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Virgin A320 von IFDG


Hor1463

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HI! Ich kriege es einfach nicht hin. Ich habe bereits die A320 von Swiss und LH mit dem CFM Triebwerk. Habe den Merge für das PSS Panel und sound durchgeführt. Alles läuft super. Jetzt wollte ich das gleiche für die Virigin mit dem IAE Triebwerk machen, aber der Jet erscheint nicht im Auswahl-Menue des FS. Was mache ich falsch?

 

Gruß Roland

(Vielleicht kann mit jemand seine aircraft.cfg für diesen Typ schicken.

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[fltsim.0]

title=IFDG A320-200 Virgin Atlantic

sim=A320V

model=A320IAE

panel=

sound=

texture=VS

kb_checklists=

kb_reference=

atc_id=

atc_airline=Virgin

atc_flight_number=1123

atc_heavy=0

ui_manufacturer=iFDG Airbus

ui_type=A320-232

ui_variation=Virgin Atlantic

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 The A320-100 was the initial version and was superseded by the A320-200 from the third quarter of 1988.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=0000000000

visual_damage=0

prop_anim_ratio=1.72

 

[General]

atc_type=Airbus

atc_model=A320

editable=0

performance=Engines\nIAE V2500 rated at 25,800 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]

reference_datum_position=0.000000,0.000000,0.000000

max_number_of_stations=50

 

station_load.0 = 0450, 0.0, 0.0, 0.0 //Weight Crew (lbs) LEAVE

station_load.1 = 3000, 0.0, 0.0, 0.0 //Weight Galleys (lbs) LEAVE

station_load.2 = 7000, 0.0, 0.0, 0.0 //Weight Baggage (lbs) Baggage

station_load.3 = 2880, 0.0, 0.0, 0.0 //Weight Cargo (lbs) Cargo

station_load.4 = 0, 0.0, 0.0, 0.0 //Weight Psgr Sect OA (lbs) First

station_load.5 = 27000, 0.0, 0.0, 0.0 //Weight Psgr Sect OB (lbs) Coach

 

empty_weight= 90400

empty_weight_roll_MOI=3900000.000000

empty_weight_pitch_MOI=3000000.000000

empty_weight_yaw_MOI=3000000.000000

empty_weight_coupled_MOI=250.000000

empty_weight_CG_position=0.000000,0.000000,0.000000

max_gross_weight=215775.000000

 

*************************************************

 

 

 

 

[GeneralEngineData]

engine_type=1

Engine.0=3.333333,-17.500000,-2.500000

Engine.1=3.333333,17.500000,-2.500000

fuel_flow_scalar=1.250000

min_throttle_limit=-0.499939

 

[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

 

[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

 

 

[fuel]

Center1=-2.000000,0.000000,0.000000,2174.000000,0.000000

LeftMain=-3.000000,-19.000000,0.000000,2060.000000,0.000000

RightMain=-3.000000,19.000000,0.000000,2060.000000,0.000000

fuel_type=2.000000

number_of_tank_selectors=1

electric_pump=1

 

 

[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=190.000000

full_flaps_stall_speed=152.000000

cruise_speed=552.421072

max_indicated_speed=350.000000

max_mach=0.821240

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=7.998491,0.000000

flaps-position.2=15.996982,0.000000

flaps-position.3=23.995472,0.000000

flaps-position.4=31.993963,0.000000

flaps-position.5=39.992454,0.000000

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=0.002000

inlet_area=22.000000

rated_N2_rpm=29920.000000

static_thrust=25000.000000

afterburner_available=0

reverser_available=1

 

 

[jet_engine]

thrust_scalar=1.0

[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=90.000000

pitch_takeoff_ga=8.000000

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=1.000000

 

 

 

[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

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sim=

 

Wäre dann das *.air File in Deinem Fall A320V.air*

 

Das solltest Du auch noch überprüfen :D

 

Mit freundlichem Gruss

 

Claudio :D

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