[fltsim.0]
title=Airbus A319-112
sim=A319-2CP6
model=
panel=
sound=
texture=km
kb_checklists=
kb_reference=
atc_id=9H-AEG
atc_id_color=0xffffffff
atc_airline=Air Malta
atc_flight_number=KM100
ui_manufacturer=Airbus
ui_type="A319-100"
ui_variation=Air Malta
description=Air Malta's new A319-112 delivered on the 4th February 2004.
Model by CSI. Repaint by Stephen J Muscat © 2004
atc_parking_types=GATE
atc_parking_codes=USA
[pitot_static]
vertical_speed_time_constant=999
[General]
atc_type=AIRBUS
atc_model=A319
performance=Power Plant: CFM56-5B6\/P\nThrust Rating: 23500 lbs st\n---------------------------------------------------------\nMAUW: 166,990 lbs\nMTOW: 166,490 lbs\nMSLW: 134,480 lbs\nMZFW: 125,565 lbs\nMFTC: 42,238 lbs\n--------------------------------------------------------\nService Ceiling: 39,000 ft\nEcon Cruise Speed: M0.780\nRange: 2,810nm
[WEIGHT_AND_BALANCE]
max_gross_weight = 145300 // (pounds)
empty_weight = 117930 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
;Moments of Inertia
empty_weight_pitch_MOI = 3172439
empty_weight_roll_MOI = 2262183
empty_weight_yaw_MOI = 3337024
empty_weight_coupled_MOI = 0
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 2.07, -18.561, -3.63 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 2.07, 18.561, -3.63 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar =0.719451
min_throttle_limit=-0.179932
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 5 , 2.0
gear_motor = 0, 5 , 2.0
autopilot = 0, 5 , 2.0
avionics_bus = 0, 10, 2.0
avionics = 1, 5 , 2.0
pitot_heat = 0, 2 , 2.0
additional_system = 0, 20, 2.0
marker_beacon = 1, 2 , 2.0
gear_warning = 0, 2 , 2.0
fuel_pump = 0, 5 , 2.0
starter1 = 0, 20, 2.0
light_nav = 0, 5 , 2.0
light_beacon = 0, 5 , 2.0
light_landing = 0, 5 , 2.0
light_taxi = 0, 5 , 2.0
light_strobe = 0, 5 , 2.0
light_panel = 0, 5 , 2.0
//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)
[contact_points]
///////0////////1///////2///////3///////4//5//////6//////7////8////9///10///11///12/13///14///15
Y X Z
point.0=1, 27.81, 0.00, -10.57, 1181.1, 0, 1.255, 55.92, 1.11, 1.1, 0.8, 8.0, 9.0, 0, 0.0, 0.0
point.1=1, -7.36, -13.74, -10.75, 1574.8, 1, 1.989, 0.00, 1.24, 1.1, 0.8, 8.3, 9.3, 2, 0.0, 0.0
point.2=1, -7.36, 13.74, -10.75, 1574.8, 2, 1.989, 0.00, 1.24, 1.1, 0.8, 8.1, 9.1, 3, 0.0, 0.0
point.3=2, -21.90, -55.06, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -21.90, 55.06, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -43.75, 0.00, -0.99, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 39.60, 0.00, 2.64, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
max_number_of_points = 21
static_pitch=-0.62 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=9.742 //feet, altitude of CG when at rest on the ground
gear_system_type=0
[Views]
eyepoint=36.6, -1.81, 5.65 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0] //trailing edge flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 14 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0 // degrees
flaps-position.2 = 17 // degrees
flaps-position.3 = 22 // degrees
flaps-position.4 = 26 // degrees
flaps-position.5 = 32 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 0.8
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.1] //flap fairings
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 14 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 0
flaps-position.2 = 17
flaps-position.3 = 22
flaps-position.4 = 26
flaps-position.5 = 32 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0
drag_scalar = 1.0
pitch_scalar= 0
system_type = 1 //Hydraulic
[flaps.2] //Slats
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 14 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 18
flaps-position.2 = 21
flaps-position.3 = 24
flaps-position.4 = 24
flaps-position.5 = 24 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0
drag_scalar = 0
pitch_scalar= 0
system_type = 1 //Hydraulic
[flaps.3] //flaperon
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 6 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 0
flaps-position.2 = 12
flaps-position.3 = 12
flaps-position.4 = 12
flaps-position.5 = 12 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0
drag_scalar = 0
pitch_scalar= 0
system_type = 1 //Hydraulic
[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
light.0 = 1, 2.847, 0.00, -4.35, csi_a320_beacon ,
light.1 = 1, 0.253, 0.00, 10.1, csi_a320_beacon ,
light.2 = 3, -66.5, 0.00, 6.07, fx_navwhih ,
light.3 = 2, -17.19, -53.95, 4.03, csi_a320_strobe ,
light.4 = 2, -17.19, 53.95, 4.03, csi_a320_strobe ,
light.5 = 3, -16.90, -53.74, 4.03, csi_a320_navred ,
light.6 = 3, -16.90, 53.74, 4.03, csi_a320_navgre ,
light.7 = 2, -66.5, 0.00, 6.07, csi_a320_strobeaft ,
[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
[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
[exits]
number_of_exits = 2
exit_rate.0 = 0.3 ;Percent per second
exit_rate.1 = 0.1 ;Percent per second
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
Center1=0.000000,0.000000,0.000000,2167.400000,0.000000
LeftMain=-3.000000,-19.000000,0.000000,2055.300000,0.000000
RightMain=-3.000000,19.000000,0.000000,2055.300000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0
[TurbineEngineData]
fuel_flow_gain=0.002000
inlet_area=33.000000
rated_N2_rpm=29920.000000
static_thrust=23500.000000
afterburner_available=0
reverser_available=1
[Reference Speeds]
flaps_up_stall_speed=144.000000
full_flaps_stall_speed=115.200000
cruise_speed=455.00
max_indicated_speed=350.000000
max_mach=0.820020
[autopilot]
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=100.000000
pitch_takeoff_ga=15.000000
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=1.800000
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
[airplane_geometry]
wing_area=1317.000000
wing_span=111.250000
wing_root_chord=25.000000
wing_dihedral=6.696167
wing_incidence=0.000000
wing_twist=-0.999756
oswald_efficiency_factor=0.592017
wing_winglets_flag=1
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=337.000000
htail_span=40.833333
htail_pos_lon=-50.000000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=231.000000
vtail_span=17.329166
vtail_sweep=0.000000
vtail_pos_lon=-35.833333
vtail_pos_vert=5.833333
elevator_area=68.000000
aileron_area=29.490000
rudder_area=95.000000
elevator_up_limit=26.000825
elevator_down_limit=26.000825
aileron_up_limit=30.000070
aileron_down_limit=30.000070
rudder_limit=30.000070
elevator_trim_limit=19.996227
spoiler_limit=59.988681
spoilerons_available=1
aileron_to_spoileron_gain=2.000000
min_ailerons_for_spoilerons=9.969466
min_flaps_for_spoilerons=0.000000
[brakes]
toe_brakes_scale=0.548265
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
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
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
