[fltsim.0] title=Fairchild C119 sim=Fairchild C119 model= panel= sound= texture= checklists= ui_manufacturer=Fairchild ui_type=C119 ui_variation=Film Prop description=Paint by Francis F Silva (Silva Design Group) to complement Daisuke Yamamoto's super model (with powerful engines fitted, 60% higher engine capacity than original) atc_heavy=0 atc_id= atc_airline= atc_flight_number=TP458 [General] atc_type=Fairchild atc_model=C119 editable=0 performance= \n \n \n \n \n \n [WEIGHT_AND_BALANCE] max_gross_weight = 36200 // (pounds) empty_weight = 16145 // (pounds) reference_datum_position = 19.25, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -20.90, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations =50 station_load.0 = "170.0, -5.4, -2.0, 0.0, Pilot" //Weight, Lat, Lon, Vert Position station_load.1 = "170.0, -5.4, 2.0, 0.0, Co-Pilot" //Weight, Lat, Lon, Vert Position station_load.2 = "680.0, -14.2, 0.0, 0.0, Passenger Row 1" //Weight, Lat, Lon, Vert Position station_load.3 = "680.0, -17.4, 0.0, 0.0, Passenger Row 2" //Weight, Lat, Lon, Vert Position station_load.4 = "680.0, -20.7, 0.0, 0.0, Passenger Row 3" //Weight, Lat, Lon, Vert Position station_load.5 = "680.0, -23.9, 0.0, 0.0, Passenger Row 4" //Weight, Lat, Lon, Vert Position station_load.6 = "510.0, -27.2, 0.0, 0.0, Passenger Row 5" //Weight, Lat, Lon, Vert Position station_load.7 = "510.0, -30.4, 0.0, 0.0, Passenger Row 6" //Weight, Lat, Lon, Vert Position station_load.8 = "340.0, -33.7, 0.0, 0.0, Passenger Row 7" //Weight, Lat, Lon, Vert Position station_load.9 = "340.0, -36.9, 0.0, 0.0, Passenger Row 8" //Weight, Lat, Lon, Vert Position station_load.10 = "500.0, -23.8, 0.0, 0.0, Forward Baggage" //Weight, Lat, Lon, Vert Position station_load.11 = "100.0, -45.5, 0.0, 0.0, Rear Cargo" //Weight, Lat, Lon, Vert Position ;Moments of Inertia empty_weight_pitch_MOI = 69699.03 empty_weight_roll_MOI = 61179.10 empty_weight_yaw_MOI = 131797.97 empty_weight_coupled_MOI = 0.0 [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 = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 p_factor_on_yaw = 0.5 torque_on_roll = 1.0 gyro_precession_on_yaw = 1.0 gyro_precession_on_pitch = 1.0 [flaps.0] //Trailing Edge Flaps type = 1 // 1 - tail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 7 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 11 // degrees flaps-position.2 = 23 // degrees flaps-position.3 = 34 // degrees flaps-position.4 = 45.0 // degrees damaging-speed = 140 // KIAS blowout-speed = 175 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [GeneralEngineData] engine_type = 3 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -9.75, -9.1, -1.8 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = -9.75, 9.1, -1.8 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 1.0 //Fuel flow scalar min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser master_ignition_switch = 1 //Master Ignition Switch [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 300.00 //Cubic inches per cylinder compression_ratio= 18.0 //Compression ratio number_of_cylinders=18 //Number of cylinders max_rated_rpm= 5700 //Max rated RPM max_rated_hp= 2200 //Max rated HP fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque= 0.3 //Starter torque factor turbocharged= 1 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp= 47 //Max design manifold pressure, (inHg) min_design_mp= 10 //Min design manifold pressure, (inHg) critical_altitude= 12500 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 12.53 //Propeller Diameter, (feet) propeller_blades= 4 //Number of propeller blades propeller_moi= 40.2 //Propeller moment of inertia beta_max= 30.0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 18.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 1400 //Miminum governed RPM prop_tc= 0.1 //Prop time-constant gear_reduction_ratio= 1.778 //Propeller gear reduction ratio fixed_pitch_beta= 0.0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit= 80.0 //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= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering beta_feather= 89.5 //Feathering pitch angle (degrees) power_absorbed_cf= 0.9 //Coefficient of friction for power absorbed by propeller in feather defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta= 0.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees) feathering_switches = 1 //Switches which invoke feathering //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 (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type [contact_points] point.0=1, -10.04, 0.0, -9.12, 1600.0, 0, 0.60, 40.0, 0.704, 2.5, 0.686, 3.0, 5.0, 0.0, 0.0, 0.0 point.1=1, -34.89, -16.06, -9.17, 1600.0, 1, 1.35, 0.0, 0.704, 2.5, 0.686, 7.0, 9.0, 7.0, 166.0, 166.0 point.2=1, -34.89, 16.06, -9.17, 1600.0, 2, 1.35, 0.0, 0.704, 2.5, 0.682, 3.0, 5.0, 7.0, 166.0, 166.0 point.3=2, -34.62, -54.74, 3.18, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0 point.4=2, -34.62, 54.74, 3.18, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0 point.5=2, -86.36, -16.06, 2.81, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0 point.6=2, -86.36, 16.06, 2.81, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0 point.7=2, 0.03, 0.0, -1.2, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4.0, 0.0, 0.0 static_pitch = 1 static_cg_height = 8.56 gear_system_type=1 //Hydraulic tailwheel_lock = 0 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 0.0 //Flap angle that activates warning at idle flap_limit_power = 16.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 1.0 //Brake scalar differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected [hydraulic_system] normal_pressure = 732.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint = -2.41, -1.74, 2.92 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -34.62, -54.74, 3.18, fx_navredh , light.1 = 3, -34.62, 54.74, 3.18, fx_navgreh , light.2 = 3, -86.36, -14.24, 5.63, fx_navwhi , light.3 = 3, -86.36, 14.24, 5.63, fx_navwhi , light.4 = 1, -82.13, -14.24, 17.89, fx_beaconh , light.5 = 1, -82.13, 14.24, 17.89, fx_beaconh , light.6 = 4, -3.00, 0.00, 1.95, fx_vclighth, light.7 = 3, -34.62, -54.74, 3.18, fx_strobeh , light.8 = 3, -34.62, 54.74, 3.18, fx_strobeh , [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 Adf.2 = 1 Transponder.1 = 0 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 =200, 1000 aileron =200, 1000 rudder =200, 1000 [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=1,0 direction_indicator.1=2,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 attitude_indicator.1 = 2 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=2,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks startup=fx_engstrt_jenny touchdown=fx_tchdwn, 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 25 max_generator_alternator_amps = 100 [fuel] LeftMain = -22.55, -6.7, -3.0, 202.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain= -22.55, 6.7, -3.0, 202.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center1 = -22.55, 0.0, -2.7, 200.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 2 electric_pump=1 [airplane_geometry] wing_area = 987.0 //Square feet wing_span = 95.0 //Feet wing_root_chord = 12.85 //Feet wing_dihedral = 5.0 //Degrees wing_incidence = 2.0 //Degrees wing_twist = -1.0 //Degrees oswald_efficiency_factor= 0.65 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 14.5 //Degrees, wing leading edge wing_pos_apex_lon = -13.00 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = -2.7 //Feet, vertical distance from reference point, positive going up htail_area = 95.8 //Square feet htail_span = 28.25 //Feet htail_pos_lon = -52.7 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = -52.7 //Feet, vertical distance from reference point, positive going up htail_incidence = -1.0 //Degrees htail_sweep = 27.0 //Degrees, horizontal tail leading edge vtail_area = 37.9 //Square feet vtail_span = 11.49 //Feet, tip to body vtail_sweep = 50.4 //Degrees, vertical tail leading edge vtail_pos_lon = -51.4 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 6.7 //Feet, vertical distance from reference point, positive going up elevator_area = 83.4 //Square feet aileron_area = 102.8 //Square feet rudder_area = 46.7 //Square feet elevator_up_limit = 30.0 //Degrees elevator_down_limit = 20.0 //Degrees aileron_up_limit = 27.0 //Degrees aileron_down_limit = 18.0 //Degrees rudder_limit = 30.0 //Degrees elevator_trim_limit = 12.0 //Degrees spoiler_limit = 0.0 //Degrees spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 0 //Aileron to spoileron gain min_ailerons_for_spoilerons = 0 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed = 67.5 //Knots True (KTAS) full_flaps_stall_speed = 61.5 //Knots True (KTAS) cruise_speed = 95.0 //Knots True (KTAS) max_indicated_speed = 224 //Red line (KIAS) [autopilot] autopilot_available= 1 flight_director_available= 0 pitch_takeoff_ga=0.0 default_vertical_speed=700.000000 autothrottle_available=0 direction_indicator=1 attitude_indicator =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 = 0.0 default_bank_mode=2 //Default to Heading Hold [forcefeedback] ground_bumps_magnitude1=2600 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.6 ground_bumps_magnitude2=1200 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.085 ground_bumps_slope2=0.65 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=3500000 ; in microseconds [stall_warning] type=1 [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second