[fltsim.0]
title=Air Transat Airbus A330-342
sim=A330-300-RR-Trent-772B
model=rrNOsat
panel=
sound=
texture=
checklists=

atc_airline=Transat
atc_id=C-GKTS
atc_flight_number=244
atc_heavy=1
atc_parking_codes=TS, TSC

ui_manufacturer=Airbus
ui_type=A330-342
ui_variation=Air Transat NC
visual_damage=1
description=Project Opensky \nAirbus 330-300 v2\nVersion 2004.7.1\n\nFS2004 \n\nEngine Type: RR Trent\n\nModel Designers\n   Shervin Ahooraei\n\nFlight Dynamics Designer\n   Warren C. Daniel\n\nMaster Texture Designer\n   Gary Hayes\n   Ben Hewitt\n\nTechnical Resource\n   Simon Ng\n   Nick Peterson\n\nAir Transat new Livery\n Xudeva Irribarra\n\nTest Pilots\n   Project Opensky Members\n\nFor proper operation: See A330 manual at: \n  www.projectopensky.com


[fltsim.1]
title=Project Opensky Airbus A330-342
sim=A330-300-RR-Trent-772B
model=rrNOsat
panel=fsx
sound=fsx
texture=
checklists=

atc_airline=Transat
atc_id=C-GKTS
atc_flight_number=243
atc_heavy=1
atc_parking_codes=TS, TSC

ui_manufacturer=Airbus
ui_type=A330-342
ui_variation=Air Transat NC
visual_damage=1
description=Project Opensky \nAirbus 330-300 v2\nVersion 2004.7.1\n\nFSX\n\nEngine Type: RR Trent\n\nModel Designers\n   Shervin Ahooraei\n\nFlight Dynamics Designer\n   Warren C. Daniel\n\nMaster Texture Designer\n   Gary Hayes\n   Ben Hewitt\n\nTechnical Resource\n   Simon Ng\n   Nick Peterson\n\nAir Transat new Livery\n Xudeva Irribarra\n\nTest Pilots\n   Project Opensky Members\n\nFor proper operation: See A330 manual at: \n  www.projectopensky.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=A330

[pitot_static]
vertical_speed_time_constant=999		//Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[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
electric_pump=0

[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
auto_spoiler_available=1
spoiler_extension_time=2.000000
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


[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
min_throttle_limit=-0.409912

[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
max_indicated_speed=330.000000
max_mach=0.870020

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

[Views]
eyepoint= 77.9, -1.800, 8.200

[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.
default_pitch_mode=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

[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, 1.845, 78.000, 0.500, 0.500, 0.510, 10.000, 10.600, 0.000, 280.000, 300.000 
point.1= 1.000, -15.5, -17.750, -13.88, 1574.803, 2.000, 2.45, -8.000, 2.3, 1.5, 0.550, 10.600, 11.800, 2.000, 280.000, 300.000  
point.2= 1.000, -15.5,  17.750, -13.88, 1574.803, 1.000, 2.45, -8.000, 2.3, 1.5, 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
point.9 = 5, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 2, 4, 0, 10, 30 
point.10 = 5, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 2, 0, 10, 30 


static_pitch= 0.104
static_cg_height= 11.420

//Nose Gear
//point.0= 1.000, 62.433, -2.000, -11.200, 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, -11.200, 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 (Left)
//point.2= 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.3= 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.4= 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.5= 1.000,  -6.667, -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

//Main Gear (Right)
//point.6= 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, 3.000, 280.000, 300.000
//point.7= 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, 3.000, 280.000, 300.000
//point.8= 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, 3.000, 280.000, 300.000
//point.9= 1.000,  -6.667,  15.500, -13.200, 1574.803, 2.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 3.000, 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
//point.16 = 5, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 2, 4, 0, 10, 30 
//point.17 = 5, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 2, 0, 10, 30 
//
//static_pitch= 0.104
//static_cg_height= 12.920
gear_system_type=0

[TailHook]
tailhook_length=1 ;(feet)
tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0

[folding_wings] 
wing_fold_system_type=4 ;0=None
fold_rates=0.12,0.11 ;Percent per second

[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

[LIGHTS]        
Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1  = 1,    7.800,   0.000,  -5.500, fx_beaconb ,
light.2  = 1,    0.200,   0.000,  14.500, fx_beaconh ,
light.3  = 4,   82.500,   0.000,   8.000, fx_vclight ,
light.4  = 2,  -40.200, -93.100,  13.380, Opensky_airbus_strobe ,
light.5  = 2,  -40.200,  93.100,  13.380, Opensky_airbus_strobe ,
light.6  = 5,   18.000,  27.000,  -4.000, Opensky_wing_light,
light.7  = 5,   19.933,   8.827,  -4.368, Opensky_wing_light,
light.8  = 5,   18.000, -27.000,  -4.000, Opensky_wing_light,
light.9  = 5,   19.933,  -8.827,  -5.368, Opensky_wing_light,
light.10 = 5,   19.700,  19.000,  -6.000, Opensky_nacelle_refl,
light.11 = 5,   19.700, -19.000,  -6.000, Opensky_nacelle_refl,
light.12 = 3, -116.000,   0.000,  11.420, Opensky_nav_yellow , 
light.13 = 2, -116.000,   0.100,  11.300, 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
Category=airplane



[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 15.000
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= 8.000
flaps-position.2= 14.000
flaps-position.3= 22.000
flaps-position.4= 32.000

[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


[electrical]
//                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot          = 0, 5 , 17.0
flap_motor         = 1, 0 ,  1.0
gear_motor         = 0, 5 , 17.0
avionics_bus       = 0, 0 ,  1.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 0 ,  1.0
additional_system  = 0, 0 ,  1.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 7, 0 , 99.0
gear_motor         = 4, 0 ,  1.0
fuel_pump          = 0, 0 ,  1.0
fuel_transfer_pump = 0, 0 ,  1.0
starter1           = 0, 20, 17.0
starter2           = 0, 0 ,  1.0
light_nav          = 0, 0 ,  1.0
light_beacon       = 0, 0 ,  1.0
light_landing      = 0, 0 ,  1.0
light_taxi         = 0, 0 ,  1.0
light_strobe       = 0, 0 ,  1.0
light_panel        = 0, 7 , 99.0
light_recognition  = 0, 0 ,  1.0
light_wing         = 0, 0 ,  1.0
marker_beacon      = 0, 0 ,  1.0
standby_vacuum     = 0, 0 ,  1.0
auto_brakes        = 0, 0 ,  1.0
hydraulic_pump     = 0, 0 ,  1.0
propeller_device   = 0, 0 ,  1.0
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
auto_brakes=4
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[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
[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