//Project Airbus A380-800 //Original FDE by Shane Olguin for Project Airbus //Last updated: 28 OCT 2008 //Final modifications by Derek Mayer //Last updated: 26 JUN 2010 [fltsim.0] title = Airbus A380-841 RR WV sim = PA380 model = panel = sound = texture = kb_checklists = kb_reference = atc_id = G-CIIV atc_airline = Speed Bird atc_flight_number = 45 ui_manufacturer = Airbus ui_type = A380-841 ui_variation = British Airways ui_typerole = "Commercial Airliner" ui_createdby = "Project Airbus" description = Project Airbus presents the Airbus A380-800. Features include dynamic wingflex (with input from several new variables), accurate LAF simulation, parallel bogies, drooping control surfaces, hardcoded double strobes, and over 40 other custom xml parts. Visit us at www.pairbus.com. \n British Airways Livery\n\n Xudeva Irribarra atc_parking_types = GATE atc_parking_codes = BA [general] atc_type = AIRBUS atc_model = A380 performance = A380-841\nRB211 Trent 970B-84\n\nMZFW: 820,120 LBS\nMMTOW: 1,124,400 LBS\nMLW: 868,620 LBS\n\nMinimum Crew: 2\nRange: 8,200nm\nService Ceiling: 43,000ft\nMmo: 0.89M\n category = airplane [reference speeds] flaps_up_stall_speed = 130.00 full_flaps_stall_speed = 115.00 cruise_speed = 510.00 max_mach = 0.89 max_indicated_speed = 340.00 [weight_and_balance] empty_weight = 611000.00 max_gross_weight = 1124400.00 reference_datum_position = 0.00, 0.00, 0.00 empty_weight_CG_position = 12.50, 0.00, 0.00 empty_weight_pitch_MOI = 42600000.00 empty_weight_roll_MOI = 22350000.00 empty_weight_yaw_MOI = 49400000.00 empty_weight_coupled_MOI = 0.00 max_number_of_stations = 9 //A380-842 config (R12 J60 Y399 TOTAL471) //Pax Zonings station_load.0 = "1950.00, 80.00, 0.000, 3.000, CAB LA R (12)" //2100lbs station_load.1 = "20050.0, 37.50, 0.000, 3.000, CAB LB Y (126)" //22050lbs station_load.2 = "14325.0, -8.00, 0.000, 3.000, CAB LC Y (91)" //15925lbs station_load.3 = "15150.0, -43.00, 0.000, 3.000, CAB LD Y (94)" //16450lbs station_load.4 = "10000.0, 30.00, 0.000, 11.00, CAB UA J (60)" //10500lbs station_load.5 = "13250.0, -35.00, 0.000, 11.00, CAB UB Y (88)" //15400lbs //Cargo & Baggage station_load.6 = "19000.0, 63.00, 0.000, -4.000, CPT 1 (63000)" //Fore (63000lbs) station_load.7 = "12000.0, -23.00, 0.000, -4.000, CPT 2 (44775)" //Aft (44775lbs) station_load.8 = "1000.00, -45.00, 0.000, -3.000, CPT B (5540)" //Bulk (5540lbs) [fuel] fuel_type = 2 number_of_tank_selectors = 4 electric_pump = 0 Lefttip = -25.00, -100.00, 2.00, 2731.54, 0.00 LeftAux = 3.00, -55.00, 1.00, 16931.58, 0.00 LeftMain = 25.00, -20.00, 0.00, 19942.61, 0.00 Center3 = -85.00, 0.00, 8.00, 6260.35, 0.00 RightMain = 25.00, 20.00, 0.00, 19942.61, 0.00 RightAux = 3.00, 55.00, 1.00, 16931.58, 0.00 Righttip = -25.00, 100.00, 2.00, 2731.54, 0.00 [generalenginedata] engine_type = 1 fuel_flow_scalar = 0.60 min_throttle_limit = -0.23 engine.0 = -6.00, -85.50, -5.50, engine.1 = 20.00, -49.00, -8.00, engine.2 = 20.00, 49.00, -8.00, engine.3 = -6.00, 85.50, -5.50, [turbineenginedata] fuel_flow_gain = 0.00135 inlet_area = 35.00 rated_N2_rpm = 9750.00 static_thrust = 80214.00 afterburner_available = 0 reverser_available = 1 [jet_engine] thrust_scalar = 1.055 [contact_points] //0 Class (1= landing gear/2= scrape point/3= skid point /4= float/5= water rudder) //1 Longitudinal Position (feet from reference datum) //2 Lateral Position (feet from reference datum, minus=Left, plus=Right ) //3 Vertical Position (feet from reference datum) //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 (max compression/static compression) //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type (0=Center gear/1=Auxiliary gear/2=Left gear/3=Right gear/4=Fuselage scrape/5=Left wing scrape/6=Right wing scrape/7=Aux. scrape 1/8=Aux. Scrape 2/9= Tail scrape) //14 IAS limit gear retraction (KIAS) //15 IAS gear damage at (KIAS) //Nosewheel travel, this model: //Main gear travel, this model: max_number_of_points = 13 // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0 = 1, 102.50, 0.00, -18.60, 1000.00, 0, 2.10, 70.00, 1.20, 2.50, 0.60, 13.00, 14.00, 0, 250.00, 250.00 //Nose landing gear point.1 = 1, -3.00, -12.50, -19.33, 1500.00, 1, 2.50, 0.00, 1.20, 2.50, 0.60, 16.50, 17.50, 2, 250.00, 250.00 //Left inboard landing gear point.2 = 1, -3.00, 12.50, -19.33, 1500.00, 2, 2.50, 0.00, 1.20, 2.50, 0.60, 15.00, 16.00, 3, 250.00, 250.00 //Right inboard landing gear point.3 = 2, -41.00, -131.00, 6.00, 700.00, 0, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5, 0.00, 0.00 //Left wing tip point.4 = 2, -41.00, 131.00, 6.00, 700.00, 0, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6, 0.00, 0.00 //Right wing tip point.5 = 2, 118.50, 0.00, -2.00, 700.00, 0, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0.00, 0.00 //Nose point.6 = 2, -110.00, 0.00, 61.00, 700.00, 0, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0.00, 0.00 //Vertical stabilizer point.7 = 2, -112.00, -49.00, 11.00, 700.00, 0, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5, 0.00, 0.00 //Left horizontal stabilizer point.8 = 2, -112.00, 49.00, 11.00, 700.00, 0, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6, 0.00, 0.00 //Right horizontal stabilizer point.9 = 2, -111.00, 0.00, 7.00, 700.00, 0, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9, 0.00, 0.00 //Tail point.10 = 2, 8.325, -85.600, -10.34, 700.00, 0, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5, 0.00, 0.00 //Left outboard engine point.11 = 2, 8.325, 85.600, -10.34, 700.00, 0, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6, 0.00, 0.00 //Right outboard engine point.12 = 5, -3.00, 0.00, 0.00, 0.00, 0, 0.00, 0.00, 50.00, 0.00, 1.00, 0.20, 0.20, 0, 0.00, 0.00 //Artificial water rudder for animations static_pitch = -0.35 static_cg_height = 18.75 tailwheel_lock = 0 gear_system_type = 1 [brakes] parking_brake = 1 toe_brakes_scale = 0.72 differential_brakes_scale = 0.45 auto_brakes = 4 [hydraulic_system] normal_pressure = 5000.00 electric_pumps = 1 engine_map = 1,1,1,1 [flight_tuning] cruise_lift_scalar = 1.00 parasite_drag_scalar = 0.90 induced_drag_scalar = 1.00 elevator_effectiveness = 1.00 aileron_effectiveness = 1.00 rudder_effectiveness = 1.00 pitch_stability = 1.10 roll_stability = 1.00 yaw_stability = 1.00 elevator_trim_effectiveness = 1.50 aileron_trim_effectiveness = 1.00 rudder_trim_effectiveness = 1.00 [airplane_geometry] wing_area = 9100.00 wing_span = 261.67 wing_root_chord = 62.00 wing_dihedral = 5.00 wing_incidence = -4.50 wing_twist = 0.00 oswald_efficiency_factor = 0.78 wing_winglets_flag = 1.00 wing_sweep = 33.50 wing_pos_apex_lon = 59.00 wing_pos_apex_vert = -5.00 htail_area = 1800.00 htail_span = 100.00 htail_pos_lon = -70.00 htail_pos_vert = 8.00 htail_incidence = -2.00 htail_sweep = 37.50 vtail_area = 1100.00 vtail_span = 43.00 vtail_sweep = 45.00 vtail_pos_lon = -60.00 vtail_pos_vert = 18.00 elevator_area = 550.00 aileron_area = 450.00 rudder_area = 350.00 elevator_up_limit = 30.00 elevator_down_limit = 20.00 aileron_up_limit = 30.00 aileron_down_limit = 20.00 rudder_limit = 30.00 elevator_trim_limit = 10.00 spoiler_limit = 50.00 aileron_to_spoileron_gain = 2.50 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 10.00 min_flaps_for_spoilerons = 0 spoilerons_available = 1 auto_spoiler_available = 1 spoiler_extension_time = 2.00 positive_g_limit_flaps_up = 4.00 positive_g_limit_flaps_down = 2.99 negative_g_limit_flaps_up = -2.99 negative_g_limit_flaps_down = -1.99 [flaps.0] //Trailing edge flaps, visual and pitch type = 1 system_type = 1 damaging-speed = 280 blowout-speed = 300 span-outboard = 0.5 extending-time = 25 lift_scalar = 0.00 drag_scalar = 0.00 pitch_scalar = 1.00 flaps-position.0 = 0 flaps-position.1 = 0 flaps-position.2 = 8 flaps-position.3 = 17 flaps-position.4 = 26 flaps-position.5 = 32 [flaps.1] //Trailing edge flaps, lift type = 1 system_type = 1 damaging-speed = 280 blowout-speed = 300 span-outboard = 0.5 extending-time = 25 lift_scalar = 1.00 drag_scalar = 0.00 pitch_scalar = 0.00 flaps-position.0 = 0 flaps-position.1 = 0 flaps-position.2 = 8 flaps-position.3 = 17 flaps-position.4 = 26 flaps-position.5 = 32 [flaps.2] //Trailing edge flaps, drag type = 1 system_type = 1 damaging-speed = 250 blowout-speed = 365 span-outboard = 0.5 extending-time = 25 lift_scalar = 0.00 drag_scalar = 1.00 pitch_scalar = 0.00 flaps-position.0 = 0 flaps-position.1 = 0 flaps-position.2 = 8 flaps-position.3 = 17 flaps-position.4 = 26 flaps-position.5 = 32 [flaps.3] //Slats type = 2 system_type = 1 damaging-speed = 290 blowout-speed = 300 span-outboard = 0.5 extending-time = 25 lift_scalar = 0.55 drag_scalar = 0.25 pitch_scalar = -1.00 flaps-position.0 = 0 flaps-position.1 = 20 flaps-position.2 = 20 flaps-position.3 = 20 flaps-position.4 = 23 flaps-position.5 = 23 [keyboard_response] elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [forcefeedback] gear_bump_nose_magnitude = 1000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 450 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 2000 crash_direction1 = 1000 crash_magnitude2 = 2000 crash_direction2 = 9000 crash_period2 = 7500 crash_duration2 = 2500000 stick_shaker_magnitude = 0 stick_shaker_direction = 0 stick_shaker_period = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 engine_generator_map = 1,1,1 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 5, 17 avionics = 1, 5, 17 pitot_heat = 0, 15, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [effects] wake = fx_wake wate = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 windshield_rain_effect_available = 1 [lights] light.0 = 3, -111.35, 0.00, 7.80, fx_navwhih light.1 = 2, -111.35, 0.00, 7.50, fx_strobeh light.2 = 1, 50.60, 1.50, 17.80, fx_beaconh light.3 = 1, 50.60, -1.50, 17.80, fx_beaconh light.4 = 1, 8.30, 0.00, -12.05, fx_beaconb light.5 = 4, 106.00, 0.00, 4.50, fx_vclighth [autopilot] autopilot_available = 1 flight_director_available = 1 default_vertical_speed = 0 autothrottle_available = 1 autothrottle_arming_required = 1 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8 max_pitch = 10.0 max_pitch_acceleration = 1.0 max_pitch_velocity_lo_alt = 2.0 max_pitch_velocity_hi_alt = 1.5 max_pitch_velocity_lo_alt_breakpoint = 20000.0 max_pitch_velocity_hi_alt_breakpoint = 28000.0 max_bank = 25.0 max_bank_acceleration = 1.8 max_bank_velocity = 3.00 max_throttle_rate = 0.20 nav_proportional_control = 16.00 nav_integrator_control = 0.17 nav_derivative_control = 0.00 nav_integrator_boundary = 2.50 nav_derivative_boundary = 0.00 gs_proportional_control = 18.0 gs_integrator_control = 0.33 gs_derivative_control = 0.00 gs_integrator_boundary = 0.70 gs_derivative_boundary = 0.00 yaw_damper_gain = 1.0 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 5.0 //Flap angle that activates warning at idle flap_limit_power = 5.5 //Flap angle that activates warning at above idle [views] eyepoint = 108.6, -2.0, 5.7 [radios] 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 [direction_indicators] direction_indicator.0 = 3,0 [attitude_indicators] attitude_indicator.0 = 2 [turn_indicators] turn_indicator.0 = 0,0 [exits] number_of_exits = 4 exit_rate.0 = 0.2 exit_rate.1 = 0.2 exit_rate.2 = 0.2 exit_rate.3 = 0.2 [pitot_static] vertical_speed_time_constant = 1 pitot_heat = 1.000000 [stall_warning] type = 2 stick_shaker = 0 [vacuum_system] max_pressure = 5.000000 vacuum_type = 2 electric_backup_pressure = 5.000000 engine_map = 1,1,1,1 [pneumatic_system] max_pressure = 20.000000 bleed_air_scalar = 1.000000 [deice_system] structural_deice_type = 1 [tailhook] //cargo doors tailhook_length = 1 tailhook_position = 0, 0, 0 [folding_wings] //1R, 5L, 5R wing_fold_system_type = 4 fold_rates = 0.2, 0.2
