// © PREMIER AIRCRAFT DESIGN
// Lockheeed C130J-30 FOR FS2004
// FSDS model, panel and XML gauge programming by Jean-Pierre Brisard
// Flight model by Bob May
// Paint by Bob May except where otherwise stated.
// November 2009


[fltsim.0]
title=Lockheed C130J-30 -RAF
sim=c130
model=RAF
panel=C130j_13
sound=C130
texture=RAF
kb_checklists=C130J_check
kb_reference=C130J_ref
atc_id=ZH888
atc_airline=Air Force
atc_flight_number=ZH888
atc_heavy=1
atc_parking_types=CARGO
ui_manufacturer=Lockheed
ui_type=Hercules C Mk 4
ui_variation=Royal Air Force 
description=ADD NEW DESCRIPTION HERE
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0


[fltsim.1]
title=Lockheed C130J-30 USAF
sim=c130
model=
panel=C130j_13
sound=C130
texture=USAF
kb_checklists=C130J_Check
kb_reference=C130J_ref
atc_id=8604
atc_airline=Air Force
atc_flight_number=8604
atc_heavy=1
atc_parking_types=CARGO
ui_manufacturer=Lockheed
ui_type=C-130J-30
ui_variation=USAF C130J-30 
description=ADD NEW DESCRIPTION HERE
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0


[fltsim.2]
title=Lockheed C130J-30 USCG
sim=c130
model=
panel=C130j_13
sound=C130
texture=USCG
kb_checklists=C130J_check
kb_reference=C130J_ref
atc_id=CG2005
atc_airline=Coast Guard
atc_flight_number=2005
atc_heavy=1
atc_parking_types=CARGO
ui_manufacturer=Lockheed
ui_type=HC-130J-30
ui_variation=U.S. Coast Guard 
description=ADD NEW DESCRIPTION HERE
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0


[fltsim.3]
//Paint by Markus Hellwig
title=Lockheed C130J-30-Blue Angels
sim=c130
model=
panel=C130j_13
sound=C130
texture=Blue_Angels
kb_checklists=C130J_check
kb_reference=C130J_ref
atc_id=BA1
atc_airline=Marine
atc_flight_number=BA1
atc_heavy=1
atc_parking_types=CARGO
ui_manufacturer=Lockheed
ui_type=C-130J-30
ui_variation=Blue Angels
description=ADD NEW DESCRIPTION HERE
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0




[General]
atc_type=LOCKHEED 
atc_model=C130 
editable=1 
performance=Military transport\nLength:112ft 9in \nWing Span: 132ft 7in \nHt: 38ft 3in\nWeight: 75800lb Empty \nPower: 4 x 4590 shp Allison (Rolls-Royce) T56-A-15 \nMax Cruise: 362 kts TAS\nStall Speed: 120 kts with flaps\nStall Speed: 152 kts clean\nService ceiling: 27,000 ft 
category=airplane

Category = airplane


[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[weight_and_balance]

// ACM V2.5
max_gross_weight =155000.0
empty_weight =75800.00000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, -0.000, -0.000
empty_weight_pitch_MOI =894165.10802
empty_weight_roll_MOI =706277.64706
empty_weight_yaw_MOI =1299060.95373
empty_weight_coupled_MOI =0.00000
CG_forward_limit = 0.000
CG_aft_limit = 1.000
max_number_of_stations =3
station_load.0= 170, -0.000, -1.500, 0.000, Pilot
station_load.1= 170, -0.000, 1.500, 0.000, Co-Pilot
station_load.2= 5010, -0.000, 0.000, 0.000, Load

 



[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 =3,  1.625, -67.36, 1.847, fx_navredh
light.1 =3,  1.625, 67.36, 1.847, fx_navgreh
light.2 =3, -63.200, 0.0,0.800, fx_navwhih
light.3 =2, 0.514, -67.360, 1.8470, fx_strobeh
light.4 =2, 0.514, 67.360, 1.8470, fx_strobeh
light.5 =1, -51.73, 0.000000, 27.96, fx_beaconh
light.6 =1, -11.40, 0.000000, -14.30, fx_beaconb
light.7 =4, 39.50000, 0.000000, -4.40000, fx_vclighth
light.8 =4, 20.00000, 0.000000, -6.40000, fx_vclighth
light.9 =4,-20.00000, 0.000000, -6.40000, fx_vclighth 

[Views]
eyepoint=37.72,-1.9,-3.2   //(feet) longitudinal, lateral, vertical distance from reference datum


[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type =5
fuel_flow_scalar =1.00000
min_throttle_limit =-0.25000
engine.0 =2.000, -32.000, 5.000
engine.1 =2.000, -19.500, 5.000
engine.2 =2.000, 19.500, 5.000
engine.3 =2.000, 32.000, 5.000

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type =2
number_of_tank_selectors =1
electric_pump =1

Center1= 0.000, 0.000, -0.000, 2500.000, 30.000
LeftMain = 0.000, -28.000, 0.000, 1256.000, 10.000
RightMain = 0.000, 28.000, 0.000, 1256.000, 10.000
fuel_dump_rate=0.02000
anemometer_pump=0
manual_pump=0
engine_driven_pump=0
electric_pump=1




[contact_points]
//Classes...What type of point    0=Unused or Ignore
//                                                      1=Wheel
//                                                      2=Scrape point
//                                                      4=Float
//                                                      5=Float Rudder
//0  Class
//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 / Water Rudder Effectiveness  (0=Undamped, 1=Critically Damped) / 1.0 = normal
//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)

static_pitch = 0.000
static_cg_height = 16.200
tailwheel_lock =0
gear_system_type =1
max_number_of_points =10

point.0 = 1, 36.999, 0, -16.325, 9000, 0, 1.5, 90, 0.2, 3.5, 0.9, 4, 4, 0, 400, 400
point.1= 1, -4.280, -7.000, -16.500, 15000, 1, 2.200, 0.000, 0.300, 2.500, 0.900, 4.000, 4.000, 2, 400.0, 400.0
point.2= 1, -4.280, 7.000, -16.500, 15000, 2, 2.200, 0.000, 0.300, 2.500, 0.900, 4.000, 4.000, 3, 400.0, 400.0
point.3= 2, -2.000, -66.000, 1.500, 0, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0
point.4= 2, -2.000, 66.000, 1.500, 0, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0
point.5= 2, -70.000, 0.000, 2.000, 0, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0
point.6= 2, 30.000, 0.000, 0.000, 0, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0
point.7= 2, 0.000, 0.000, -5.000, 0, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0
point.8= 5, 0.600, -0.000, -0.500, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4

[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
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111

[airplane_geometry]

wing_area =1745.00000
wing_span =132.00000
wing_root_chord =13.88068
wing_dihedral =2.00000
wing_incidence =0.00000
wing_twist =0.00000
oswald_efficiency_factor =0.70000
wing_winglets_flag =1
wing_sweep =0.00000
wing_pos_apex_lon =3.30768
wing_pos_apex_vert =0.00000
htail_area =217.76000
htail_span =50.26000
htail_pos_lon =-63.27538
htail_pos_vert =0.00000
htail_incidence =0.00000
htail_sweep =0.00000
vtail_area =129.08000
vtail_span =23.42000
vtail_sweep =0.00000
vtail_pos_lon =-60.98793
vtail_pos_vert =3.30000
elevator_area =120.60000
aileron_area =125.64000
rudder_area =82.16000
elevator_up_limit =25.00000
elevator_down_limit =25.00000
aileron_up_limit =20.00000
aileron_down_limit =20.00000
rudder_limit =30.00000
elevator_trim_limit =20.00000
spoiler_limit =0.00000
aileron_to_spoileron_gain =3.00000
spoiler_handle_available =0
min_ailerons_for_spoilerons =10.00000
min_flaps_for_spoilerons =0.00000
spoilerons_available =1
spoiler_extension_time=0.00000
auto_spoiler_available=1
positive_g_limit_flaps_up=3.70000
negative_g_limit_flaps_up=-2.96000
positive_g_limit_flaps_down=2.59000
negative_g_limit_flaps_down=-2.22000
load_safety_factor=1.00000

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1,1,1
electric_always_available = 0
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 0, 5, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[Reference Speeds]
flaps_up_stall_speed= 150.000 
full_flaps_stall_speed= 120.000 
cruise_speed=292.00000 
max_mach                =0.72000
max_indicated_speed     =360.00000

[flight_tuning]
cruise_lift_scalar=1.00000 
parasite_drag_scalar=1.50000 
induced_drag_scalar=1.00000 
elevator_effectiveness=1.50000 
aileron_effectiveness=1.00000 
rudder_effectiveness=1.00000 
pitch_stability=1.00000 
roll_stability=1.00000 
yaw_stability=1.00000 
elevator_trim_effectiveness=0.90700 
aileron_trim_effectiveness=1.00000 
rudder_trim_effectiveness=1.00000 
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
p_factor_on_yaw=0.00000
torque_on_roll=0.00000
gyro_precession_on_roll=0.00000
gyro_precession_on_yaw=0.00000

[TurbineEngineData]
fuel_flow_gain             =0.01100
inlet_area                 =2.00000
rated_N2_rpm           =20000.00000
static_thrust              =100.00000
afterburner_available=0
reverser_available=0
afterburner_throttle_threshold=0.00200
ThrustSpecificFuelConsumption=0.00200
AfterBurnThrustSpecificFuelConsumption=0.00200

[turboprop_engine]
power_scalar           =3.00000
maximum_torque     =16320.57792

[JET_ENGINE]
thrust_scalar =1.00000  

[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
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=25
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=16
nav_integrator_control=0.17
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control  =18 
gs_integrator_control    =0.33
gs_derivative_control    =0
gs_integrator_boundary   =0.7
gs_derivative_boundary   =0
yaw_damper_gain =1
default_pitch_mode=0
default_bank_mode=0
use_no_default_bank=1
use_no_default_pitch=1

[gear_warning_system]
gear_warning_available =1
pct_throttle_limit =0.10000
flap_limit_idle    =5.00000
flap_limit_power   =25.50000

[brakes]
parking_brake =1
toe_brakes_scale =1.24000
auto_brakes=1
hydraulic_system_scalar=0.00000
differential_braking_scale=0.00000

[hydraulic_system]
normal_pressure =3000.00000
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,1,1   //pumps on Eng1,2,3,4

[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 

[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 

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

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

[exits]
number_of_exits = 3
exit_rate.0 = 0.1                               ;Percent per second
exit_rate.1 = 0.2                               ;Percent per second
exit_rate.2 = 0.2                               ;Percent per second


[stall_warning]
type=2
stick_shaker=1

[folding_wings]
wing_fold_system_type=4
fold_rates=0.5, 0.5

[tailhook]
tailhook_length= 4.000
tailhook_position= 0.000, 0.000, 0.000
cable_force_adjust=1.0

[Flaps.0]
type= 1
system_type=1
span-outboard= 0.500
extending-time= 5.0
damaging-speed=423.0
blowout-speed=470.0
flaps-position.0=0.00,0.000
flaps-position.1=10.000,0.000
flaps-position.2=20.000,0.000
flaps-position.3=34.000,0.000
flaps-position.4=45.000.,0.000
lift_scalar=1.05
drag_scalar=1.1000
pitch_scalar=0.0000


[propeller]
thrust_scalar=1.00000
propeller_type=0
propeller_diameter=13.50000 
propeller_blades=6
propeller_moi=301.33201 
beta_max=65.00000 
beta_min=15.00000 
min_gov_rpm=22500.00000
prop_tc=0.01000 
gear_reduction_ratio=13.54000 
fixed_pitch_beta=0.00000 
low_speed_theory_limit=80.00000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=700.00000 
beta_feather=80.00000 
power_absorbed_cf=0.90000 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=1.00000 
minimum_reverse_beta=-14.00000


[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[deice_system]
structural_deice_type=0