AALAirbusBoeingPilotFS9

Hi guys. I have the CLS A300 & 767 and the QW 757 in FS9. I noticed that the FMC's of the CLS 767 & the QW 757 can calculate the V speeds for takeoff & landing, but the CLS A300 FMC does not. I installed the ISG FMC & panel gauges for CLS A300. I am unable to calculate V speeds with the FMC from ISG I use for the A300. So my question is, is there a utility for FS9 that can calculate V speeds for any aircraft?

so I was testing the flight 1 super 80 in FS9 and I notice the autopilot dials are black and that the avionics are not functional, showing red tape and altimeter reading "off". The engines are on. I wonder what is the problem. How can it be resolved?? here's the photo of the issue: http://postimg.org/image/dkk36ywkd/

hello everyone. In FS9 I notice that there are 2 buildings near KEWR, left of 22R (I have the Imaginesim EWR scenery). So my question is, how can these buildings be excluded? I tried using the FlattEx utility to remove it, and it didn't work. What can be the problem? here's a link to the image of the issue:http://postimg.org/image/6ponplqvz/

Hi guys. So when I run FS9 on my desktop, I get good frames ( usually around 30+ fps), but if I install the ENB bloom effect, FS9 starts lagging, so I had to remove it. How can that issue be fixed?

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?