[fltsim.0]
title=A320-212 iFDG Finnair
sim=Airbus320-200CFM
model=
panel=
sound=
texture=fin
kb_checklists=
kb_reference=
atc_id=OH-LXI
atc_airline=Finnair
atc_flight_number=1123
atc_heavy=0
ui_manufacturer=iFDG Airbus
ui_type="A320-214"
ui_variation=Finnair
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 The A320-100 was the initial version and was superseded by the A320-200 from the third quarter of 1988.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.
atc_id_color=0000000000
visual_damage=0
prop_anim_ratio=1.72
[General]
atc_type=Airbus
atc_model=A320
editable=0
performance=Engines\nCFM56-5B4 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, 0.0, 0.0
empty_weight_CG_position = -1.45, 0.0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170.0, 41.91, -2.0, 1.64, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170.0, 41.91, 2.0, 1.64, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "11115.0, 18.9, 0.0, 1.64, Front cabin" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "3505.0, 29.17, 0.0, -3.28, Front cargo" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "4000.0, -50.45, 0.0, 3.05, Rear cargo" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "11310.0, -18.49, 0.0, 1.64, Rear cabin" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_roll_MOI = 1725000
empty_weight_pitch_MOI = 2450000
empty_weight_yaw_MOI = 1950000
empty_weight_coupled_MOI = 0
[fuel]
LeftMain = -0.82, -6.16, -0.82, 1829.5, 0.0
RightMain = -0.82, 6.16, -0.82, 1829.5, 0.0
LeftAux = -4.93, -26.7, 0.82, 232.0, 0.0
RightAux = -4.93, 26.7, 0.82, 232.0, 0.0
Center1 = 0.0, 0.0, -4.11, 2180.0, 0.0
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump = 0
[airplane_geometry]
wing_area=1317.5
wing_span=111.25
wing_root_chord=17.67
wing_dihedral=4.499
wing_incidence=-0.784
wing_twist=0.0
oswald_efficiency_factor=0.75
wing_winglets_flag=1
wing_sweep=25.0
wing_pos_apex_lon=16.0
wing_pos_apex_vert=0.0
htail_area=337.0
htail_span=41.67
htail_pos_lon=-50.0
htail_pos_vert=0.0
htail_incidence=0.0
htail_sweep=0.0
vtail_area=249.0
vtail_span=17.992
vtail_sweep=0.0
vtail_pos_lon=-35.83
vtail_pos_vert=5.83
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
spoilerons_available=1
aileron_to_spoileron_gain=1.10
min_ailerons_for_spoilerons=11
min_flaps_for_spoilerons=0
[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 = 21.0
flaps-position.0 = 0.0
flaps-position.1 = 7.0
flaps-position.2 = 14.0
flaps-position.3 = 21.0
flaps-position.4 = 28.0
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 = 18
flaps-position.0 = 0
flaps-position.1 = 0
flaps-position.2 = 5
flaps-position.3 = 10
flaps-position.4 = 10
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 = 1.15
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
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 6.98, -10.7, -2.4 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 6.98, 10.7, -2.4 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.055 //Scalar for fuel flow efficiency
min_throttle_limit = -0.27; //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 29.0
rated_N2_rpm = 29920
static_thrust = 26500
afterburner_available = 0
reverser_available = 1
[jet_engine]
thrust_scalar=1.0
[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 800.0
autothrottle_available = 1
autothrottle_arming_required = 1
autothrottle_takeoff_ga = 1
autothrottle_max_rpm = 100
pitch_takeoff_ga = 8.0
autoland_available = 1
use_no_default_pitch = 1
use_no_default_bank = 1
default_pitch_mode =0
default_bank_mode =0
max_pitch = 10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint = 20000.0
max_pitch_velocity_hi_alt_breakpoint = 28000.0
max_bank = 25.00
max_bank_acceleration = 1.80
max_bank_velocity = 3.00
max_throttle_rate = 0.10
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 = 0.00
[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)
point.0 = 1, 33.85, 0.0, -11.1, 1574.8, 0.0, 1.68, 75.0, 0.41, 2.5, 0.65, 9.0, 9.4, 0.0, 0.0, 0.0
point.1 = 1, -3.80, -12.417, -11.4, 1574.803, 1.0, 1.68, 0.0, 1.0, 2.5, 0.52, 13.0, 11.7, 2.0, 0.0, 0.0
point.2 = 1, -3.80, 12.417, -11.4, 1574.803, 2.0, 1.68, 0.0, 1.0, 2.5, 0.52, 13.1, 11.9, 3.0, 0.0, 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
point.7 = 5, -50.9, -19.25, -19.3, 1600, 0.0, 0.0, 70.0, 0.0, 0.0, 5.0, 3.0, 3.2, 0.0, 0.0, 0.0
point.8 = 5, -50.9, 19.25, -19.3, 1600, 0.0, 0.0, 70.0, 0.0,
static_pitch=0
static_cg_height=10.9
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 0 //Normal
pct_throttle_limit = 0.1 //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=43.22074,-1.723061,4.355627 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
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
[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
[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
[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
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[effects]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=iFDG_A320_touchdown, 1
startup=iFDG_A320_startup
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[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
[stall_warning]
type=2
[smokesystem]
smoke.0 = 0.80052, -18.00157, 43.23110, iFDG_A320_flap
smoke.1 = 0.80052, -18.00157, -43.23110, iFDG_A320_flap
[folding_wings]
wing_fold_system_type=4
fold_rates=0.11,0.13
[TailHook]
tailhook_length=1 ;(feet)
tailhook_position=0, 0, 0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1
