[fltsim.0]
title=A300-600R AMERICAN
sim=JF_AB6v2
model=
panel=
sound=
texture=
description=American flies the A306R on its routes between BOS, JFK, MIA, and the Caribbean.
ui_manufacturer=Airbus
ui_type=A300-600R
ui_variation=American Airlines
atc_heavy=0
atc_id=N325AA
atc_airline=American
atc_flight_number=426
[General]
atc_type=AIRBUS
atc_model=A300
performance=Powerplants:Two 262.4kn (59,000lb)General Electric CF6-80C2A1's or two 249kn (56,000lb) Pratt & Whitney PW4156s.\nPerformance:A300-600R Max cruising speed897km\/h (484kts). Long range cruising speed 875km\/h (472kts). Typical airline range with reserves and stanard fuel 7505km (4050nm).\nPrduction: Over 250 A300-600R delivered.
[pitot_static]
vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[GeneralEngineData]
engine_type= 1
Engine.0 = 20.180, -25.600, -8.100
Engine.1 = 20.180, 25.600, -8.100
fuel_flow_scalar= 1.000
[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 70.000
rated_N2_rpm= 29920.000
static_thrust= 56000.000
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar=1.000
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
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_panel=0, 5 , 17.0
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points]
point.0= 1.000, 52.800, 0.000, -13.850, 1181.100, 0.000, 3.500, 55.920, 0.800, 2.500, 0.900, 11.000, 11.000, 0.000, 0.000, 0.000
point.1= 1.000, -11.100, -17.500, -15.333, 1574.800, 1.000, 3.500, 0.000, 1.000, 2.500, 0.900, 12.000, 12.000, 2.000, 0.000, 0.000
point.2= 1.000, -11.100, 17.500, -15.333, 1574.800, 2.000, 3.500, 0.000, 1.000, 2.500, 0.900, 12.500, 12.500, 3.000, 0.000, 0.000
point.3= 2.000, -25.000, -73.500, 7.060, 787.400, 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, -25.000, 73.500, 7.060, 787.400, 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, -88.300, 0.000, 2.140, 787.400, 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, 78.200, 0.000, -3.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
max_number_of_points=21
static_pitch= -0.912
static_cg_height= 13.500
[Views]
eyepoint=70.25, -1.6, 5.20 //(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
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator=150, 250
aileron=150, 250
rudder=150, 250
[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
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second
[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=2000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
[fuel]
Center1= 0.000, 0.000, 0.000, 4313.000, 0.000
LeftMain= -12.000, -19.000, 0.000, 6000.000, 0.000
RightMain= -12.000, 19.000, 0.000, 6000.000, 0.000
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
[airplane_geometry]
wing_area= 2800.000
wing_span= 147.100
wing_root_chord= 18.000
wing_dihedral= 6.200
wing_incidence= 1.000
wing_twist= -0.500
oswald_efficiency_factor= 0.750
wing_winglets_flag= 1
wing_sweep= 28.000
wing_pos_apex_lon= 15.000
wing_pos_apex_vert= 0.000
htail_area= 738.000
htail_span= 55.700
htail_pos_lon= -84.000
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 30.000
vtail_area= 374.000
vtail_span= 21.000
vtail_sweep= 35.000
vtail_pos_lon= -81.000
vtail_pos_vert= 5.800
elevator_area= 69.000
aileron_area= 46.900
rudder_area= 86.200
elevator_up_limit= 27.000
elevator_down_limit= 20.500
aileron_up_limit= 20.000
aileron_down_limit= 20.000
rudder_limit= 26.000
elevator_trim_limit= 20.000
spoiler_limit= 60.000
spoilerons_available= 0
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 10.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed= 160.000
full_flaps_stall_speed= 125.000
cruise_speed= 465.000
[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= 0.200
extending-time= 23.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 300.000
lift_scalar= 0.550
drag_scalar= 0.550
pitch_scalar= 0.550
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 5.000, 0.000
flaps-position.4= 10.000, 0.000
flaps-position.5= 15.000, 0.000
flaps-position.6= 25.000, 0.000
flaps-position.7= 30.000, 0.000
flaps-position.8= 40.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.800
extending-time= 21.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.350
drag_scalar= 0.350
pitch_scalar= 0.350
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 5.000, 0.000
flaps-position.4= 10.000, 0.000
flaps-position.5= 15.000, 0.000
flaps-position.6= 25.000, 0.000
flaps-position.7= 30.000, 0.000
flaps-position.8= 40.000, 0.000
[Flaps.2]
type= 2
span-outboard= 0.600
extending-time= 3.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.050
drag_scalar= 0.050
pitch_scalar= 0.050
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.500, 0.000
flaps-position.2= 0.500, 0.000
flaps-position.3= 0.500, 0.000
flaps-position.4= 0.500, 0.000
flaps-position.5= 0.500, 0.000
flaps-position.6= 1.000, 0.000
flaps-position.7= 1.000, 0.000
flaps-position.8= 1.000, 0.000
[WEIGHT_AND_BALANCE]
MTW = 365800 // Added by LyonsMark
MLW = 304200 // Added by LyonsMark
Pax_Weight = 232 // Weight in pounds of passengers Added by LyonsMark
Cargo_Weight = 0 // Weight in pounds of cargo Added by LyonsMark
Fuel_Weight = 31772 // Weight in pounds of loaded fuel Added by LyonsMark
empty_weight = 235720 // Weight in pounds (total weight) Added by LyonsMark
ZFW_Weight = 198600 // Added by LyonsMark
Fuel_Capacity = 74956 // Added by LyonsMark
Cargo_Capacity = 76900 // Added by LyonsMark
1Class_Pax = 345 // Added by LyonsMark
2Class_Pax = 250 // Added by LyonsMark
3Class_Pax = 0 // Added by LyonsMark
Aircraft_Type = AIRBUS A300 // Added by LyonsMark
Aircraft_Length = 177 // Added by LyonsMark
Aircraft_WingSpan = 147 // Added by LyonsMark
empty_weight_pitch_MOI=7546800 // Modified by LyonsMark
empty_weight_roll_MOI=2184600 // Modified by LyonsMark
empty_weight_yaw_MOI=6752400 // Modified by LyonsMark
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_coupled_MOI=0.000000
