// 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 PW cubana
sim=pai332v6
model=PW
panel=
sound=
texture=CUB
kb_checklists=
kb_reference=
atc_id=
atc_id_color=0xffffffff
atc_airline=cubana
atc_flight_number=3456
atc_parking_codes=CUB
atc_parking_types=GATE
ui_manufacturer=Project AI
ui_type=AIRBUS A330-200
ui_variation=cubana de aviacion
atc_heavy=1
description=Project AI A332 Only for use with AI Traffic!
