[fltsim.0] title=C-130H Hercules IRIAF sim=c130h model= panel= sound= texture=IRIAF kb_checklists=C130HCHECK kb_reference=C130HREF description=The C-130H\nModel: Original model Simshed . IRIAF repaint by Arman Riazat ui_manufacturer=Lockheed Martin ui_type=C-130H Hercules ui_variation=IRIAF atc_heavy=15 atc_id=67-0779 atc_airline=Air Force atc_flight_number=538 [General] atc_type=C130 C3 editable=0 Category=airplane [WEIGHT_AND_BALANCE] empty_weight=59320 // Empty weight of aircraft DOW (lbs) reference_datum_position=0,0,0 // (feet) distance from FS Reference: (1/4 chord, centerline, waterline) empty_weight_CG_position=0,0,0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 // Payload weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //The Zero Fuel Weight of this aircraft is 17600 kg equal 38801 pounds // Moment 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 max_gross_weight=125000.500000 [Reference Speeds] flaps_up_stall_speed=98.000000 full_flaps_stall_speed=78.000000 cruise_speed=290.000 max_indicated_speed=330.000000 max_mach=0.656982 [pitot_static] vertical_speed_time_constant=2.0 // Increasing this value will cause a faster reaction in the VSI pitot_heat=1.000000 [flight_tuning] cruise_lift_scalar=0.700 parasite_drag_scalar=0.600 induced_drag_scalar=0.800 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.400 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 Cargo Drop_aircraft [GeneralEngineData] engine_type=5 Engine.0=0.0, -20.5, 0.000 Engine.1=0.0, -12.5, 0.000 Engine.2=0.0, 12.5, 0.000 Engine.3=0.0, 20.5, 0.000 fuel_flow_scalar=0.75 min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.01 inlet_area=1.100 rated_N2_rpm=32000.000 static_thrust=500.000 afterburner_available=0 [turboprop_engine] power_scalar =1.000 maximum_torque = 16600.000 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 [propeller] thrust_scalar=1.25 propeller_type=0 propeller_diameter=13.280 propeller_blades=4 propeller_moi=80.000 beta_max=45.0 beta_min=11.500 min_gov_rpm=32994.000 prop_tc=0.002 // original value .002 gear_reduction_ratio=24.686400 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=350.000 beta_feather=79.300 power_absorbed_cf=0.900 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=0.000 minimum_reverse_beta=-25.000 [fuel] // Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=-3.560000,-14.230000,4.060000,3041.000000,3.000000 RightMain=-3.560000,14.230000,4.060000,3041.000000,3.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=793.000 wing_span=95.120 wing_root_chord=15.200 wing_dihedral=2.500 wing_incidence=2.500 wing_twist=-0.967 oswald_efficiency_factor=0.750 wing_winglets_flag=0 wing_sweep=6.000 wing_pos_apex_lon=1.000 wing_pos_apex_vert=5.100 htail_area=149.000 htail_span=32.520 htail_pos_lon=-37.600 htail_pos_vert=4.100 htail_incidence=0.000 htail_sweep=10.000 vtail_area=186.000 vtail_span=14.103 vtail_sweep=25.000 vtail_pos_lon=-33.030 vtail_pos_vert=5.100 elevator_area=35.600 aileron_area=79.400 rudder_area=56.000 elevator_up_limit=30.000 elevator_down_limit=20.000 aileron_up_limit=25.000 aileron_down_limit=25.000 rudder_limit=30.00 elevator_trim_limit=15.000 spoiler_limit=90.000 spoilerons_available=1 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 auto_spoiler_available=0 spoiler_extension_time=10.000000 positive_g_limit_flaps_up=3.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-1.299145 negative_g_limit_flaps_down=-1.099359 Cargo Drop_aircraft [contact_points] //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) // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0=1, 36.52, 0.0, -5.52, 1574.8, 0.0, 1.24, 70.0, 0.25, 2.5, 0.518, 8.0, 8.0, 0, 0, 0 point.1=1, -8.33, -16.00, -5.52, 2500.8, 1.0, 1.435, 0.0, 0.41, 2.5, 0.634, 12.0, 12.0, 2, 0, 0 point.2=1, -8.33, 16.00, -5.52, 2500.8, 2.0, 1.435, 0.0, 0.41, 2.5, 0.634, 11.0, 11.0, 3, 0, 0 point.3=2, 33.300, 0.000, -1.220, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0, 0 point.4=2, -7.110, -48.270, 6.100, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0, 0 point.5=2, -7.110, 48.270, 6.100, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0, 0 point.6=2, -49.600, 0.000, 0.450, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9, 0, 0 point.7=2, -2.030, -48.270, 6.100, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0, 0 point.8=2, -2.030, 48.270, 6.100, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0, 0 point.9=2, -42.170, -15.240, 5.800, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0, 0 point.10=2, -42.170, 15.240, 5.800, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0, 0 point.11=2, 9.150, -12.700, 2.450, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0, 0 point.12=2, 9.150, 12.700, 2.540, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0, 0 point.13=2, -28.250, 0.000, -4.060, 400.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9, 0, 0 max_number_of_points=14 static_pitch=0.000000 static_cg_height=5.0 gear_system_type=1 [Views] eyepoint=37.00, -1.6, 6.8 // VC view //eyepoint=30.50, -3.6, 9.5 // astrodome view //eyepoint=18.00, -4.8, 3.0 // viewpoint in front of cargo bay //eyepoint=-18.00, 0.0, 3.0 // viewpoint in rear of cargo bay [LIGHTS] // type, longitudinal, lateral, vertical distance (feet) from reference datum, filename // Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.1=1, -41.0, -0.300, 13.5, fx_beaconh light.2=1, -20.3, -0.000, -4.0, fx_beaconh light.3=2, -1.8, -66.10, 11.3, fx_strobeh light.4=2, -1.8, 66.10, 11.3, fx_strobeh light.5=4, 35.44, 2.8, 7.0, fx_vclight light.6=4, 18.44, 0.0, 6.8, fx_navwhih light.7=3, -54.0, 0.00, 32.02, fx_beaconh // tailfin light light.8=2, -1.0, 65.80, 11.3, fx_navred light.9=2, -1.0, -65.80, 11.3, fx_navgre light.10=4, 0.44, 0.0, 6.8, fx_navwhih light.11=4, -12.44, 0.0, 6.8, fx_navwhih light.12=4, -22.44, 0.0, 6.8, fx_navwhih light.13=4, 39.44, -1.6, 5.0, fx_vclight light.14=4, 37.44, 1.6, 5.0, fx_vclight light.15=1, -41.0, -0.300, 13.5, fx_strobeh light.16=1, -20.3, -0.000, -3.9, fx_beaconh light.17=2, -64.0, -1.0, 9.0, fx_navwhi light.18=2, -64.0, 1.0, 9.0, fx_navwhi light.19=4, 39.44, 0.0, 6.0, fx_vclightwhi.fx [Flaps.0] type=1 span-outboard=0.500000 extending-time=10.000000 system_type=0 flaps-position.0=0.000,0.000 flaps-position.1=10.000,0.000 flaps-position.2=15.000,0.000 flaps-position.3=20.000,0.000 flaps-position.4=25.000,0.000 flaps-position.5=30.000,0.000 flaps-position.6=35.000,0.000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1500 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. autothrottle_available=1 autothrottle_arming_required=-256 autothrottle_takeoff_ga=-256 autothrottle_max_rpm=190.000000 pitch_takeoff_ga=8.000 autoland_available=1 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 default_pitch_mode=0 default_bank_mode=0 [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 [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 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [forcefeedback] stick_shaker_magnitude=8000 ; 0 - 10000 stick_shaker_direction=18000 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=5700 ; 0 - 10000 gear_bump_left_direction=355000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=5700 ; 0 - 10000 gear_bump_right_direction=79000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=720 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.035 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 [brakes] toe_brakes_scale=0.762963 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=25.783101 flap_limit_idle=15.011494 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 /=========================================================== [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second //=========================================================== [SMOKESYSTEM] smoke.0=80, -10.3,-33.8, fx_MR2_Smoke.fx smoke.1=80, -10.3,-18.3, fx_MR2_Smoke.fx smoke.2=80, -10.3, 18.3, fx_MR2_Smoke.fx smoke.3=80, -10.3, 33.8, fx_MR2_Smoke.fx //=========================================================== [TailHook] tailhook_length=4 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0.9 //=========================================================== [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=2