[fltsim.0] title=MAI C130H HAF sim=AI_C130H_DF model= panel= sound= texture=HAF_H atc_airline=HELLENIC AIR FORCE atc_parking_types=MIL_CARGO atc_parking_codes=M003,C130 atc_heavy=0 ui_manufacturer=Lockheed ui_type=Lockheed C-130H Hercules ui_variation=Hellenic Air Force description=Repaint by Kostis Prassas [General] atc_type =LOCKHEED atc_model =C130 editable = 1 performance =* Weight: 86705 lbs Max 175000 lbs * Power: 0 hp MIL 0 hp WEP * 4.0g Corner speed: 232 mph * Max speed @ SL: 379 mph * Max speed: 420 mph @ 15000 ft * Climb rate: 2100 ft/min @ 223 mph Flight Model By: David Friswell Aussim 11/9/03 06:30 PM Flight Model Workbook V2.83.59 [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 175000 empty_weight = 76105 reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -1, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 11 station_load.0 = 0, 41.5, -2, 2 station_load.1 = 0, 41.5, 2, 2 station_load.2 = 0, 40, 0, 2 station_load.3 = 0, 17.2, 0, 0 station_load.4 = 0, -14, 0, 0 station_load.5 = 0, 0, 0, 0 station_load.6 = 0, 0, 0, 0 station_load.7 = 0, 0, 0, 0 station_load.8 = 0, 0, 0, 0 station_load.9 = 0, 0, 0, 0 station_load.10 = 0, 0, 0, 0 empty_weight_pitch_MOI = 935921 empty_weight_roll_MOI = 775397 empty_weight_yaw_MOI = 1555517 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 [GeneralEngineData] engine_type = 5 Engine.0 = 8.333333, -31, 4.5 Engine.1 = 8.333333, -15, 3.2 Engine.2 = 8.333333, 15, 3.2 Engine.3 = 8.333333, 31, 4.5 fuel_flow_scalar = 1 min_throttle_limit=-0.250000 max_contrail_temperature=-27 [propeller] thrust_scalar = 1 propeller_type = 0 propeller_diameter = 15 propeller_blades = 8 propeller_moi = 314.4 beta_max = 65 beta_min = 20 min_gov_rpm = 22440 prop_tc = 0.01 gear_reduction_ratio = 17.4 fixed_pitch_beta = 0 low_speed_theory_limit = 80 prop_sync_available = 1 prop_deice_available = 1 prop_feathering_available = 1 prop_auto_feathering_available = 1 min_rpm_for_feather = 700 beta_feather = 88.5 power_absorbed_cf = 0.9 defeathering_accumulators_available = 1 prop_reverse_available = 1 minimum_on_ground_beta = 1 minimum_reverse_beta = -24 rotation = 1, 1, 1, 1 [TurbineEngineData] fuel_flow_gain = 0.019 inlet_area = 4.67041087791901E-02 rated_N2_rpm = 29920 static_thrust = 158 afterburner_available = 0 reverser_available = 1 [turboprop_engine] power_scalar = 1 maximum_torque = 12759.2424040573 [folding_wings] wing_fold_system_type = 4 fold_rates = 0.12, 0.11 [TailHook] tailhook_length = 4 tailhook_position = -15, 0, -1 cable_force_adjust = 1 [contact_points] max_number_of_points = 17 point.0 = 1, 29.82, 0.00, -9.49, 2000, 0, 2, 55.92, 0.14, 2.5, 0.82, 5, 5, 0, 0, 0 point.1 = 1, -6.52, -6.90, -9.49, 2000, 1, 3.47, 0, 0.62, 2.5, 0.62, 5, 5, 2, 0, 0 point.2 = 1, -6.43, 6.70, -9.49, 2000, 2, 3.47, 0, 0.62, 2.5, 0.62, 5, 5, 3, 0, 0 point.3 = 2, 40.234, 0.000, -3.675, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.4 = 2, -60.806, 0.000, 5.206, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.5 = 2, -26.812, 0.000, -7.044, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.6 = 2, -1.393, -61.556, 6.125, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.7 = 2, -1.393, 61.250, 6.125, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.8 = 2, -49.168, -0.306, 26.950, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.9 = 2, 23.084, 0.000, -7.044, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.10 = 2, -4.150, -5.819, -7.044, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.11 = 2, -4.150, 4.593, -7.044, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.12 = 39.34, 0, -9.49, 1500, 0, 0.5, 22, 0.3, 2.5, 0.7, 4, 4, 0, point.13 = -1.62, -6.9, -9.49, 1500, 0, 0.5, 22, 0.3, 2.5, 0.7, 4, 4, 0, point.14 = -6.52, -6.9, -9.49, 1500, 0, 0.5, 22, 0.3, 2.5, 0.7, 4, 4, 0, point.15 = -1.63, 6.7, -9.49, 1500, 0, 0.5, 22, 0.3, 2.5, 0.7, 4, 4, 0, point.16 = -6.43, 6.7, -9.49, 1500, 0, 0.5, 22, 0.3, 2.5, 0.7, 4, 4, 0, static_pitch = -0.0004 //degrees (pitch when loaded on ground) static_cg_height=9.494 //feet, altitude of CG when at rest on the ground gear_system_type=1 [Views] eyepoint= 41.5, -2.3, 2.1 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 3 flaps-position.0 = 0 flaps-position.1 = 15, 241 flaps-position.2 = 30, 231 flaps-position.3 = 50, 221 flaps-position.4 = 70, 211 flaps-position.5 = 90, 201 damaging-speed = 241 blowout-speed = 261 system_type = 1 lift_scalar = 0 drag_scalar = 0 pitch_scalar = 1 [flaps.1] //Leading Edge Flaps - Lift type = 2 span-outboard = 0.5 extending-time = 3 flaps-position.0 = 0 flaps-position.1 = 10 flaps-position.2 = 20 flaps-position.3 = 30 flaps-position.4 = 40 flaps-position.5 = 30 damaging-speed = 241 blowout-speed = 261 system_type = 1 lift_scalar = 1 drag_scalar = 0 pitch_scalar = 0 [flaps.2] //Leading Edge Flaps - Drag type = 2 span-outboard = 0.5 extending-time = 3 flaps-position.0 = 0 flaps-position.1 = 4 flaps-position.2 = 5 flaps-position.3 = 6 flaps-position.4 = 7 flaps-position.5 = 40 damaging-speed = 241 blowout-speed = 261 system_type = 1 lift_scalar = 0 drag_scalar = 1 pitch_scalar = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 1 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 0, 20, 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 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [LIGHTS] light.0 = 3, -1.3, -61.437, 6.0, fx_navred light.1 = 3, -1.3, 61.437, 6.0, fx_navgre light.2 = 3, -58.0, 0, 5.4, fx_navwhi light.3 = 2, -1.2, -61.437, 5.2, fx_strobe light.4 = 2, -1.2, 61.437, 5.2, fx_strobe light.5 = 2, 0, 0, -8.6, fx_strobe light.6 = 1, -54.6, 0, 23.2, fx_beacon light.7 = 4, 32.7, -1.8, 0.6, fx_vclight [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 contrail=fx_A_I_Contrail [autopilot] autopilot_available = 1 flight_director_available = 0 default_vertical_speed = 1000 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8 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 [fuel] LeftMain = 0, -6, 4.2, 2000, 0 RightMain = 0, 6, 4.2, 2000, 0 LeftAux = 0, -10, 4.2, 1480, 0 RightAux = 0, 10, 4.2, 1480, 0 fuel_type = 2 number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 1745 wing_span = 132.583333333333 wing_root_chord = 13.1615336266499 wing_dihedral = 2.5 wing_incidence = 2 wing_twist = -1 oswald_efficiency_factor = 0.87986901278334 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 3.29038340666248 wing_pos_apex_vert = 0 htail_area = 339.1 htail_span = 50.8 htail_pos_lon = -55.3 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 202.1 vtail_span = 23.2 vtail_sweep = 0 vtail_pos_lon = -54.6 vtail_pos_vert = 0 elevator_area = 145 aileron_area = 125.6 rudder_area = 69.8 elevator_up_limit = 27.501974 elevator_down_limit = 20.626481 aileron_up_limit = 19.480565 aileron_down_limit = 14.896903 rudder_limit = 23.49127 elevator_trim_limit = 19.480565 spoiler_limit = 0 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 100.3 full_flaps_stall_speed = 77.9 cruise_speed =340 max_indicated_speed=396.000000 max_mach=0.591357 [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 [brakes] toe_brakes_scale=0.740889 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.000000 flap_limit_idle=15.000000 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=1250.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
