[fltsim.0]
title=Boeing 777-200LR Emirates
sim=777200LR
model=
panel=
sound=
texture=EMU
ui_manufacturer=Boeing
ui_type=777-200LR
ui_variation=Emirates
ui_typerole="Commercial Airliner"
ui_createdby="D. Grindele/D. Trapp"
atc_id=A6-EMD
atc_airline=Emirates
atc_flight_number=221
atc_parking_types=GATE_HEAVY, RAMP_GA_LARGE
atc_parking_codes=UAE
atc_heavy=1
description="Boeing 777-200LR for FSX:\n\nThis model is an accurate representation of the aircraft used by Emirates for non-stop flights from OMDB-KDFW and back.\n\nFirst landing at DFW was at 08:45 CST, 2 February 2012.\nFirst takeoff from DFW was at 11:55 CST, 2 February 2012.\n\nTextures By: David Grindele\nSound By: Luke Hogan\nPanel BY: Marco Spada\nReal World Flight/Engine Dynamics and Data By:\nDouglas E. Trapp\nFS Flight Dynamics Engineer\nKC6ZOF@Yahoo.com\nFebruary 2012\n"
[CameraDefinition.0]
Title = "Landing Gear"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the landing gear and left wing inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .58
ShowWeather = Yes
InitialXyz = -11, -4.1, -16
InitialPbh = 0, 0, 44
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Left Side Window"
Guid = {0ae3f864-da10-4e5a-977c-b9bba47d6f7a}
Description = View of the left wing from the passenger cabin
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -5.5, 0.75, -13
InitialPbh = 0, 0, 265
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.2]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 40.8, 1.4, 4.0
InitialPbh = 6, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[General]
performance="Length: 209.083 ft\nHeight At Tail: 61.5 ft\nWingspan: 212.583 ft\nPowerplant:\n2 General Electric GE90-115B1 Turbofan @ 115,300 lbf ea\nVMO/MMO: 331 KIAS/Mach .9\nCockpit Crew: 2\nAttendents: 15\nPassengers: 301\nTotal Souls Onboard: 318\nPayload: 89,953 lb\nService Ceiling: 43,100 ft\nEmpty Weight: 320,000 lb\nMTOW: 766,000 lb\nTaxi Weight: 768,000 lb\nMLW: 492,000 lb (23% Fuel Remaining)\nFuel Capacity: 53,440 US Gal\nRange: 8,865 nm @ FL350E, Mach .84\nMax Range: 9,400 nm @ FL410E, Mach .84\nNormal Cruise Speed: Mach .84\n"
atc_type=BOEING
atc_model=B772
editable=1
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 766000 // (pounds)
empty_weight = 320000 // (pounds)
reference_datum_position = 0, 0, 0 // (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
//Taxi Weight = 768,000 lb
//Souls = 318 = 62,010 lb (17 Crew, 301 Pax)
//Cargo = 32,232 lb
//Payload = 89,953 lb
station_load.0 = "195.000000,90.000000,-5.000000,8.000000,Pilot 1"
station_load.1 = "195.000000,90.000000,5.000000,8.000000,Pilot 2"
station_load.2 = "3315.000000,80.000000,0.000000,7.000000,16+1 1st Class Fore"
station_load.3 = "11895.000000,45.000000,0.000000,7.000000,58+3 Business Fore"
station_load.4 = "8190.000000,0.000000,0.000000,7.000000,40+2 Economy Cntr"
station_load.5 = "38220.000000,-45.000000,0.000000,7.000000,187+9 Economy Aft"
station_load.6 = "25281.000000,64.542000,0.000000,-8.000000,Cargo Fore"
station_load.7 = "2662.000000,-33.541667,0.000000,-6.000000,Cargo Aft"
;Moments of Inertia
empty_weight_pitch_MOI = 18000000
empty_weight_roll_MOI = 5500000
empty_weight_yaw_MOI = 16300000
empty_weight_coupled_MOI= 0.0
[fuel]
//47,890 US Gal = 321,466 lb (wings)
//5,550 US Gal = 37,185 lb (fuselage)
//53,440 US Gal = 358,048 lb (total)
LeftMain = 0.0, -35.0, 0.0, 23945.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 0.0, 35.0, 0.0, 23945.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1 = -23.0, 0.0, -8.0, 1850.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2 = -33.0, 0.0, -8.0, 1850.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center3 = -43.0, 0.0, -8.0, 1850.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
fuel_dump_rate = 0.0167 //Percent of max quantity per second, i.e. about 1 minute for full fuel
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 4605.0 //Square feet
wing_span = 212.583 //Feet
wing_root_chord = 40.000 //Feet
wing_aspect_ratio = 8.68 //
wing_dihedral = 7.0 //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 = 31.64 //Degrees, wing leading edge
wing_pos_apex_lon = 25.0 //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 = 1150.0 //Square feet
htail_span = 70.625 //Feet
htail_pos_lon = -100.0 //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 = 31.64 //Degrees, horizontal tail leading edge
vtail_area = 585.0 //Square feet
vtail_span = 32.917 //Feet, tip to body
vtail_sweep = 41.64 //Degrees, vertical tail leading edge
vtail_pos_lon = -108.3 //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 = 140.0 //Square feet
aileron_area = 65.0 //Square feet
rudder_area = 225.0 //Square feet
elevator_up_limit = 30.0 //Degrees
elevator_down_limit = 25.0 //Degrees
aileron_up_limit = 30.0 //Degrees
aileron_down_limit = 10.0 //Degrees
rudder_limit = 27.3 //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
auto_spoiler_available=1
spoiler_extension_time=1.500000
positive_g_limit_flaps_up=4.273504
positive_g_limit_flaps_down=3.205128
negative_g_limit_flaps_up=-3.205128
negative_g_limit_flaps_down=-2.136752
[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_indicated_speed=331.0
max_mach=0.9
[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 = 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 = 250 // KIAS
blowout-speed = 290 // KIAS
lift_scalar = 0.65
drag_scalar = 0.60
pitch_scalar= 0.05
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 = 25 // 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 = 250 // KIAS
blowout-speed = 290 // KIAS
lift_scalar = 0.40
drag_scalar = 0.40
pitch_scalar= 0.05
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 = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0.5 // degrees
flaps-position.2 = 0.6 // degrees
flaps-position.3 = 0.7 // degrees
flaps-position.4 = 0.8 // degrees
flaps-position.5 = 0.9 // degrees
flaps-position.6 = 1.0 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 290 // KIAS
lift_scalar = 0.10
drag_scalar = 0.05
pitch_scalar= 0.05
system_type = 1 //Hydraulic
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.750
aileron_effectiveness=2.002
rudder_effectiveness=1.250
pitch_stability=1.250
roll_stability=1.250
yaw_stability=1.250
elevator_trim_effectiveness=1.250
aileron_trim_effectiveness=1.250
rudder_trim_effectiveness=1.250
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1500.0
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_max_rpm = 112
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=30.000000
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
[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 = 0.8 //Scalar for fuel flow efficiency
ThrustSpecificFuelConsumption=0.817 //Percent FSC
min_throttle_limit=-0.299927 //Max Reverse Thrust
[SMOKESYSTEM]
smoke.0=0.5, -32.6, -8.4, fx_smoke_f6
smoke.1=0.5, 32.6, -8.4, fx_smoke_f6
[TurbineEngineData]
//GE90-115B1 Real World Data
fuel_flow_gain = 0.002 //Gain on fuel flow
bypass_ratio = 9.0 //N1-N2 Pressure Gain Ratio
inlet_area = 90.508532 //Square Feet, engine nacelle inlet area
bypass_ratio=9.0
rated_N1_rpm= 2355.000
rated_N2_rpm= 9332.000
static_thrust = 115300 //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
[Views]
eyepoint = 90.0, -2.65, 2.25
[contact_points]
//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, 87.42, 0.00, -17.50, 1181.1, 0, 3.500, 70.0, 1.0, 2.5, 0.7200, 15.0, 15.0, 0, 0.0, 0.0
point.1=1, -19.50, -12.00, -19.00, 1574.8, 1, 4.167, 20.0, 1.0, 2.5, 0.7500, 15.0, 15.0, 2, 0.0, 0.0
point.2=1, -19.50, 12.00, -19.00, 1574.8, 2, 4.167, 20.0, 1.0, 2.5, 0.7500, 15.0, 15.0, 3, 0.0, 0.0
point.3=2, -14.17, -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, -14.17, 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
static_cg_height = 17.56
gear_system_type=0
[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
[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
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[exits]
number_of_exits = 2
exit.0= 0.10, 62.600, -7.000, 7.000, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.1= 0.09, -21.500, 5.500, -6.800, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
[TailHook]
tailhook_length=1 ;(feet)
tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0
[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.075,0.075 ;Percent per second
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -102.25, 0.00, 6.25, fx_shockwave_navwhi_l_nl ,
light.1=2, -102.25, 0.00, 3.00, fx_shockwave_strobe_l_nl ,
light.2=1, 39.00, 0.00, 10.50, fx_shockwave_beaconh ,
light.3=1, 20.25, 0.00, -11.50, fx_shockwave_beaconb ,
light.4=4, 103.50, 0.00, 5.50, fx_shockwave_vclight_l ,
light.5=5, 35.70, -12.00, -3.80, fx_Shockwave_landing_light // Shockwave light
light.6=5, 35.70, 12.00, -3.80, fx_Shockwave_landing_light // Shockwave light
light.7=5, 90.10, -0.42, -9.50, fx_Shockwave_landing_light // Shockwave light
light.8=5, 90.10, 0.42, -9.50, fx_Shockwave_landing_light // Shockwave light
light.9=2, -28.10, -100.10, 6.00, fx_shockwave_strobe_l_nl ,
light.10=2, -28.10, 100.10, 6.00, fx_shockwave_strobe_l_2 ,
[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
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 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
[brakes]
toe_brakes_scale=1.0
parking_brake=1
auto_brakes=4
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=29.220848
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=1
