[fltsim.0]
title=Project Opensky Boeing 777-300ER General Electric 90-115B1 kawa
sim=Boeing 777-300ER General Electric 90-115B1
model=
panel=
sound=
texture=ka
checklists=
atc_airline=KAWA
atc_id=KCFS223
atc_flight_number=223
atc_heavy=1
atc_parking_types=GATE, RAMP
atc_parking_codes=KAL
ui_manufacturer=Project Opensky
ui_type=Boeing 777-300ER
ui_variation=KAWA Airlines
visual_damage=1
description=Project Opensky Boeing 777-300\nVersion 2-2008.1.0\n\nModel Designers\n   Hiroshi Igami\n   Yosuke Ube\n\nMaster Textures\n   Yosuke Ube\n\nFlight Dynamics Designer\n   Brandon D. Henry\n\nFlight Dynamics Assistant\n   Philip Foglar\n\nSound Designer\n   Emil Serafino\n\nTechnical Resource\n   Aaron Seymour\n\nTest Pilots\n   Project Opensky Members\n\nMaximun Range:\n   7,930 nautical miles (14,685 km)\n\n\nTypical city pairs: \nSan Francisco - Tokyo\nTokyo - Singapore\n Honolulu - Seoul
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0


[weight_and_balance]
max_gross_weight = 660000
empty_weight = 347800
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 41600000
empty_weight_roll_MOI = 42000000
empty_weight_yaw_MOI = 67500000
empty_weight_coupled_MOI = 1000
max_number_of_stations = 7

station_load.0 = "4200, 70, 0, 5, 1st Class - 24 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)  
station_load.1 = "9450, 40, 0, 5, Business Class - 54 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)  
station_load.2 = "28875, -10, 0, 5, Econ Front - 165 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)  
station_load.3 = "20125, -55, 0, 5, Econ Rear - 115 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)  
station_load.4 = "11250, 50, 0, 0, Fore Cargo" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)  
station_load.5 = "11250, -50, 0, 0, Aft Cargo " //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)  
station_load.6 = "1000, -70, 0, 0, Bulk Cargo" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)  


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 1, 28.5, 0, 12.4, Opensky_beacon
light.1 = 1, 4.75, 0, -9, Opensky_beacon
light.2 = 3, -127, 0, 4.5, Opensky_nav_yellow
light.3 = 8, 32.7, -10.1, 1.3, Opensky_nav_yellow
light.4 = 8, 32.7, 10.1, 1.3, Opensky_nav_yellow
light.5 = 4, 105, 0, 5.4, Opensky_747_vclight
light.6 = 2, -127.9, 0, 8.5, fx_strobeh
light.7 = 4, 105, -2.2, 5.328, Opensky_747_vclight
light.8 = 4, 105, 2.2, 5.328, Opensky_747_vclight
light.9 = 8, 12.5, 23, 0, Opensky_nacelle_refl
light.10 = 8, 12.5, -23, 0, Opensky_nacelle_refl
light.11 = 8, 25, 30, 0, Opensky_wing_light
light.12 = 8, 25, -30, 0, Opensky_wing_light
light.13 = 8, 0, 56, 0, Opensky_wing_light
light.14 = 8, 0, -56, 0, Opensky_wing_light

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 0.735
min_throttle_limit = -0.32
engine.0 = 10.0, -32.583, -10.500
engine.1 = 10.0,  32.583, -10.500

[smokesystem]
smoke.0 = -15, 22, 32, Opensky_revspray
smoke.1 = -15, 22, -32, Opensky_revspray

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = opensky_sparks, 1
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 3
electric_pump = 1

Center1 = 10, 0, -4, 14220, 10
LeftMain = -5, -35, 0, 6200, 6
LeftAux = -10, -49.705, 0, 9300, 6
RightMain = -5, 35, 0, 6200, 6
RightAux = -10, 49.705, 0, 9300, 6


[contact_points]
static_pitch = 0
static_cg_height = 14.5
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 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)

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


//[contact_points]
//static_pitch = 0
//static_cg_height = 16.4
//tailwheel_lock = 0
//gear_system_type = 1
//max_number_of_points = 28

        //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)

//point.0 = 1, 91.243, -1.5, -16.5, 1881.102, 0, 1.6, 70, 1, 1.8, 2.4, 7, 9, 0, 240, 280
//point.1 = 1, 91.243,  1.5, -16.5, 1881.102, 0, 1.6, 70, 1, 1.8, 2.4, 7, 9, 0, 240, 280

//point.2 = 1,  -14.800, -20.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280
//point.3 = 1,  -14.800, -15.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280
//point.4 = 1,   -9.800, -20.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280
//point.5 = 1,   -9.800, -15.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280
//point.6 = 1,   -5.000, -20.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280
//point.7 = 1,   -5.000, -15.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280
//point.8 = 1,  -14.800,  20.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280
//point.9 = 1,  -14.800,  15.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280
//point.10 = 1,  -9.800,  20.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280
//point.11 = 1,  -9.800,  15.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280
//point.12 = 1,  -5.000,  20.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280
//point.13 = 1,  -5.000,  15.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280


//point.14 = 2,  -44.167, -99.916,  10.000,  787.401, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
//point.15 = 2,  -44.167,  99.916,  10.000,  787.401, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
//point.16 = 2, -108, 0, -0.6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
//point.17 = 2, 88.417, 0, -7.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.18 = 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.19 = 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.20 = 2, 14, -32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0
//point.21 = 2, 14, 32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0
//point.22 = 2, 105, 0, -4.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.23 = 2, 100, 0, 8.9, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
//point.24 = 2, -127, 0, 41.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
//point.25 = 2, -128.5, 35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 5, 9, 0, 0
//point.26 = 2, -128.5, -35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 6, 9, 0, 0
//point.27 = 2, -81.5, 0, -6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0


[keyboard_response]
elevator = 100.000, 200.000
aileron = 100.000, 200.000
rudder = 100.000, 200.000


[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1.0
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[airplane_geometry]
wing_area = 4605.000
wing_span = 205
wing_root_chord = 50.000
wing_dihedral = 6.218
wing_incidence = 1.000
wing_twist = -0.500
oswald_efficiency_factor = 0.600
wing_winglets_flag = 1
wing_sweep = 35
wing_pos_apex_lon = 30.000
wing_pos_apex_vert = 0.000
htail_area = 1291
htail_span = 70
htail_pos_lon = -96.5
htail_pos_vert = 5
htail_incidence = 0.000
htail_sweep = 40.000
vtail_area = 573.000
vtail_span = 35
vtail_sweep = 45
vtail_pos_lon = -85
vtail_pos_vert = 8.800
elevator_area = 137.000
aileron_area = 68.000
rudder_area = 232.000
elevator_up_limit = 24.000
elevator_down_limit = 18.000
aileron_up_limit = 24.000
aileron_down_limit = 18.000
rudder_limit = 32.000
elevator_trim_limit = 16.000
spoiler_limit = 45.000
aileron_to_spoileron_gain = 1.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 12.000
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 = 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

[flight_tuning]
cruise_lift_scalar=1.00 
parasite_drag_scalar=0.55 
induced_drag_scalar=0.88 
elevator_effectiveness=1.00 
aileron_effectiveness=1.60 
rudder_effectiveness=1.00 
pitch_stability=1.00 
roll_stability=1.00 
yaw_stability=1.00 
elevator_trim_effectiveness=0.40 
aileron_trim_effectiveness=0.50 
rudder_trim_effectiveness=0.50 

[General]
performance=Passengers\n3-class conf: 301 \n2-class conf: N/A \n1-class conf: N/A\n\nCargo\n14 LD-3 containers aft \n600 cubic Ft (17 cubic m)\nTotal lower hold volume: 7,120 cu ft \n\nDimensions\nSpan 212 ft 7 in\nLength 242 ft 4 in\nHeight 61 ft 5 in \n  (--max  58 ft 8 in--min)\n\nEngines: General Electric 90-115B1\nTO Thrust Rating: 115,100 lb\n\nMax Fuel Cap.: 47,890 gal\nMaxTOW: 775,000 lb\nZFW: 524,000 lb\n\nMax Range: 7,930 nautical miles (14,685 km)\nTypical Cruise Speed \n  @ FL350: M.84 
atc_type=BOEING 
atc_model=B773 
editable=0 

[pitot_static]
vertical_speed_time_constant=999		//Increasing this value will cause a more instantaneous reaction in the VSI

[jet_engine]
thrust_scalar=1.000 

[TurbineEngineData]
bypass_ratio=6.400000
fuel_flow_gain=0.001 
inlet_area=65.962 
rated_N2_rpm=29920.000 
static_thrust=115100.000 
afterburner_available=0 
reverser_available=1 

[Reference Speeds]
flaps_up_stall_speed=174.000 
full_flaps_stall_speed=158.000
cruise_speed=485.00 
max_indicated_speed=330.000000
max_mach=0.890020

[Views]
eyepoint=104.000, -1.756, 5.15

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=800.000 
autothrottle_available=1 
autothrottle_arming_required= 1
autothrottle_takeoff_ga= 1
autothrottle_max_rpm= 110.000
pitch_takeoff_ga=8.00  //0.000
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=0.300000
max_pitch_velocity_lo_alt_breakpoint= 7000.000000
max_pitch_velocity_hi_alt_breakpoint=24000.000000
max_bank=30.000000
max_bank_acceleration=1.200000
max_bank_velocity=2.000000
max_throttle_rate=0.024
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=1.000000

[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 

[flaps.0]      //Inboard Trailing Edge
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 4.2                                  // 0.0 .. 1.0
extending-time   = 35                                   // 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 = 0.82
drag_scalar = 0.95
pitch_scalar= 0.60
system_type = 1                                         //Hydraulic

[flaps.1]    //Outboard Trailing Edge
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 4.8                                  // 0.0 .. 1.0
extending-time   = 35                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 5                                    // degrees
flaps-position.2 = 10                                    // 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 = 0.40
drag_scalar = 0.50
pitch_scalar= 0.30
system_type = 1                                         //Hydraulic

[flaps.2]     //Inboard Leading Edge Slats
type             = 2                                     // 1 - tail, 2 - lead
span-outboard    = 4.5                                   // 0.0 .. 1.0
extending-time   = 18                                    // seconds
flaps-position.0 = 0                                     // degrees
flaps-position.1 = 5                                     // degrees
flaps-position.2 = 5                                     // degrees
flaps-position.3 = 5                                     // degrees
flaps-position.4 = 5                                     // degrees
flaps-position.5 = 20                                    // degrees
flaps-position.6 = 20                                    // degrees
damaging-speed   = 260                                   // KIAS
blowout-speed    = 300                                   // KIAS
lift_scalar = 0.30
drag_scalar = 0.30
pitch_scalar= 0.30
system_type = 1                                          //Hydraulic

[direction_indicators]
direction_indicator.0=3,0 

[brakes]
toe_brakes_scale=0.580
parking_brake=1
[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
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[TailHook]    // For opening cargo door.
tailhook_length=1                               ;(feet)
tailhook_position = 0.0, 0.0, 0.0            ;(feet) longitudinal, lateral, vertical positions from datum
[folding_wings]  // For opening main deck cargo door.
wing_fold_system_type = 4                       ;0=None
fold_rates = 0.05,1.00                    ;Percent per second
[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

