[fltsim.0] title=SGA A300B4-200 Ariana Afghan Airlines sim=a300B4-2c-v1 model= panel= sound= texture=Ariana kb_checklists= kb_reference= atc_airline=Ariana atc_flight_number=3541 atc_id= atc_heavy=1 ui_manufacturer=Airbus ui_type=A300B4-200 ui_variation=Ariana Afghan Airlines description=Ariana Afghan Airlines Airbus A300 B4-203, painted by Thomas Lo Gerfo. Model by SGA. visual_damage=1 [FORCEFEEDBACK] STICK_SHAKER_MAGNITUDE=3000 STICK_SHAKER_DIRECTION=0 STICK_SHAKER_PERIOD=111111 GEAR_BUMP_NOSE_MAGNITUDE=3000 GEAR_BUMP_NOSE_DIRECTION=18000 GEAR_BUMP_NOSE_DURATION=250000 GEAR_BUMP_LEFT_MAGNITUDE=2700 GEAR_BUMP_LEFT_DIRECTION=35500 GEAR_BUMP_LEFT_DURATION=250000 GEAR_BUMP_RIGHT_MAGNITUDE=2700 GEAR_BUMP_RIGHT_DIRECTION=00500 GEAR_BUMP_RIGHT_DURATION=250000 GROUND_BUMPS_MAGNITUDE1=1600 GROUND_BUMPS_ANGLE1=8900 GROUND_BUMPS_INTERCEPT1=3.0 GROUND_BUMPS_SLOPE1=0.20 GROUND_BUMPS_MAGNITUDE2=400 GROUND_BUMPS_ANGLE2=9100 GROUND_BUMPS_INTERCEPT2=1.075 GROUND_BUMPS_SLOPE2=0.035 CRASH_MAGNITUDE1=10000 CRASH_DIRECTION1=01000 CRASH_MAGNITUDE2=10000 CRASH_DIRECTION2=9000 CRASH_PERIOD2=75000 CRASH_DURATION2=500000 [FLIGHT_TUNING] PITCH_STABILITY=8.000 ROLL_STABILITY=3.000 YAW_STABILITY=1.315 ELEVATOR_EFFECTIVENESS=2.000 AILERON_EFFECTIVENESS=2.800 RUDDER_EFFECTIVENESS=2.800 CRUISE_LIFT_SCALAR=1.250 PARASITE_DRAG_SCALAR=1.150 INDUCED_DRAG_SCALAR=2.000 ELEVATOR_TRIM_EFFECTIVENESS=1.000 AILERON_TRIM_EFFECTIVENESS=1.000 RUDDER_TRIM_EFFECTIVENESS=1.000 [ELECTRICAL] electric_always_available=1 [GENERAL] \\N ATC_TYPE=AIRBUS ATC_MODEL=A300 performance=Cruisingspeed: Mach 0,78 - 0,80\nMTOW: 150000 kgs\nSeating: 314 (AirInter)\nMax. Thrust: 50400 Lbs \/110% N1\nEngines: GE-CF6-50C2\nRunwaylength: 2000 m\n\n [pitot_static] vertical_speed_time_constant=5 [FUEL] CENTER1=0.000, 0.000, -1.700, 3619.631, 0.000 LEFTAUX=0.000, -17.000, 0.000, 4442.056, 0.000 RIGHTAUX=0.000, 17.000, 0.000, 4442.056, 0.000 LEFTMAIN=0.000, -40.000, 0.000, 1151.763, 0.000 RIGHTMAIN=0.000, 40.000, 0.000, 1151.763, 0.000 NUMBER_OF_TANK_SELECTORS=2 fuel_type=2.000000 electric_pump=0 [airplane_geometry] // not real values but more realistic in FS2004 wing_area=2358.000000 wing_span=144.000000 wing_root_chord=12.000000 wing_dihedral=6.218262 wing_incidence=0.000000 wing_twist=-0.499878 oswald_efficiency_factor=0.700 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=689.000000 htail_span=53.333333 htail_pos_lon=-65.000000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=490.000000 vtail_span=25.238859 vtail_sweep=0.000000 vtail_pos_lon=-58.333333 vtail_pos_vert=5.833333 elevator_area=206.000000 aileron_area=73.840000 rudder_area=200.100000 elevator_up_limit=31.512679 elevator_down_limit=26.000825 aileron_up_limit=30.000070 aileron_down_limit=30.000070 rudder_limit=30.000070 elevator_trim_limit=37.242257 spoiler_limit=59.988681 spoilerons_available=1 aileron_to_spoileron_gain=1.500000 min_ailerons_for_spoilerons=1.1 min_flaps_for_spoilerons=0.000000 [CONTACT_POINTS] point.0 = 1.000, 54.300, 0.000, -12.18, 1574.803, 0.000, 1.840, 55.900, 1.430, 1.430, 0.999, 10.000, 10.000, 0.000, 300.000, 250.000 point.1 = 1.000, -3.000, -15.50, -13.15, 1574.803, 1.000, 2.133, 0.000, 1.722, 1.250, 0.950, 10.000, 10.000, 2.000, 300.000, 250.000 point.2 = 1.000, -3.000, 15.50, -13.15, 1574.803, 2.000, 2.133, 0.000, 1.722, 1.250, 0.950, 10.000, 10.000, 3.000, 300.000, 250.000 point.3=2, -34.00, -86.00, 8.40, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 5, 0, 0 point.4=2, -34.00, 86.00, 8.40, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 6, 0, 0 point.5=2, 97.50, 0.00, 6.00, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 9, 0, 0 point.6=2, -93.50, 0.00, 25.00, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 point.7=2, -85.50, 0.00, 11.50, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 point.8=2, -46.50, 0.00, -1.65, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 max_number_of_points= 10 static_pitch= 0.050 static_cg_height= 10.90 gear_system_type= 0 [Views] eyepoint=68.50,-1.25,6.75 //(feet) longitudinal, lateral, vertical distance from reference datum [GENERALENGINEDATA] ENGINE_TYPE=1 Engine.0 = 20.180, -25.600, -8.100 Engine.1 = 20.180, 25.600, -8.100 FUEL_FLOW_SCALAR=0.798891 min_throttle_limit=-0.1 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=70.000 rated_N2_rpm=29920.000 static_thrust=50400.000 afterburner_available=0 reverser_available=1 [jet_engine] thrust_scalar=1.000 [REFERENCE SPEEDS] FLAPS_UP_STALL_SPEED=145.000 FULL_FLAPS_STALL_SPEED=116.000 CRUISE_SPEED=675.425 max_indicated_speed=340.000000 max_mach=0.839990 [KEYBOARD_RESPONSE] ELEVATOR=116.000000,180.000000 AILERON=113.000000,174.000000 RUDDER=300.000000,300.000000 [AUTOPILOT] AUTOPILOT_AVAILABLE=1 FLIGHT_DIRECTOR_AVAILABLE=1 DEFAULT_VERTICAL_SPEED=1000.000000 AUTOTHROTTLE_AVAILABLE=1 AUTOTHROTTLE_ARMING_REQUIRED=1 AUTOTHROTTLE_TAKEOFF_GA=1 AUTOTHROTTLE_MAX_RPM=110.000000 PITCH_TAKEOFF_GA=8.000000 default_pitch_mode=0 default_bank_mode=0 max_pitch=20.000000 max_pitch_acceleration=9.900000 max_pitch_velocity_lo_alt=9.900000 max_pitch_velocity_hi_alt=9.900000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=2.000000 max_bank_velocity=3.0000000 max_throttle_rate=9.900000 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=1.000000 [DIRECTION_INDICATORS] DIRECTION_INDICATOR.0=3,0 [WEIGHT_AND_BALANCE] MTW=332583 // Added by LyonsMark MLW=293132 // Added by LyonsMark Pax_Weight=221 // Weight in pounds of passengers Added by LyonsMark Cargo_Weight=0 // Weight in pounds of cargo Added by LyonsMark // Fuel_Weight=99180 // Weight in pounds of loaded fuel Added by LyonsMark empty_weight=224810.000 // 224810.000 // ZFW_Weight=224810 // Added by LyonsMark Fuel_Capacity=99180 // Added by LyonsMark Cargo_Capacity=0 // Added by LyonsMark 1Class_Pax=345 // Added by LyonsMark 2Class_Pax=250 // Added by LyonsMark 3Class_Pax=0 // Added by LyonsMark Aircraft_Type=AIRBUS A300 // Added by LyonsMark reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 6.500, 0.000, -4.000 max_number_of_stations = 50 station_load.0=0.000000,0.000000,0.000000,0.000000 station_load.1 = "0.0, 0.0, 0.0, 0.0, FsStation" station_load.2 = "0.0, 0.0, 0.0, 0.0, FsStation" station_load.3 = "0.0, 0.0, 0.0, 0.0, FsStation" station_load.4 = "0.0, 0.0, 0.0, 0.0, FsStation" station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation" station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation" empty_weight_roll_MOI=20080000.000 empty_weight_pitch_MOI=58280000.000 empty_weight_yaw_MOI=9500000.000 empty_weight_coupled_MOI=000000.000 max_gross_weight=332583.600 CG_forward_limit=0.000 CG_aft_limit=1.000 [Flaps.0] // flaps type=1 span-outboard=0.800 extending-time=25.000 system_type=1 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=1.000 flaps-position.0=0.000, 0.000 flaps-position.1=0.000, 0.000 flaps-position.2=8.00, 0.000 flaps-position.3=16.000, 0.000 flaps-position.4=25.000, 0.000 [flaps.1] // Kruger flaps type = 2 // 1 - tail, 2 - lead span-outboard = 0.2 // 0.0 .. 1.0 extending-time = 2.5 // seconds flaps-position.0 = 0 // flaps-position.1 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.2] // Slats type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 5 // seconds flaps-position.0 = 0 // flaps-position.1 = 0.5 // flaps-position.2 = 0.5 // flaps-position.3 = 0.5 // flaps-position.4 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Adf.2=1 Transponder.1=1 Marker.1=1 [SMOKESYSTEM] // vert, long, lat, effect smoke.0= -10.000, 15.000, 26.000, fx_engsmoke , [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo, 10=cabin light.0=3, -19.65, -73.20, 7.40, fx_navred, light.1=3, -19.65, 73.20, 7.40, fx_navgre, light.2=2, -20.60, -73.60, 7.40, fx_strobe, light.3=2, -20.60, 73.60, 7.40, fx_strobe, light.4=1, -31.5, 0.00, -4.60, fx_beaconb, light.5=1, 7.5, 0.00, 13.20, fx_beaconh, light.6=4, 68.50, 0.00, 6.75, fx_vclight, light.7=9, -73.00, -12.00, 25.00, DC10logo , light.8=9, -73.00, 12.00, 25.00, DC10logo , light.9=9, -73.00, -12.00, 25.00, DC10logo , light.10=9, -73.00, 12.00, 25.00, DC10logo , [exits] //Shift+E for L2, Shift+E+2 for L1 and R2 number_of_exits = 2 exit_rate.0 = 0.4 exit_rate.1 = 0.4 [TailHook] //Landing lights extend/retract. tailhook_length= 4 tailhook_position= 0.0, 0.0, 0.0 cable_force_adjust= 0.5 [folding_wings] //cargo doors, R1, L/R4... wing_fold_system_type= 4 fold_rates= 0.110,0.400 [brakes] toe_brakes_scale=1.000000 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=2 [turn_indicators] turn_indicator.0=1,0
