[fltsim.0] title=Flight Options Citation V sim=Cessna Citation 2 model= panel= sound= texture=Flight Options kb_checklists= ui_manufacturer=AI Aircraft ui_type=Citation V ui_variation=Flight Options atc_heavy=0 atc_id= atc_airline=Flight Options atc_flight_number= atc_parking_codes=FOP atc_parking_types=RAMP description=Cessna Citation V\nAI model by Dee Waldron\nFS Community Projects\nwww.simufly.com [General] atc_type=Citation atc_model= editable=1 performance=Lenght: 47.2 feet\nWing Span: 52.2 feet\nWeight: 14,000 lbs (max takeoff)\nPower: (2) Pratt & Whitney\n\tJT15D-4 [WEIGHT_AND_BALANCE] max_gross_weight=20450.0 // (pounds) empty_weight=11700.0 // (pounds) reference_datum_position=0, 0, 0 // (feet) distance from FS Ref position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-0, 0, 0 // (feet) long, lat, vert distance from specified datum max_number_of_stations=50 station_load.0=170, 14.0, -1.2, 0.0 //Pilot Weight(lbs), long, lat, vert positions from datum (feet) station_load.1=170, 14.0, 1.2, 0.0 //Co-Pilot station_load.2=170, 10.0, -1.2, 0.0 //Pssngr 1 station_load.3=170, 10.0, 1.2, 0.0 //Pssngr 2 station_load.4=170, 5.0, -1.2, 0.0 //Pssngr 3 station_load.5=170, 5.0, 1.2, 0.0 //Pssngr 4 station_load.6=170, 0.0, -1.2, 0.0 //Pssngr 5 station_load.7=170, 0.0, 1.2, 0.0 //Pssngr 6 //station_load.8=170, 0.0, -1.2, 0.0 //Pssngr 7 //station_load.9=170, 0.0, 1.2, 0.0 //Pssngr 8 station_load.10=100, 12.5, 0.0, 0.0 //Baggage1 station_load.11=50, 18.2, 0.0, 0.0 //Baggage2 ;Moments of Inertia empty_weight_pitch_MOI=50000 empty_weight_roll_MOI=45000 empty_weight_yaw_MOI=70000 empty_weight_coupled_MOI=0.0 [electrical] max_battery_voltage=12.0 generator_alternator_voltage=13.8 max_generator_alternator_amps=40.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus=0, 10, 9.5 avionics=1, 5 , 9.5 additional_system=0, 20, 9.5 marker_beacon=1, 2 , 9.0 fuel_pump=0, 5 , 9.0 [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 [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-12.8, -4.9, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-12.8, 4.9, 0.8 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.0025 //Gain on fuel flow inlet_area=4.2895 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=3500 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=1.0 //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] //Gear point.0=1, 17.70, 0.00, -4.00, 1181.1, 0, 0.6349, 46.8, 0.4197, 2.5, 0.5878, 10.0, 10.0, 0, 0.0, 0.0 point.1=1, -1.70, -9.65, -4.00, 1574.8, 1, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 2, 0.0, 0.0 point.2=1, -1.70, 9.65, -4.00, 1574.8, 2, 0.6349, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 3, 0.0, 0.0 //Scrape point.3=2, 0.00, -29.50, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, 0.00, 29.50, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -25.00, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 23.00, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch=0.0000 //degrees (pitch when loaded on ground) static_cg_height=4.000 //feet, altitude of CG when at rest on the ground gear_system_type=0 [Views] eyepoint=14.00, -1.00, 3.40 //(feet) longitudinal, lateral, vertical distance from reference datum [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.70, -29.75, 0.60, fx_navredm , light.1=3, 0.70, 29.75, 0.60, fx_navgrem , light.2=3, -25.10, 0.00, 2.60, fx_navwhi , light.3=2, 0.60, -29.75, 0.60, fx_strobeh , light.4=2, 0.60, 29.75, 0.60, fx_strobeh , light.5=1, -25.70, 0.00, 13.50, fx_beacon , light.6=1, 0.00, 0.00, -1.60, fx_beaconb , [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees flaps-position.1=8 // degrees flaps-position.2=20 // degrees flaps-position.3=40 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [fuel] Center1=0.00, 0.00, 0.00, 359.0, 0.0 //Long (feet), Lat (feet), Vert (feet), Usable(gal), Unusable (gal) LeftMain=0.00, -10.0, 0.00, 268.5, 0.0 //Long (feet), Lat (feet), Vert (feet), Usable(gal), Unusable (gal) RightMain=0.00, 10.0, 0.00, 268.5, 0.0 //Long (feet), Lat (feet), Vert (feet), Usable(gal), Unusable (gal) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=312.0 //Square feet wing_span=45.8 //Feet wing_root_chord=7.3 //Feet wing_dihedral=2.5 //Degrees wing_incidence=0.5 //Degrees wing_twist=-1.5 //Degrees oswald_efficiency_factor=0.8 //Measure of lift effeciency of wing wing_winglets_flag=1 //Are winglets available? wing_sweep=35.0 //Degrees, wing leading edge wing_pos_apex_lon=-28.0 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_area=67.0 //Square feet htail_span=17.2 //Feet htail_pos_lon=-59.1 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=2.0 //Degrees htail_sweep=25.0 //Degrees, horizontal tail leading edge vtail_area=42.0 //Square feet vtail_span=7.4 //Feet, tip to body vtail_sweep=30.0 //Degrees, vertical tail leading edge vtail_pos_lon=-55.0 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=4.1 //Feet, vertical distance from reference point, positive going up elevator_area=17.0 //Square feet aileron_area=13.5 //Square feet rudder_area=7.3 //Square feet elevator_up_limit=17.0 //Degrees elevator_down_limit=15.5 //Degrees aileron_up_limit=18.0 //Degrees aileron_down_limit=18.0 //Degrees rudder_limit=30.0 //Degrees elevator_trim_limit=15.0 //Degrees spoiler_limit=60.0 //Degrees spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=4.6 //Aileron to spoileron gain min_ailerons_for_spoilerons=5 //Degrees min_flaps_for_spoilerons=0.0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=112.0 //Knots True (KTAS) full_flaps_stall_speed=102.0 //Knots True (KTAS) cruise_speed=464.0 //Knots True (KTAS) max_indicated_speed=330.000000 max_mach=0.810010 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_max_rpm=90 autothrottle_takeoff_ga=0 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 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=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 //Cessna Citation 2 for AI Traffic //Model by D.E. Waldron (Copyright) //All rights reserved. [brakes] toe_brakes_scale=1.000000 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=15.011494 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
