[FLTSIM.0] Title=Cessna Citation Bravo Sim=CE550 Model= Panel= Sound= Texture= KB_Checklists=c550_Check KB_Reference=c550_Ref ATC_ID=TG-BAC UI_Manufacturer=Cessna UI_Type=Citation Bravo UI_Variation=BAC International Bank Description=FS2004/FS2002 Cessna Citation C550 Bravo BAC International Bank. An Excellent Repaint of Keith A. Whyte's Cessna Citation Bravo. This Livery is Based on the Cessna Citation Bravo of BAC International Bank. This Aircraft was Owned by the Major PVC Manufacturer in Costa Rica, Durman Esquviel, They Have A Cessna Citation Excel (XL). BAC International Bank Owns Banks In Florida, Grand Cayman, Guatemala, El Salvador, Honduras, Nicaragua, Costa Rica & Panama. The Aircraft Owns a Guatemalan Tail Number and Flies To MRPV Tobias Bolaños, Costa Rica Frequently. I think That Their Aicraft Resides in Guatemala. [General] ATC_type=Cessna ATC_model=C550 Editable=1 Performance=Improved climb and cruise over Citation II. [Jet_Engine] Thrust_Scalar=1.000 [Flight_Tuning] Cruise_Lift_Scalar= 1.000 Parasite_Drag_Scalar= 1.000 Induced_Drag_Scalar= 1.000 Pitch_Stability= 1.000 Roll_Stability= 0.900 Yaw_Stability= 1.000 Elevator_Effectiveness= 0.800 Aileron_Effectiveness= 0.700 Rudder_Effectiveness= 1.000 [WEIGHT_AND_BALANCE] Max_Gross_Weight=13800.0 Reference_Datum_Position=0,0,0 Empty_Weight_CG_position=0,0,0 Empty_Weight=7750.0 Max_Number_of_Stations = 50 // Load # = Wt. Long Lat Vert. station_load.0 = 170, 0.0, -1.2, 0.0 // Pilot station_load.1 = 170, 0.0, 1.2, 0.0 // Co-Pilot station_load.2 = 170, 0.0, -1.2, 0.0 // Pax 1 station_load.3 = 170, 0.0, 1.2, 0.0 // Pax 2 station_load.4 = 170, 0.0, -1.2, 0.0 // Pax 3 station_load.5 = 170, 0.0, 1.2, 0.0 // Pax 4 station_load.6 = 0, 0.0, -1.2, 0.0 // Pax 5 station_load.7 = 0, 0.0, 1.2, 0.0 // Pax 6 station_load.8 = 0, 0.0, -1.2, 0.0 // Pax 7 station_load.9 = 0, 0.0, 1.2, 0.0 // Pax 8 station_load.10 = 140, 0.0, 0.0, 0.0 // Bag 1 station_load.11 = 140, 0.0, 0.0, 0.0 // Bag 2 empty_weight_roll_MOI = 51576.0 empty_weight_pitch_MOI= 43509.0 empty_weight_yaw_MOI = 71814.0 empty_weight_coupled_MOI=1300.0 [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 40.0 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 [pitot_static] vertical_speed_time_constant=10.0 [fuel] LeftMain= 0.0,0.0,0.0,350.0,0.0 RightMain=0.0,0.0,0.0,350.0,0.0 fuel_type=2 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=323.0 wing_span=51.7 wing_root_chord=7.3 wing_dihedral=0.35 wing_incidence=1.0 wing_twist=-1.0 oswald_efficiency_factor=0.8 wing_winglets_flag=0 wing_sweep=0.0 wing_pos_apex_lon=0.0 wing_pos_apex_vert=0.0 htail_area=63.0 htail_span=17.5 htail_pos_lon=-25.5 htail_pos_vert=0.0 htail_incidence=0.0 htail_sweep=25.0 vtail_area=50.0 vtail_span=8.0 vtail_sweep=30.0 vtail_pos_lon=-24.0 vtail_pos_vert=5.8 elevator_area=15.75 aileron_area=13.52 rudder_area=8.50 elevator_up_limit=27.5 elevator_down_limit=20.6 aileron_up_limit=14.5 aileron_down_limit=14.5 rudder_limit=23.5 elevator_trim_limit=19.4 spoiler_limit=59.0 spoilerons_available=0 aileron_to_spoileron_gain=0 min_ailerons_for_spoilerons=0 min_flaps_for_spoilerons=0 [contact_points] point.0=1, 17.30, 0.00, -5.08, 1575, 0.0, 0.70, 46.0, 0.2, 2.5, 0.85, 5, 5, 0,0,0 point.1=1, -.90, -6.67, -5.18, 1575, 1.0, 0.94, 0.0, 0.5, 2.5, 0.53, 5, 5, 2,0,0 point.2=1, -.90, 6.67, -5.18, 1575, 2.0, 0.94, 0.0, 0.5, 2.5, 0.53, 5, 5, 3,0,0 point.3=2, 3.16, -22.83, -1.00, 1575, 0.0, 0.00, 0.0, 0.0, 0.0, 0.00, 0, 0, 5,0,0 point.4=2, 3.16, 22.83, -1.00, 1575, 0.0, 0.00, 0.0, 0.0, 0.0, 0.00, 0, 0, 6,0,0 point.5=2, -22.10, 0.00, 0.63, 1575, 0.0, 0.00, 0.0, 0.0, 0.0, 0.00, 0, 0, 9,0,0 point.6=2, 26.41, 0.00, -2.83, 1575, 0.0, 0.00, 0.0, 0.0, 0.0, 0.00, 0, 0, 4,0,0 static_pitch=0.0 static_cg_height=4.41 gear_system_type=0 [Views] eyepoint=-14.0, -1.31, 1.64 [Radios] 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 [Flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 5 // seconds system_type = 0 flaps-position.0 = 0 // degrees flaps-position.1 = 5 // degrees flaps-position.2 = 10 // degrees flaps-position.3 = 15 // degrees flaps-position.4 = 30 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS [GeneralEngineData] engine_type=1 Engine.0=-8.4,-5.0,0.83 // Long, Lat, Vert Engine.1=-8.4, 5.0,0.83 // Long, Lat, Vert Fuel_Flow_Scalar=1.75 min_throttle_limit=-0.200012 [TurbineEngineData] fuel_flow_gain=0.0025 inlet_area=4.5 rated_N2_rpm=29920.0 static_thrust=2700.0 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=87.0 //Knots True (KTAS) full_flaps_stall_speed=78.0 //Knots True (KTAS) cruise_speed=427.0 //Knots True (KTAS) max_indicated_speed=564.453125 max_mach=0.839844 [Autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=3000.0 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_max_rpm=90 autothrottle_takeoff_ga=0 pitch_takeoff_ga=8.0 use_no_default_bank=1 use_no_default_pitch=1 default_pitch_mode=0 default_bank_mode=0 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 [keyboard_response] elevator= 150.0,250.0 aileron= 150.0,250.0 rudder= 150.0,250.0 [direction_indicators] direction_indicator.0=3,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.1, -26.34, -.15, fx_navred , light.1=3, 0.1, 26.34, -.15, fx_navgre , light.2=3, -22.30, 0.00, 1.1, fx_navwhi , light.3=2, 0.50, -26.30, -.15, fx_strobe , light.4=2, 0.50, 26.30, -.15, fx_strobe , light.5=1, -22.00, 0.00, 10.8, fx_beacon , light.6=4, 14.55, 0.00, 1.04, fx_vclight, [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [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=1.542283 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
