[fltsim.0] title=C123 Provider USAAF sim=C123 model= panel= sound= texture= kb_checklists= kb_reference= ui_manufacturer=Fairchild ui_type=C123 ui_variation=USAAF atc_id=US326 prop_anim_ratio=-1.3 atc_airline=Greenland Air atc_flight_number=1123 description=Fairchild C123 Provider USAAF - Span: 32m Length: 24.5m Height: 11m Weight: 60,000 lbs. max. Engines: 2xP&W R-2800s Crew: 3/4 Maximum speed: 240 mph. Cruising speed: 170 mph. Range: 1,825 miles Service Ceiling: 28,000 ft. [General] performance=Fairchild C123 Provider USAAF Autor - Vladimir Zhyhulskiy, Ukraine, http:\\fscargo.narod.ru atc_type=C123 atc_model=C123 editable=0 =============================================================== [WEIGHT_AND_BALANCE] empty_weight_coupled_MOI=0.000 max_gross_weight=33000.000 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=170, 21.8, -1.75, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, 21.8, 1.75, 0.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=5660, -4.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight=27650.000 empty_weight_roll_MOI=84655.000000 empty_weight_pitch_MOI=155879.000000 empty_weight_yaw_MOI=55690.000000 ======================================================= ===================================================================== [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second ===================================================================== ======================================================= [fuel] LeftMain=-3.100,-31.500000,7.700,420.000000,0.000000 LeftAux=-2.100,-18.000000,7.100, 310.500000,0.000000 RightMain=-3.100,31.500000,7.700, 420.000000,0.000000 RightAux=-2.100,18.000000,7.100, 310.500000,0.000000 fuel_type=2.000 number_of_tank_selectors=1 ======================================================= [contact_points] //0 Class //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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal //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) point.0=1, 21.6, 0.0, -5.8, 3200, 0, 1.7, 25.0, 0.9, 1.8 0.70, 3, 3, 0, 160, 230 point.1=1, -3.8, -13.6, -5.8, 2200, 1, 1.7, 0, 0.8, 1.5, 0.70, 8, 7, 2, 160, 230 point.2=1, -3.8, 13.6, -5.8, 2200, 2, 1.7, 0, 0.8, 1.5, 0.70, 8, 7, 3, 160, 230 point.3=2, -1.11, -46.5, 6.3, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.4=2, -1.11, 46.5, 6.3, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.5=2, -44, 0, 6.3, 2400, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.6=2, 31.4, 0, .8, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 4 max_number_of_points=21 static_pitch=0.0 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=5.0 //altitude of CG when at rest on the ground ============================================================== [GeneralEngineData] engine_type=5 Engine.0=0.0, -12.5, 0.000 Engine.1=0.0, 12.5, 0.000 fuel_flow_scalar=1.000 //Scalar for fuel flow efficiency [TurbineEngineData] fuel_flow_gain=0.011 //Gain on fuel flow //try .014 instead of .011 inlet_area=1.000 //Square Feet, engine nacelle inlet area rated_N2_rpm=42920.000 //RPM, second stage compressor rated value static_thrust=158.000 //Lbs, max rated static thrust at Sea Level afterburner_available=0 reverser_available=1 [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 propeller_diameter=11.300 propeller_blades=3 propeller_moi=55.000 beta_max=38.200 beta_min=11.800 min_gov_rpm=27520.000 prop_tc=0.011 gear_reduction_ratio=22.787 fixed_pitch_beta=0.000 low_speed_theory_limit=80.000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=700.000 beta_feather=83.200 power_absorbed_cf=0.900 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=8.300 minimum_reverse_beta=-13.50 [turboprop_engine] power_scalar=1.0 //Scalar on Turboprop power maximum_torque=4860.000 //max take-off rating is 4860 ft-lb at 1210 RPM ================================================================== [Reference Speeds] flaps_up_stall_speed=103.000 //at 38,000lbs full_flaps_stall_speed=60.000 //at 27,000lbs cruise_speed=223 //at 10,000' [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=150.000, 250.000 aileron=150.000, 250.000 rudder=150.000, 250.000 [Views] eyepoint=20.650, -1.550, 1.500 //(feet)22.250 - 3.8 longitudinal, lateral, vertical distance from reference datum [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1200.000 autothrottle_available=1 pitch_takeoff_ga=8.000 autothrottle_max_rpm=20000.000000 use_no_default_bank=1 use_no_default_pitch=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 [direction_indicators] direction_indicator.0=3,0 ================================================= flaps.0] type=2 // 1 - trail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=22 // seconds flaps-position.0=0 // degrees flaps-position.1=5 // degrees flaps-position.2=15 // degrees flaps-position.3=20 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=0.7 drag_scalar=0.5 pitch_scalar=0.6 system_type=1 //Hydraulic [flaps.1] type=1 // 1 - trail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=11 // seconds flaps-position.0=0 // degrees flaps-position.1=5 // degrees flaps-position.2=15 // degrees flaps-position.3=20 // degrees damaging-speed=200 // KIAS blowout-speed=250 // KIAS lift_scalar=0.3 drag_scalar=0.5 pitch_scalar=0.4 system_type=1 //Hydraulic ================================================= [flight_tuning] cruise_lift_scalar=1.0 //the angle of attack (and thus pitch) for a cruise condition parasite_drag_scalar=1.00 //air flow interference and skin friction induced_drag_scalar=1.0 //from production of lift elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.5 pitch_stability=1.000 roll_stability=1.000 yaw_stability=0.8 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 ====================================================== [EFFECTS] dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 water=fx_spray =========================================================== [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 4.6, -54.3, 9.7, fx_navred , light.1=3, 4.6, 54.3, 9.7, fx_navgre , light.2=2, 4.6, 54.3, 9.7, fx_strobe , light.3=2, 4.6, -54.3, 9.7, fx_strobe , \\light.4=1, -39.4, 0.0, 30.2, fx_beacon , light.5=1, -5.3, 0.0, -2.9, fx_beacon , light.8=4, 20.27, 2.00, 1.30, fx_vclight light.9=4, -4.27, 0.00,0.50, fx_vclight light.10=4, 25.27, 0.00, 8.30, fx_vclight light.11=4, 26.27, 0.00, 7.50, fx_vclight light.13=1, -39.9, 0.1, 28.9, fx_beacon , ======================================================================= [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 [forcefeedback] stick_shaker_magnitude=4000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=2000 ; 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=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 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 [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 [pitot_static] vertical_speed_time_constant=9 //Increasing this value will cause a more instantaneous reaction in the VSI ================================================================================== [airplane_geometry] wing_area=860.000000 wing_span=93.000000 wing_root_chord=12.583333 wing_dihedral=4.998779 wing_incidence=2.999268 wing_twist=-2.493896 oswald_efficiency_factor=0.427682 wing_winglets_flag=1 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=217.000000 htail_span=31.166667 htail_pos_lon=-43.250000 htail_pos_vert=0.000000 htail_incidence=0.999756 htail_sweep=0.000000 vtail_area=170.000000 vtail_span=14.866069 vtail_sweep=0.000000 vtail_pos_lon=-43.666667 vtail_pos_vert=22.000000 elevator_area=60.985000 aileron_area=23.220000 rudder_area=50.275000 elevator_up_limit=9.740283 elevator_down_limit=8.623015 aileron_up_limit=10.314386 aileron_down_limit=10.314386 rudder_limit=11.493533 elevator_trim_limit=8.594367 spoiler_limit=34.371165 spoilerons_available=1 aileron_to_spoileron_gain=1.000000 min_ailerons_for_spoilerons=5.729578 min_flaps_for_spoilerons=0.000000
