[fltsim.0] title=PAF C-130H sim=AI Lockheed C-130H model= panel= sound= texture= kb_checklists= kb_reference= atc_id= atc_airline=Pakistan Air Force atc_flight_number= atc_heavy=0 ui_manufacturer=Lockheed ui_type=C-130H ui_variation=PAF atc_id_color=0000000000 visual_damage=0 atc_parking_types=Mil_Combat description=AI Lockheed C-130H Hercules by Henry Tomkiewicz.Textures By Muhammad Sarmad Khan. [fltsim.1] title=PAF C-130H-1 sim=AI Lockheed C-130H model=wing_tanks panel= sound= texture=1 kb_checklists= kb_reference= atc_id= atc_airline=Pakistan Air Force atc_flight_number= atc_heavy=0 ui_manufacturer=Lockheed ui_type=C-130H ui_variation=PAF1 atc_id_color=0000000000 visual_damage=0 atc_parking_types=Mil_Combat description=AI Lockheed C-130H Hercules by Henry Tomkiewicz.Textures By Muhammad Sarmad Khan. [General] atc_type=Lockheed atc_model=C130 editable=1 performance=AI Aircraft [WEIGHT_AND_BALANCE] empty_weight=71000 max_gross_weight=155000 reference_datum_position=0.0, 0.0, 0.0 // (feet) empty_weight_CG_position=4.8, 0.0, 0.0 // (feet) max_number_of_stations=50 station_load.0 = "170.0, 31.0, -1.5, 0.0, Pilot" station_load.1 = "170.0, 31.0, 1.5, 0.0, Co-Pilot" station_load.2 = "510.0, 25.0, 0.0, 0.0, Crew" station_load.3 = "7000.0, 5.0, 0.0, 0.0, Payload" ;Moments of Inertia empty_weight_pitch_MOI=1000000 empty_weight_roll_MOI=696271 empty_weight_yaw_MOI=1289428 empty_weight_coupled_MOI=0 [GeneralEngineData] engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0= -5.0, -33.8, 4.0 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1= -5.0, -16.8, 4.0 Engine.2= -5.0, 16.8, 4.0 Engine.3= -5.0, 33.8, 4.0 fuel_flow_scalar=1.00 //Scalar for fuel flow efficiency min_throttle_limit= -0.30 [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter = 13.0 //Propeller Diameter, (feet) propeller_blades = 4 //Number of propeller blades propeller_moi = 100 //Propeller moment of inertia beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min = 12 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm = 25520 //Miminum governed RPM prop_tc = 0.004 //Prop time-constant gear_reduction_ratio = 17.0 //Propeller gear reduction ratio fixed_pitch_beta = 0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit = 80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available = 1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available = 1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather = 700 //Minimum RPM for prop feathering beta_feather = 79.3 //Feathering pitch angle (degrees) power_absorbed_cf = 0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available = 1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta = 1.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta = -14.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain = 0.011 //Gain on fuel flow inlet_area = 1.0 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 6000 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar = 1.0 //Scalar on Turboprop power maximum_torque = 12000 //Maximum torque available (ft-lbs) [SMOKESYSTEM] smoke.0= -5.0, -33.8, 4.0, fx_smoke_r smoke.1= -5.0, -16.8, 4.0, fx_smoke_r smoke.2= -5.0, 16.8, 4.0, fx_smoke_r smoke.3= -5.0, 33.8, 4.0, fx_smoke_r [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=0.7 aileron_effectiveness=1.7 rudder_effectiveness=1.0 pitch_stability=1.9 roll_stability=0.4 yaw_stability=1.0 elevator_trim_effectiveness=1.3 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [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, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 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, 29.80, 0.00, -9.0, 5000, 0, 1.60, 80.0, 0.8, 0.8, 0.5, 11, 11, 0, 0, 0 point.1=1, -4.50, -7.00, -9.3, 5000, 1, 1.60, 0.0, 0.8, 0.8, 0.5, 7, 7, 2, 0, 0 point.2=1, -4.50, 7.00, -9.3, 5000, 2, 1.60, 0.0, 0.8, 0.8, 0.5, 7, 7, 3, 0, 0 static_pitch=-0.1 static_cg_height=8.8 gear_system_type=0 [Views] eyepoint=35.0, -1.20, 5.0 [flaps.0] type=1 span-outboard=0.8 extending-time=10 flaps-position.0=0 flaps-position.1=5 flaps-position.2=15 flaps-position.3=25 flaps-position.4=40 damaging-speed=250 blowout-speed=300 lift_scalar=0.5 drag_scalar=0.5 pitch_scalar=0.0 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [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, 250 aileron=150, 250 rudder=150, 250 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 1.60, -66.30, 7.65, fx_navredm, light.1=3, 1.60, 66.30, 7.65, fx_navgrem, light.2=3, -58.30, 0.00, 6.10, fx_navwhih, light.3=2, 1.60, -66.40, 7.65, fx_strobeh, light.4=2, 1.60, 66.40, 7.65, fx_strobeh, light.5=1, -48.50, 0.00, 29.50, fx_beaconb, light.6=5, 1.90, -22.60, 5.50, fx_landing, light.7=5, 1.90, 22.60, 5.50, fx_landing, light.8=5, 12.90, -7.10, 1.50, fx_landing, light.9=5, 12.90, 7.10, 1.50, fx_landing, light.10=1, 23.50, 0.00, -7.40, fx_beaconb, [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [fuel] LeftMain=0,-16,0,1605,0 LeftAux=0,-20,0,1662,0 RightMain=0,16,0,1605,0 RightAux=0,20,0,1662,0 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=2200 wing_span=125 wing_root_chord=20.0 wing_dihedral=3.0 wing_incidence=3.0 oswald_efficiency_factor=0.7 wing_twist=0.0 wing_winglets_flag=0 wing_sweep=20.0 wing_pos_apex_lon=8.0 wing_pos_apex_vert=0.0 htail_area=338.0 htail_span=52.0 htail_pos_lon=-50.0 htail_pos_vert=0.0 htail_incidence=0.0 htail_sweep=0.0 vtail_area=224.0 vtail_span=20.0 vtail_sweep=20.0 vtail_pos_lon=-40.0 vtail_pos_vert=3.0 elevator_area=80.0 aileron_area=52.28 rudder_area=58.0 elevator_up_limit=27.0 elevator_down_limit=20.0 aileron_up_limit=19.0 aileron_down_limit=14.0 rudder_limit=23.0 elevator_trim_limit=19.0 spoiler_limit=90.0 spoilerons_available=0 aileron_to_spoileron_gain=0.0 min_ailerons_for_spoilerons=0.0 min_flaps_for_spoilerons=0.0 [Reference Speeds] flaps_up_stall_speed=117 full_flaps_stall_speed=96 cruise_speed=340 max_indicated_speed=320 max_mach=0.6 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 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 [brakes] toe_brakes_scale=0.8 parking_brake=1 [gear_warning_system] gear_warning_available=1 [hydraulic_system] electric_pumps=1 engine_map=1,1,1,1 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
