[fltsim.0] title=USAF_C-32A Tail No. 80001 sim=USAF_C-32A model= panel= sound= texture= panel_alias = sound_alias = kb_checklists= kb_reference= atc_id=80001 atc_id_color=0xffffffff atc_airline=Air Force atc_flight_number=2112 ui_manufacturer=Boeing ui_type=C-32A ui_variation=USAF Executive Transport, C-32A description=United States Air Force C-32A, Executive Transport. This aircraft is the first of four C-32A Transports that are used by Congressional Executives and other Government officials for business travel. Tail No. 80001 is specifically reserved for use by the Vice President of the United States, and was named "Air Force Two". GMAX model by Mike Stone, authentic textures by Kevin Stewart. atc_heavy=0 [General] atc_type=BOEING atc_model=B752 editable=1 performance=Max cruising speed 914km/h (493kt), economical cruising speed 850km/h (460kt). Range with P&W engines and 186 passengers 5053km (2728nm), with RR engines 4758km (2569nm). Range at optional max takeoff weight with P&W engines 7277km (3929nm), with RR engines 6888km (3719nm). 757-200PF - Speeds same. Range with 22,680kg payload and P&W engines 7195km (3885nm), with RR engines 6857km (3700nm). [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] max_gross_weight = 220000.000 empty_weight = 125750.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 0.000 max_number_of_stations = 50 station_load.0 = 19000.000, 0.000, 0.000, 0.000 ;Moments of Inertia empty_weight_pitch_MOI = 10000000.000 empty_weight_roll_MOI = 2000000.000 empty_weight_yaw_MOI = 6000000.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.000 induced_drag_scalar =1.000 elevator_effectiveness =1.000 aileron_effectiveness =1.000 rudder_effectiveness =1.000 pitch_stability =2.002 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =0.502 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 [SMOKESYSTEM] smoke.0=90.0,-27.3,-61.0, fx_WingVortex smoke.1=90.0,-27.3,-48.0, fx_WingVortex smoke.2=90.0,-27.3,48.0, fx_WingVortex smoke.3=90.0,-27.3,61.0, fx_WingVortex [GeneralEngineData] engine_type = 1 Engine.0 = 0.000, -22.000, -6.000 Engine.1 = 0.000, 22.000, -6.000 fuel_flow_scalar = 1.000 [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 24.000 rated_N2_rpm = 29920.000 static_thrust = 37400.000 afterburner_available = 0 reverser_available = 1 [jet_engine] thrust_scalar =1.000 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor = 0, 5 , 17.0 gear_motor = 0, 5 , 17.0 autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 20, 17.0 marker_beacon = 1, 2 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 17.0 starter1 = 0, 20, 17.0 light_nav = 0, 5 , 17.0 light_beacon = 0, 5 , 17.0 light_landing = 0, 5 , 17.0 light_taxi = 0, 5 , 17.0 light_strobe = 0, 5 , 17.0 light_panel = 0, 5 , 17.0 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0= 1.000, 40.000, 0.000, -12.300, 1181.100, 0.000, 1.442, 55.920, 0.800, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000 point.1= 1.000, -7.750, -8.580, -12.800, 1574.800, 1.000, 1.442, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000 point.2= 1.000, -7.750, 8.580, -12.800, 1574.800, 2.000, 1.442, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000 point.3= 2.000, -14.170, -47.330, -10.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -14.170, 47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -54.000, 0.000, 2.830, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 max_number_of_points = 21 static_pitch= 0.620 static_cg_height= 11.500 [Views] eyepoint=43.7, -1.31, 3.55 //(feet) longitudinal, lateral, vertical distance from reference datum [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 Transponder.1 = 1 Marker.1 = 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -24.31, -62.04, 3.97, fx_navredm , light.1 = 3, -24.31, 62.04, 3.97, fx_navgrem , light.2 = 3, -86.15, 0.00, 6.30, fx_navwhih , light.3 = 2, -21.59, -61.95, 4.00, fx_strobeh , light.4 = 2, -21.59, 61.95, 4.00, fx_strobeh , light.5 = 1, 5.38, 0.00, -6.21, fx_beaconb , light.6 = 1, 29.30, 0.00, 9.79, fx_beaconh , light.7 = 4, 61.43, 0.00, 5.36, fx_vclight , [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 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [EFFECTS] wake=fx_wake_ss //water=fx_spray water=fx_waterland dirt=fx_tchdrt concrete=fx_sparks ;touchdown=fx_tchdwn_s, 1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm = 90 autothrottle_takeoff_ga=1 pitch_takeoff_ga = 8; [fuel] Center1 = 0.000, 0.000, 0.000, 5000.000, 0.000 LeftMain = -3.000, -19.000, 0.000, 3600.000, 0.000 RightMain = -3.000, 19.000, 0.000, 3600.000, 0.000 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 [airplane_geometry] wing_area = 1994.000 wing_span = 124.000 wing_root_chord = 25.000 wing_dihedral = 5.000 wing_incidence = 1.000 wing_twist = -0.500 oswald_efficiency_factor= 0.750 wing_winglets_flag = 0 wing_sweep = 25.000 wing_pos_apex_lon = 8.000 wing_pos_apex_vert = 0.000 htail_area = 600.000 htail_span = 52.000 htail_pos_lon = -70.000 htail_pos_vert = 4.000 htail_incidence = 0.000 htail_sweep = 30.000 vtail_area = 360.000 vtail_span = 24.000 vtail_sweep = 35.000 vtail_pos_lon = -70.000 vtail_pos_vert = 10.000 elevator_area = 84.000 aileron_area = 28.000 rudder_area = 120.000 elevator_up_limit = 22.500 elevator_down_limit = 19.500 aileron_up_limit = 20.000 aileron_down_limit = 20.000 rudder_limit = 26.000 elevator_trim_limit = 20.000 spoiler_limit = 60.000 spoilerons_available = 1 aileron_to_spoileron_gain = 3.000 min_ailerons_for_spoilerons = 10.000 min_flaps_for_spoilerons = 0.000 [Reference Speeds] flaps_up_stall_speed = 142.000 full_flaps_stall_speed = 113.000 cruise_speed = 477.000 [forcefeedback] 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=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 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 [Flaps.0] type= 1 span-outboard= 0.300 extending-time= 8.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 flaps-position.2= 5.000, 0.000 flaps-position.3= 15.000, 0.000 flaps-position.4= 20.000, 0.000 flaps-position.5= 25.000, 0.000 flaps-position.6= 30.000, 0.000 [Flaps.1] type= 1 span-outboard= 0.400 extending-time= 8.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 flaps-position.2= 5.000, 0.000 flaps-position.3= 15.000, 0.000 flaps-position.4= 20.000, 0.000 flaps-position.5= 25.000, 0.000 flaps-position.6= 30.000, 0.000 [Flaps.2] type= 2 span-outboard= 0.800 extending-time= 2.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000