[fltsim.0] title=Lockheed C-130 sim=c130 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=5301 atc_airline=USAF atc_flight_number=1123 atc_parking_types=GATE,RAMP ui_manufacturer=Lockheed ui_type=C-130 ui_variation=USAF description=Lockheed WC-130 of the 403rd Weather Recon. Squadron 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 [SMOKESYSTEM] smoke.0=0.00, -08.00, 31.00, FX_C130_SMOKE.fx smoke.1=0.00, -08.00, 14.00, FX_C130_SMOKE.fx smoke.2=0.00, -08.00, -14.00, FX_C130_SMOKE.fx smoke.3=0.00, -08.00, -31.00, FX_C130_SMOKE.fx [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=10.000, 0.000 flaps-position.3=20.000, 0.000 flaps-position.4=30.000, 0.000 flaps-position.5=40.000, 0.000
