//Aircraft sections are automatically added by the livery tool at the end of the file

[fltsim.0]
title=Alitalia Project Airbus A321-200
ui_variation=Alitalia
sim=pa321-cfm56
model=
panel=
sound=
texture=
checklists=
description=Project Airbus A321-200\n\nAlitalia livery\n Xudeva Irribarra\n\n\n
atc_id=I-BIXR
atc_airline=Alitalia
atc_flight_number=432
atc_parking_code=AZA
created_by=Project Airbus
ui_manufacturer=Airbus
ui_type=A321-111
visual_damage=1
atc_heavy=0



[fltsim.1]
title=Alitalia Airbus A321-112
ui_variation=Alitalia
sim=pa321-cfm56
model=
panel=fsx
sound=fsx
texture=
checklists=
description=Project Airbus A321-200\n\nAlitalia livery\n Xudeva Irribarra\n\n\n
atc_id=I-BIXR
atc_airline=Alitalia
atc_flight_number=432
atc_parking_code=AZA
created_by=Project Airbus
ui_manufacturer=Airbus
ui_type=A321-111
visual_damage=1
atc_heavy=0

[general]
performance=A321-211\nCFM56-5B3\n\nMZFW: 71,500 kg\nMTOW: 89,000 kg\nMLW: 75,500 kg\n\nMMO: 0.82\nVMO: 350 kt\nCeiling: 39,100 ft\n\nCrew: 2\nPassengers: 220
atc_type=Airbus
atc_model=A321
Category=airplane


[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


[weight_and_balance]
//A321-211/231 config
      
//Pax Zonings
station_load.0= "9395.2,  29.24, 0.000, 0.000,  CAB OA (74)" //Forward Section 
station_load.1= "9116.6,  -3.33, 0.000, 0.000,  CAB OB (74)" //Middle Section 
station_load.2= "8985.1, -31.34, 0.000, 0.000,  CAB OC (72)" //Rear Section  

//Cargo & Baggage
station_load.3= "3880.1,  28.11, 0.000, 0.000,  CPT FOR"     //Forward Compartment (12500lbs) 
station_load.4= "3986.9, -18.46, 0.000, 0.000,  CPT AFT"     //Aft Compartment     (12500lbs) 
station_load.5= "952.5,  -39.22, 0.000, 0.000,  CPT BLK"     //Bulk Compartment    (03300lbs) 

//Basic Weight

empty_weight=120847.4
empty_weight_roll_MOI=959904.000000
empty_weight_pitch_MOI=1710000.000000
empty_weight_yaw_MOI=1230000.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=196210
reference_datum_position=0.0000,0.000000,0.000000
empty_weight_CG_position=0.63,0.000000,0.000000
CG_forward_limit=0.18
CG_aft_limit=0.40

//Weight & Balance prepared by DM.


[airplane_geometry]
wing_area=1317.503
wing_span=111.833333
wing_root_chord=13.76
wing_dihedral=3.298901
wing_incidence=-3.5
wing_twist=-1.600000
oswald_efficiency_factor=0.745  
wing_winglets_flag=1
wing_sweep=25.0000
wing_pos_apex_lon=16.813 
wing_pos_apex_vert=0.70000
htail_area=333.681
htail_span=41.666667
htail_pos_lon=-57.33688
htail_pos_vert=6.500000
htail_incidence=1.500000
htail_sweep=0.000000
vtail_area=231.424
vtail_span=17.991665
vtail_sweep=0.000000
vtail_pos_lon=-54.51698
vtail_pos_vert=19.915
elevator_area=76.500000
aileron_area=57.0
rudder_area=56.200000
elevator_up_limit=25.0
elevator_down_limit=15.0
aileron_up_limit=25.0
aileron_down_limit=15.0
rudder_limit=25.0
elevator_trim_limit=13.5
spoiler_limit=50.0 //35.0
spoilerons_available=1          
aileron_to_spoileron_gain=1.5        
min_ailerons_for_spoilerons=12             
min_flaps_for_spoilerons=0                   
auto_spoiler_available=1
spoiler_extension_time=1.500000
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
fuel_flow_scalar=1.09  
Engine.0=6.500000,-18.95,-5.125
Engine.1=6.500000,18.95,-5.125
min_throttle_limit=-0.43
max_contrail_temperature = -30


[reference speeds]
flaps_up_stall_speed=128.000
full_flaps_stall_speed=102.000
cruise_speed=462.0
max_indicated_speed=350.000000
max_mach=0.820


[autopilot]
autopilot_available=1
flight_director_available=1 
default_vertical_speed=1000
autothrottle_available=1 
//use_no_default_pitch=			1
//use_no_default_bank=			1
pitch_takeoff_ga=18 
autothrottle_arming_required=		1
autothrottle_takeoff_ga=		1
autothrottle_max_rpm=			96.5
default_pitch_mode=0
default_bank_mode=0
max_pitch=				10.00
max_pitch_acceleration=		 	2.00
max_pitch_velocity_lo_alt=		4.00
max_pitch_velocity_hi_alt=		1.50  
max_pitch_velocity_lo_alt_breakpoint=	20000
max_pitch_velocity_hi_alt_breakpoint=	24000
max_bank=				25.00
max_bank_acceleration=			2.0
max_bank_velocity=			3.0
max_throttle_rate=			0.30
nav_proportional_control=		12.00
nav_integrator_control=			0.05
nav_derivative_control=			0.01
nav_integrator_boundary=		0.5
nav_derivative_boundary=		0.35
gs_proportional_control=		15.0 
gs_integrator_control=			0.30
gs_derivative_control=			0.00
gs_integrator_boundary=			0.7
gs_derivative_boundary=			0.00
yaw_damper_gain=			1.00


[direction_indicators]
direction_indicator.0=3,0


[effects]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1


[radios]
Audio.1= 1
Com.1  = 1, 1
Com.2  = 1, 1
Nav.1  = 1, 0, 1
Nav.2  = 1, 0, 0
Adf.1  = 1
Transponder.1= 1
Marker.1= 0

[contact_points]
	//0  Class	(1= landing gear/2= scrape point/3= skid point /4= float/5= water rudder)
	//1  Longitudinal Position	(feet from reference datum)
	//2  Lateral Position	(feet from reference datum, minus=Left, plus=Right )
	//3  Vertical Position	(feet from reference datum)
	//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	(max compression/static compression)
	//10 Damping Ratio	(0=Undamped, 1=Critically Damped)
	//11 Extension Time	(seconds)
	//12 Retraction Time	(seconds)
	//13 Sound Type	(0=Center gear/1=Auxiliary gear/2=Left gear/3=Right gear/4=Fuselage scrape/5=Left wing scrape/6=Right wing scrape/7=Aux. scrape 1/8=Aux. Scrape 2/9= Tail scrape)
	//14 IAS limit gear retraction	(KIAS)
	//15 IAS gear damage at	(KIAS)
	//Nosewheel travel, this model:
	//Main gear travel, this model:

static_pitch=-0.319722
static_cg_height=11.60811023622

point.0 = 1,  50.80,   0.0,  -11.96,  800, 0.0, 1.533, 68.0, 1.00, 1.44, 0.68, 13.2, 12.9, 0.0, 252.0, 282.0
point.1 = 1,  -4.20, -12.45, -12.27, 1200, 1.0, 1.680,  0.0, 0.72, 1.54, 0.81, 14.0, 13.7, 2.0, 252.0, 282.0
point.2 = 1,  -4.20,  12.45, -12.27, 1200, 2.0, 1.680,  0.0, 0.72, 1.54, 0.80, 14.2, 13.3, 2.0, 252.0, 282.0
point.3 = 2, -13.75, -54.58,  -0.50, 750,  0.0, 0.000,  0.0, 0.0,  0.00, 0.00,  0.0,  0.0, 5.0,   0.0,   0.0
point.4 = 2, -13.75,  54.58,  -0.50, 750,  0.0, 0.000,  0.0, 0.0,  0.00, 0.00,  0.0,  0.0, 6.0,   0.0,   0.0
point.5 = 2, -65.25,   0.00,   0.05, 750,  0.0, 0.000,  0.0, 0.0,  0.00, 0.00,  0.0,  0.0, 9.0,   0.0,   0.0
point.6 = 2,  66.16,   0.00,  -3.16, 750,  0.0, 0.000,  0.0, 0.0,  0.00, 0.00,  0.0,  0.0, 4.0,   0.0,   0.0
gear_system_type=0


[fuel]
Center1=   4.15,   0.0, -4.00, 2166.0, 6.1 
Center2=   4.15,   0.0, -4.00,  790.0, 4.5   //ACT 1
Center3=   4.15,   0.0, -4.00,  790.0, 4.5   //ACT 2

LeftMain=  0.10, -19.6,  1.40, 1815.0, 6.0   //3.45 
RightMain= 0.10,  19.6,  1.40, 1815.0, 6.0   //3.45

LeftAux=  -7.00, -36.4,  2.20,  232.0, 0.0 
RightAux= -7.00,  36.4,  2.20,  232.0, 0.0

fuel_type=2.0
number_of_tank_selectors=1
electric_pump=0


[keyboard_response]
aileron=180.000000,130.000000


[pitot_static]
vertical_speed_time_constant=99               
pitot_heat=1.000000


[views]
eyepoint=58.9, -1.90, 4.06


[flaps.0]
span-outboard=0.500000
extending-time=21.000000
system_type=1
type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=0.0
flaps-position.2=10.0
flaps-position.3=14.0
flaps-position.4=21.0 
flaps-position.5=25.0 
lift_scalar=0.0
drag_scalar=0.0

[flaps.1]     
type=2                                    // slats
span-outboard=0.95                                  // 0.0 .. 1.0
extending-time=21                                  // seconds
flaps-position.0=0   
flaps-position.1=18,
flaps-position.2=18, 
flaps-position.3=22, 
flaps-position.4=22,  
flaps-position.5=27,                                    
blowout-speed=260                               // KIAS
lift_scalar=0.10
drag_scalar=0.43
pitch_scalar=0.3
system_type=1 

[flaps.2] //ailerons
type=2
span-outboard=0.85
extending-time=13.000
system_type=1
damaging-speed=233.000
blowout-speed=250.000
flaps-position.0=0.000,
flaps-position.1=0.000, 
flaps-position.2=5.000, 
flaps-position.3=5.000, 
flaps-position.4=5.000, 
flaps-position.5=5.000, 
lift_scalar=0.25
drag_scalar=0.20

[flaps.3]  //actual flaps
type=1
span-outboard=0.85
extending-time=21.000
system_type=1
damaging-speed=233.000
blowout-speed=250.000
flaps-position.0=0.000,
flaps-position.1=0.000,  
flaps-position.2=10.000, 
flaps-position.3=14.000, 
flaps-position.4=21.000, 
flaps-position.5=25.000,  
lift_scalar=1.50  //0.66
drag_scalar=0.48


[jet_engine]
thrust_scalar=1.0


[turbineenginedata]
fuel_flow_gain=0.00247
inlet_area=29.3000
rated_N2_rpm=14950.000000
static_thrust=25233.000000  //CFM56-5B3 corrected value. Actual T/O 32000 MCP 29090.
afterburner_available=0
reverser_available=1
bypass_ratio=4.50


[exits]
number_of_exits=2
exit_rate.0=0.19       
exit_rate.1=0.17  


[flight_tuning]
elevator_effectiveness=1.0
pitch_stability=1.2
roll_stability=1.0
yaw_stability=1.0
aileron_trim_effectiveness=0.9
rudder_trim_effectiveness=1.1
cruise_lift_scalar     = 1.35 
parasite_drag_scalar=1.0
induced_drag_scalar=1.0


[lights]
light.0=3, -77.90, -0.15,  4.80, fx_navwhih
light.1=2, -77.90,  0.15,  4.80, fx_strobeh
light.2=1,   6.80,  0.00, -5.80, fx_beaconh
light.3=1,   3.83,  0.00,  8.47, fx_beaconh
light.4=4,  58.00,  0.00,  3.50, fx_vclighth


[smokesystem]
smoke.0=88.0,-17.3,-39.8, fx_contrail_320
smoke.1=88.0,-17.3,39.8, fx_contrail_320


[TailHook]
tailhook_length=4                              
tailhook_position=-15.0, 0.0, -1.0            
cable_force_adjust=0.9

[folding_wings]
wing_fold_system_type=4                    
fold_rates=0.18,0.19                       


[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 200
electric_always_available = 1
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 0 , 17.0
avionics           = 1, 0 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 0 , 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
starter2           = 0, 20 , 17.0
light_nav          = 0, 0 , 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, 0 , 17.0
light_cabin        = 0, 0 , 17.0
auto_brakes        = 0, 0 , 17.0
standby_vacuum     = 0, 0 , 17.0
hydraulic_pump     = 0, 0 , 17.0
fuel_transfer_pump = 0, 0 , 17.0
light_recognition  = 0, 0 , 17.0
light_wing         = 0, 0 , 17.0
light_logo         = 0, 0 , 17.0
directional_gyro   = 0, 0 , 17.0
directional_gyro_slaving = 0, 0 , 17.0


[brakes]
toe_brakes_scale=0.58
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


//FDE copyright Peter Binamira - //peter@philskies.net
//Finalization by Derek Mayer - //mayerderek@hotmail.com
//For Project Airbus A321 0nly
[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