[fltsim.0]
title=C-130 Hercules
sim=FSDS L-100 HERCULES
model=
panel=
sound=
texture=
checklists=
kb_checklists=c-130h_check
kb_reference=c-130h_ref
atc_type=Hercules L100
atc_id_enable=1
atc_id_color=0xffffffff
atc_id=
atc_airline=
atc_flight_number
editable=0
ui_manufacturer=Lockheed/Martin
ui_type=Dragon Air

description=L-100 HERCULES   Press the " \/ " (spoiler) key to open the rear cargo hold doors and ramp.\nModel and FDE by :Adrian Brausch\nRepaint by: Luca De Battista
atc_heavy=1
ui_variation=


[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

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

[electrical]
max_battery_voltage=0

[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

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

[SMOKESYSTEM]
smoke.0=0.00, -10.00, 37.00, fx_smoke_rx.fx
smoke.1=0.00, -10.00, 18.00, fx_smoke_rx.fx
smoke.2=0.00, -10.00, -18.00, fx_smoke_rx.fx
smoke.3=0.00, -10.00, -37.00, fx_smoke_rx.fx


[General]
performance=Powerplant  4x4,050 ehp Allison T56-A-7 turboprop                                       Cruise Speed\t 325 kts\n
                                                               
Maximum Range\t 3,791 km\n                                                                         
Service Ceiling\t 33,000 ft\n                                                                             
Max Takeoff Weight 175,000 lb\n\n\n\n\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=72892.000000
empty_weight_roll_MOI=1955508.000000
empty_weight_pitch_MOI=1801180.000000
empty_weight_yaw_MOI=2243626.000000
empty_weight_coupled_MOI=1300.000000
max_gross_weight=108475.699

[fuel]
Center1=0.000000,0.000000,0.000000,2313.000000,0.000000
LeftMain=0.000000,-19.000000,0.000000,1499.000000,0.000000
RightMain=0.000000,19.000000,0.000000,1499.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=1388.000000
wing_span=99.000000
wing_root_chord=13.166667
wing_dihedral=5.998535
wing_incidence=0.000000
wing_twist=1.697388
oswald_efficiency_factor=0.532780
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=320.000000
htail_span=42.833333
htail_pos_lon=-25.000000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=165.000000
vtail_span=14.645819
vtail_sweep=0.000000
vtail_pos_lon=-40.000000
vtail_pos_vert=12.000000
elevator_area=100.000000
aileron_area=26.800000
rudder_area=56.200000
elevator_up_limit=17.188734
elevator_down_limit=17.188734
aileron_up_limit=20.053523
aileron_down_limit=20.053523
rudder_limit=14.323945
elevator_trim_limit=19.996227
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[contact_points]
point.0=1.000000,29.083333,0.000000,-9.916667,1574.803150,0.000000,1.251998,50.940000,0.595698,2.500000,0.979892,15.000000,15.000000,0.000000,0.000000,0.000000
point.1=1.000000,-9.750000,-7.666667,-9.750000,1574.803150,1.000000,1.251998,0.000000,0.888456,2.500000,0.802368,20.000000,20.000000,2.000000,0.000000,0.000000
point.2=1.000000,-9.750000,7.666667,-9.750000,1574.803150,2.000000,1.251998,0.000000,0.888456,2.500000,0.802368,20.000000,20.000000,3.000000,0.000000,0.000000
point.3=2.000000,7.500000,-36.250000,-3.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,7.500000,36.250000,-3.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-24.750000,0.000000,-7.166667,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,30.250000,0.000000,-7.083333,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.000000
static_cg_height=8.502099

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=6.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=3.999245,0.000000
flaps-position.2=7.998491,0.000000
flaps-position.3=11.997736,0.000000
flaps-position.4=15.996982,0.000000
flaps-position.5=19.996227,0.000000
flaps-position.6=23.995472,0.000000
flaps-position.7=27.994718,0.000000
flaps-position.8=31.993963,0.000000
flaps-position.9=35.993209,0.000000
flaps-position.10=39.992454,0.000000

[GeneralEngineData]
engine_type=1
Engine.0=8.333333,-23.333333,4.166667
Engine.1=8.333333,-15.000000,4.166667
Engine.2=8.333333,15.000000,4.166667
Engine.3=8.333333,23.333333,4.166667
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002000
inlet_area=19.600000
rated_N2_rpm=29920.000000
static_thrust=10500.000000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=75.000000
full_flaps_stall_speed=60.000000
cruise_speed=458.007124

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

[Views]
eyepoint=31.808768,-1.717315,3.588419
[direction_indicators]
direction_indicator.0=3,0