[fltsim.0]
title=Airbus A330-223 - Air Caraibes (F-OPTP)
sim=A330-200-PW-PW4000
model=pwSAT
panel=
sound=
texture=Air_Caraibes
checklists=
atc_airline=French West
atc_id=F-OPTP
atc_flight_number=TX536
atc_heavy=1
atc_parking_codes=FWI
atc_parking_types=GATE
ui_manufacturer=Airbus1
ui_type=A330-223
ui_variation=Air Caraibes (2004-2009)
description=Loués auprès ILFC à Air Caraibes du 08-12-2003 au 29-05-2009 vendu passe de F-OPTP à F-GRTP à l'etat française Vendu par ILFC 45 millions deuros,lavion est finalement acheté 50 millions deuros.avion qui totalisant 50 000 heures de vol
visual_damage=1
[fltsim.1]
title=Airbus A330-223 - Air Sarko one (F-GRTP-F-ZWUG-F-RARF)
sim=A330-200-PW-PW4000
model=pwSAT
panel=
sound=
texture=sarko_one
checklists=
atc_airline=French air force
atc_id=F-GRTP
atc_flight_number=Cotam Unite
atc_heavy=1
atc_parking_codes=FWI
atc_parking_types=GATE
ui_manufacturer=Airbus1
ui_type=A330-223
ui_variation=Air Sarko One (2009-2012)
description=Refondu par Sabena Technics en F-ZWUG avec transformations une chambre, avec lit double, mais une simple douche, une salle de communication ultrasophistiquée mais capable d'assurer un contact permanent entre le président et son administration, un centre médical et des leurres antimissiles pour la sécurité, 60 places passagers mais avec des équipements de travail... plus Deux moteurs neufs pour un coût net de 23,4 millions deuros F-GRTP Avion présidentiel Tout compris, lavion a finalement coûté 259,5 millions deuros, contre 226 millions prévus initialement. Mise en service 11 novembre 2010 F-RARF l'utilise pour la première fois par Nicolas Sarkozy pour se rendre à Séoul où se déroule le sommet du G20
[fltsim.2]
title=Airbus A330-223 - Air Holland one (F-RARF)
sim=A330-200-PW-PW4000
model=pwSAT
panel=
sound=
texture=holland_one
checklists=
atc_airline=French air force
atc_id=F-RARF
atc_flight_number=Cotam Unite
atc_heavy=1
atc_parking_codes=FWI
atc_parking_types=GATE
ui_manufacturer=Airbus1
ui_type=A330-223
ui_variation=Air Holland One (2012-?)
description=Cotam Unite nom indicatif est rebaptisé Air Hollande One par la presse, dans la continuité de l'ancien surnom. François Hollande l'utilise pour la première fois le 18 mai 2012 à l'occasion de sa visite aux États-Unis pour le sommet du G8 à Camp David.
[fltsim.3]
title=Airbus A330-223 - Swiss International Air Lines (HB-IQB)
sim=A330-200-PW-PW4000
model=pwSAT
panel=
sound=
texture=Swiss
checklists=
atc_airline=French air force
atc_id=HB-IQB
atc_flight_number=TX536
atc_heavy=1
atc_parking_codes=FWI
atc_parking_types=GATE
ui_manufacturer=Airbus1
ui_type=A330-223
ui_variation=Swiss International Air Lines (2002-fin2003)
description=Loués auprès ILFC de 31-03-2002 à 08-12-2003 Swiss International
[fltsim.4]
title=Airbus A330-223 - Swissair (HB-IQB)
sim=A330-200-PW-PW4000
model=pwSAT
panel=
sound=
texture=Swissair
checklists=
atc_airline=French air force
atc_id=HB-IQB
atc_flight_number=TX536
atc_heavy=1
atc_parking_codes=FWI
atc_parking_types=GATE
ui_manufacturer=Airbus1
ui_type=A330-223
ui_variation=Swissair (1998-2002)
description=Avion achete par ILFC +ou- 150 millions deuros n° Airbus vol Toulouse F-WWKZ premier vol le 21-10-1998 , Loués à Swissair mis en service HB-IQB le 09-11-1998 à 03-2002 Swissair 2002 à 08-12-2003 loues à Swiss International
//***************************************************************************************
[General]
performance=Passengers\n1-présidentiel conf 2009: 58 passages \n3-Swissair Air Caraibes conf 1998 2009: 253 \n2-Swissair Air Caraibes conf1998 2009 : 293\nCargo\n26\/27 LD3 containers \/ 10 Pallets \n\nTotal lower hold volume: 4,800 cu ft \n\nDimensions\nSpan 197 ft 10 in\nLength 193 ft 7 in\nHeight 54 ft 11 in \n\nEngines: GE CF6-80E1\nTO Thrust Rating: 72,000 lb\n\nMax Fuel Cap.: 36,750 gal\nMaxTOW: 507,400 lb\nZFW: 343,242 lb\n\nMax Range: 6,650 nm\nTypical Cruise Speed \n FL350: M.82
atc_type=AIRBUS
atc_model=A332
[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= 343242.000
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= 507000.000
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
[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, 11050.000, 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= -85.100
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= -79.576
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= 32.000
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= 0.4000
min_throttle_limit=-0.409912
[TurbineEngineData]
bypass_ratio=5.30
fuel_flow_gain= 0.001
inlet_area= 52.547
rated_N2_rpm= 29922.000
static_thrust= 72000.000
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar =0.840
[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= 68.55, -1.800, 8.2
[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, 51.233, 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, -84.717, 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, 91.817, 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= 10.420
//Nose Gear
//point.0= 1.000, 51.233, -2.000, -10.200, 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, 51.233, 2.000, -10.200, 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, -12.200, 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, -12.200, 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, -12.200, 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, -12.200, 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, -12.200, 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, -12.200, 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, -12.200, 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, -12.200, 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, -84.717, 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, 91.817, 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= 11.920
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
[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, 73.000, 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, -111.900, 0.000, 11.420, Opensky_nav_yellow ,
light.13 = 2, -111.900, 0.100, 11.300, fx_strobeh ,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[Flaps.0]
type=1
span-outboard=1.0
extending-time=20
system_type=1
flaps-position.0= 0
flaps-position.1= 2
flaps-position.2= 8
flaps-position.3=14
flaps-position.4=22
flaps-position.5=32
damaging-speed = 240
blowout-speed = 260
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
[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
[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
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
