[fltsim.0] title=CC-130H_Canadian Forces - FS2K sim=cc130_2k model= panel= sound= texture= checklists= kb_checklists=c-130h_check kb_reference=c-130h_ref ui_manufacturer=Lockheed ui_type=Hercules ui_variation=Camo Green visual_damage=1 description=Lockheed\/Martin C-130E Hercules -DND CAF 130315.\nCirca. 1989 - CFB Trenton\nSee included Pilots Manual and text files for further INFO and how to handle and operate. Original Design by Barry Blaisdell, Flight Dynamics by Jens Borgstroem, CF Livery Repaint by Larry Smith - this CFG updated by Larry Smith. Premier Aircraft Design atc_heavy=0 atc_id=315 atc_enable=1 atc_airline=Canfor atc_flight_number=315 [General] performance=Lgth:99 ft \/Wing Span:132 ft \/ Ht:36ft\nRange: 4,000 nm \/ Serv. Ceilg: 35,000 ft\nWeight: 155,000 lbs. MTOW\nPower: 4 Allison T56-A-15 Turbo Shafts\nMax Cruise: .55 Mach\/Stall Speed: 120\/90\nRange: 2700nm with full load\\ atc_type=LOCKHEED atc_model=C130 [WEIGHT_AND_BALANCE] 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=0.000000,0.000000,0.000000,0.000000 empty_weight=84060.000 empty_weight_roll_MOI=1256375.000 empty_weight_pitch_MOI=1701571.000 empty_weight_yaw_MOI=2154912.000 empty_weight_coupled_MOI=1300.000 max_gross_weight=148513.998 CG_forward_limit=0.000 CG_aft_limit=1.000 [GeneralEngineData] engine_type=1 Engine.0=-5.000, -23.000, 2.750 Engine.1=-5.000, -11.500, 2.750 Engine.2=-5.000, 11.500, 2.750 Engine.3=-5.000, 23.000, 2.750 fuel_flow_scalar=1.000 [TurbineEngineData] fuel_flow_gain=0.001 inlet_area=13.349 rated_N2_rpm=29920.000 static_thrust=11124.400 afterburner_available=0 reverser_available=1 [contact_points] point.0=1.000, 30.333, 0.000, -4.750, 1574.803, 0.000, 1.530, 51.840, 0.389, 2.500, 0.568, 15.000, 15.000, 0.000, 0.000, 0.000 point.1=1.000, -9.500, -6.167, -4.750, 1574.803, 1.000, 1.530, 0.000, 0.389, 2.500, 0.568, 17.000, 17.000, 2.000, 0.000, 0.000 point.2=1.000, -9.500, 6.167, -4.750, 1574.803, 2.000, 1.530, 0.000, 0.389, 2.500, 0.568, 17.000, 17.000, 3.000, 0.000, 0.000 point.3=2.000, -6.583, -66.000, 9.250, 1574.803, 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, -6.583, 66.000, 9.250, 1574.803, 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, -30.000, 0.000, -0.417, 1574.803, 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, 30.333, 0.000, -0.417, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=0.000 static_cg_height=5.168 [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 [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [Radios] Audio.1=1 Com.1=1,1 Com.2=1,1 Nav.1=1,1,1 Nav.2=1,1 adf.1=1,1 Transponder.1=1 Marker.1=1 Dme.1=1 [Views] eyepoint=31.796, -1.666, 6.254 [LIGHTS] [keyboard_response] elevator=150.000, 250.000 aileron=150.000, 250.000 rudder=150.000, 250.000 [direction_indicators] direction_indicator.0=3,0 [fuel] LeftMain=0.000, -41.667, 0.000, 2500.000, 0.000 LeftAux=0.000, -12.500, 0.000, 2310.000, 0.000 RightMain=0.000, 41.667, 0.000, 2500.000, 0.000 RightAux=0.000, 12.500, 0.000, 2310.000, 0.000 fuel_type=2.000 number_of_tank_selectors=1 [SMOKESYSTEM] smoke.0=5.00, 5.00, 38.00, fx_smoke_rx smoke.1=5.00, 5.00, 18.00, fx_smoke_rx smoke.2=5.00, 5.00, -18.00, fx_smoke_rx smoke.3=5.00, 5.00, -38.00, fx_smoke_rx [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [airplane_geometry] wing_area=1744.000 wing_span=132.667 wing_root_chord=13.167 wing_dihedral=1.500 wing_incidence=0.000 wing_twist=-0.500 oswald_efficiency_factor=1.027 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=430.000 htail_span=52.667 htail_pos_lon=-49.250 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=0.000 vtail_area=215.000 vtail_span=16.718 vtail_sweep=0.000 vtail_pos_lon=-44.250 vtail_pos_vert=5.833 elevator_area=107.500 aileron_area=62.640 rudder_area=36.550 elevator_up_limit=27.502 elevator_down_limit=20.626 aileron_up_limit=19.481 aileron_down_limit=14.897 rudder_limit=23.491 elevator_trim_limit=19.481 spoiler_limit=59.989 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=120.000 full_flaps_stall_speed=96.000 cruise_speed=263.685 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=2500.000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000 pitch_takeoff_ga=8.000 use_no_default_pitch=1use_no_default_bank=1 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=2.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [forcefeedback] 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=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 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 [Flaps.0] type=1 span-outboard=0.500 extending-time=13.000 system_type=0 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=1.000 flaps-position.0=0.000, 0.000 flaps-position.1=3.999, 0.000 flaps-position.2=7.998, 0.000 flaps-position.3=11.998, 0.000 flaps-position.4=15.997, 0.000 flaps-position.5=19.996, 0.000 flaps-position.6=23.995, 0.000 flaps-position.7=27.995, 0.000 flaps-position.8=31.994, 0.000 flaps-position.9=35.993, 0.000
