[fltsim.0]
title=SGA A300B4-200 Eastern
sim=a310
model=
panel=
sound=
texture=ea
kb_checklists=
kb_reference=
atc_airline=Eastern
atc_flight_number=472
atc_id=N214EA
atc_heavy=1
ui_manufacturer=Airbus
ui_type=A300B4-200
ui_variation=Eastern Airlines
description=Fictional N214EA tribute livery...less a tribute and more a "please leave me alone now..."
visual_damage=1

[fltsim.1]
title=SGA A300B4-200 Olympic (old colours)
sim=a310
model=
panel=
sound=
texture=old
kb_checklists=
kb_reference=
atc_airline=Olympic
atc_flight_number=472
atc_id=SX-BEB
atc_heavy=1
ui_manufacturer=Airbus
ui_type=A300B4-200
ui_variation=Olympic Airways 1980's colours
description=These colours were worn by the Airbus fleet of Olympic in the 80's textures by Tony Madge tonymadge@yahoo.com
visual_damage=1

[fltsim.2]
title=SGA A300B4-200 Olympic (new colours)
sim=a310
model=
panel=
sound=
texture=new
kb_checklists=
kb_reference=
atc_airline=Olympic
atc_flight_number=472
atc_id=SX-BEB
atc_heavy=1
ui_manufacturer=Airbus
ui_type=A300B4-200
ui_variation=Olympic Airways present colours
description=These colours are worn by the Airbus fleet textures by Tony Madge tonymadge@yahoo.com
visual_damage=1


[General]
performance = FDE Copyright by FrankWeiƟ\n2 x GE CF6-80C2A2 @ 48,080 lbs\nMTOW\t337,365 lbs\nMLW\t271,215 lbs\nMZFW\t249,165 lbs\nActual ZFW\199,025(203,000) lbs\nCruise\tM0.80\nMax alt.\t41,000 ft\nRange\t4,350(4,800) nm\nVmo\/Mmo\t360kts\/.84M 
atc_type = AIRBUS
atc_model = A310-300

[pitot_static]
vertical_speed_time_constant = 1

[WEIGHT_AND_BALANCE]
max_gross_weight = 337365.000
empty_weight = 179025.000  //81300 kg
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 6.030, 0.000, -4.000
max_number_of_stations = 50
station_load.0 = 23975.000, 6.030, 0.000, -4.000

;Moments of Inertia
empty_weight_pitch_MOI = 4956356.000
empty_weight_roll_MOI = 10142035.000
empty_weight_yaw_MOI = 5531785
empty_weight_coupled_MOI = 209895.000
CG_forward_limit = 0.000
CG_aft_limit = 1.000

[flight_tuning]
cruise_lift_scalar = 1.500
parasite_drag_scalar = 1.050
induced_drag_scalar = 1.250
elevator_effectiveness = 1.000
aileron_effectiveness = 1.000
rudder_effectiveness = 0.950
pitch_stability = 1.000
roll_stability = 1.000
yaw_stability = 1.015
elevator_trim_effectiveness = 0.700
aileron_trim_effectiveness = 1.000
rudder_trim_effectiveness = 1.000
landing_gear_drag_scalar = 1.300

[GeneralEngineData]
engine_type = 1
Engine.0 = 20.180, -25.600, -8.100
Engine.1 = 20.180, 25.600, -8.100
fuel_flow_scalar = 0.635
min_throttle_limit=-0.349915

[TurbineEngineData]
fuel_flow_gain = 0.00085
inlet_area = 47.080
rated_N2_rpm = 11055.000
static_thrust = 48080.000
afterburner_available = 0
reverser_available = 1

[jet_engine]
thrust_scalar =0.950

[electrical]
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 20, 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
light_logo = 0, 5 , 17.0

[contact_points]
point.0 = 1.000, 54.300, 0.000, -12.18, 1574.803, 0.000, 1.840, 80.000, 1.430, 1.450, 0.600, 10.000, 10.000, 0.000, 180.000, 250.000
point.1 = 1.000, -3.000, -15.50, -13.15, 1574.803, 1.000, 2.133, 0.000, 1.722, 1.250, 0.550, 10.000, 10.000, 2.000, 180.000, 250.000
point.2 = 1.000, -3.000, 15.50, -13.15, 1574.803, 2.000, 2.133, 0.000, 1.722, 1.250, 0.550, 10.000, 10.000, 3.000, 180.000, 250.000

point.3=2, -34.00, -86.00,   8.40,  787, 0, 0.0,  0, 0.000, 0.0, 0.0,  0.0,  0.0, 5,   0,   0
point.4=2, -34.00,  86.00,   8.40,  787, 0, 0.0,  0, 0.000, 0.0, 0.0,  0.0,  0.0, 6,   0,   0
point.5=2,  97.50,   0.00,   6.00,  787, 0, 0.0,  0, 0.000, 0.0, 0.0,  0.0,  0.0, 9,   0,   0
point.6=2, -93.50,   0.00,  25.00,  787, 0, 0.0,  0, 0.000, 0.0, 0.0,  0.0,  0.0, 4,   0,   0
point.7=2, -85.50,   0.00,  11.50,  787, 0, 0.0,  0, 0.000, 0.0, 0.0,  0.0,  0.0, 4,   0,   0
point.8=2, -46.50,   0.00,  -1.65,  787, 0, 0.0,  0, 0.000, 0.0, 0.0,  0.0,  0.0, 4,   0,   0

max_number_of_points=	10
static_pitch=		0.050
static_cg_height=	10.90
gear_system_type=	0

[Views]
eyepoint=68.50,-1.25,6.75   //(feet) longitudinal, lateral, vertical distance from reference datum

[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=3, -19.65, -73.20,  7.40, fx_navred,
light.1=3, -19.65,  73.20,  7.40, fx_navgre,

light.2=2, -20.60, -73.60,  7.40, fx_strobe,
light.3=2, -20.60, 73.60,  7.40, fx_strobe,

light.4=1, -31.50,   0.00, -4.60, fx_beaconb,
light.5=1,   7.50,   0.00,  13.20, fx_beaconh,

light.6=4,  68.50,   0.00, 6.75, fx_vclight,

light.7=3, -73.00, -12.00, 25.00, DC10logo ,
light.8=3, -73.00,  12.00, 25.00, DC10logo ,

[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250

[direction_indicators]
direction_indicator.0 = 3,0

[exits]			//Shift+E for L2, Shift+E+2 for L1 and R2
number_of_exits = 2
exit_rate.0 = 0.4
exit_rate.1 = 0.4

[TailHook]		//Landing lights extend/retract. Just like everyone else. But we did it first.
tailhook_length=	4
tailhook_position=	0.0, 0.0, 0.0
cable_force_adjust=	0.5

[folding_wings]		//cargo doors, R1, L/R4...
wing_fold_system_type=	4
fold_rates=		0.110,0.400

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

[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 000.000001
autothrottle_available = 1
autothrottle_arming_required = 1
autothrottle_max_rpm = 104
autothrottle_takeoff_ga = 1
pitch_takeoff_ga = 8.000
use_no_default_bank = 1
use_no_default_pitch = 1
default_pitch_mode=0
default_bank_mode=0
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

[fuel]
Center1= 0.000, 0.000, 0.000, 5189.000, 5.000        //main center tank
Center2= -8.000, 0.000, 5.400, 1625.000, 5.000       //trim tank
// Center3= -2.000, 0.000, 0.000, 3817.000, 5.000    //add. center tank, uncomment for -304ET model
LeftMain= 0.000, -30.000, 0.000, 3685.500, 5.000
LeftAux= 0.000, -50.000, 0.000, 977.500, 5.000
RightMain= 0.000, 30.000, 0.000, 3685.500, 5.000
RightAux= 0.000, 50.000, 0.000, 977.500, 5.000
fuel_type = 2
number_of_tank_selectors = 1
electric_pump=0

[airplane_geometry]
wing_area = 2358.000
wing_span = 144.030
wing_root_chord = 27.500
wing_dihedral = 3.964
wing_incidence = 0.500
wing_twist = -1.000
oswald_efficiency_factor = 0.750
wing_winglets_flag = 1
wing_sweep = 28.000
wing_pos_apex_lon = 19.390
wing_pos_apex_vert = -3.100
htail_area = 672.700
htail_span = 53.300
htail_pos_lon = -58.000
htail_pos_vert = 5.400
htail_incidence = 0.000
htail_sweep = 28.000
vtail_area = 486.900
vtail_span = 26.900
vtail_sweep = 45.000
vtail_pos_lon = -43.100
vtail_pos_vert = 9.300
elevator_area = 206.700
aileron_area = 73.840
rudder_area = 146.100
elevator_up_limit = 25.000
elevator_down_limit = 20.000
aileron_up_limit = 20.000
aileron_down_limit = 20.000
rudder_limit = 25.000
elevator_trim_limit = 9.000
spoiler_limit = 50.000
spoilerons_available = 1
aileron_to_spoileron_gain = 2.500
min_ailerons_for_spoilerons = 3.000
min_flaps_for_spoilerons = 0.000

[Reference Speeds]
flaps_up_stall_speed = 140.000
full_flaps_stall_speed = 105.000
cruise_speed = 470.000
max_indicated_speed=340.000000
max_mach=0.839990

[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

[Flaps.0]
type=1
span-outboard=0.840
extending-time=20.000
system_type=0
damaging-speed=230.000
blowout-speed=280.000
lift_scalar=0.400
drag_scalar=1.000
pitch_scalar=0.500
flaps-position.0=0.000, 0.000
flaps-position.1=0.000, 0.000
flaps-position.2=15.000, 0.000
flaps-position.3=20.000, 0.000
flaps-position.4=40.000, 0.000

[Flaps.1]
type=1
span-outboard=0.100
extending-time=2.000
system_type=1
damaging-speed=265.000
blowout-speed=280.000
lift_scalar=0.100
drag_scalar=0.400
pitch_scalar=0.100
flaps-position.0=0.000, 0.000
flaps-position.1=5.000, 0.000
flaps-position.2=5.000, 0.000
flaps-position.3=5.000, 0.000
flaps-position.4=5.000, 0.000

[Flaps.2]
type=2
span-outboard=0.960
extending-time=10.000
system_type=0
damaging-speed=265.000
blowout-speed=300.000
lift_scalar=0.100
drag_scalar=0.900
pitch_scalar=0.200
flaps-position.0=0.000, 0.000
flaps-position.1=15.000, 0.000
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
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