Help with Overland SMS A300?

[AALAirbusBoeingPilotFS9 0]

Hello, I have an issue with the Overland SMS A300. While I was test flying the SMS A300-600R in FS2004, I noticed that the SMS A300-600 has a tendency to accelerate too fast on takeoff. I rotate it at about 165 knots, then, after a few seconds after takeoff, it accelerates to almost 200 knots. What can be the problem?

 

I know I posted this previously on flightsim, I did not get suggestions on how to resolve this issue w/ my plane so I thought I might ask it on here.

 

Here is my configuration of the SMS A300-600R:

 

 

[fltsim.0]

title=A300B4-605R American Airlines N7055A

sim=A300-600R

model = GE_VC

panel =

sound =

texture = AAL N7055A AMERICAN

atc_airline = AMERICAN

atc_flight_number = 0

checklists =

atc_id = N7055A

atc_heavy = 1

atc_parking_code = AAL

atc_parking_types = Gate Heavy Gate Small Gate Medium

description=Overland Co.,Ltd. Products --- Airbus A300-600R\n\nL1 Cabin Door [shift+E] then [1]\nL2 Cabin Door Wing Fold/Extend\nCargo Door Operate with Door Display Gauge\nL3/R3 Cabin Door Tailhook Extend/Retruct

ui_createdby = "Simmer's Sky"

ui_manufacturer = Airbus

ui_type = A300B4-605R

ui_variation = American Airlines N7055A

visual_damage = 1

editable = 0

 

 

[General]

visual_damage=0 // 0=off, 1=on

atc_type=AIRBUS

atc_model=A306

editable=0

performance=Cruise Speed\t472kt\nMaximum Range\t3,600 nm\nService Ceiling\t32,400 ft\nMax Takeoff Weight\t375,855 lb\nSeating\t\t266 to 361\nCargo Capacity\t22 LD3 containers\n

Category=airplane

 

 

[WEIGHT_AND_BALANCE]

max_gross_weight=375855 // (pounds)

empty_weight=200700 // (pounds)

 

reference_datum_position=0, 0, -5 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)

empty_weight_CG_position=0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum

 

max_number_of_stations=20

 

//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

 

station_load.0 = "170.0, -77.0, -2.0, 0.0, Pilot"

station_load.1 = "170.0, -77.0, 2.0, 0.0, Co-Pilot"

station_load.2 = "1360.0, -43.5, 0.0, 0.0, Crew"

station_load.3 = "5950.0, -52.7, 0.0, 0.0, Business Class"

station_load.4 = "23800.0, -4.3, 0.0, 0.0, Coach 1-18"

station_load.5 = "15470.0, 42.6, 0.0, 0.0, Coach 19-30"

station_load.6 = "4000.0, -49.0, 0.0, -6.0, Forward Baggage"

station_load.7 = "2000.0, 29.0, 0.0, -6.0, Aft Baggage"

 

 

;Moments of Inertia

empty_weight_pitch_MOI=4100000

empty_weight_roll_MOI =3200000

empty_weight_yaw_MOI =3300000

empty_weight_coupled_MOI=0.0

empty_weight_coupled_MOI=0.0

[flight_tuning]

cruise_lift_scalar=1.061

parasite_drag_scalar=0.950

induced_drag_scalar=1.100

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 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop

Engine.0=12.1, -26.6, -7.0 //(feet) longitudinal, lateral, vertical distance from reference datum

Engine.1=12.1, 26.6, -7.0 //(feet) longitudinal, lateral, vertical distance from reference datum

fuel_flow_scalar=0.624 //Scalar for fuel flow efficiency

min_throttle_limit=-0.29000

 

[TurbineEngineData]

fuel_flow_gain=0.1 //Gain on fuel flow

inlet_area=35.0 //Square Feet, engine nacelle inlet area

rated_N2_rpm=11055.000 //RPM, second stage compressor rated value

static_thrust=56210.000 //Lbs, max rated static thrust at Sea Level

afterburner_available=0 //Afterburner available?

reverser_available=1.000 //Thrust reverser available?

 

[jet_engine]

thrust_scalar=1.080

 

[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_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

 

//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, 59.42, 0.00, -13.97, 1181.1, 0, 2.220, 75.0, 0.27, 0.95, 0.8135,13.5,13.5, 0, 0.0, 0.0

point.1=1, -5.50, -14.50, -14.91, 1574.8, 1, 2.520, 0.0, 1.11, 1.50, 0.7470,16.5, 16.5, 2, 0.0, 0.0

point.2=1, -5.50, 14.50, -14.91, 1574.8, 2, 2.520, 0.0, 1.11, 1.50, 0.7470, 16.5, 16.5, 3, 0.0, 0.0

 

point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0

point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0

point.5=2, -73.33, 0.00, 2.50, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0

point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0

point.7= 5, -70.90, -15.250, -17.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.0, 1.2, 0, 0.0, 0.0

point.8= 5,-400.90, 15.250, -17.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.1, 1.5, 0, 0.0, 0.0

 

 

 

static_pitch=-0.38

static_cg_height=18.95

gear_system_type=0

 

//AES Orgvalue:static_pitch=-0.38

static_pitch=.15

//AES Orgvalue:static_cg_height=18.95

static_cg_height=18.79

gear_system_type=0

 

 

[Views]

eyepoint=73.75, -1.53, 4.65

 

[Flaps.0]

type= 1

span-outboard= 0.840

extending-time= 25.000

system_type= 0

damaging-speed= 225.000

blowout-speed= 240.000

lift_scalar= 0.650

drag_scalar= 0.650

pitch_scalar= 1.550

flaps-position.0= 0.000, 0.000

flaps-position.1= 0.000, 0.000

flaps-position.2= 26.500, 0.000

flaps-position.3= 29.000, 0.000

flaps-position.4= 33.500, 0.000

 

[Flaps.1]

type= 1

span-outboard= 0.100

extending-time= 3.500

system_type= 0

damaging-speed= 260.000

blowout-speed= 280.000

lift_scalar= 0.030

drag_scalar= 0.030

pitch_scalar= 0.500

flaps-position.0= 0.000, 0.000

flaps-position.1= 9.200, 0.000

flaps-position.2= 9.200, 0.000

flaps-position.3= 9.200, 0.000

flaps-position.4= 9.200, 0.000

 

[Flaps.2]

type= 2

span-outboard= 0.970

extending-time= 14.000

system_type= 0

damaging-speed= 260.000

blowout-speed= 280.000

lift_scalar= 0.001

drag_scalar= 0.300

pitch_scalar= 0.001

flaps-position.0= 0.000, 0.000

flaps-position.1= 17.000, 0.000

flaps-position.2= 17.000, 0.000

flaps-position.3= 17.000, 0.000

flaps-position.4= 25.000, 0.000

[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.1 = 1, -29.50, 0.00, -7.55, fx_shockwave_beacon_rotating_red ,

light.2 = 1, 11.50, 0.00, 11.00, fx_shockwave_beaconh ,

light.3 = 3, -91.50, 0.00, 9.00, fx_shockwave_navwhi_l ,

light.4 = 2, -91.50, 0.00, 9.00, fx_shockwave_strobe_sm ,

light.5 = 4, 73.50, 0.00, 6.90, fx_vclighth ,

light.6 = 6, 62.50, 0.0, -7.5, fx_shockwave_landing_light_double_small , // Shockwave light

light.7 = 5, 4.25, 12.0, -4.0, fx_Shockwave_landing_light , // Shockwave light

light.8 = 5, 4.25, -12.0, -4.0, fx_Shockwave_landing_light , // Shockwave light

light.9 = 5, 4.31, 12.0, -4.0, QW757_wingscan

light.10 = 5, 4.31, -12.0, -4.0, QW757_wingscan

light.11 = 5, 4.25, 12.0, -4.0, Opensky_nacelle_refl

light.12 = 5, 4.25, -12.0, -4.0, Opensky_nacelle_refl

light.13 = 5, 4.25, 12.0, -4.0, Opensky_wing_light

light.14 = 5, 4.25, -12.0, -4.0, Opensky_wing_light

light.15 = 5, 4.25, 12.0, -4.0, Opensky_nav_yellow

light.16 = 5, 4.25, -12.0, -4.0, Opensky_nav_yellow

light.17 = 5, 4.35, 12.0, -4.0, Opensky_nav_yellow

light.18 = 5, 4.35, -12.0, -4.0, Opensky_nav_yellow

 

[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

 

[fuel]

Center1 = 0.0, 0.0, -4.0, 4650.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

LeftAux = 0.0, -35.0, 0.0, 1225.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

RightAux = 0.0, 35.0, 0.0, 1225.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

LeftMain = 0.0, -35.0, 0.0, 4640.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

RightMain = 0.0, 35.0, 0.0, 4640.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

Center2 = 0.0, 0.0, -4.0, 1625.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA

number_of_tank_selectors=1

electric_pump=0

 

[airplane_geometry]

wing_area=2798.70 //Square feet

wing_span=147.10 //Feet

wing_root_chord=25.46 //28 Feet

wing_dihedral=5.2 //Degrees

wing_incidence=1.0 //Degrees

wing_twist=0.5 //Degrees

oswald_efficiency_factor=0.77 //Measure of lift effeciency of wing

wing_winglets_flag=1 //Are winglets available?

wing_sweep=28.0 //Degrees, wing leading edge

wing_pos_apex_lon=22.5 //15 Feet, longitudinal distance from reference point, negative going aft

wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up

htail_area=756.9 //Square feet

htail_span=54.23 //Feet

htail_pos_lon=-69.33 //Feet, longitudinal distance from reference point, negative going aft

htail_pos_vert=7.2 //Feet, vertical distance from reference point, positive going up

htail_incidence=1.000 //Degrees

htail_sweep=37.5 //Degrees, horizontal tail leading edge

vtail_area=568.2 //Square feet

vtail_span=20.9 //Feet, tip to body

vtail_sweep=34.5 //Degrees, vertical tail leading edge

vtail_pos_lon=-61.91 //Feet, longitudinal distance from reference point, negative going aft

vtail_pos_vert=10.8 //Feet, vertical distance from reference point, positive going up

elevator_area=115.2 //57 Square feet

aileron_area=55.3 //25 Square feet

rudder_area=192.55 //58 Square feet

elevator_up_limit=20.0 //Degrees

elevator_down_limit=20.0 //Degrees

aileron_up_limit=18.0 //Degrees

aileron_down_limit=18.0 //Degrees

rudder_limit=30.0 //Degrees

elevator_trim_limit=20.0 //Degrees

spoiler_limit=75.0 //Degrees

spoilerons_available=1 //Spoilerons Available?

aileron_to_spoileron_gain=3 //Aileron to spoileron gain

min_ailerons_for_spoilerons=10 //Degrees

min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate

auto_spoiler_available=1

spoiler_extension_time=2.000000

positive_g_limit_flaps_up=4.000000

positive_g_limit_flaps_down=3.000000

negative_g_limit_flaps_up=-3.000000

negative_g_limit_flaps_down=-2.000000

 

[Reference Speeds]

flaps_up_stall_speed=110.0 //Knots True (KTAS)

full_flaps_stall_speed=108.0 //Knots True (KTAS)

cruise_speed=610.0 //Knots True (KTAS)

max_indicated_speed=600.000000

max_mach=2.950000

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1500.0

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.

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

 

 

[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

 

[brakes]

toe_brakes_scale=0.489926 ; brakes_scale 0 to none 1 to hard

parking_brake=1

auto_brakes=4

 

[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

stick_shaker=1

 

[attitude_indicators]

attitude_indicator.0=1

 

[turn_indicators]

turn_indicator.0=1,0

 

[folding_wings]

wing_fold_system_type=4 ;0=None

fold_rates=0.12,0.11 ;Percent per second

 

[TailHook]

tailhook_length=4 ;(feet)

tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum

cable_force_adjust=0.0

 

[pitot_static]

pitot_heat=1.000000

[vacuum_system]

max_pressure=5.150000

vacuum_type=2

electric_backup_pressure=0.000000

engine_map=0,0,0,0

[pneumatic_system]

max_pressure=18.000000

bleed_air_scalar=1.000000

[deice_system]

structural_deice_type=0

[keyboard_response]

elevator=110.000000,220.000000

aileron=110.000000,220.000000

rudder=110.000000,220.000000

[direction_indicators]

direction_indicator.0=3,0

 

My question for the configuration is- what needs to be edited on here?