//iFDG A320-214 updated to V1.4 and optimized to FSx by Franco Baratti
[fltsim.0]
title=A320-214 Airone CFM
sim=A320-200CFM
model=
panel=
sound=
texture=Airone
kb_checklists=
kb_reference=
atc_id=
atc_airline=
atc_flight_number=1123
atc_heavy=0
ui_manufacturer=iFDG Airbus
ui_type="A320-214"
ui_variation=Airone
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 The A320-100 was the initial version and was superseded by the A320-200 from the third quarter of 1988.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 Franco Baratti"
atc_id_color=0000000000
visual_damage=0
prop_anim_ratio=1.72
[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
Category=airplane
[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
min_throttle_limit=-0.269958
[Reference Speeds]
flaps_up_stall_speed=128.000
full_flaps_stall_speed=102.000
cruise_speed=455.020
max_indicated_speed=350.000000
max_mach=0.820020
[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
default_pitch_mode=0
default_bank_mode=0
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=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000
[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]
//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, -10.8, 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, -11.45, 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, -11.45, 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
[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
electric_pump=0
[keyboard_response]
aileron=180.000000,130.000000
[pitot_static]
vertical_speed_time_constant=1
pitot_heat=1.000000
[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=3
exit.0=0.2, 35.00, -6.0, 7.0, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.1=0.2, -25.00, 5.85, -3.0, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.2=0.2, 35.00, 6.0, 7.0, 2
[airplane_geometry]
fly_by_wire=1
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
auto_spoiler_available=1
spoiler_extension_time=1.200000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
[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]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//Tail Lights
light.0 = 3, -72.26, 0, 5.08, iFDG_A320_whitenav
light.1 = 2, -72.26, 0, 5.08, iFDG_A320_whitestrobe_tail
//Wing strobes
light.2 = 2, -17.00, -55.44, 4.41, iFDG_A320_whitestrobe
light.3 = 2, -17.00, 55.44, 4.41, iFDG_A320_whitestrobe
//Beacon lights
light.4 = 1, 3.070, 0, 9.00, iFDG_A320_redbeacon_top
light.5 = 1, 6.381, 0, -4.862, iFDG_A320_redbeacon_bottom
//Logo lights
light.6 = 5, -64.257, 11.41, 5.866, iFDG_A320_logo
light.7 = 5, -64.257, -11.41, 5.866, iFDG_A320_logo
//Inspection lights
light.8 = 5, 21.777, 6.463, 1.791, iFDG_A320_inspection
light.9 = 5, 21.777, -6.463, 1.791, iFDG_A320_inspection
[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
[brakes]
toe_brakes_scale=0.503555
parking_brake=1
auto_brakes=4
[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
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[altimeters]
altimeter.0=1
altimeter.1=1
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0
