08-08-2013, 12:05 PM
Its sounds like a simple bug that can be fixed but still no solution 
Attached is my CFG: Anyone's help will be highly appreciated!
[General]
atc_type=BOEING
atc_model=B773
editable=0
performance="Cruise Speed \nMach 0.84 555 mph 893 kmh\n\nEngine options \nP&W 4000\nRR Trent 800\nGE 90
series\n\nMaximum Range \n5,960 nm 6,859 sm 11,038 km\n\nService Ceiling \n42,000 ft 12,800 m\n\nFuel
Capacity \n45,220 U.S. gal 171,160 L \n\nMaximum Takeoff Weight \n660,000 lb 299,370 kg\n\nLength \n242 ft, 4 in
73.9 m\n\nWingspan \n199 ft, 11 in 60.9 m\n\nHeight \n60 ft, 8 in 18.5 m\n\nSeating \nSeats 386 to 550 \n\nCargo
Capacity \n7,552 ft 213.8 m\n"
[weight_and_balance]
// ACM V2.5
max_gross_weight = 775000
empty_weight = 366940
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 24500000
empty_weight_roll_MOI = 17500000
empty_weight_yaw_MOI = 9821453
empty_weight_coupled_MOI = 0
max_number_of_stations = 14
station_load.0 = 720, 112,7, 0, 4.12, Cockpit Crew
station_load.1 = 1080, 0, 0, Cabin Crew
station_load.2 = 1800, 85, 0, 0, First Class
station_load.3 = 11880, 40, 0, 0, Business Class
station_load.4 = 24840, 0, 0, 0, Coach Y1
station_load.5 = 24840, -20, 0, 0, Coach Y2
station_load.6 = 0, 0, 0, 0, Containers P. 1 (FRT)
station_load.7 = 500, 10, 0, 0, Containers P. 2 (FRT/MAIL)
station_load.8 = 12670, -30, 0, 0, Containers P. 3 (BGGE)
station_load.9 = 12670, -60, 0, 0, Containers P. 4 (BGGE)
station_load.10 = 200, -70, 0, Bulk Cargo P. 5 (BULK)
station_load.11 = 543, 0, 0, Meals
station_load.12 = 139, 0, 0, Potable Water
station_load.13 = 20, 0, 0, Lav Service
[GeneralEngineData]
//JFDVD
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 0.759
//fuel_flow_scalar = 0.90
//default_fuel_flow_scalar = 0.825
min_throttle_limit = -0.51
engine.0 = 32.75, -32.03, -7.41,
engine.1 = 32.75, 32.03, -7.41,
[smokesystem]
smoke.0 = 5.90, -27.40, 77.13, fx_pss_fuel_jett
smoke.1 = 5.9, -27.4, -77.13, fx_pss_fuel_jett
smoke.2 = -15, 22, 32, Opensky_revspray
smoke.3 = -15, 22, -32, Opensky_revspray
smoke.4 = 5, -5, 55, Opensky_conden
smoke.5 = 5, -5, -55, Opensky_conden
smoke.6 = 5, -35, 75, Opensky_vortex
smoke.7 = 5, -35, -75, Opensky_vortex
[effects]
wake = fx_wake
water = fx_spray
waterspeed = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
startup = fx_pss_startup
windshield_rain_effect_available = 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 4
electric_pump = 1
Center1 = 5, 0, -4, 27290, 3
LeftMain = 5, -35, 0, 9300, 3
LeftAux = -10, -60, 3, 4370, 0
RightMain = 5, 35, 0, 9300, 3
RightAux = -10, 60, 3, 4370, 0
[contact_points]
//AES Orgvalue:static_pitch = 0.1
static_pitch=-.05
//AES Orgvalue:static_cg_height = 17.56
static_cg_height=14.5
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 17
Point.0= 1, 92.500, 0.000, -16.750, 1881.102, 0, 2.0, 70.0, 1.200, 1.800, 1.5, 7.000, 9.000, 0.000, 240.000, 280.000
Point.1= 1, -10.900, -20.291, -18.250, 2574.803, 1, 2.6, 0.0, 1.700, 1.100, 1.5, 10.900, 11.900, 2.000, 240.000, 280.000
Point.2= 1, -10.900, 20.291, -18.250, 2574.803, 2, 2.6, 0.0, 1.700, 1.100, 1.5, 8.100, 13.100, 3.000, 240.000, 280.000
point.3 = 2, -44.167, -99.916, 10.000, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -44.167, 99.916, 10.000, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -108, 0, -0.6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 88.417, 0, -7.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 10.000, -32.583, -8.500, 787.401, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7.0, 0.0, 0.0
point.8 = 2, 10.000, 32.583, -8.500, 787.401, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8.0, 0.0, 0.0
point.9 = 2, 14, -32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0
point.10 = 2, 14, 32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0
point.11 = 2, 105, 0, -4.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.12 = 2, 100, 0, 8.9, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.13 = 2, -127, 0, 41.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.14 = 2, -128.5, 35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 5, 9, 0, 0
point.15 = 2, -128.5, -35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 6, 9, 0, 0
point.16 = 2, -81.5, 0, -6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
//point.0 = 1, 100.6083, 0, -17.5803, 1181.1, 0, 4.521, 65, 1, 2.5, 0.7235, 13, 14, 0, 270, 270
//point.1 = 1, -6.76, -20, -18.5905, 1574.8, 1, 4.521, 8, 1.91, 2.5, 0.747, 13, 14, 2, 270, 270
//point.2 = 2, 30.8612, -31.5494, -14.1458, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.3 = 2, 30.8612, 31.5494, -14.1458, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.4 = 1, -6.76, 20, -18.5905, 1574.8, 2, 4.521, 8, 1.91, 2.5, 0.747, 12.9, 13.9, 3, 270, 270
//point.5 = 2, -115, -36, 9, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
//point.6 = 2, -38.4, -105, 12.5, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
//point.7 = 2, -115, 36, 9, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
//point.8 = 2, -38.4, 105, 12.5, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
//point.9 = 2, -116.5152, 0, 44.1266, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
//point.10 = 2, -115.5083, 0, 3.1359, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.11 = 2, -85.5589, 0, -4.8617, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.12 = 2, -56.4399, 0, -8.5634, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.13 = 2, -116.3871, 0, 3.9812, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
//point.14 = 2, 50.4709, 0, 13.0267, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.15 = 2, 120.1817, 0, 0.4276, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.16 = 5, 0.0, 0.0, -10.0, 1600, 0.0, 0.0, 50.0, 0.0, 0.0, 1.00, 1.0, 1.0, 0, 0.0, 0.0
[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[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
[airplane_geometry]
wing_area = 4604.801
wing_span = 212.58
wing_root_chord = 21.65
wing_dihedral = 3.90
wing_incidence = 1.0
wing_twist = -2
oswald_efficiency_factor = 0.91
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 5.40
wing_pos_apex_vert = -4.46
htail_area = 1089.954
htail_span = 70.04
htail_pos_lon = -100.23
htail_pos_vert = 5.78
htail_incidence = 0.0
htail_sweep = 40
vtail_area = 572.963
vtail_span = 33.23
vtail_sweep = 35
vtail_pos_lon = -94.60
vtail_pos_vert = 10.63
elevator_area = 137.0
aileron_area = 76.5
rudder_area = 232.0
elevator_up_limit = 30.0
elevator_down_limit = 20.0
aileron_up_limit = 26.0
aileron_down_limit = 25.0
rudder_limit = 25.0
elevator_trim_limit = 20.0
spoiler_limit = 45.0
aileron_to_spoileron_gain = 1.5
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 9
min_flaps_for_spoilerons = 0
spoilerons_available = 1
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 1
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
[flight_tuning]
cruise_lift_scalar=1.30
parasite_drag_scalar=1.45
induced_drag_scalar=1.45
elevator_effectiveness=1.40
aileron_effectiveness=2.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=0.5
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[TurbineEngineData]
fuel_flow_gain=0.0010 //Gain on fuel flow
inlet_area=93.800 //Square Feet, engine nacelle inlet area
rated_N2_rpm=11292 //RPM, second stage compressor rated value
static_thrust=115540 //GE90-115B Lbs, max rated static thrust at Sea Level
afterburner_available=0 //Afterburner available?
reverser_available=1 //Thrust reverser available?
[jet_engine]
thrust_scalar=0.993
[gear_warning_system]
gear_warning_available = 0 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 5.0 //Flap angle that activates warning at idle
flap_limit_power = 25.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 1 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint=103.002, -1.756, 5.20
[Flaps.0] //Inboard Krueger
type= 2
span-outboard= 0.100
extending-time= 30.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 275.000
lift_scalar= 0.0
drag_scalar= 0.0000
pitch_scalar= 0.0
flaps-position.0= 0.000, 0.000
flaps-position.1= 30.000, 265.000
[Flaps.1] //Slat
type= 2
span-outboard= 0.800
extending-time= 30.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 275.000
lift_scalar= 0.02100
drag_scalar= 0.300
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.500, 265.000
flaps-position.2= 15.500, 245.000
flaps-position.3= 15.500, 230.000
flaps-position.4= 15.500, 225.000
flaps-position.5= 30.000, 200.000
flaps-position.6= 30.000, 180.000
[Flaps.2] //Inboard Flap
type= 1
span-outboard= 0.200
extending-time= 45.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 275.000
lift_scalar= 0.4750
drag_scalar= 0.250
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.1000, 265.000
flaps-position.2= 5.000, 245.000
flaps-position.3= 15.000, 230.000
flaps-position.4= 20.000, 225.000
flaps-position.5= 25.000, 200.000
flaps-position.6= 30.000, 180.000
[Flaps.3] //Outboard Flap
type= 1
span-outboard= 0.600
extending-time= 45.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 275.000
lift_scalar= 0.4750
drag_scalar= 0.300
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.10, 265.000
flaps-position.2= 5.000, 245.000
flaps-position.3= 15.000, 230.000
flaps-position.4= 20.000, 225.000
flaps-position.5= 25.000, 200.000
flaps-position.6= 30.000, 180.000
[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, 1
Adf.1=1,1
Adf.2=1,1
Transponder.1=1
Marker.1=1
[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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[exits]
number_of_exits = 4
exit_rate.0 = 0.10 ;Percent per second
exit_rate.1 = 0.08 ;Percent per second
exit_rate.2 = 0.10 ;Percent per second
exit_rate.3 = 0.08 ;Percent per second
[Reference Speeds]
flaps_up_stall_speed=150.0 //Knots True (KTAS)
full_flaps_stall_speed=120.0 //Knots True (KTAS)
cruise_speed=482.0 //Knots True (KTAS)
max_mach = 0.90
max_indicated_speed = 330 //Red line (KIAS)
Attached is my CFG: Anyone's help will be highly appreciated!
[General]
atc_type=BOEING
atc_model=B773
editable=0
performance="Cruise Speed \nMach 0.84 555 mph 893 kmh\n\nEngine options \nP&W 4000\nRR Trent 800\nGE 90
series\n\nMaximum Range \n5,960 nm 6,859 sm 11,038 km\n\nService Ceiling \n42,000 ft 12,800 m\n\nFuel
Capacity \n45,220 U.S. gal 171,160 L \n\nMaximum Takeoff Weight \n660,000 lb 299,370 kg\n\nLength \n242 ft, 4 in
73.9 m\n\nWingspan \n199 ft, 11 in 60.9 m\n\nHeight \n60 ft, 8 in 18.5 m\n\nSeating \nSeats 386 to 550 \n\nCargo
Capacity \n7,552 ft 213.8 m\n"
[weight_and_balance]
// ACM V2.5
max_gross_weight = 775000
empty_weight = 366940
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 24500000
empty_weight_roll_MOI = 17500000
empty_weight_yaw_MOI = 9821453
empty_weight_coupled_MOI = 0
max_number_of_stations = 14
station_load.0 = 720, 112,7, 0, 4.12, Cockpit Crew
station_load.1 = 1080, 0, 0, Cabin Crew
station_load.2 = 1800, 85, 0, 0, First Class
station_load.3 = 11880, 40, 0, 0, Business Class
station_load.4 = 24840, 0, 0, 0, Coach Y1
station_load.5 = 24840, -20, 0, 0, Coach Y2
station_load.6 = 0, 0, 0, 0, Containers P. 1 (FRT)
station_load.7 = 500, 10, 0, 0, Containers P. 2 (FRT/MAIL)
station_load.8 = 12670, -30, 0, 0, Containers P. 3 (BGGE)
station_load.9 = 12670, -60, 0, 0, Containers P. 4 (BGGE)
station_load.10 = 200, -70, 0, Bulk Cargo P. 5 (BULK)
station_load.11 = 543, 0, 0, Meals
station_load.12 = 139, 0, 0, Potable Water
station_load.13 = 20, 0, 0, Lav Service
[GeneralEngineData]
//JFDVD
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 0.759
//fuel_flow_scalar = 0.90
//default_fuel_flow_scalar = 0.825
min_throttle_limit = -0.51
engine.0 = 32.75, -32.03, -7.41,
engine.1 = 32.75, 32.03, -7.41,
[smokesystem]
smoke.0 = 5.90, -27.40, 77.13, fx_pss_fuel_jett
smoke.1 = 5.9, -27.4, -77.13, fx_pss_fuel_jett
smoke.2 = -15, 22, 32, Opensky_revspray
smoke.3 = -15, 22, -32, Opensky_revspray
smoke.4 = 5, -5, 55, Opensky_conden
smoke.5 = 5, -5, -55, Opensky_conden
smoke.6 = 5, -35, 75, Opensky_vortex
smoke.7 = 5, -35, -75, Opensky_vortex
[effects]
wake = fx_wake
water = fx_spray
waterspeed = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
startup = fx_pss_startup
windshield_rain_effect_available = 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 4
electric_pump = 1
Center1 = 5, 0, -4, 27290, 3
LeftMain = 5, -35, 0, 9300, 3
LeftAux = -10, -60, 3, 4370, 0
RightMain = 5, 35, 0, 9300, 3
RightAux = -10, 60, 3, 4370, 0
[contact_points]
//AES Orgvalue:static_pitch = 0.1
static_pitch=-.05
//AES Orgvalue:static_cg_height = 17.56
static_cg_height=14.5
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 17
Point.0= 1, 92.500, 0.000, -16.750, 1881.102, 0, 2.0, 70.0, 1.200, 1.800, 1.5, 7.000, 9.000, 0.000, 240.000, 280.000
Point.1= 1, -10.900, -20.291, -18.250, 2574.803, 1, 2.6, 0.0, 1.700, 1.100, 1.5, 10.900, 11.900, 2.000, 240.000, 280.000
Point.2= 1, -10.900, 20.291, -18.250, 2574.803, 2, 2.6, 0.0, 1.700, 1.100, 1.5, 8.100, 13.100, 3.000, 240.000, 280.000
point.3 = 2, -44.167, -99.916, 10.000, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -44.167, 99.916, 10.000, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -108, 0, -0.6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 88.417, 0, -7.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 10.000, -32.583, -8.500, 787.401, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7.0, 0.0, 0.0
point.8 = 2, 10.000, 32.583, -8.500, 787.401, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8.0, 0.0, 0.0
point.9 = 2, 14, -32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0
point.10 = 2, 14, 32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0
point.11 = 2, 105, 0, -4.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.12 = 2, 100, 0, 8.9, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.13 = 2, -127, 0, 41.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.14 = 2, -128.5, 35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 5, 9, 0, 0
point.15 = 2, -128.5, -35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 6, 9, 0, 0
point.16 = 2, -81.5, 0, -6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
//point.0 = 1, 100.6083, 0, -17.5803, 1181.1, 0, 4.521, 65, 1, 2.5, 0.7235, 13, 14, 0, 270, 270
//point.1 = 1, -6.76, -20, -18.5905, 1574.8, 1, 4.521, 8, 1.91, 2.5, 0.747, 13, 14, 2, 270, 270
//point.2 = 2, 30.8612, -31.5494, -14.1458, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.3 = 2, 30.8612, 31.5494, -14.1458, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.4 = 1, -6.76, 20, -18.5905, 1574.8, 2, 4.521, 8, 1.91, 2.5, 0.747, 12.9, 13.9, 3, 270, 270
//point.5 = 2, -115, -36, 9, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
//point.6 = 2, -38.4, -105, 12.5, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
//point.7 = 2, -115, 36, 9, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
//point.8 = 2, -38.4, 105, 12.5, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
//point.9 = 2, -116.5152, 0, 44.1266, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
//point.10 = 2, -115.5083, 0, 3.1359, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.11 = 2, -85.5589, 0, -4.8617, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.12 = 2, -56.4399, 0, -8.5634, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.13 = 2, -116.3871, 0, 3.9812, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
//point.14 = 2, 50.4709, 0, 13.0267, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.15 = 2, 120.1817, 0, 0.4276, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.16 = 5, 0.0, 0.0, -10.0, 1600, 0.0, 0.0, 50.0, 0.0, 0.0, 1.00, 1.0, 1.0, 0, 0.0, 0.0
[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[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
[airplane_geometry]
wing_area = 4604.801
wing_span = 212.58
wing_root_chord = 21.65
wing_dihedral = 3.90
wing_incidence = 1.0
wing_twist = -2
oswald_efficiency_factor = 0.91
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 5.40
wing_pos_apex_vert = -4.46
htail_area = 1089.954
htail_span = 70.04
htail_pos_lon = -100.23
htail_pos_vert = 5.78
htail_incidence = 0.0
htail_sweep = 40
vtail_area = 572.963
vtail_span = 33.23
vtail_sweep = 35
vtail_pos_lon = -94.60
vtail_pos_vert = 10.63
elevator_area = 137.0
aileron_area = 76.5
rudder_area = 232.0
elevator_up_limit = 30.0
elevator_down_limit = 20.0
aileron_up_limit = 26.0
aileron_down_limit = 25.0
rudder_limit = 25.0
elevator_trim_limit = 20.0
spoiler_limit = 45.0
aileron_to_spoileron_gain = 1.5
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 9
min_flaps_for_spoilerons = 0
spoilerons_available = 1
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 1
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
[flight_tuning]
cruise_lift_scalar=1.30
parasite_drag_scalar=1.45
induced_drag_scalar=1.45
elevator_effectiveness=1.40
aileron_effectiveness=2.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=0.5
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[TurbineEngineData]
fuel_flow_gain=0.0010 //Gain on fuel flow
inlet_area=93.800 //Square Feet, engine nacelle inlet area
rated_N2_rpm=11292 //RPM, second stage compressor rated value
static_thrust=115540 //GE90-115B Lbs, max rated static thrust at Sea Level
afterburner_available=0 //Afterburner available?
reverser_available=1 //Thrust reverser available?
[jet_engine]
thrust_scalar=0.993
[gear_warning_system]
gear_warning_available = 0 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 5.0 //Flap angle that activates warning at idle
flap_limit_power = 25.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 1 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint=103.002, -1.756, 5.20
[Flaps.0] //Inboard Krueger
type= 2
span-outboard= 0.100
extending-time= 30.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 275.000
lift_scalar= 0.0
drag_scalar= 0.0000
pitch_scalar= 0.0
flaps-position.0= 0.000, 0.000
flaps-position.1= 30.000, 265.000
[Flaps.1] //Slat
type= 2
span-outboard= 0.800
extending-time= 30.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 275.000
lift_scalar= 0.02100
drag_scalar= 0.300
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.500, 265.000
flaps-position.2= 15.500, 245.000
flaps-position.3= 15.500, 230.000
flaps-position.4= 15.500, 225.000
flaps-position.5= 30.000, 200.000
flaps-position.6= 30.000, 180.000
[Flaps.2] //Inboard Flap
type= 1
span-outboard= 0.200
extending-time= 45.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 275.000
lift_scalar= 0.4750
drag_scalar= 0.250
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.1000, 265.000
flaps-position.2= 5.000, 245.000
flaps-position.3= 15.000, 230.000
flaps-position.4= 20.000, 225.000
flaps-position.5= 25.000, 200.000
flaps-position.6= 30.000, 180.000
[Flaps.3] //Outboard Flap
type= 1
span-outboard= 0.600
extending-time= 45.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 275.000
lift_scalar= 0.4750
drag_scalar= 0.300
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.10, 265.000
flaps-position.2= 5.000, 245.000
flaps-position.3= 15.000, 230.000
flaps-position.4= 20.000, 225.000
flaps-position.5= 25.000, 200.000
flaps-position.6= 30.000, 180.000
[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, 1
Adf.1=1,1
Adf.2=1,1
Transponder.1=1
Marker.1=1
[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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[exits]
number_of_exits = 4
exit_rate.0 = 0.10 ;Percent per second
exit_rate.1 = 0.08 ;Percent per second
exit_rate.2 = 0.10 ;Percent per second
exit_rate.3 = 0.08 ;Percent per second
[Reference Speeds]
flaps_up_stall_speed=150.0 //Knots True (KTAS)
full_flaps_stall_speed=120.0 //Knots True (KTAS)
cruise_speed=482.0 //Knots True (KTAS)
max_mach = 0.90
max_indicated_speed = 330 //Red line (KIAS)
I am just looking for help in fsp
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