[fltsim.0] title=A300-600R Areoflot sim=JF_AB6v2 model= panel= sound= texture= description=Country of origin: Europe(France, Germany, Spain and UK) ui_manufacturer=Airbus ui_type=A300-600R ui_variation=Areoflot atc_heavy=0 atc_id=F-OGQT atc_airline=Areoflot atc_flight_number=1008 [General] atc_type=AIRBUS atc_model=A300 performance=Powerplants:Two 262.4kn (59,000lb)General Electric CF6-80C2A1's or two 249kn (56,000lb) Pratt & Whitney PW4156s.\nPerformance:A300-600R Max cruising speed897km\/h (484kts). Long range cruising speed 875km\/h (472kts). Typical airline range with reserves and stanard fuel 7505km (4050nm).\nPrduction: Over 250 A300-600R delivered. [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= 370000.000 empty_weight= 198600.000 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= 75000.000, -10.000, 0.000, 0.000 ;Moments of Inertia empty_weight_pitch_MOI= 6172439.000 empty_weight_roll_MOI= 3262183.000 empty_weight_yaw_MOI= 13337024.000 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=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type= 1 Engine.0= 4.750, -16.100, -2.500 Engine.1= 4.750, 16.100, -2.500 fuel_flow_scalar= 1.000 [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 70.000 rated_N2_rpm= 29920.000 static_thrust= 56000.000 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_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, 52.800, 0.000, -13.850, 1181.100, 0.000, 3.500, 55.920, 0.800, 2.500, 0.900, 11.000, 11.000, 0.000, 0.000, 0.000 point.1= 1.000, -11.100, -17.500, -15.333, 1574.800, 1.000, 3.500, 0.000, 1.000, 2.500, 0.900, 12.000, 12.000, 2.000, 0.000, 0.000 point.2= 1.000, -11.100, 17.500, -15.333, 1574.800, 2.000, 3.500, 0.000, 1.000, 2.500, 0.900, 12.500, 12.500, 3.000, 0.000, 0.000 point.3= 2.000, -25.000, -73.500, 7.060, 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, -25.000, 73.500, 7.060, 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, -88.300, 0.000, 2.140, 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, 78.200, 0.000, -3.000, 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= -0.912 static_cg_height= 13.500 [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 [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 water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 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, 4313.000, 0.000 LeftMain= -12.000, -19.000, 0.000, 6000.000, 0.000 RightMain= -12.000, 19.000, 0.000, 6000.000, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area= 2800.000 wing_span= 147.100 wing_root_chord= 18.000 wing_dihedral= 6.200 wing_incidence= 1.000 wing_twist= -0.500 oswald_efficiency_factor= 0.750 wing_winglets_flag= 1 wing_sweep= 28.000 wing_pos_apex_lon= 15.000 wing_pos_apex_vert= 0.000 htail_area= 738.000 htail_span= 55.700 htail_pos_lon= -84.000 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 30.000 vtail_area= 374.000 vtail_span= 21.000 vtail_sweep= 35.000 vtail_pos_lon= -81.000 vtail_pos_vert= 5.800 elevator_area= 69.000 aileron_area= 46.900 rudder_area= 86.200 elevator_up_limit= 27.000 elevator_down_limit= 20.500 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= 0 aileron_to_spoileron_gain= 3.000 min_ailerons_for_spoilerons= 10.000 min_flaps_for_spoilerons= 0.000 [Reference Speeds] flaps_up_stall_speed= 160.000 full_flaps_stall_speed= 125.000 cruise_speed= 465.000 [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= 0.200 extending-time= 23.000 system_type= 1 damaging-speed= 260.000 blowout-speed= 300.000 lift_scalar= 0.550 drag_scalar= 0.550 pitch_scalar= 0.550 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 flaps-position.2= 2.000, 0.000 flaps-position.3= 5.000, 0.000 flaps-position.4= 10.000, 0.000 flaps-position.5= 15.000, 0.000 flaps-position.6= 25.000, 0.000 flaps-position.7= 30.000, 0.000 flaps-position.8= 40.000, 0.000 [Flaps.1] type= 1 span-outboard= 0.800 extending-time= 21.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.350 drag_scalar= 0.350 pitch_scalar= 0.350 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 flaps-position.2= 2.000, 0.000 flaps-position.3= 5.000, 0.000 flaps-position.4= 10.000, 0.000 flaps-position.5= 15.000, 0.000 flaps-position.6= 25.000, 0.000 flaps-position.7= 30.000, 0.000 flaps-position.8= 40.000, 0.000 [Flaps.2] type= 2 span-outboard= 0.600 extending-time= 3.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.050 drag_scalar= 0.050 pitch_scalar= 0.050 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.500, 0.000 flaps-position.2= 0.500, 0.000 flaps-position.3= 0.500, 0.000 flaps-position.4= 0.500, 0.000 flaps-position.5= 0.500, 0.000 flaps-position.6= 1.000, 0.000 flaps-position.7= 1.000, 0.000 flaps-position.8= 1.000, 0.000