Thanks hansatdg for your help: compiled, closed and reopened but no "The fruit stand" shows under AirFrance B777 all pax model ...
[General]
atc_type=BOEING
atc_model=B773
editable=0
performance=Cruise Speed\tMach .84\nMaximum Range\t5,720 nm\nService Ceiling\t35,000 ft\nMax Takeoff Weight\t660,000 lb\nSeating\t\t336 to 550\nCargo Capacity\t20 standard LD3 containers \n
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
[weight_and_balance]
max_gross_weight = 151000
empty_weight = 103170
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 9, 0, 0
empty_weight_pitch_MOI = 3160000
empty_weight_roll_MOI = 3262183
empty_weight_yaw_MOI = 4337024
empty_weight_coupled_MOI = 0
max_number_of_stations = 9
station_load.0 = "170.0, 41.0, -1.5, 0.0, Pilot"
station_load.1 = "170.0, 41.0, 1.5, 0.0, Co-Pilot"
station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew"
station_load.3 = "1360.0, 25.5, 0.0, 0.0, First Class"
station_load.4 = "8160.0, 11.0, 0.0, 0.0, Coach 3-10"
station_load.5 = "8160.0, -10.0, 0.0, 0.0, Coach 11-18"
station_load.6 = "7140.0, -30.5, 0.0, 0.0, Coach 19-25"
station_load.7 = "10000.0, 20.5, 0.0, 0.0, Forward Baggage"
station_load.8 = "4000.0, -27.5, 0.0, 0.0, Aft Baggage"
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -30.49, -100.25, 8.63, fx_navred
light.1 = 3, -30.49, 100.25, 8.63, fx_navgre
light.2 = 3, -119.90, 0, 4.77, fx_navwhi
light.3 = 3, -41.33, -107.27, 9.30, fx_navwhi
light.4 = 3, -41.33, 107.27, 9.30, fx_navwhi
light.5 = 2, -31.56, -101.09, 8.72, fx_strobe
light.6 = 2, -31.56, 101.09, 8.72, fx_strobe
light.7 = 2, -119.90, 0, 8.49, fx_strobe
light.8 = 1, 9.42, 0, -8.50, fx_beaconb
light.9 = 1, 55.09, 0, 13.35, fx_beaconb
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1
engine.0 = 10.76, -31.96, -6.84,
engine.1 = 10.76, 31.96, -6.84,
min_throttle_limit=-0.1400
max_contrail_temperature=-25
[TurbineEngineData]
fuel_flow_gain=0.002 //Gain on fuel flow..
inlet_area=19.6 //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920 //RPM, second stage compressor rated value
static_thrust=28000 //Lbs, max rated static thrust at Sea Level
afterburner_available=0 //Afterburner available?
reverser_available=1 //Thrust reverser available?
[jet_engine]
thrust_scalar=1.0
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 1
Center1 = 0, 0, 0, 2313, 0
LeftMain = -3, -19, 0, 1500, 0
RightMain = -3, 19, 0, 1500, 0
electric_pump=0
[contact_points]
static_pitch = -0.45
static_cg_height = 16.35
max_number_of_points = 7
point.0 = 1, 99.8100, 0.0, -16.173, 1574.8, 0, 1.442, 55.92, 0.8, 2.5, 0.6, 6.0, 6.0, 0, 220, 250
point.1 = 1, -8.5822, -18, -17.4528, 1574.8, 1, 1.442, 0.000, 1.0, 2.5, 0.9, 8.9, 8.9, 2, 220, 250
point.2 = 1, -8.5822, 18, -17.4528, 1574.8, 2, 1.442, 0.000, 1.0, 2.5, 0.9, 9.1, 9.1, 3, 220, 250
point.3 = 2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4 = 2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5 = 2, -66.70, 0.00, -7.03, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6 = 2, 114.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
gear_system_type=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 = 2337.0
wing_span = 126.46
wing_root_chord = 28.58
wing_dihedral = 6.19
wing_incidence = 1.0
wing_twist = -0.5
oswald_efficiency_factor = 0.85
wing_winglets_flag = 0
wing_sweep = 28
wing_pos_apex_lon = 18.58
wing_pos_apex_vert = 0
htail_area = 338.0
htail_span = 50.15
htail_pos_lon = -59.65
htail_pos_vert = 0
htail_incidence = 0.0
htail_sweep = 34
vtail_area = 224.0
vtail_span = 28.77
vtail_sweep = 42
vtail_pos_lon = -50.76
vtail_pos_vert = 5.53
elevator_area = 70.5
aileron_area = 26.9
rudder_area = 56.2
elevator_up_limit = 22.5
elevator_down_limit = 19.5
aileron_up_limit = 20.0
aileron_down_limit = 20.0
rudder_limit = 26.0
elevator_trim_limit = 20.0
spoiler_limit = 60.0
aileron_to_spoileron_gain = 3
min_ailerons_for_spoilerons = 10
min_flaps_for_spoilerons = 0
spoilerons_available = 1
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
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=1.2
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=0.8
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[gear_warning_system]
gear_warning_available = 1 //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 = 0.485 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint=43.7, -1.31, 3.7 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 20 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 1 // degrees
flaps-position.2 = 2 // degrees
flaps-position.3 = 5 // degrees
flaps-position.4 = 10 // degrees
flaps-position.5 = 15 // degrees
flaps-position.6 = 25 // degrees
flaps-position.7 = 30 // degrees
flaps-position.8 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.1
drag_scalar = 0.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.1] //Inboard Leading Edge Flaps
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 4 // seconds
flaps-position.0 = 0 //
flaps-position.4 = 0.5
flaps-position.5 = 1.0 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.1
drag_scalar = 0.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.2] //Outboard Leading Edge Slat
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 7 // seconds
flaps-position.0 = 0 //
flaps-position.4 = 0.5
flaps-position.5 = 1.0 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.1
drag_scalar = 0.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[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
[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 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8 ;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=30.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[Reference Speeds]
flaps_up_stall_speed = 150.0 //Knots True (KTAS)
full_flaps_stall_speed = 120.0 //Knots True (KTAS)
cruise_speed = 494.0 //Knots True (KTAS)
max_mach = 0.85
max_indicated_speed = 330 //Red line (KIAS)
[stall_warning]
type=2