[fltsim.0]
title=Airbus A319-110 Swiss International Air Lines
ui_variation=Swiss International Air Lines
sim=pa319-cfm56
model=cfm
panel=
sound=
texture=lx
checklists=
description=Project Airbus A319. Visual model by Andy Warden and Derek Mayer. Base textures by Demetris Themistocleous and Alessandro Savarese. Flight model & Sounds by Peter Binamira. Copyright Project Airbus 2008.\n\n\n\n\n\n
atc_id=HB-IPY
atc_airline=Swiss
atc_flight_number=451
ui_manufacturer=Project Airbus
ui_type=A319-110
visual_damage=1
atc_heavy=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









[WEIGHT_AND_BALANCE]
//A319-112 config 

//Pax Zonings
station_load.0= "5705.3, 17.24, 0.000, 0.000,  CAB OA (47)"  
station_load.1= "5808.6,  -3.33, 0.000, 0.000,  CAB OB (47)"   
station_load.2= "5003.1, -20.34, 0.000, 0.000, CAB OC (46)" 


//Cargo & Baggage
station_load.3= "2021.1,  19.17, 0.000, -3.000, CPT 1"   //Compartment 1 (5000lbs)   16.13
station_load.4= "2086.5, -14.13, 0.000, -3.000, CPT 4"   //Compartment 4 (6660lbs)  -16.34
station_load.5= "800.5, -24.85, 0.000, -2.000,  CPT 5"   //Compartment 5 (3300lbs) -31.19


//Basic Weight/Index=       39657 kgs  |              48.5
//Crew 2/4      Cockpit       160 kgs  |              -1.9
//              Cabin         280 kgs  |               0.2
//Pantry   - REGIONAL         612 kgs  |              -0.5
//Dry Operating Weight=     40709 kgs  |              46.3
----------------------------------------------------------- 
//DOW/DOI=                  40709 kgs  |  89748 lbs   46.3
-----------------------------------------------------------

empty_weight=89748.0
empty_weight_roll_MOI=931400.000000
empty_weight_pitch_MOI=1100000.000000
empty_weight_yaw_MOI=1000000.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=166756
reference_datum_position=0.0000,0.000000,0.000000
empty_weight_CG_position=0.69,0.000000,0.000000
CG_forward_limit=0.17
CG_aft_limit=0.37


//Weight & Balance prepared by PB. (Version 150 Y)



[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  //.76
wing_winglets_flag=1
wing_sweep=25.0000
wing_pos_apex_lon=16.102  //17.655  //15.982 //13.3
wing_pos_apex_vert=0.90000
htail_area=333.681
htail_span=41.666667
htail_pos_lon=-50.703
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=-48.865
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=35.0
spoilerons_available=1          
aileron_to_spoileron_gain=1.5        
min_ailerons_for_spoilerons=12             
min_flaps_for_spoilerons=0                   


[General]
performance=A319-112\nCFM56-5B6\n\nMZFW: 58,500 KG\nMTOW: 68,000 KG\nMLW: 62,500 KG\n
atc_type=Airbus
atc_model=A319

[GeneralEngineData]
engine_type=1
fuel_flow_scalar=1.00  //CRZ SFC 1.09
Engine.0=6.500000,-18.95,-5.125
Engine.1=6.500000,18.95,-5.125
min_throttle_limit=-0.499939  //-0.4


[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=0.825



[autopilot]
autopilot_available=1
flight_director_available=1 
default_vertical_speed=0 
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=			92.5
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  //2.00
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=			0.20
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 //11.0
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_tchdwn320, 1

[RADIOS]
// Radio Type=avail?,sby freq?,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= 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)

static_pitch=-0.319722
static_cg_height=11.60811023622

point.0=1.0, 32.83, 0.0000,-11.72, 800,0.0,1.5,68.0,0.70,1.4390000,0.68,13.200000,12.900000,0.000000,252.000000,282.000000
point.1=1.0,-4.160,-12.458,-12.22,1200,1.0,1.9,0.00,0.72,1.5419948,0.81,14.000000,13.700000,2.000000,252.000000,282.000000
point.2=1.0,-4.160, 12.458,-12.22,1200,2.0,1.9,0.00,0.72,1.5419948,0.80,14.200000,13.300000,3.000000,252.000000,282.000000
point.3=2.0,-13.750000,-54.583333,-0.500000,750.924659,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.0,-13.750000,54.583333,-0.500000,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0
point.5=2.0,-63.250000,0.0,4.050,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0
point.6=2.0,46.666667,0.0,-4.166667,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0
point.7=5.0,-3.000, 0,0000,0.0000, 1600, 0, 0.00, 50.0, 0.0,  0.0, 1.00, 0.2, 0.2, 0, 0.0, 0.0
gear_system_type=0


[fuel]
Center1=   1.95,   0.0, -4.00, 2179.6, 8.0 

LeftMain=  2.35, -19.6,  1.40, 1829.6, 5.0   //3.45 
RightMain= 2.35,  19.6,  1.40, 1829.6, 5.0   //3.45

LeftAux=  -5.50, -36.4,  2.20,  232.5, 5.0 
RightAux= -5.50,  36.4,  2.20,  232.5, 5.0

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               

[Views]
eyepoint=41.22074, -1.73061,4.155627


[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=13.0
flaps-position.3=20.0
flaps-position.4=29.0 
flaps-position.5=40.0 

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=15.000, 
flaps-position.4=20.000, 
flaps-position.5=40.000,  
lift_scalar=0.66  //1.178
drag_scalar=0.75

[jet_engine]
thrust_scalar=1.000

[TurbineEngineData]  
fuel_flow_gain=0.0018  //0.00194
inlet_area=21.3000
rated_N2_rpm=15183.000000
static_thrust=21630.000000  //MCT CFM56-5B6 21630 5B5 20250 Underpower 24570
afterburner_available=0
reverser_available=1
bypass_ratio=5.90

[exits]
number_of_exits=2
exit_rate.0=0.19                             ;Percent per second
exit_rate.1=0.17                             ;Percent per second


[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 //36
parasite_drag_scalar=1.0
induced_drag_scalar=0.98


[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//light.0=3, -14.00, -54.9,  2.45, fx_navred320pa ,
//light.1=3, -14.00,  54.9,  2.45, fx_navgre320pa ,
light.2=3, -62.00, 0.00, 4.70, fx_navwhi320pa ,
light.3=2, -62.10,   0.00,  4.70, fx_strobe2320pa ,
//light.4=2, -14.22, -54.91,  2.45, fx_strobe320pa ,
//light.5=2, -14.22,  54.91,  2.45, fx_strobe320pa ,
light.6=1,   6.8,   0.00, -5.80, fx_beacon320pa ,
light.7=1,   3.83,   0.00,  8.47, fx_beacon320pa ,
light.8=4,  40.41,   0.00,  4.00, fx_vclight ,


[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                               ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.9

[folding_wings]
wing_fold_system_type=4                    
fold_rates=0.11,0.13                         ;Percent per second

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 200
electric_always_available = 1
flap_motor         = 0, 0 , 17.0
gear_motor         = 0, 0 , 17.0
autopilot          = 0, 0 , 17.0
avionics_bus       = 0, 0 , 17.0
avionics           = 0, 0 , 17.0
pitot_heat         = 0, 0 , 17.0
additional_system  = 0, 0 , 17.0
marker_beacon      = 0, 0 , 17.0
gear_warning       = 0, 0 , 17.0
fuel_pump          = 0, 0 , 17.0
starter1           = 0, 0 , 17.0
starter2           = 0, 0 , 17.0
light_nav          = 0, 0 , 17.0
light_beacon       = 0, 0 , 17.0
light_landing      = 0, 0 , 17.0
light_taxi         = 0, 0 , 17.0
light_strobe       = 0, 0 , 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 //0.59
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

//FDE copyright Peter Binamira - //[email protected]
//Finalization by Derek Mayer - //[email protected]
//-For Project Airbus A319 0nly-