[fltsim.0]
title=A320-200 Armavia
sim=Airbus320-200CFM
model=
panel=
sound=
texture=Arm
kb_checklists=
kb_reference=
atc_id=EK32008
atc_airline=ARMAVIA
atc_flight_number=568
atc_heavy=0
ui_manufacturer=Airbus
ui_type="A320-200"
ui_variation=Armavia
description="The 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 The A320-100 was the initial version and was superseded by the A320-200 from the third quarter of 1988.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 Albaro Villegas and Ric Barker. Master Textures by Ben Jones. FDE by Pedro Oliveira. Textures by ....."
atc_id_color=0xffffffff
visual_damage=0
prop_anim_ratio=1.72  

[fltsim.1]
title=A320-200 Aeroflot
sim=Airbus320-200CFM
model=
panel=
sound=
texture=Aer
kb_checklists=
kb_reference=
atc_id=EK32009
atc_airline=Aeroflot
atc_flight_number=569
atc_heavy=0
ui_manufacturer=Airbus
ui_type="A320-200"
ui_variation=Aeroflot
description="The 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 The A320-100 was the initial version and was superseded by the A320-200 from the third quarter of 1988.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 Albaro Villegas and Ric Barker. Master Textures by Ben Jones. FDE by Pedro Oliveira. Textures by ....."
atc_id_color=0xffffffff
visual_damage=0


[General]
atc_type=Airbus 
atc_model=A320 
editable=0 
performance=Engines\nCFM-56 5B rated at 26,500 lbs\n\nTypical Cruise Speed\n0.78 Mach at 35,000 ft\n\nMax Speed\nVmo 350 kts    Mmo 0.82 Mach\n\nRange(150 pax)\n2,900 nm (5,374 km)\n\nMax Fuel\n42,230 lbs (6,303 US gal)\n\nMax Takeoff Weight\n162,040 lbs\n\nMax Gross Weight (taxi weight)\n162,900 lbs\n\nMax Payload\n42,370 lbs 

[pitot_static]
vertical_speed_time_constant = 1

[weight_and_balance]
max_gross_weight = 162900
empty_weight = 90400
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -1.45, 0, 0
empty_weight_pitch_MOI = 2550000
empty_weight_roll_MOI = 1725000
empty_weight_yaw_MOI = 3950000
empty_weight_coupled_MOI = 0
max_number_of_stations = 6

station_load.0 = "170.0,   41.91,  -2.0, 1.64, Pilot"
station_load.1 = "170.0,   41.91,  2.0, 1.64, Co-Pilot"
station_load.2 = "11115.0,  18.9,  0.0, 1.64, Front cabin"
station_load.3 = "3505.0,  29.17,  0.0, -3.28, Front cargo"
station_load.4 = "4000.0, -50.45,  0.0, 3.05, Rear cargo"
station_load.5 = "11310.0, -18.49,  0.0, 1.64, Rear cabin"


[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

//Navigation 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

//Tail Lights
light.4 = 3, -72.16, 0, 5.08, iFDG_A320_whitenav
light.5 = 2, -72.18, 0, 5.08, iFDG_A320_whitestrobe_tail

//Wing strobes
light.6 = 2, -16.41, -54.68, 3.15, iFDG_A320_whitestrobe
light.7 = 2, -16.41, 54.68, 3.15, iFDG_A320_whitestrobe

//Beacon lights
light.8 = 1, 3.070, 0, 9.00, iFDG_A320_redbeacon_top
light.9 = 1, 6.381, 0, -4.862, iFDG_A320_redbeacon_bottom

//Logo lights
light.10 = 5, -64.257, 11.41, 5.866, iFDG_A320_logo
light.11 = 5, -64.257, -11.41, 5.866, iFDG_A320_logo

//Inspection lights
light.12 = 5, 21.777, 6.463, 1.791, iFDG_A320_inspection
light.13 = 5, 21.777, -6.463, 1.791, iFDG_A320_inspection


[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.055
engine.0 = 4, -19.04, -4.81,
engine.1 = 4, 19.04, -4.81,
min_throttle_limit=-0.269958

[smokesystem]
smoke.0 = 0.80052, -18.00157, 43.23110, iFDG_A320_flap
smoke.1 = 0.80052, -18.00157, -43.23110, iFDG_A320_flap


[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = iFDG_A320_touchdown, 1
startup = iFDG_A320_startup

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1

Center1 = 0, 0, -4.11, 2180, 0
LeftMain = -0.82, -6.16, -0.82, 1829.5, 0
LeftAux = -4.93, -26.7, 0.82, 232, 0
RightMain = -0.82, 6.16, -0.82, 1829.5, 0
RightAux = -4.93, 26.7, 0.82, 232, 0
electric_pump=0


[contact_points]
static_pitch = 0
static_cg_height = 10.9
max_number_of_points = 7

point.0 = 1, 35.5709, 0, -11.1, 1574.8, 0, 1.68, 75, 0.9, 1.167, 0.4, 9, 9.4, 0, 0, 0
point.1 = 1, -6.4, -12, -11.2, 1574.803, 1, 1.68, 0, 1.2, 1.16, 0.3, 11.7, 13, 2, 0, 0
point.2 = 1, -6.4, 12, -11.2, 1574.803, 2, 1.68, 0, 1.2, 1.16, 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


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[airplane_geometry]
wing_area = 1320.000000
wing_span = 111.25
wing_root_chord = 17.67
wing_dihedral = 5.11
wing_incidence = -0.784
wing_twist = 0
oswald_efficiency_factor = 0.75
wing_winglets_flag = 1
wing_sweep = 25.0
wing_pos_apex_lon = 7.2
wing_pos_apex_vert = -1.65
htail_area = 337.0
htail_span = 41.67
htail_pos_lon = -59
htail_pos_vert = 4.4
htail_incidence = -1
htail_sweep = 22
vtail_area = 249.0
vtail_span = 20
vtail_sweep = 35
vtail_pos_lon = -51
vtail_pos_vert = 8.75
elevator_area = 70.5
aileron_area = 26.8
rudder_area = 56.2
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
aileron_to_spoileron_gain = 1
min_ailerons_for_spoilerons = 10
min_flaps_for_spoilerons = 0
spoilerons_available = 1

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 0, 17
avionics = 1, 0, 17
pitot_heat = 0, 2, 17
additional_system = 0, 0, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 0, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 0, 17

[Reference Speeds]
flaps_up_stall_speed=128.0 
full_flaps_stall_speed=102.0 
cruise_speed=455.0 
max_mach                 = 0.82
max_indicated_speed      = 350.0

[Flaps.0]
type=1
span-outboard         = 0.8
extending-time        = 14
flaps-position.0      = 0.0
flaps-position.1      = 5.0
flaps-position.2      = 10.0
flaps-position.3      = 15.0
flaps-position.4      = 20.0
flaps-position.5      = 35.0
damaging-speed        = 233.0
blowout-speed         = 250.0
lift_scalar           = 0.85
drag_scalar           = 0.8
pitch_scalar          = 1.1
system_type           = 1                   //Hydraulic

[flaps.1]     
type=2                                      // 1 - tail, 2 - lead
span-outboard         = 0.8
extending-time        = 4
flaps-position.0      = 0
flaps-position.1      = 18
flaps-position.2      = 27
flaps-position.3      = 27
flaps-position.4      = 27
flaps-position.5      = 27
damaging-speed        = 260
blowout-speed         = 270
lift_scalar           = 0.4
drag_scalar           = 0.3
pitch_scalar          = 1.2
system_type           = 1                   //Hydraulic

[flight_tuning]
cruise_lift_scalar=1.0 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=1.0 
aileron_effectiveness=1.0 
rudder_effectiveness=1.0 
pitch_stability=1.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 

[TurbineEngineData]
fuel_flow_gain=0.002 
inlet_area=29.0 
rated_N2_rpm=29920 
static_thrust=26550 
afterburner_available=0 
reverser_available=1 

[jet_engine]
thrust_scalar=1.0 

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=700.000000 
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=113.000000
pitch_takeoff_ga=10.000000 
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=1.8
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control              = 9.00
nav_integrator_control                = 0.25
nav_derivative_control                = 0.00
nav_integrator_boundary               = 2.50
nav_derivative_boundary               = 0.00
gs_proportional_control               = 9.52
gs_integrator_control                 = 0.26
gs_derivative_control                 = 0.00
gs_integrator_boundary                = 0.70
gs_derivative_boundary                = 0.00
yaw_damper_gain                       = 1.00


[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.125     //Percent throttle that activates warning
flap_limit_idle    =  5.0     //Flap angle that activates warning at idle
flap_limit_power   = 25.5     //Flap angle that activates warning at above idle
[brakes]
toe_brakes_scale=0.66
parking_brake=1
[hydraulic_system]
normal_pressure=3000.0    //PSI
electric_pumps=0          //no electric pumps
engine_map=1,1,0,0        //pumps on Eng1,2

[Views]
eyepoint=43.72074,-1.723061,4.355627              ; Longitude, Latitude and Vertical position from Reference Point, (FEET)

[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]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2 
attitude_indicator.1 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[exits]
number_of_exits = 2
exit_rate.0 = 0.4                       ;Percent per second
exit_rate.1 = 0.4                       ;Percent per second

[stall_warning]
type=2
[folding_wings]
wing_fold_system_type=4
fold_rates=0.11,0.13
[Views]
eyepoint=43.22074,-1.723061,4.355627 ///(feet) longitudinal, lateral, vertical distance from reference datum3
[exits]
number_of_exits = 2
exit_rate.0 = 0.2                               ;Percent per second
exit_rate.1 = 0.2                               ;Percent per second

[TailHook]
tailhook_length=1                               ;(feet)
tailhook_position=0, 0, 0          ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1