[fltsim.0]
title=A320-214 Air Malta 9H-ADY
sim=A320-214 AMC 9H-ADY.air
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=9H-ADY
atc_airline=Air Malta
atc_flight_number=AMC100
atc_heavy=0
ui_manufacturer=Airbus
ui_type=A320-214
ui_variation=Air Malta - 9H-ADY
description=Air Malta\nAirbus A320-214\n9H-ADY\n- - - - - - - - - - - - - -\nThe A320 was launched on March 2, 1984. It is the first subsonic commercial aircraft with fly-by-wire controls. First flight took place on February 22, 1987. The A320-100 was the initial version and was superseded by the A320-200 from the third quarter of 1988. The A320-200 differs from the A320-100 in having wingtip fences, a wing center-section fuel tank, and a higher MTOW. Model by iFDG. Textures by André Silva.
atc_id_color=0000000000
visual_damage=0
prop_anim_ratio=1.72

[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]

reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000


station_load.0=310.000, 43.000, 0.000, 0.000 //(crew)
station_load.1=5920.000, 32.000, 0.000, 0.000 //frontmost cabin
station_load.2=3150.000, 25.000, 0.000, 0.000 //front cargo bay
station_load.3=6920.000, 15.000, 0.000, 0.000 //center cabin
station_load.4=4400.000, -15.000, 0.000, 0.000 //rearmost cargo bay
station_load.5=8840.000, -23.000, 0.000, 0.000 //rearmost cabin


//total load=29,540lbs, empty wt. 98,500lbs (29,540+98,500= 128,040lbs/58.2T)
empty_weight=98500.000
empty_weight_roll_MOI=1801400.000000
empty_weight_pitch_MOI=3580000.000000
empty_weight_yaw_MOI=2000000.000000
empty_weight_coupled_MOI=1200.000000
max_gross_weight=170270.099

//aircraft.cfg file by Peter Binamira. Must be used with the PA A320 aircrafts. 07/24/02

[General]
performance=July 24, 2002 revision 008\n\n\n\n
atc_type=aIRBUS
atc_model=A320

[GeneralEngineData]
engine_type=1
fuel_flow_scalar=1.12
Engine.0=10.000000,-18.833333,-3.933333
Engine.1=10.000000,18.833333,-3.933333


[Reference Speeds]
flaps_up_stall_speed=128.000
full_flaps_stall_speed=102.000
cruise_speed=455.020

[autopilot]
autoland_available=0
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=87.00000
pitch_takeoff_ga=8.000000
use_no_default_pitch=1
use_no_default_bank=1

[direction_indicators]
direction_indicator.0=3,0

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

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

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[contact_points]
point.0 = 1, 35.5709, 0, -11.1, 1574.8, 0, 1.68, 75, 1.2, 1.3, 0.4, 9, 9.4, 0, 0, 0
point.1 = 1, -6.4, -12, -11.2, 1574.803, 1, 1.68, 0, 1.2, .80, 0.3, 11.7, 13, 2, 0, 0
point.2 = 1, -6.4, 12, -11.2, 1574.803, 2, 1.68, 0, 1.2, .80, 0.3, 10.2, 12.9, 3, 0, 0
point.3 = 2, -13.75, -54.58,   -0.5,    750.925, 0.0, 0.0,   0.0, 0.0,  0.0, 0.0,    0.0,  0.0, 5.0, 0.0, 0.0
point.4 = 2, -13.75,  54.58,   -0.5,    750.925, 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, -71.25,   0.0,     0.75,   750.925, 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,  51.67,   0.0,    -8.17,   750.925, 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=1
static_pitch=-0.370
static_cg_height=11.230

[fuel]
Center1=0.000, 0.000, -4.000, 2180.0, 8.000
LeftMain=-5.000, -15.000, 0.000, 1829.5, 5.000
RightMain=-5.000, 15.000, 0.000, 1829.5, 5.000
LeftAux=-8.5,  -30.0, -3.0,   232.0, 0.0
RightAux=-8.5,  30.0, -3.0,  232.0, 0.0
fuel_type=2.000000
number_of_tank_selectors=1
fuel_type=2.000000

[keyboard_response]
aileron=180.000000,130.000000

[pitot_static]
vertical_speed_time_constant=1               

[Views]
eyepoint=43.22074,-1.723061,4.355627


[Flaps.0]
type=1
span-outboard=0.800
extending-time=21.000
system_type=1
damaging-speed=233.000
blowout-speed=250.000
flaps-position.0=0.000,
flaps-position.1=7.000,
flaps-position.2=14.000,
flaps-position.3=21.000,
flaps-position.4=28.000,
flaps-position.5=35.000,
lift_scalar=0.85
drag_scalar=0.8
pitch_scalar=7.0

[flaps.1]     
type=2                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=18                                  // seconds
flaps-position.0=0   
flaps-position.1=0,
flaps-position.2=5, 
flaps-position.3=10, 
flaps-position.4=10,  
flaps-position.5=27,                                    
blowout-speed=260                               // KIAS
lift_scalar=0.4
drag_scalar=0.3
system_type=1 

[jet_engine]
thrust_scalar=1.000

[GROUND_REACTION]
MAX_STEERING_ANGLE=75

[TurbineEngineData]
fuel_flow_gain=0.002380
inlet_area=31.000000
rated_N2_rpm=29920.000000
static_thrust=26500.000000
afterburner_available=0
reverser_available=1

[exits]
number_of_exits=2
exit_rate.0=0.2                               ;Percent per second
exit_rate.1=0.08                             ;Percent per second

[airplane_geometry]
wing_area=1320.000000
wing_span=111.833333
wing_root_chord=16.666667
wing_dihedral=4.498901
wing_incidence=-0.783823
wing_twist=0.000000
oswald_efficiency_factor=0.650
wing_winglets_flag=1
wing_sweep=25.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=337.000000
htail_span=41.666667
htail_pos_lon=-50.000000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=249.000000
vtail_span=17.991665
vtail_sweep=0.000000
vtail_pos_lon=-35.833333
vtail_pos_vert=5.833333
elevator_area=70.500000
aileron_area=26.800000
rudder_area=56.200000
elevator_up_limit=28.0
elevator_down_limit=20.0
aileron_up_limit=26.0
aileron_down_limit=26.0
rudder_limit=25.0
elevator_trim_limit=18.5
spoiler_limit=35.0
spoilerons_available=1          
aileron_to_spoileron_gain=1.10        
min_ailerons_for_spoilerons=11             
min_flaps_for_spoilerons=0                   

[flight_tuning]
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=0.95
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.2
aileron_trim_effectiveness=0.9
rudder_trim_effectiveness=1.1

[lights]
light.0 = 3, -16.115, -54.50, 3.11, iFDG_A320_rednav
light.1 = 3, -15.888, -54.32, 3.11, iFDG_A320_rednav
light.2 = 3, -16.115, 54.50, 3.11, iFDG_A320_greennav
light.3 = 3, -15.888, 54.32, 3.11, iFDG_A320_greennav
light.4 = 3, -72.16, 0, 5.08, iFDG_A320_whitenav
light.5 = 2, -72.18, 0, 5.08, iFDG_A320_whitestrobe_tail
light.6 = 2, -16.41, -54.68, 3.13, iFDG_A320_whitestrobe
light.7 = 2, -16.41, 54.68, 3.13, iFDG_A320_whitestrobe
light.8 = 2, -16.41, -54.68, 3.17, iFDG_A320_whitestrobe
light.9 = 2, -16.41, 54.68, 3.17, iFDG_A320_whitestrobe
light.10 = 1, 3.070, 0, 9.00, iFDG_A320_redbeacon_top
light.11 = 1, 6.381, 0, -4.862, iFDG_A320_redbeacon_top
light.12 = 5, -64.257, 11.41, 5.866, iFDG_A320_logo
light.13 = 5, -64.257, -11.41, 5.866, iFDG_A320_logo

[ground_reaction]
main_gear_static_compression=1.5	// (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=0.9            // (feet), The distance the center gear strut is compressed when at rest on the ground

[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

[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


[fltsim.1]
title=A320 Sound
sim=A320-214  9H-ADY.air
model=
panel=
sound=sound_
texture=
kb_checklists=
kb_reference=
atc_id=OO-TCH
atc_airline=Air Malta
atc_flight_number=FQ100
atc_heavy=0
ui_manufacturer=Airbus
ui_type=A320-214
ui_variation=sons teste
description=Airbus A320-200 by Project Airbus. Flight dynamics by Peter Binamira. www.the-wu.org\/projectairbus
atc_id_color=0000000000
visual_damage=0
prop_anim_ratio=1.72
[FSHS_AIBLAST]
OldName=Airbus
NewName=aIRBUS