[fltsim.0]
title=A319-112 eurowings
sim=A319PBv4
model=cfm
panel=
sound=
texture=ew
kb_checklists=
kb_reference=
atc_id=D-AKNJ
atc_airline=EUROWINGS
atc_flight_number=EW319
atc_heavy=0
ui_manufacturer=Airbus
ui_type=iFDG A319-100 CFM
ui_variation=eurowings
description=The A319 program was launched at the Paris Airshow in June 1993 on the basis of just six orders placed by ILFC late in 1992 and the predicted better prospects of the commercial airliner market, which were certainly realised. The first A319 airline order came from French carrier Air Inter (since merged into Air France), whose order for six was announced in February 1994. Since then Swissair, Air Canada, Lufthansa, Northwest, United, US Airways and British Airways are among the major customers that have ordered more than 500 A319s. Model by Albaro Villegas and Ric Barker. Master Textures by Ben Jones. \nFlight Dynamics and Eurowings Livery by Peter Beddig
atc_id_color=0000000000
visual_damage=0
prop_anim_ratio=1.72
[General]
atc_type=AIRBUS
atc_model=A319
editable=1
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
guid=e76d55c4c6489c3d60a64b2ef2de549a
[pitot_static]
vertical_speed_time_constant = 1
[weight_and_balance]
max_gross_weight = 142000.000
empty_weight = 88400.000
reference_datum_position = -0.500, 0.000, -1.600
empty_weight_CG_position = -5.000, 0.000, 0.000
max_number_of_stations = 50
station_load.0 =340.000000, 37.700000, 0.000000, 0.000000, Pilots
station_load.1 =510.000000, -5.000000, 0.000000, 0.000000, Stewards
station_load.2 =9180.000000, 12.000000, 0.000000, 0.000000, PAX Row 1-9
station_load.3 =13600.000000, -17.700000, 0.000000, 0.000000, PAX Row 10-22
station_load.4 =1610.000000, 15.600000, 0.000000, -2.000000, Front cargo
station_load.5 =2410.000000, -17.400000, 0.000000, -2.000000, Rear cargo
;Moments of Inertia
empty_weight_pitch_MOI = 3172439.000
empty_weight_roll_MOI = 2262183.000
empty_weight_yaw_MOI = 3337024.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -15.615, -54.50, 4.71, iFDG_A320_rednav
light.1 = 3, -15.388, -54.32, 4.71, iFDG_A320_rednav
light.2 = 3, -15.615, 54.50, 4.71, iFDG_A320_greennav
light.3 = 3, -15.388, 54.32, 4.71, iFDG_A320_greennav
light.4 = 3, -64.30, 0.00, 6.69, iFDG_A320_whitenav
light.5 = 2, -64.30, 0.00, 6.67, iFDG_A320_whitestrobe_tail
light.6 = 2, -15.91, -54.68, 4.75, iFDG_A320_whitestrobe
light.7 = 2, -15.91, 54.68, 4.75, iFDG_A320_whitestrobe
light.8 = 1, 3.57, 0.00, 10.60, iFDG_A320_redbeacon_top
light.9 = 1, 6.881, 0.00, -3.26, iFDG_A320_redbeacon_bottom
light.10 = 3,-56.23, 11.50, 7.46, iFDG_A320_logo
light.11 = 3,-56.23, -11.50, 7.46, iFDG_A320_logo
light.12 = 5, 22.277, 6.463, 3.39, iFDG_A320_inspection
light.13 = 5, 22.277, -6.463, 3.39, iFDG_A320_inspection
//light.14 = 3, -6.0, -14.4, -7.3, iFDG_A320_whitenav
//light.14 = 3, 29.4, -1.2, -7.3, iFDG_A320_whitenav
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
Engine.0 = 9.600, -19.000, -5.400
Engine.1 = 9.600, 19.000, -5.400
fuel_flow_scalar = 0.900
min_throttle_limit = -0.30 //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear
//[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
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -2.000, -20.000, -1.200, 3150.400, 0.000
RightMain = -2.000, 20.000, -1.200, 3150.400, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[contact_points]
point.0= 1.000, 33.400, 0.000, -8.820, 1181.100, 0.000, 1.442, 60.000, 0.500, 0.870, 0.950, 4.000, 4.000, 0.000, 220.000, 250.000
point.1= 1.000, -8.000, -12.500, -9.500, 1574.800, 1.000, 1.875, 0.000, 0.900, 1.500, 0.900, 7.000, 7.000, 2.000, 220.000, 250.000
point.2= 1.000, -8.000, 12.500, -9.500, 1574.800, 2.000, 1.875, 0.000, 0.900, 1.500, 0.900, 7.000, 7.000, 3.000, 220.000, 250.000
point.3= 2.000, -14.170, -47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -14.170, 47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -54.000, 0.000, 2.830, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
max_number_of_points = 11
static_pitch= -0.600
static_cg_height= 10.200
gear_system_type= 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
[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
[airplane_geometry]
wing_area = 1317.500
wing_span = 111.300
wing_root_chord = 17.800
wing_dihedral = 5.600
wing_incidence = 1.000
wing_twist = -0.500
oswald_efficiency_factor= 0.750
wing_winglets_flag = 1
wing_sweep = 25.000
wing_pos_apex_lon = 8.000
wing_pos_apex_vert = -2.000
htail_area = 333.700
htail_span = 40.800
htail_pos_lon = -49.200
htail_pos_vert = 4.200
htail_incidence = 0.000
htail_sweep = 29.000
vtail_area = 231.400
vtail_span = 20.600
vtail_sweep = 34.000
vtail_pos_lon = -44.400
vtail_pos_vert = 8.000
elevator_area = 70.500
aileron_area = 26.900
rudder_area = 56.200
elevator_up_limit = 22.500
elevator_down_limit = 19.500
aileron_up_limit = 20.000
aileron_down_limit = 20.000
rudder_limit = 26.000
elevator_trim_limit = 20.000
spoiler_limit = 60.000
spoilerons_available = 1
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000
[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, 5, 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2, 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, 5 , 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, 5 , 17.0
[Reference Speeds]
flaps_up_stall_speed = 142.000
full_flaps_stall_speed = 113.000
cruise_speed = 477.000
max_mach = 0.82
max_indicated_speed = 340 //Red line (KIAS)
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =1.000
rudder_effectiveness =1.000
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[TurbineEngineData]
fuel_flow_gain = 0.004
inlet_area = 22.600
rated_N2_rpm = 29920.000
static_thrust = 23500.000
afterburner_available = 0
reverser_available = 1.000
[jet_engine]
thrust_scalar =1.000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=200
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8
use_no_default_bank=1
use_no_default_pitch=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=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 33.0 //Flap angle that activates warning at idle
flap_limit_power = 25.0 //Flap angle that activates warning at above id
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.885 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 1 //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)
[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 = 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
[TailHook]
tailhook_length=1 ;(feet)
tailhook_position=0, 0, 0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1
[folding_wings]
wing_fold_system_type=4
fold_rates=0.11,0.13
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 24.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 13.000, 0.000
flaps-position.3= 23.000, 0.000
flaps-position.4= 34.000, 0.000
flaps-position.5= 42.000, 0.000
[Flaps.1]
type= 2
span-outboard= 0.950
extending-time= 8.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 1.000, 0.000
flaps-position.3= 2.000, 0.000
flaps-position.4= 2.000, 0.000
flaps-position.5= 3.000, 0.000
