[fltsim.0]
title=Pan American Airbus 330-300
sim=A330-300-RR-Trent-772B
model=
panel=
sound=
texture=
checklists=

atc_airline=PAN AM
atc_id=N367PA
atc_flight_number=235
atc_heavy=1

ui_manufacturer=Airbus
ui_type=A330-300
ui_variation=Pan American Airways
visual_damage=1
description=Project Opensky \nAirbus 330-300\nVersion 2002.5.0\n\nFS2002 Only\n\nEngine Type: RR Trent 772B\n\nModel Designers\n   Shervin Ahooraei\n\nFlight Dynamics Designer\n   Warren C. Daniel\n\nPaint Designer\n   C. Vincent Cho\n\nTechnical Resource\n   Simon Ng\n   Nick Peterson\n\nTest Pilots\n   Project Opensky Members\n\nFor proper operation: See A330 manual at: \n  www.project-opensky.com

[WEIGHT_AND_BALANCE]
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

empty_weight= 354700.000

empty_weight_roll_MOI= 8955743.000
empty_weight_pitch_MOI= 22600873.000
empty_weight_yaw_MOI= 22751035.000
empty_weight_coupled_MOI= 1000.000

max_gross_weight= 515700.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar     =1.000
parasite_drag_scalar   =1.500
induced_drag_scalar    =1.300
elevator_effectiveness =1.200
aileron_effectiveness  =1.500
rudder_effectiveness   =2.500
pitch_stability        =1.500
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000


atc_type=AIRBUS AIRCRAFT
atc_model=A332

[pitot_static]
vertical_speed_time_constant=999		//Increasing this value will cause a more instantaneous reaction in the VSI

[fuel]
//Center1= 0.000, 0.000, -4.000, 16260.000, 0.000
Center2= -83.676, 0.000, 0.000, 1617.000, 3.000
LeftMain= -7.000, -37.983, 0.000, 11147.000, 3.000
RightMain= -7.000, 37.983, 0.000, 11147.000, 3.000
LeftAux= -13.000, -70.269, 0.000, 974.000, 3.000
RightAux= -13.000, 70.269, 0.000, 974.000, 3.000

fuel_type= 2.000                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors= 1

[airplane_geometry]
wing_area= 3892.000
wing_span= 197.833
wing_root_chord= 20.000
wing_dihedral= 6.218
wing_incidence= 0.000
wing_twist= -0.500
oswald_efficiency_factor= 0.600
wing_winglets_flag= 1
wing_sweep= 30.000
wing_pos_apex_lon= 25.000
wing_pos_apex_vert= 0.000
htail_area= 1050.000
htail_span= 69.700
htail_pos_lon= -89.200
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 40.000
vtail_area= 690.000
vtail_span= 27.300
vtail_sweep= 35.000
vtail_pos_lon= -83.676
vtail_pos_vert= 5.800
elevator_area= 137.000
aileron_area= 68.000
rudder_area= 232.000
elevator_up_limit= 24.000
elevator_down_limit= 18.000
aileron_up_limit= 25.000
aileron_down_limit= 25.000
rudder_limit= 45.000
elevator_trim_limit= 15.000
spoiler_limit= 35.000
spoilerons_available= 0
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 9.969
min_flaps_for_spoilerons= 0.000


[GeneralEngineData]
engine_type= 1
Engine.0= 15.166, -30.386, -7.583
Engine.1= 15.166, 30.386, -7.583
fuel_flow_scalar= 0.4370

[TurbineEngineData]
bypass_ratio=4.66
fuel_flow_gain= 0.001
inlet_area= 48.150
rated_N2_rpm= 29922.000
static_thrust= 71100.000
afterburner_available= 0
reverser_available= 1

[jet_engine]
thrust_scalar =0.800

[Reference Speeds]
flaps_up_stall_speed= 132.000
full_flaps_stall_speed= 124.000
cruise_speed= 460.000

[keyboard_response]
elevator= 100.000, 200.000
aileron= 100.000, 200.000
rudder= 50.000, 100.000

[Views]
eyepoint= 78.502, -1.756, 9.628

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 800.000
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_takeoff_ga= 1
autothrottle_max_rpm= 105.000
pitch_takeoff_ga= 8.000
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.

[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

[direction_indicators]
direction_indicator.0=3,0

[contact_points]

        //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)

point.0= 1.000, 62.433, 0.000, -10.625, 1181.102, 0.000, 4.845, 78.000, 0.500, 0.500, 0.510, 7.000, 9.000, 0.000, 280.000, 300.000 
point.1= 1.000, -11.067, -17.750, -13.350, 1574.803, 2.000, 2.45, -8.000, 1.800, 1.600, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000  
point.2= 1.000, -11.067,  17.750, -13.350, 1574.803, 1.000, 2.45, -8.000, 1.800, 1.600, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000  
point.3= 2.000, -14.167, -95.917, 0.000, 787.402, 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, -14.167, 95.917, 0.000, 787.402, 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, -120.667, 0.000, 2.500, 787.402, 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, 88.417, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 2.000, 14.167, -99.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.8= 2.000, 0.000, 44.750, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000

static_pitch= 0.104
static_cg_height= 11.420

//Nose Gear
//point.0= 1.000, 62.433, -2.000, -11.500, 1181.102, 0.000, 4.845, 78.000, 1.000, 2.400, 0.510, 7.000, 9.000, 0.000, 280.000, 300.000
//point.1= 1.000, 62.433,  2.000, -11.500, 1181.102, 0.000, 4.845, 78.000, 1.000, 2.400, 0.510, 7.000, 9.000, 0.000, 280.000, 300.000
//
//Main Gear Right
//point.2= 1.000, -11.067, -20.500, -13.200, 1574.803, 2.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000
//point.3= 1.000, -11.067, -15.000, -13.200, 1574.803, 2.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000
//point.4= 1.000,  -6.667, -20.500, -13.200, 1574.803, 2.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000
//point.5= 1.000,  -6.667, -15.000, -13.200, 1574.803, 2.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000
//
//Main Gear Left
//point.6= 1.000, -11.067,  20.500, -13.200, 1574.803, 1.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000
//point.7= 1.000, -11.067,  15.000, -13.200, 1574.803, 1.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000
//point.8= 1.000,  -6.667,  20.500, -13.200, 1574.803, 1.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000
//point.9= 1.000,  -6.667,  15.500, -13.200, 1574.803, 1.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000
//
//Scrape Points
//point.10= 2.000, -14.167, -95.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
//point.11= 2.000, -14.167, 95.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
//point.12= 2.000, -120.667, 0.000, 2.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
//point.13= 2.000, 88.417, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
//point.14= 2.000, 14.167, -99.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
//point.15= 2.000, 0.000, 44.750, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
//
//static_pitch= 0.104
//static_cg_height= 12.920

[LIGHTS]        
Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1 = 1,  7.8,  0.00, -5.5, fx_beaconb ,
light.2 = 1, 0.20,  0.00, 14.5, fx_beaconh ,
light.3 = 4, 81.41, 0.00,  8.0, fx_vclight ,
light.4 = 3, -116.00,  0.00,  11.42, fx_navwhih , 
light.5 = 2, -116.00,  0.1,   11.3, fx_strobeh , 
light.6 = 2, -40.20,-93.10, 13.38, fx_strobeh ,
light.7 = 2, -40.20, 93.10, 13.38, fx_strobeh ,
light.8 = 2, -48.00,-94.40, 13.38, fx_strobeh ,
light.9 = 2, -48.00, 94.40, 13.38, fx_strobeh ,


[General]
performance=Passengers\n2-class conf: 335 \n1-class conf: 440\n\nCargo\n32\/33 LD3 containers \/ 11 Pallets \n600 cubic Ft (17 cubic m)\nTotal lower hold volume: 5,656 cu ft \n\nDimensions\nSpan 197 ft 10 in\nLength 208 ft 11 in\nHeight 54 ft 11 in \n\nEngines: RR Trent 772B\nTO Thrust Rating: 71,100 lb\n\nMax Fuel Cap.: 24,700 gal\nMaxTOW: 515,700 lb\nZFW: 354,700 lb\n\nMax Range: 4,750 nm\nTypical Cruise Speed \n  @ FL350: M.82
atc_type=AIRBUS
atc_model=A330

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 25.000
system_type= 1
damaging-speed= 200.000
blowout-speed= 250.000
lift_scalar= 1.000
drag_scalar= 1.500
pitch_scalar= 3.000
flaps-position.0= 0.000
flaps-position.1= 1.000
flaps-position.2= 5.000
flaps-position.3= 10.000
flaps-position.4= 20.000
flaps-position.5= 25.000
flaps-position.6= 30.000

[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 12.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.500
pitch_scalar= 3.000
flaps-position.0= 0.000
flaps-position.1= 20.000

[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