[fltsim.0]
title=Airbus A300-600R Olympic
sim=a306Rge
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Airbus
ui_type=A300-600R
ui_variation=CRUZEIRO
description=Project Airbus A300-600R Cruzeiro. p Model by Thomas Ruth, Textures by Paulo Christofani (c) 2002
atc_heavy=1
atc_id=PPCLB
atc_airline=Varig
atc_flight_number=293

[forcefeedback]
stick_shaker_magnitude=3000
stick_shaker_direction=0
stick_shaker_period=111111
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=1600
ground_bumps_angle1=8900
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=400
ground_bumps_angle2=9100
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

[jet_engine]
thrust_scalar=1.131

[flight_tuning]
pitch_stability=0.751
roll_stability=0.920
yaw_stability=0.820
elevator_effectiveness=1.401
aileron_effectiveness=2.101
rudder_effectiveness=2.701

[WEIGHT_AND_BALANCE]
empty_weight=196025.000

reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000


station_load.0=420.000, 41.000, 0.000, 0.000
station_load.1=4000.000, 19.000, 0.000, 0.000
station_load.2=8000.000, 28.000, 0.000, 0.000
station_load.3=18000.000, 3.000, 0.000, 0.000
station_load.4=8000.000, -40.000, 0.000, 0.000
station_load.5=6340.000, 25.000, 0.000, 0.000
station_load.6=9220.000, 30.000, 0.000, 0.000
station_load.7=14480.000, 18.000, 0.000, 0.000
station_load.8=13480.000, -83.000, 0.000, 0.000


//total load=81,940lbs + ZFW 196,025= 277,965lbs or 126,348kgs
empty_weight_roll_MOI=9080000.000
empty_weight_pitch_MOI=13280000.000
empty_weight_yaw_MOI=9500000.000
empty_weight_coupled_MOI=650000.000
max_gross_weight=437277.595
CG_forward_limit=0.000
CG_aft_limit=1.000


[electrical]

max_battery_voltage=28.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=40.0
avionics_bus=0, 0, 1
avionics=1, 0, 1
starter1=0, 0, 1
starter2=0, 0, 1
fuel_transfer_pump=0, 0, 1
flap_motor=0, 0, 1
gear_motor=0, 0, 1
autopilot=0, 0, 1
pitot_heat=0, 0, 1
additional_system=0, 0, 1
marker_beacon=1, 0, 1
gear_warning=0, 0, 1
fuel_pump=0, 0, 1
light_nav=0, 0, 1
light_beacon=0, 1, 1
light_landing=0, 0, 1
light_taxi=0, 0, 1
light_strobe=0, 1, 1
light_panel=0, 0, 1
auto_brake=0, 0, 1
standby_vacuum=0, 0, 1
hydraulic_pump=0, 0, 1
light_recognition=0, 0, 1
light_wing=0, 0, 1
light_logo=0, 0, 1

//aircraft.cfg file by Peter Binamira. Must be used with the PA A300-600R aircrafts. 09/30/01
//PA A300-600R .air files won't be optimized without this aircraft.cfg file.

[General]
performance=Max cruising speed: 897km\/h \nRange at typical airline operating weight: 7540km (4070nm) with GE CF6-80C2A1.\nDimensions: Wing span 44.84m (147ft 1in), length 54.08m (177ft 5in), height 16.62m (54ft 6.5in).\n
atc_type=AIRBUS
atc_model=A306

[fuel]
Center1=0.000, 0.000, -4.000, 5232.000, 3.000
LeftMain=-7.000, -30.000, 0.000, 9273.000, 3.000
RightMain=-7.000, 30.000, 0.000, 9273.000, 3.000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=2700.000
wing_span=147.000
wing_root_chord=19.083
wing_dihedral=3.598
wing_incidence=0.758
wing_twist=2.296
oswald_efficiency_factor=0.869
wing_winglets_flag=65281
wing_sweep=0.000
wing_pos_apex_lon=0.000
wing_pos_apex_vert=0.000
htail_area=748.000
htail_span=53.333
htail_pos_lon=-84.000
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=0.000
vtail_area=487.000
vtail_span=25.161
vtail_sweep=0.000
vtail_pos_lon=-81.667
vtail_pos_vert=28.250
elevator_area=69.000
aileron_area=44.240
rudder_area=69.700
elevator_up_limit=27.502
elevator_down_limit=20.626
aileron_up_limit=19.481
aileron_down_limit=14.897
rudder_limit=23.491
elevator_trim_limit=19.481
spoiler_limit=59.989
spoilerons_available=0
aileron_to_spoileron_gain=0.140
min_ailerons_for_spoilerons=9.969
min_flaps_for_spoilerons=0.000

[contact_points]
point.0=1.000, 52.750, 0.000, -13.833, 1574.803, 0.000, 3.531, 67.980, 0.571, 2.500, 0.912, 13.000, 13.000, 0.000, 0.000, 0.000
point.1=1.000, -9.750, -16.250, -15.333, 1574.803, 1.000, 3.531, 0.000, 2.043, 2.500, 1.273, 14.600, 14.600, 2.000, 0.000, 0.000
point.2=1.000, -9.750, 16.250, -15.333, 1574.803, 2.000, 3.531, 0.000, 2.043, 2.500, 1.273, 15.000, 15.000, 3.000, 0.000, 0.000
point.3=2.000, -28.083, -74.083, 2.583, 1574.803, 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, -28.083, 74.083, 2.583, 1574.803, 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, -79.667, 0.000, 1.333, 1574.803, 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, 56.417, 0.000, 1.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=-0.912
static_cg_height=13.546

[GeneralEngineData]
engine_type=1
Engine.0=8.583, -11.500, -3.167
Engine.1=8.583, 11.500, -3.167
fuel_flow_scalar=1.000

[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=96.000
rated_N2_rpm=30150.000
static_thrust=49000.000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=145.000
full_flaps_stall_speed=116.000
cruise_speed=675.425

[keyboard_response]
elevator=116.000000,180.000000
aileron=113.000000,174.000000
rudder=300.000000,300.000000

[Views]
eyepoint=65.898745,-2.153051,7.215285

[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

[direction_indicators]
direction_indicator.0=3,0

[Flaps.0]
type=1
span-outboard=0.500
extending-time=27.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=9.998, 0.000
flaps-position.2=19.996, 0.000
flaps-position.3=29.994, 0.000
flaps-position.4=39.992, 0.000