[fltsim.0]
title=fsp773v3 Defolt-1
sim=Boeing777-300
model=GE(ER)
panel=
sound=
texture=1
atc_id=N777
atc_airline=Soar
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=AI
ui_type=Boeing 777-300
ui_variation=Defolt-1
description=FSP Boeing 777-300 tuning by Hiro
atc_parking_types=GATE
atc_parking_codes=

[fltsim.1]
title=fsp773v3 Defolt-2
sim=Boeing777-300
model=GE(ER)
panel=
sound=
texture=2
atc_id=N777J
atc_airline=Pacifica
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=AI
ui_type=Boeing 777-300
ui_variation=Defolt-2
description=FSP Boeing 777-300 tuning by Hiro
atc_parking_types=GATE
atc_parking_codes=

[General]
visual_damage=0 		// 0=off, 1=on
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

[WEIGHT_AND_BALANCE]
max_gross_weight=660000                  // (pounds)
empty_weight=283600                      // (pounds)

reference_datum_position = 10.0, 0.0, 0.0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-12.0, 0.0, 0.0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0 =  "170.0,  86.0,  -2.0,    0.0, Pilot"                  //Weight (lbs),
station_load.1 =  "170.0,  86.0,   2.0,    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 ="24000.0, -10.0,   0.0,    0.0, Coach 10-25"            //Weight (lbs),
station_load.6 ="22400.0, -52.5,   0.0,    0.0, Coach 26-40"            //Weight (lbs),
station_load.6 ="22400.0, -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 =6500000
empty_weight_yaw_MOI  =12300000
empty_weight_coupled_MOI=0.0

[flight_tuning]
cruise_lift_scalar=1.0
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, -8.4                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=10.5,  32.6, -8.4                    //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1                            //Scalar for fuel flow efficiency
min_throttle_limit=-0.250000

[TurbineEngineData]
fuel_flow_gain=0.002                          //Gain on fuel flow
inlet_area=113.0                              //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                            //RPM, second stage compressor rated value
static_thrust=95000                           //Lbs, max rated static thrust at Sea Level
afterburner_available=0                       //Afterburner available?
reverser_available=1                          //Thrust reverser available?

[jet_engine]
thrust_scalar=0.920

[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,  90.42,   0.00, -19.25, 1181.1, 0, 4.521, 70.0, 0.45, 1.5, 0.7235, 4.0, 4.0, 0, 0.0, 0.0
point.1=1, -18.50, -17.80, -21.10, 1574.8, 1, 4.521,  0.0, 1.51, 2.5, 0.7470, 6.9, 6.9, 2, 0.0, 0.0
point.2=1, -18.50,  17.80, -21.10, 1574.8, 2, 4.521,  0.0, 1.51, 2.5, 0.7470, 7.1, 7.1, 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=-0.75
static_cg_height=19.60
gear_system_type=0

[Views]
eyepoint=103.5, -2.25, 2.0

[flaps.0]      //Inboard Trailing Edge
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.2                                  // 0.0 .. 1.0
extending-time=25                                   // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=0                                    // degrees
flaps-position.2=5                                    // degrees
flaps-position.3=15                                   // degrees
flaps-position.4=20                                   // degrees
flaps-position.5=25                                   // degrees
flaps-position.6=30                                   // degrees
damaging-speed=260                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=0.55
drag_scalar=0.55
pitch_scalar=0.55
system_type=1                                         //Hydraulic

[flaps.1]    //Outboard Trailing Edge
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=23                                   // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=0                                    // degrees
flaps-position.2=5                                    // degrees
flaps-position.3=15                                   // degrees
flaps-position.4=20                                   // degrees
flaps-position.5=25                                   // degrees
flaps-position.6=30                                   // degrees
damaging-speed=260                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=0.35
drag_scalar=0.35
pitch_scalar=0.35
system_type=1                                         //Hydraulic

[flaps.2]     //Inboard Leading Edge Slats
type=2                                    // 1 - tail, 2 - lead
span-outboard=0.5                                  // 0.0 .. 1.0
extending-time=4                                    // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=0.5                                  // degrees
flaps-position.2=0.5                                  // degrees
flaps-position.3=0.5                                  // degrees
flaps-position.4=0.5                                  // degrees
flaps-position.5=1.0                                  // degrees
flaps-position.6=1.0                                  // degrees
damaging-speed=260                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=0.05
drag_scalar=0.05
pitch_scalar=0.05
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

[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, -127.10,   0.00,  5.30, fx_strobeh ,
light.2 = 1,   -1.70,  -0.01, -11.65, fx_beaconb ,
light.3 = 1,   45.40,  -0.01,  9.90, fx_beaconb ,
light.4 = 3, -126.80,   0.00,  1.30, fx_navwhih ,
light.5 = 3, -38.08, -99.03, 5.66, fx_navredh
light.6 = 3, -38.08, 99.03, 5.66, fx_navgreh
light.7 = 2, -38.75, -99.45, 5.70, fx_strobeh
light.8 = 2, -38.75, 99.45, 5.70, fx_strobeh







[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, 26100.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  = -7.0, -35.0,  0.0,  9300.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -7.0,  35.0,  0.0,  9300.0, 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=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=0.6      	//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=26.1            	//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=-84.0                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0                 	//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=-93.3                //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=5.8                 	//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=150.0          //Knots True (KTAS)
full_flaps_stall_speed=120.0        //Knots True (KTAS)
cruise_speed=330.0                 	//Knots True (KTAS)
max_indicated_speed=330.000000
max_mach=0.900000

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
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=0.61000000
parking_brake=1

[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

[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