[fltsim.0] title=Air Algerie Airbus A380 sim=AI_A380 model= panel= sound= texture=d atc_id=N380NW atc_airline= atc_flight_number=380 ui_manufacturer=Air Algerie Airbus A380 ui_type=A380 ui_variation=Rafik_pilote atc_heavy=1 atc_parking_types=GATE atc_parking_codes=A380 visual_damage=0 description= [General] atc_type=Airbus atc_model=A380 editable=0 performance=\n\n\n\n Category=airplane [General] visual_damage=1// 0=off, 1=on atc_type=AIRBUS atc_model=A380 editable=1 performance= Category=airplane [fltsim.1] title=AI_A380 NWA Logos sim=AI_A380 model= panel= sound= texture=nwa_logos atc_id=N381NW atc_airline=Northwest atc_flight_number=381 ui_manufacturer=AI_AIRBUS ui_type=A380 ui_variation=Northwest Airlines Twin Cities atc_heavy=1 atc_parking_types=GATE atc_parking_codes=A380 visual_damage=0 description= [General] visual_damage=1// 0=off, 1=on atc_type=AIRBUS atc_model=A380 editable=1 performance= Category=airplane [WEIGHT_AND_BALANCE] max_gross_weight=1278900.000 empty_weight=1212750.000 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=0.000000,0.000000,0.000000,0.000000 ;Moments of Inertia empty_weight_pitch_MOI=43000000.000 empty_weight_roll_MOI=20100000.000 empty_weight_yaw_MOI=20700000.000 empty_weight_coupled_MOI=0.000 CG_forward_limit=0.000 CG_aft_limit=0.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=2.000 induced_drag_scalar=1.000 elevator_effectiveness=0.500 aileron_effectiveness=1.500 rudder_effectiveness=1.000 pitch_stability=0.2500 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=-8.080, -83.250, -2.600 Engine.1=17.560, -47.580, -5.780 Engine.2=17.560, 47.580, -5.780 Engine.3=-8.080, 83.250, -2.600 fuel_flow_scalar=0.0001 min_throttle_limit=-0.20 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=113.000 rated_N2_rpm=29920.000 static_thrust=70000.000 afterburner_available=1 reverser_available=1.000 [jet_engine] thrust_scalar=1.0 [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, 89.220, 0.000, -16.500, 1181.100, 0.000, 4.521, 50.000, 1.300, 2.250, 1.323, 6.500, 6.600, 0.000, 0.000, 0.000 point.1=1.000, -4.500, -20.400, -18.800, 1574.800, 1.000, 4.521, 0.000, 2.910, 1.500, 1.747, 6.950, 6.950, 2.000, 0.000, 0.000 point.2=1.000, -4.500, 20.400, -18.800, 1574.800, 2.000, 4.521, 0.000, 2.910, 1.500, 1.747, 7.000, 7.000, 3.000, 0.000, 0.000 point.3=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, 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, -83.330, 0.000, 2.500, 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 //point.7=1.000, 5.200,-20.200, -10.500, 1574.800, 1.000, 4.521, 0.000, 1.910, 1.500, 1.747, 6.900, 6.900, 2.000, 0.000, 0.000 //point.8=1.000, 5.200,20.200, -10.500, 1574.800, 2.000, 4.521, 0.000, 1.910, 1.500, 1.747, 7.100, 7.100, 3.000, 0.000, 0.000 static_pitch=-0.50 static_cg_height=15.80 gear_system_type=1 [Views] eyepoint=105.15, -2.60, 7.54 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.1=1, 26.40, 0.00, 20.15, fx_beaconh , light.2=1, 35.93, 0.00, -9.25, fx_beaconh , light.3=3, -114.67, 0.00, 12.91, fx_navwhih, [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [fuel] LeftMain=0.000, -35.000, 0.000, 50.000, 0.000 RightMain=0.000, 35.000, 0.000, 50.000, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=9100.000 wing_span=266.000 wing_root_chord=61.000 wing_dihedral=6.200 wing_incidence=0.000 wing_twist=0.000 oswald_efficiency_factor=0.800 wing_winglets_flag=1 wing_sweep=32.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=1090.000 htail_span=70.700 htail_pos_lon=-100.000 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=40.000 vtail_area=573.000 vtail_span=27.300 vtail_sweep=35.000 vtail_pos_lon=-108.300 vtail_pos_vert=5.800 elevator_area=137.000 aileron_area=68.000 rudder_area=232.000 elevator_up_limit=30.000 elevator_down_limit=30.000 aileron_up_limit=30.000 aileron_down_limit=15.000 rudder_limit=25.000 elevator_trim_limit=20.000 spoiler_limit=60.000 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 auto_spoiler_available=1 spoiler_extension_time=3.000000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 [Reference Speeds] flaps_up_stall_speed=185.000 full_flaps_stall_speed=135.000 cruise_speed=590 max_indicated_speed=562 max_mach=0.92 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=600.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 use_no_default_bank=1 use_no_default_pitch=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 [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 [brakes] toe_brakes_scale=0.35 parking_brake=1 auto_brakes=4 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=34.950426 flap_limit_idle=19.480565 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [Flaps.0] type=1 span-outboard=0.700 extending-time=50.000 system_type=1 damaging-speed=260.000 blowout-speed=300.000 lift_scalar=0.85 drag_scalar=1.000 pitch_scalar=0.000 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=12.000, 0.000 flaps-position.5=20.000, 0.000 flaps-position.6=28.000, 0.000 flaps-position.7=35.000, 0.000 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0