[fltsim.0]
title=Lockheed C-130
sim=c130
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=995
atc_airline=FACH
atc_flight_number=179
atc_parking_types=GATE,RAMP
ui_manufacturer=Lockheed
ui_type=C-130
ui_variation=FACH
description=Lockheed C-130H version civil, Paint by Hugo espinosa
atc_heavy=0
[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
