[fltsim.0]
title=Airbus A300-600 BERUGA
sim=pac300600stge
model=
panel=
sound=
texture=
checklists=
description=AIRBUS A300-600ST\n\nThe A300-600 is optimised for maximum profitability in the demanding mid-size regional market. With the capability to operate profitably on extended range routes, it incorporates many technological features not found on competing airliners. These improve reliability and reduce operating costs. The A300-600 layout and has a range of 4,000 nm\/7,700 km.\n\n\n\n\n\n\n
ui_manufacturer=
ui_type=AIRBUS A300-600
ui_variation=
atc_heavy=0
atc_id=
atc_airline=AIRBUS 
atc_flight_number=BLG01

[General]
performance=The overall length: 56.20 m \nSpan: 44.84 m \nAll high 17.23 m \nInstallation capacity main deck : 1,400 m3 (49,440 ft3)  \nUnderfloor bulk :17.3 m3 (611 ft3)  \nInstallation weight: 47,000 kg (103,590 lb.) \nTakeoff weight :155,000 kg (341,713 lb.)  \nsecond series distance: 1,660-4,632 km  \nCruising speed :0.7 Mach \nMost ultrahigh altitude: 10,670 m (35,000 ft.)\n\nMake by AKIRA TAKAHSHI
atc_type=
atc_model=A330

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight= 275000.000
empty_weight_roll_MOI= 22080000.000
empty_weight_pitch_MOI= 19280000.000
empty_weight_yaw_MOI= 14500000.000
empty_weight_coupled_MOI= 650000.000
max_gross_weight= 395633.497
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[fuel]
Center1= 0.000, 0.000, -4.000, 6275.000, 3.000
LeftMain= -7.000, -30.000, 0.000, 5865.000, 3.000
RightMain= -7.000, 30.000, 0.000, 5865.000, 3.000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 2800.000
wing_span= 147.000
wing_root_chord= 19.083
wing_dihedral= 3.598
wing_incidence= 1.000
wing_twist= -0.994
oswald_efficiency_factor= 0.932
wing_winglets_flag= 65535
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=-1
aileron_to_spoileron_gain=0.140000
min_ailerons_for_spoilerons=9.969466
min_flaps_for_spoilerons=0.000000

[contact_points]
point.0= 1.000, 52.750, 0.000, -13.583, 1574.803, 0.000, 3.243, 67.980, 0.560, 2.500, 0.474, 12.000, 12.000, 0.000, 0.000, 0.000
point.1= 1.000, -9.750, -16.250, -14.583, 1574.803, 1.000, 3.243, 0.000, 0.573, 2.500, 0.468, 14.000, 14.000, 2.000, 0.000, 0.000
point.2= 1.000, -9.750, 16.250, -14.583, 1574.803, 2.000, 3.243, 0.000, 0.573, 2.500, 0.468, 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= 15.448

[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= 0.003
inlet_area= 105.600
rated_N2_rpm= 30150.000
static_thrust= 59000.000
afterburner_available= 0
reverser_available= 1

[Reference Speeds]
flaps_up_stall_speed= 145.000
full_flaps_stall_speed= 116.000
cruise_speed= 318.787

[keyboard_response]
elevator=136.000000,222.000000
aileron=173.000000,254.000000
rudder=300.000000,300.000000

[Views]
eyepoint=65.116982,-2.332472,0.102526

[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


[jet_engine]
thrust_scalar = 1.35

[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
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 20.000
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