[fltsim.0] title=Cessna Citation Mustang sim=cessmust model= panel= sound= texture= atc_id=N848C ui_manufacturer=Cessna ui_type=Mustang ui_variation=jje description=First deliveries of the 4-passenger Cessna Citation Mustang are expected in late 2006. This one was made with Flight Sim Design Studio 2.11 (FSDS2) by ABACUS Publishing (abacuspub.com). [General] atc_type=Cessna atc_model=Mustang editable=1 performance=Cruise Speed: 340 KTAS\nCeiling: 41,000 ft\nDesigner: Chuck Dome\nDate: May 2003 [WEIGHT_AND_BALANCE] max_gross_weight=10000 // (pounds) empty_weight=7000 // (pounds) reference_datum_position=-0.5, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170, 5.0, -2.0, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, 5.0, 2.0, 0.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=30000 empty_weight_roll_MOI=18200 empty_weight_yaw_MOI=36500 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=0.7 [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-8.3, -4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-8.3, 4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=0.7 //Scalar for fuel flow efficiency min_throttle_limit=0.000000 [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=2750 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=0 //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] point.0=1, 11.00, 0.00, -4.55, 1574, 0, 0.596, 39.9, 0.170, 2.5, 0.9516, 4.0, 4.0, 0, 0.0, 0.0 point.1=1, -2.90, -8.58, -4.79, 1574, 1, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.0, 4.0, 2, 0.0, 0.0 point.2=1, -2.90, 8.58, -4.79, 1574, 2, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.0, 4.0, 3, 0.0, 0.0 point.3=2, -3.33, -23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -3.33, 23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -22.67, 0.00, 0.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 23.08, 0.00, -1.50, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch=0.0 static_cg_height=4.3 gear_system_type=1 [Views] eyepoint=10.0, -1.25, 2.0 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees flaps-position.1=15 // degrees flaps-position.2=25 // degrees flaps-position.3=40 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS [Radios] [Radios] // Radio Type = available, 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 [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] LeftMain=0.0, -9.5, -1.0, 115.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux=0.0, -6.0, -1.5, 50.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=0.0, 9.5, -1.0, 115.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux=0.0, 6.0, -1.5, 50.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=310.0 //Square feet wing_span=45.0 //Feet wing_root_chord=6.9 //Feet wing_dihedral=6.0 //Degrees wing_incidence=1.0 //Degrees wing_twist=-1.5 //Degrees oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing wing_winglets_flag=1 //Are winglets available? wing_sweep=1.0 //Degrees, wing leading edge wing_pos_apex_lon=2.1 //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=-22.6 //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=0.5 //Degrees htail_sweep=20.0 //Degrees, horizontal tail leading edge vtail_area=42.0 //Square feet vtail_span=7.4 //Feet, tip to body vtail_sweep=40.0 //Degrees, vertical tail leading edge vtail_pos_lon=-20.5 //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=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=96.0 //Knots True (KTAS) full_flaps_stall_speed=76.8 //Knots True (KTAS) cruise_speed=315.0 //Knots True (KTAS) max_indicated_speed=2010.000000 max_mach=3.000000 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1800.0 autothrottle_available= 1 autothrottle_arming_required= 1 autothrottle_max_rpm = 90 autothrottle_takeoff_ga= 0 pitch_takeoff_ga = 8; max_pitch=10.0 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=0.10 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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation light.0=1, -15.30, 0.00, 9.10, fx_beacon , light.1=2, -0.80, -20.10, -0.60, fx_strobe , light.2=2, -0.80, 20.10, -0.60, fx_strobe , light.3=3, -0.80, -20.10, -0.60, fx_navred , light.4=3, -0.80, 20.10, -0.60, fx_navgre , light.5=3, -15.30, 0.00, 9.10, fx_navwhi , [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 [brakes] toe_brakes_scale=1.525925 parking_brake=1 [gear_warning_system] gear_warning_available=0 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
