//*For Flight Simulator 2002/2004* //*Copyright© 2002 By Eaglesoft Development Group* //*All Rights Reserved* //*Flight Model by Rob Young //*March3rd 2004 RY Service Release 1 [fltsim.0] title=Eaglesoft Citation X Deluxe sim=CitationX model= panel= sound= texture= kb_checklists= atc_id=7237 ui_manufacturer=Cessna ui_type=Eaglesoft Citation X Deluxe ui_variation=Blue and Maroon Sweep description=The Citation X will climb to 43,000 feet in just 30 minutes at its maximum takeoff weight, lifting you swiftly to transcontinental and transatlantic crossing altitudes. And the Citation X is certified to fly as high as 51,000 feet - where fuel efficiency is optimized and airline traffic is nonexistent. At 600 mph, the Citation X will run the mile in a sizzling six seconds. It covers 3,300 nautical miles in less time than any other business jet. It streaks from LA to New York in under four hours. And it shrinks the New York-to-London flight to under six hours. The Citation X can cross half a dozen time zones without a refueling stop. It combines cruising speeds of Mach .92 with true intercontinental and transatlantic range. The Citation X is no conventional aircraft. No other business aircraft in the world flies so far, so fast, on so little. [fltsim.1] title=EagleSoft Citation X Standard sim=CitationX model=1 panel= sound= texture= kb_checklists= atc_id=7237 ui_manufacturer=Cessna ui_type=Eaglesoft Citation X Standard ui_variation=Maroon Grey Ribbon description=The Citation X will climb to 43,000 feet in just 30 minutes at its maximum takeoff weight, lifting you swiftly to transcontinental and transatlantic crossing altitudes. And the Citation X is certified to fly as high as 51,000 feet - where fuel efficiency is optimized and airline traffic is nonexistent. At 600 mph, the Citation X will run the mile in a sizzling six seconds. It covers 3,300 nautical miles in less time than any other business jet. It streaks from LA to New York in under four hours. And it shrinks the New York-to-London flight to under six hours. The Citation X can cross half a dozen time zones without a refueling stop. It combines cruising speeds of Mach .92 with true intercontinental and transatlantic range. The Citation X is no conventional aircraft. No other business aircraft in the world flies so far, so fast, on so little. [fltsim.2] title=EagleSoft Citation X Light sim=CitationX model=2 panel= sound= texture= kb_checklists= atc_id=7237 ui_manufacturer=Cessna ui_type=Eaglesoft Citation X Light ui_variation=Brown Gold Silk description=The Citation X will climb to 43,000 feet in just 30 minutes at its maximum takeoff weight, lifting you swiftly to transcontinental and transatlantic crossing altitudes. And the Citation X is certified to fly as high as 51,000 feet - where fuel efficiency is optimized and airline traffic is nonexistent. At 600 mph, the Citation X will run the mile in a sizzling six seconds. It covers 3,300 nautical miles in less time than any other business jet. It streaks from LA to New York in under four hours. And it shrinks the New York-to-London flight to under six hours. The Citation X can cross half a dozen time zones without a refueling stop. It combines cruising speeds of Mach .92 with true intercontinental and transatlantic range. The Citation X is no conventional aircraft. No other business aircraft in the world flies so far, so fast, on so little. [fltsim.3] title=EagleSoft Citation X Ultra Light sim=CitationX model=3 panel=1 sound= texture= kb_checklists= atc_id=7237 ui_manufacturer=Cessna ui_type=Eaglesoft Citation X Ultra Light ui_variation=Blue Grey Ribbon description=The Citation X will climb to 43,000 feet in just 30 minutes at its maximum takeoff weight, lifting you swiftly to transcontinental and transatlantic crossing altitudes. And the Citation X is certified to fly as high as 51,000 feet - where fuel efficiency is optimized and airline traffic is nonexistent. At 600 mph, the Citation X will run the mile in a sizzling six seconds. It covers 3,300 nautical miles in less time than any other business jet. It streaks from LA to New York in under four hours. And it shrinks the New York-to-London flight to under six hours. The Citation X can cross half a dozen time zones without a refueling stop. It combines cruising speeds of Mach .92 with true intercontinental and transatlantic range. The Citation X is no conventional aircraft. No other business aircraft in the world flies so far, so fast, on so little. [fltsim.4] title=Eaglesoft Citation X Deluxe - MAN.UTD sim=CitationX model=4 panel=4 sound= texture=1 kb_checklists= atc_id=7237 ui_manufacturer=Cessna ui_type=Eaglesoft Citation X Deluxe ui_variation=Blue and Maroon Sweep and MAN.UTD description=The Citation X will climb to 43,000 feet in just 30 minutes at its maximum takeoff weight, lifting you swiftly to transcontinental and transatlantic crossing altitudes. And the Citation X is certified to fly as high as 51,000 feet - where fuel efficiency is optimized and airline traffic is nonexistent. At 600 mph, the Citation X will run the mile in a sizzling six seconds. It covers 3,300 nautical miles in less time than any other business jet. It streaks from LA to New York in under four hours. And it shrinks the New York-to-London flight to under six hours. The Citation X can cross half a dozen time zones without a refueling stop. It combines cruising speeds of Mach .92 with true intercontinental and transatlantic range. The Citation X is no conventional aircraft. No other business aircraft in the world flies so far, so fast, on so little. [General] atc_type=Cessna atc_model=C750 editable=1 performance="Please see your Eaglesoft Development Group Cessna Citation X documentation for performance information. Available on our Downloads Page" [WEIGHT_AND_BALANCE] max_gross_weight=36400.0 // (pounds) empty_weight=21600.0 // (pounds) reference_datum_position=0.00, 0.00, 0.00 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline) empty_weight_CG_position=-1.0, 0.00, 0.0 // -3.9 (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0="170, 19.0, 0, 0.0, Pilot" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) station_load.1="170, 19.0, 0, 0.0, Co-Pilot" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) station_load.2="170, 11.5, 0, 0.0, Passenger 1" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) station_load.3="170, -22.5,0, 0.0, Passenger 2" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) station_load.4="170, -26.7,0, 0.0, Passenger 3" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) station_load.5="170, -26.7,0, 0.0, Passenger 4" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) station_load.6= "170, -30.9,0, 0.0, Passenger 5" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) station_load.7= "170, -30.9,0, 0.0, Passenger 6" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) ;Moments of Inertia empty_weight_pitch_MOI=280000 empty_weight_roll_MOI=176000 empty_weight_yaw_MOI=110000 empty_weight_coupled_MOI=0.0 [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.5 max_generator_alternator_amps=400.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus=0, 5 , 9.5 avionics=1, 5 , 9.5 additional_system=0, 2 , 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=1.12 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 [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-10.4, -5.2, 4.0 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-10.4, 5.2, 4.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.176 //Scalar for fuel flow efficiency min_throttle_limit=-0.35 //Minimum percent throttle. Generally negative for turbine reverser [TurbineEngineData] fuel_flow_gain=0.0030 inlet_area=1.74 // 1.94 rated_N2_rpm=29920 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=1.09 //DO NOT CHANGE!!! //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, 22.4, 0.00, -4.42, 1181.1, 0, 0.6349, 49.0, 0.2400, 2.5, 0.5460, 8.0, 8.0, 0, 260.0, 260.0 point.1=1, -3.2, -5.30, -4.96, 1574.8, 1, 0.6349, 0.0, 0.5300, 2.5, 0.5456, 9.0, 9.0, 2, 260.0, 260.0 point.2=1, -3.2, 5.30, -4.96, 1574.8, 2, 0.6349, 0.0, 0.5300, 2.5, 0.5456, 9.0, 9.0, 3, 260.0, 260.0 point.3=2, -15.8, -31.4, 0.70, 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, -15.8, 31.4, 0.70, 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, -25.6, 0.00, 3.20, 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, 29.0, 0.00, -0.08, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch=-0.82 static_cg_height=4.6 gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available=1 //Normal pct_throttle_limit=0.1 //Percent throttle that activates warning flap_limit_idle=15.0 //Flap angle that activates warning at idle flap_limit_power=30.0 //Flap angle that activates warning at above idle [brakes] parking_brake=1 //Parking brake available toe_brakes_scale=0.5 //Brake scalar [hydraulic_system] normal_pressure=3000.0 //PSI electric_pumps=1 //electric pumps enabled engine_map=1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=20.2, -.825, 3.15 //RH //Longitudinal, Lateral, Vertical (feet) //;eyepoint= 20.310204, -1.1, 3.35 //BH //Longitudinal, Lateral, Vertical (feet) //[RYViews] ;eyepoint=19.9, -1.1, 3.45 //RY ;eyepoint= 20.9, -1.1, 3.35 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo, 10=cockpit light.0=3, -14.80, -31.2, 0.883441, fx_navredm , light.1=3, -14.80, 31.2, 0.883441, fx_navgrem , light.2=3, -34.971428, 0.00, 11.37128, fx_navwhi , light.3=1, -4.930720, 0.00, -2.383679, fx_beaconb , //belly beacon light.4=2, -15.95, -31.400158, 0.895627, fx_strobe , //Leftwing strobe light.5=2, -15.95, 31.400158, 0.895627, fx_strobe , //Rightwing strobe light.6=1, -27.428572, 0.00, 13.495714, fx_beaconh ,//Horz StabBeacon light.7=5, 7.09, -4.048980, -0.970262, fx_landing ,//Left light.8=5, 7.09, 4.048980, -0.970262, fx_landing ,//right light.9=10, 21.00, 0.00, 2.25, citx_panelflood.fx, light.10=10, 21.00, 0.00, 0.25, citx_panelflood.fx, light.11=8, 11.3, -18.6, 7.60, citx_icelight //rightwing icelight light.12=8, 11.3, 18.6, 7.60, citx_icelight //leftwing icelight light.13=8, 8.85, -3.1, -.1, fx_navwhi.fx //rightwing icelight point source light.14=8, 8.85, 3.1, -.1, fx_navwhi.fx //leftwing icelight point source [SMOKESYSTEM] smoke.1=-13.3, -22.6, -22.6, fx_contrail_s.fx smoke.2=-13.3, -22.60, 22.6, fx_contrail_s.fx smoke.3=-13.3, -22.6, -22.6, fx_contrail_s.fx smoke.4=-13.3, -22.60, 22.6, fx_contrail_s.fx smoke.5=-13.3, -22.6, -22.6, fx_contrail_s.fx smoke.6=-13.3, -22.60, 22.6, fx_contrail_s.fx [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=1.0 // 0.0 .. 1.0 extending-time=10 // seconds flaps-position.0=0 // degrees flaps-position.1=0.01 // degrees flaps-position.2=5 // degrees flaps-position.3=15 flaps-position.4=35 damaging-speed=250 // KIAS blowout-speed=300 // KIAS system_type=0 [flaps.1] type=2 // 1 - tail, 2 - lead span-outboard=1.0 // 0.0 .. 1.0 extending-time=2 // seconds flaps-position.0=0 // degrees flaps-position.1=3 // degrees damaging-speed=250 // KIAS blowout-speed=300 system_type=0 [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, 1 Adf.1=1,0 Transponder.1=1 Marker.1=1 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0=2 attitude_indicator.1=1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwnCX, 1 [fuel] Center1= 0.0, 0.0, -1.5, 895.52, 0.0 LeftMain= 0.0, 6.5, -0.8, 522.0, 0.0 RightMain=0.0,-6.5, -0.8, 522.0, 0.0 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=2 electric_pump=1 [airplane_geometry] wing_area=390.0 //Square feet wing_span=63.9 //Feet wing_root_chord=14.9 //Feet wing_dihedral=3.0 //Degrees wing_incidence=0.5 //Degrees wing_twist=-1.5 //Degrees oswald_efficiency_factor=0.86 //Measure of lift effeciency of wing 0.816 wing_winglets_flag=0 //Are winglets available? wing_sweep=26.0 //Degrees, wing leading edge wing_pos_apex_lon=7.9 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.5 //Feet, vertical distance from reference point, positive going up htail_area=67.0 //Square feet htail_span=25.6 //Feet htail_pos_lon=-27.82 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=11.724 //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=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=18.3 //Square feet elevator_up_limit=17.0 //Degrees elevator_down_limit=16.5 //Degrees aileron_up_limit=18.0 //Degrees aileron_down_limit=16.0 //Degrees rudder_limit=70.0 //Degrees elevator_trim_limit=22.0 //Degrees spoiler_limit=75.0 //Degrees spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=5.6 //Aileron to spoileron gain min_ailerons_for_spoilerons=10 //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=494.0 //MAX Knots True (KTAS) max_mach=0.922 max_indicated_speed=350 //Red line (KIAS) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=2200.0 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_max_rpm=97.5 autothrottle_takeoff_ga=0 pitch_takeoff_ga=8; max_pitch=12.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.07 nav_proportional_control=11.00 nav_integrator_control=0.20 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=1.0 Use_no_default_bank=1 Use_no_default_pitch=1 default_pitch_mode=0 default_bank_mode=0 [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 [stall_warning] type=1
