[fltsim.0] title=C130 Hercules FAB (camouflage) sim=C130zh model= panel= sound= texture=2 kb_checklists= kb_reference= ui_manufacturer=Lockheed ui_type=C130 atc_id=2459 prop_anim_ratio=-1.4 atc_airline=59 atc_flight_number=59 ui_variation=FAB-Camuflado description=C130 Hercules FAB V2 - Projeto FAB Veteranos - Cristiano Magnani [fltsim.1] title=FAB - Cinza sim=C130zh model= panel= sound= texture=3 kb_checklists= kb_reference= ui_manufacturer=Lockheed ui_type=C130 atc_id=2474 prop_anim_ratio=-1.4 atc_airline=74 atc_flight_number=74 ui_variation=FAB Primeira Cor GTT description=C130 Hercules FAB V2 - Projeto FAB Veteranos - Cristiano Magnani [fltsim.2] title=C130 Hercules FAB cinza 40 anos sim=C130zh model= panel= sound= texture=4 kb_checklists= kb_reference= ui_manufacturer=Lockheed ui_type=C130 atc_id=2473 prop_anim_ratio=-1.4 atc_airline=73 atc_flight_number=73 ui_variation=FAB-C130 40 anos description=C130 Hercules FAB V2 - Projeto FAB Veteranos - Cristiano Magnani [fltsim.3] title=C130 Hercules FAB antartida sim=C130zh model= panel= sound= texture=5 kb_checklists= kb_reference= ui_manufacturer=Lockheed ui_type=C130 atc_id=2466 prop_anim_ratio=-1.4 atc_airline=66 atc_flight_number=66 ui_variation=FAB Antartida description=C130 Hercules FAB V2 - Projeto FAB Veteranos - Cristiano Magnani [fltsim.4] title=C130 Hercules FAB cinza sim=C130zh model= panel= sound= texture=6 kb_checklists= kb_reference= ui_manufacturer=Lockheed ui_type=C130 atc_id=2477 prop_anim_ratio=-1.4 atc_airline=77 atc_flight_number=77 ui_variation=FAB-Cinza description=C130 Hercules FAB V2 - Projeto FAB Veteranos - Cristiano Magnani [fltsim.5] title=C130 Hercules FAB SAR sim=C130zh model= panel= sound= texture=7 kb_checklists= kb_reference= ui_manufacturer=Lockheed ui_type=C130 atc_id=2433 prop_anim_ratio=-1.4 atc_airline=33 atc_flight_number=33 ui_variation=FAB SAR description=C130 Hercules FAB V2 - Projeto FAB Veteranos - Cristiano Magnani //=========================================================== [WEIGHT_AND_BALANCE] empty_weight=35542 // 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) station_load.0=379,31,0,0 // Weight Pilots (lbs) station_load.1=190,27,0,0 // Weight stewards in front (lbs) station_load.2=190,-19,0,0 // Weight stewards in rear (lbs) station_load.3=331,20.5,0,0 // Weight cargo 1 (lbs) station_load.4=776,-23,0,0 // Weight cargo 2 (lbs) station_load.5=190,16.1,0,0 // Weight passengers row 1 (lbs) station_load.6=758,13.6,0,0 station_load.7=569,11,0,0 station_load.8=569,8.4,0,0 station_load.9=569,5.8,0,0 station_load.10=758,3.2,0,0 station_load.11=379,0.6,0,0 station_load.12=569,-1.9,0,0 station_load.13=569,-4.5,0,0 station_load.14=569,-7.1,0,0 station_load.15=569,-9.7,0,0 station_load.16=379,-12.3,0,0 station_load.17=758,-14.9,0,0 station_load.18=190,-17.4,0,0 //The Zero Fuel Weight of this aircraft is 17600 kg equal 38801 pounds // Moment of Inertia empty_weight_roll_MOI=287051 empty_weight_pitch_MOI=233733 empty_weight_yaw_MOI=283747 empty_weight_coupled_MOI=0 max_gross_weight=45900 CG_forward_limit=0.000 CG_aft_limit=1.000 [Reference Speeds] flaps_up_stall_speed=78.000000 full_flaps_stall_speed=68.000000 cruise_speed=360.000 max_indicated_speed=320.000000 max_mach=0.556982 [pitot_static] vertical_speed_time_constant=2.0 // Increasing this value will cause a faster reaction in the VSI /=========================================================== [flight_tuning] cruise_lift_scalar=1.000 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 /=========================================================== [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=-0.300000 /=========================================================== [TurbineEngineData] fuel_flow_gain=0.005 inlet_area=1.100 rated_N2_rpm=29920.000 static_thrust=400.000 afterburner_available=0 [turboprop_engine] power_scalar=1.0 maximum_torque=11124.000 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=6 propeller_moi=80.000 beta_max=45.0 beta_min=11.500 min_gov_rpm=24994.000 prop_tc=0.002 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=-20.000 /=========================================================== [fuel] // Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=-6.560000,-14.230000,4.060000,1078.000000,3.000000 RightMain=-6.560000,14.230000,4.060000,1078.000000,3.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 /=========================================================== [airplane_geometry] wing_area=753.000 wing_span=95.120 wing_root_chord=11.200 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=59.400 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 /=========================================================== [Views] eyepoint=23.370 , -1.520, 1.650 // (feet) longitudinal, lateral, vertical distance from reference datum /=========================================================== [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, -4.6, fx_beaconb light.3=2, -1.8, -68.1, 9.9, fx_strobeh light.4=2, -1.8, 68.1, 9.9, fx_strobeh light.5=4, 29.5, 0.00, 7.1, fx_vclight light.6=4, 23.5, 0.00, 3.8, fx_vclight light.7 = 3, -59.00, 0.00, 35.02, fx_navwhih , /=========================================================== /=========================================================== /=========================================================== [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, 20.440, 0.000, -7.400, 1800.0, 0.000, 1.000, 40.000, 0.300, 1.500, 0.600, 5.500, 4.500, 0, 270, 390 point.1=1, -6.100, -17.600, -7.400, 2400.0, 1.000, 1.410, 0.000, 0.300, 1.500, 0.600, 6.000, 5.000, 2, 270, 390 point.2=1, -6.100, 17.600, -7.400, 2400.0, 2.000, 1.410, 0.000, 0.300, 1.500, 0.600, 6.500, 5.500, 3, 270, 390 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=0.500000 static_cg_height=7.200 gear_system_type=0 /=========================================================== /=========================================================== /=========================================================== [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=5.000,0.000 flaps-position.2=10.000,0.000 flaps-position.3=15.000,0.000 flaps-position.4=20.000,0.000 flaps-position.5=25.000,0.000 flaps-position.6=35.000,0.000 /=========================================================== [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=500 use_no_default_pitch=0 // 0 = Default to current pitch mode, 1 = No default pitch mode. use_no_default_bank=0 // 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=90.000 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 /=========================================================== [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=1.0000 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 [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=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 //=========================================================== [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 //===========================================================