Merge B777-200 Overland X PSS (2D)

Pessoal,

Este é um Merge que utilizo nos meus B772 sendo aeronave da Overland e painel PSS , aqui funciona perfeitamente, para aqueles que desejam experimentar é só copiar e colar na pasta Aircraft.cfg .

Abs.

Marcio.

[fltsim.0]
title=FSPAP 777-200 BRITISH AIRWAYS
sim=PSSB777LR-GE
model=rr
panel=
sound=
texture=BAW
atc_id=G-YMML
atc_airline=SPEED BIRD
atc_flight_number=26
atc_heavy=1
ui_manufacturer=Simmer's Sky
ui_type=Boeing 777-200LR (110B1)
ui_variation=BRITISH AIRWAYS (No VC)
description=Overland Co.,Ltd. Products --- Boeing 777-200\n\nL1 Cabin Door [Shift+E] then [1]\nL2 Cabin Door Wing Fold/Extend\nCargo Door [Shift+E] then [2]\nAPU Door Tailhook Extend/Retruct


[General]
visual_damage=1 // 0=off, 1=on
atc_type=BOEING
atc_model=B772
editable=0
performance=Cruise Speed\tMach .84\nMaximum Range\t5,960 nm\nService Ceiling\t35,000 ft\nMax Takeoff Weight\t580,000 lb\nSeating\t\t305 to 440\nCargo Capacity\t7,552 CU ft\nGE90 105B

[WEIGHT_AND_BALANCE]
max_gross_weight=766000 // (pounds)
empty_weight=315000 // (pounds)

reference_datum_position=0, 0,-3 // (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=50

station_load.0 = "170.0, 97.0, -2.25, 0.0, Pilot" //Weight (lbs),
station_load.1 = "170.0, 97.0, 2.25, 0.0, Co-Pilot" //Weight (lbs),
station_load.2 = "850.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs),
station_load.3 = "1920.0, 72.0, 0.0, 0.0, First Class" //Weight (lbs),
station_load.4 ="14400.0, 31.0, 0.0, 0.0, Coach 1-9" //Weight (lbs),
station_load.5 ="14000.0, -10.0, 0.0, 0.0, Coach 10-25" //Weight (lbs),
station_load.6 ="12400.0, -52.5, 0.0, 0.0, Coach 26-40" //Weight (lbs),
station_load.6 ="12400.0, -72.5, 0.0, 0.0, Coach 41-55" //Weight (lbs),
station_load.7 = "2000.0, 47.0, 0.0, -6.0, Forward Cargo" //Weight (lbs),
station_load.8 = "500.0, -67.0, 0.0, -6.0, Aft Cargo" //Weight (lbs),

;Moments of Inertia
empty_weight_pitch_MOI=8000000
empty_weight_roll_MOI=15500000
empty_weight_yaw_MOI=12300000
empty_weight_coupled_MOI=0.0

[flight_tuning]
cruise_lift_scalar=1.07
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=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0


[GeneralEngineData]
engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=10.5, -32.6, -5.4 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=10.5, 32.6, -5.4 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 0.950
min_throttle_limit = -0.51

[TurbineEngineData]
fuel_flow_gain=0.001 //Gain on fuel flow
inlet_area=99.35 //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920 //RPM, second stage compressor rated value
static_thrust=110100 //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

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 0
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

//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, 85.82, 0.00, -16.38, 1181.1, 0, 4.521, 70.0, 0.83, 2.5, 0.7235, 11.2, 11.2, 0, 0.0, 0.0
point.1=1, -9.50, -17.30, -16.90, 1574.8, 1, 4.521, 0.0, 0.91, 1.5, 0.6470, 11.9, 11.9, 2, 0.0, 0.0
point.2=1, -9.50, 17.30, -16.90, 1574.8, 2, 4.521, 0.0, 0.91, 1.5, 0.6470, 11.1, 11.1, 3, 0.0, 0.0
point.3=2, -10.17, -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, -10.17, 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, -83.33, 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

static_pitch= -0.41
static_cg_height=19.30
gear_system_type=1

//[smokesystem]
smoke.0 = 5.9, -26.2, 77.2, fx_pss_fuel_jett
smoke.1 = 5.9, -26.2, -77.3, fx_pss_fuel_jett

[Views]
eyepoint=96.3, -2.19, 5.2

[Flaps.0] //Inboard Krueger
type= 2
span-outboard= 0.100
extending-time= 15.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 270.000
lift_scalar= 0.0
drag_scalar= 0.0000
pitch_scalar= 0.0
flaps-position.0= 0.000, 0.000
flaps-position.1= 30.000, 255.000

[Flaps.1] //Slat
type= 2
span-outboard= 0.800
extending-time= 15.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 270.000
lift_scalar= 0.02100
drag_scalar= 0.300
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.500, 255.000
flaps-position.2= 15.500, 235.000
flaps-position.3= 15.500, 215.000
flaps-position.4= 15.500, 195.000
flaps-position.5= 30.000, 185.000
flaps-position.6= 30.000, 170.000

[Flaps.2] //Inboard Flap
type= 1
span-outboard= 0.200
extending-time= 25.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 270.000
lift_scalar= 0.4950
drag_scalar= 0.250
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.1000, 255.000
flaps-position.2= 5.0000, 235.000
flaps-position.3= 15.000, 215.000
flaps-position.4= 20.000, 195.000
flaps-position.5= 25.000, 185.000
flaps-position.6= 30.000, 170.000

[Flaps.3] //Outboard Flap
type= 1
span-outboard= 0.600
extending-time= 25.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 270.000
lift_scalar= 0.4950
drag_scalar= 0.300
pitch_scalar= 0.00
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.10, 235.000
flaps-position.2= 5.000, 215.000
flaps-position.3= 15.000, 196.000
flaps-position.4= 20.000, 195.000
flaps-position.5= 25.000, 185.000
flaps-position.6= 30.000, 170.000

[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

[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


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1 = 2, -104.60, 0.00, 8.30, fx_shockwave_strobe_l_2 ,
light.2 = 1, 8.40, -0.01, -8.65, fx_shockwave_beaconb ,
light.3 = 1, 38.30, -0.01, 12.90, fx_shockwave_beaconh ,
light.4 = 3, -104.40, 0.00, 4.30, fx_shockwave_navwhi_l_nl ,
light.5 = 4, 97, 3, 5.5, fx_shockwave_vclight_l ,
light.6 = 5, 33.80, 12.26, -1.8, fx_shockwave_landing_light_narrow ,
light.7 = 5, 33.80, -12.26, -1.8, fx_shockwave_landing_light_narrow ,
light.8 = 6, 87.00, 0.0, -7.30, fx_shockwave_landing_light_double_small ,
light.9 = 4, 97, -3, 5.5, fx_shockwave_vclight_l

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
startup = fx_pss_startup, 1
windshield_rain_effect_available = 1

[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second


[fuel]
Center1 = 1.0, 0.0, -4.0, 20550, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -6.0, -30.0, 0.0, 9300.0, 2.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -6.0, 30.0, 0.0, 9300.0, 2.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = -9, -49, 0.0, 4370, 0
RightAux = -9, 49, 0.0, 4370, 0
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=4
electric_pump=1

[airplane_geometry]
wing_area=4605.0 //Square feet
wing_span=199.92 //Feet
wing_root_chord=23.0 //Feet
wing_dihedral=6.2 //Degrees
wing_incidence=1.0 //Degrees
wing_twist=-0.5 //Degrees
oswald_efficiency_factor=0.864 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=32.0 //Degrees, wing leading edge
wing_pos_apex_lon=38.1 //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=1090.0 //Square feet
htail_span=70.7 //Feet
htail_pos_lon=-74.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=5.0 //Feet, vertical distance from reference point, positive going up
htail_incidence=0.0 //Degrees
htail_sweep=40.0 //Degrees, horizontal tail leading edge
vtail_area=573.0 //Square feet
vtail_span=27.3 //Feet, tip to body
vtail_sweep=35.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-63.3 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=12.8 //Feet, vertical distance from reference point, positive going up
elevator_area=137.0 //Square feet
aileron_area=68.0 //Square feet
rudder_area=232.0 //Square feet
elevator_up_limit=30.0 //Degrees
elevator_down_limit=30.0 //Degrees
aileron_up_limit=30.0 //Degrees
aileron_down_limit=15.0 //Degrees
rudder_limit=25.0 //Degrees
elevator_trim_limit=20.0 //Degrees
spoiler_limit=60.0 //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

[Reference Speeds]
flaps_up_stall_speed=138.0 //Knots True (KTAS)
full_flaps_stall_speed=122.0 //Knots True (KTAS)
cruise_speed=482.0 //Knots True (KTAS)
max_mach = 0.90
max_indicated_speed = 350

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required= 1
autothrottle_max_rpm = 108.5
autothrottle_takeoff_ga= 1
pitch_takeoff_ga=8 ;
max_pitch=10.0
max_pitch_acceleration=0.88
max_pitch_velocity_lo_alt=0.7
max_pitch_velocity_hi_alt=0.4
max_pitch_velocity_lo_alt_breakpoint=11000.0
max_pitch_velocity_hi_alt_breakpoint=25000.0
max_bank=25.0
max_bank_acceleration=1.4
max_bank_velocity=2.8
max_throttle_rate=0.08
nav_proportional_control=11.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=19.0
gs_integrator_control=0.530
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.110



[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=0.7000000
parking_brake=1
differential_braking_scale = 1.0

[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

[hydraulic_system]
electric_pumps=1
engine_map=1,1,0,0
normal_pressure=3000.000000

[stall_warning]
type=2

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 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