// Do not remove or edit this section. // This section is for PAI Installer information and will not interfere with aircraft behaviour [Project AI] Version=6.02 // FDE Revision by Oliver Caspers // // End of Project AI specific settings [General] atc_type=AIRBUS atc_model=A330 editable=1 performance=Cruise Speed\tMach .84\nMaximum Range\t5,600 nm\nService Ceiling\t36,400 ft\nMax Takeoff Weight\t580,000 lb\nSeating\t\t368 to 550\nCargo Capacity\t7,552 CU ft\n [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 = 468000.0 empty_weight = 264875.0 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = -3.000, 0.000, 0.000 max_number_of_stations =50 station_load.0 =85000.0,-8.0,0.0,0.0 ;Moments of Inertia empty_weight_pitch_MOI = 6200000 empty_weight_roll_MOI = 4000000 empty_weight_yaw_MOI = 8900000 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar=1.1 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness =1.4 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 = 5.4, -25.6, -3.500 Engine.1 = 5.4, 25.6, -3.500 fuel_flow_scalar = 1.000 min_throttle_limit = -0.15 //Minimum percent throttle. Generally negative for turbine reverser max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 19.6 rated_N2_rpm = 29920.000 static_thrust = 67500 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 [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 = 25.5 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.75 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=74.2, -1.8, 6.1 //(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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [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=2500 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm = 93 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=0.10 nav_proportional_control=12.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=25.0 gs_integrator_control=0.53 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [fuel] Center1 = 0.000, 0.000, -1.000, 12750.0, 0.000 LeftMain = -6.8, -13.5, 0.000, 12000.0, 0.000 RightMain = -6.8, 13.5, 0.000, 12000.0, 0.000 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 3908.4 wing_span = 197.9 wing_root_chord = 35.1 wing_dihedral = 4.200 wing_incidence = 2.00 wing_twist = -0.400 oswald_efficiency_factor= 0.75 wing_winglets_flag = 1 wing_sweep = 35.0 wing_pos_apex_lon = 10.1 wing_pos_apex_vert = 1.500 htail_area = 644.4 htail_span = 54.0 htail_pos_lon = -92.9 htail_pos_vert = 9.5 htail_incidence = 0.000 htail_sweep = 35.000 vtail_area = 456.8 vtail_span = 24.3 vtail_sweep = 42.000 vtail_pos_lon = -75.4 vtail_pos_vert = 12.1 elevator_area = 93.7 aileron_area = 82.0 rudder_area = 147.6 elevator_up_limit = 22.500 elevator_down_limit = 21.500 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 = 137.000 full_flaps_stall_speed = 112.000 cruise_speed = 495.000 max_mach = 0.86 max_indicated_speed = 330 //Red line (KIAS) [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 [stall_warning] type=2 [flaps.0] //Trailing Edge Flaps type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 20 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 1 // degrees flaps-position.2 = 2 // degrees flaps-position.3 = 5 // degrees flaps-position.4 = 10 // degrees flaps-position.5 = 20 // degrees flaps-position.6 = 30 // degrees flaps-position.7 = 40 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.8 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.1] //Outboard Leading Edge Slat type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 3 // seconds flaps-position.0 = 0 // flaps-position.1 = 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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.1 = 1, 3.00, 0.00, -10.40, fx_beaconb , light.2 = 1, 52.00, 0.00, 9.90, fx_beaconh , light.3 = 1, 3.00, 0.00, -10.40, fx_beaconb , light.4 = 1, 52.00, 0.00, 9.90, fx_beaconh , //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, 61.8, 0.0, -15.9, 1181.100, 0.000, 1.250, 55.920, 0.65, 2.500, 0.75, 4.000, 4.000, 0.000, 0.000, 0.000 point.1=1.000, -20.2, -12.9, -16.6, 1574.800, 1.000, 2.000, 0.000, 0.8, 2.500, 0.8, 6.900, 6.900, 2.000, 0.000, 0.000 point.2=1.000, -20.2, 12.9, -16.6, 1574.800, 2.000, 2.000, 0.000, 0.8, 2.500, 0.8, 7.100, 7.100, 3.000, 0.000, 0.000 point.3=2.000, -44.5, -97.0, 8.1, 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, -44.5, 97.0, 8.1, 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, -113.1, 0.000, 9.4, 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, 56.5, 0.000, -4.0, 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=-0.2 static_cg_height=16.1 gear_system_type=1 //Hydraulic [fltsim.0] title=PAI A332 RR tsc sim=pai332v6 model=RR panel= sound= texture=TSC kb_checklists= kb_reference= atc_id=ts-rep atc_id_color=0xffffffff atc_airline=TRANSAT atc_flight_number=9450 atc_parking_codes=TSC atc_parking_types=GATE ui_manufacturer=Project AI ui_type=AIRBUS A330-200 ui_variation=transat air atc_heavy=1 description=Project AI A332 Only for use with AI Traffic!