[fltsim.0]
title=A300-600 INTER  
sim=A300-601
model=
panel=
sound=
texture=
kb_checklists=
description=Airbus A300-600\nOriginal Model: Jaefree Lin\nProject RABBIT FS2002  V.3.\nMario Coelho (www.bluestarsim.cjb.net\nFrom specifications of an A300-600 of Korean Air.
ui_manufacturer=Airbus
ui_type=A300-600
ui_variation=EA TransAfrica
atc_heavy=1
atc_id=C9-DIU
atc_type=Airbus
atc_model=A300-600
atc_airline=INTER
atc_flight_number=313
ui_manufacturer=Airbus

[Radios]   // *** These tunings do depend on the panel you use !
Audio.1=1
Com.1=1, 0
// Com.2=1, 1
// Nav.1=1, 1, 1
// Nav.2=1, 1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 1
Adf.1=1
Transponder.1=1
Marker.1=1

[General]
performance=May 2002, stdizier@irit.fr \nBy Patrick Saint-Dizier.\n
atc_type=AIRBUS
atc_model=A306

[jet_engine]
thrust_scalar=1.000
[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=0.981
roll_stability=1.4  // Keyboard =0.980
yaw_stability=1.4 // keyboard = 0.980
parasite_drag_scalar=1.180
induced_drag_scalar=1.180
elevator_effectiveness=1.001
aileron_effectiveness=2.501
rudder_effectiveness=2.501


[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_bank=1   
use_no_default_pitch=0   



[fuel]
Center1=0.000000,0.000000,0.000000,12060.000000,0.000000
LeftMain=0.000000,0.000000,0.000000,4050.000000,0.000000
RightMain=0.000000,0.000000,0.000000,4050.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1



[Reference Speeds]
flaps_up_stall_speed=135.000000
full_flaps_stall_speed=108.000000
cruise_speed=341.709057
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=76.638369,0.000000,2.921998


[SMOKESYSTEM]
smoke.0=-39.00,-7.00,52.00, fx_oldjetsmoke             
smoke.1=-36.00,-4.00,34.00, fx_oldjetsmoke
smoke.2=-36.00,-4.00, -34.00, fx_oldjetsmoke
smoke.3=-39.00,-7.00, -52.00, fx_oldjetsmoke

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second


[direction_indicators]
direction_indicator.0=3,0
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=236000.000000
empty_weight_roll_MOI=13680000.000000
empty_weight_pitch_MOI=32880000.000000
empty_weight_yaw_MOI=21990000.000000
empty_weight_coupled_MOI=1000.000000
[airplane_geometry]
wing_area=3781.000000
wing_span=165.000000
wing_root_chord=22.916667
wing_dihedral=3.598022
wing_incidence=0.000000
wing_twist=-0.999756
oswald_efficiency_factor=6.569469
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=853.000000
htail_span=53.333333
htail_pos_lon=-87.500000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=514.000000
vtail_span=25.849565
vtail_sweep=0.000000
vtail_pos_lon=-74.666667
vtail_pos_vert=5.833333
elevator_area=188.250000
aileron_area=112.000000
rudder_area=82.280000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
[contact_points]
point.0=1.000000,56.416667,0.000000,-15.250000,1574.803150,0.000000,3.072423,70.620000,0.535318,2.500000,0.484528,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1.000000,-10.666667,-16.916667,-15.416667,1574.803150,1.000000,3.072423,0.000000,0.535319,2.500000,0.484535,5.000000,5.000000,2.000000,0.000000,0.000000
point.2=1.000000,-10.666667,16.916667,-15.416667,1574.803150,2.000000,3.072423,0.000000,0.535319,2.500000,0.484535,5.000000,5.000000,3.000000,0.000000,0.000000
point.3=2.000000,-28.083333,-74.083333,2.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-28.083333,74.083333,2.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-79.666667,0.000000,1.333333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,56.416667,0.000000,1.333333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=-0.137329
static_cg_height=15.197946
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=9.998114,0.000000
flaps-position.2=19.996227,0.000000
flaps-position.3=29.994341,0.000000
flaps-position.4=39.992454,0.000000
[GeneralEngineData]
engine_type=1
Engine.0=-6.416667,-26.000000,-7.083333
Engine.1=-6.416667,26.000000,-7.083333
fuel_flow_scalar=1.000000
[TurbineEngineData]
fuel_flow_gain=0.001975
inlet_area=65.529840
rated_N2_rpm=29920.000000
static_thrust=54608.200000
afterburner_available=0
reverser_available=1