[fltsim.0] title=Lockheed HC-130 sim=c130 model= panel= sound= texture=USCG kb_checklists= kb_reference= atc_id= atc_airline=USCG atc_flight_number=1123 atc_parking_types=GATE,RAMP ui_manufacturer=Coast Guard ui_type=HC-130H ui_variation=HC-130H Hercules description=HC-130 by Mike Stone\Panel by Ken Mitchell\Paint & Panel modifications by Ray Brower atc_heavy=0 [fltsim.1] title=Lockheed HC-130 a sim=c130 model= panel= sound= texture= kb_checklists= kb_reference= atc_id= atc_airline= atc_flight_number=1123 atc_parking_types=GATE,RAMP ui_manufacturer=Coast Guard ui_type=HC-130H aa ui_variation=HC-130H Hercules 2 description=HC-130 by Mike Stone\Panel by Ken Mitchell\Paint & Panel modifications by Ray Brower 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 [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 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1200.000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=1 autothrottle_max_rpm=105.000 pitch_takeoff_ga=8.000 use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode. use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode. [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] direction_indicator.0=1,0