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


[fltsim.0]
title=Airbus A320-214 CFM Sharklets Airbus house colors
sim=pa320-cfm56
sound=
model=cfmshark
texture=airbusshark
atc_airline=AIRBUS
panel=
checklists=
atc_id=F-WWIQ
atc_flight_number=
atc_heavy=0
ui_manufacturer=Airbus
ui_type=A320 CFM Sharklets
ui_variation=Airbus F-WWIQ
visual_damage=1
description=Project Airbus A320-214 with sharklets

[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]
//Cebu Pacific A320-214  RP-C3241 config
      

//Pax Zonings
station_load.0= "7605.9, 21.24, 0.000, 0.000,  CAB OA (60)"  
station_load.1= "7149.6,  -3.33, 0.000, 0.000,  CAB OB (60)"   
station_load.2= "6541.1, -26.34, 0.000, 0.000, CAB OC (59)" 
-ok

//Cargo & Baggage
station_load.3= "2921.1,  22.10, 0.000, 0.000, CPT 1"   //Compartment 1 (7500lbs) 
station_load.4= "3086.5, -11.99, 0.000, 0.000,  CPT 3"   //Compartment 3 (5349lbs) 
station_load.5= "1190.5, -22.67, 0.000, 0.000, CPT 4"   //Compartment 4 (4652lbs) 
station_load.6= "171.96, -33.11, 0.000, 0.000,  CPT 5"   //Compartment 5 (3300lbs) 


//Basic Weight                42637 kgs  |   93998 lb    
//Crew 3/4(1 OBS)=              520 kgs  |    1146 lbs    
//Pantry Wgt Sector- DOM=       570 kgs  |    1257 lbs   
----------------------------------------------------------- 
//Dry Operating Weight/Index= 43727 kgs  |  96401 lbs   56.5
-----------------------------------------------------------
//"weights in kilos"
//ZFWCG/MACZFW= 31.8% / 56.7

empty_weight=96401.4
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=169756
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 PB. (Version 179 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  
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                   


[General]
performance=A320-214\nCFM56-5B4\n\nMZFW: 61,000 kg\nMTOW: 77,000 kg\nMLW: 64,500 kg
atc_type=Airbus
atc_model=A320

//Cebu Pacific weight config

[GeneralEngineData]
engine_type=1
fuel_flow_scalar=1.09  
Engine.0=13.500000,-18.95,-5.125
Engine.1=13.500000,18.95,-5.125
min_throttle_limit=-0.43


[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]
static_pitch=-0.319722
static_cg_height=11.60811023622

point.0=1.0, 38.84,0.0,-11.9619,800,0.0,1.53379,68.0,1.0,1.4390,0.680000, 13.2,12.9,0.000000,252.000000,282.0
point.1=1.0,-3.660,-12.458,-12.22,1200,1.000000,1.680382,0.000000,0.72,1.5419948,0.81,14.000000,13.700000,2.000000,252.000000,282.000000
point.2=1.0,-3.660,12.458,-12.22,1200,2.000000,1.680382,0.000000,0.72,1.5419948,0.80,14.200000,13.300000,2.000000,252.000000,282.000000
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,-71.250000,0.0,0.750,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0
point.6=2.0,51.666667,0.0,-8.166667,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0
gear_system_type=0


[fuel]
Center1=   4.15,   0.0, -4.00, 2179.6, 8.0 
LeftMain=  3.31, -19.6,  1.40, 1829.6, 5.0   //3.45 
LeftAux=  -4.80, -36.4,  2.20,  232.5, 5.0 
RightMain= 3.31,  19.6,  1.40, 1829.6, 5.0   //3.45
RightAux= -4.80,  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=43.22074, -1.73061,4.355627

[Flaps.0]
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=15.000, 
flaps-position.3=20.000, 
flaps-position.4=26.000, 
flaps-position.5=35.000,  
lift_scalar=0.0
drag_scalar=0.0


[flaps.1]     //slats
type=2                                  
span-outboard=0.95                              
extending-time=20                        
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                         
lift_scalar=0.35
drag_scalar=0.45
pitch_scalar=0.3
system_type=1 

[flaps.2] //ailerons
type=2
span-outboard=0.85
extending-time=11.000
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=0.20
drag_scalar=0.32

[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=35.000,  
lift_scalar=0.62  
drag_scalar=1.08

[jet_engine]
thrust_scalar=1.000

[TurbineEngineData]
fuel_flow_gain=0.00197
inlet_area=29.3000
rated_N2_rpm=15183.000000
static_thrust=24370.000000  //do not change! 
afterburner_available=0
reverser_available=1
bypass_ratio=5.40

[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 

[lights]
light.0=4,  44.41,  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=0.11,0.13                        

[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
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
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


[brakes]
toe_brakes_scale=0.544
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]
//-for Project Airbus A320 0nly-