileron_up_limit        = 18.000
aileron_down_limit      = 18.000
rudder_limit            = 30.000
elevator_trim_limit     = 15.000
spoiler_limit           = 0.000
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    = 100.000
full_flaps_stall_speed  = 75.000
cruise_speed            = 308.000
max_mach                = 0.60
max_indicated_speed     = 265                   //Red line (KIAS)

[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= 150.0, 250.0
aileron= 150.0, 250.0
rudder= 150.0, 250.0

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[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, -1.52, -65.60,  7.57, fx_navredm ,
light.1 = 3, -1.52,  65.60,  7.57, fx_navgrem ,
light.2 = 3, -55.19,   0.00,  6.87, fx_navwhih ,
light.3 = 3, -1.52, -65.40,  7.57, fx_strobeh ,
light.4 = 3, -1.52,  65.40,  7.57, fx_strobeh ,
light.5 = 2, -45.90,   0.00, 28.75, fx_beaconh ,
light.6 = 1,  22.19,   0.00, -7.27, fx_beaconh ,
light.7 = 4,  31.15,   0.00,  5.24, fx_vclighth ,

[stall_warning]
type=2
[direction_indicators]
direction_indicator.0=3,0

[folding_wings]
wing_fold_system_type=4
fold_rates=0.5, 0.5

[tailhook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=1.0

[Flaps.0]
type= 1
span-outboard= 0.700
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 0.400
flaps-position.0= 0.000, 0.000
flaps-position.1= 8.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 40.000, 0.000