[fltsim.0]
title=Plane0  FREEWARE_COPYRIGHT_TenkuuDevelopersStudio_01JUN2013 OPTANT1110000000_OPTDEC00000 TDS B787-8 Qantas airways VH-EAA
sim=Boeing 787-800 GE
model=
panel=
sound=
texture=Qantas
checklists=
atc_airline=Qantas
atc_id=QF111
atc_flight_number=12
atc_heavy=1
atc_parking_types=GATE,RAMP
atc_parking_code=QFA
ui_manufacturer=TDS
ui_type=787-8
ui_variation=Qantas airways
visual_damage=1
description=The Boeing 787 Dreamliner is a long-range, mid-size wide-body, twin-engine jet airliner developed by Boeing Commercial Airplanes. It seats 210 to 290 passengers, depending on the variant. Boeing states that it is the company's most fuel-efficient airliner and the world's first major airliner to use composite materials for most of its construction.[4] The 787 consumes 20% less fuel than the similarly-sized Boeing 767.[5] Some of its distinguishing features include a four-panel windshield, noise-reducing chevrons on its engine nacelles, and a smoother nose contour.  The aircraft's initial designation was 7E7, prior to its renaming in January 2005.[6] The first 787 was unveiled in a roll-out ceremony on July 8, 2007, at Boeing's Everett assembly factory, by which time it had become the fastest-selling wide-body airliner in history with 677 orders.[7] By October 2011, 797 Boeing 787s had been ordered by 57 customers, with ILFC having the largest number on order.[8]  The 787 development and production has involved a large-scale collaboration with numerous suppliers around the globe. Final assembly is at the Boeing Everett Factory in Everett, Washington. Aircraft will also be assembled at a new factory in North Charleston, South Carolina. Both sites will deliver 787s to airline customers. Originally planned to enter service in May 2008, the project has suffered from multiple delays. The airliner's maiden flight took place on December 15, 2009, and completed flight testing in mid-2011. Final Federal Aviation Administration and European Aviation Safety Agency certification was received in late August 2011 and the first model was delivered in late September 2011. It entered commercial service on October 26, 2011.
\n\nTypical city pairs: \n   London-LA\n   LA-Tokyo\n   Tokyo-Sydney
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0


[weight_and_balance]

max_gross_weight = 502433
empty_weight = 252499
reference_datum_position = 10, 0, 0
empty_weight_CG_position = -10, 0, 0
empty_weight_pitch_MOI = 18000000
empty_weight_roll_MOI = 5500000
empty_weight_yaw_MOI = 16300000
empty_weight_coupled_MOI = 2048
max_number_of_stations = 5

station_load.0 = 3450, 34.07, 0, -0.24
station_load.1 = 3450, -8.69, 0, 0
station_load.2 = 8400, -54.10, 0, 0
station_load.3 = 7000, 36.44, 0, -5.62, F. Cargo
station_load.4 = 7000, -47.88, 0, -5.62, R. Cargo


[lights]

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

light.0 = 8, 7.7, -27, -1, tdsb8_wing_light
light.1 = 8, 7.7, 27, -1, tdsb8_wing_light
light.2 = 3, 54.787, 0, -8.5, tdsnose_gearwell
light.3 = 3, 54.787, 0, -8.5, fx_beaconb

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 0.50
min_throttle_limit = -0.25
engine.0 = 1, -32.42, -7.95, 
engine.1 = 1, 32.42, -7.95, 

[jet_engine]
thrust_scalar = 1.24

[TurbineEngineData]
bypass_ratio=10.00000
fuel_flow_gain=0.004 
inlet_area=56
rated_N1_rpm=2401.00
rated_N2_rpm=13391.000 
static_thrust=72300.00
afterburner_available=0 
reverser_available=1 

[smokesystem]
smoke.0 = -6.360, 14.000, -26.060, Opensky_revspray
smoke.1 = -6.360, 14.000, 26.060, Opensky_revspray

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
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 = 2
electric_pump = 1

Center1 = 13.86, 0, -7.01, 22150, 50
LeftMain = 0, -27.61, -2.02, 5542.6, 27.4
RightMain = 0, 27.61, -2.02, 5542.6, 27.4


[contact_points]
static_pitch = -1
static_cg_height = 19.0275
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 28


point.0 = 1,  54.75722,  1.2825,  -18.5, 1100, 0, 1.66, 70, 1.0, 2.07021, 0.85,  10.0, 13, 0, 270, 285
point.1 = 1,  54.75722, -1.2825,  -18.5, 1100, 0, 1.66, 70, 1.0, 2.07021, 0.85,  10.0, 13, 0, 270, 285
point.2 = 1, -17.4028,  -18,      -18.9, 1100, 1, 2.05, 0,  1.9, 1.0207,  0.95,   9.9, 13, 2, 270, 285
point.3 = 1, -22.6639,  -18,      -18.9, 1100, 1, 2.05, 0,  1.9, 1.13289, 0.95,   9.9, 13, 2, 270, 285
point.4 = 1, -22.6639,  -14.1335, -18.9, 1100, 1, 2.05, 0,  1.9, 1.13289, 0.95,   9.9, 13, 2, 270, 285
point.5 = 1, -17.4028,  -14.1335, -18.9, 1100, 1, 2.05, 0,  1.9, 1.13289, 0.95,   9.9, 13, 2, 270, 285
point.6 = 1, -17.4028,   14.1335, -18.9, 1100, 2, 2.05, 0,  1.9, 1.13289, 0.95,   9.9, 13, 3, 270, 285
point.7 = 1, -22.6639,   14.1335, -18.9, 1100, 2, 2.05, 0,  1.9, 1.13289, 0.95,   9.9, 13, 3, 270, 285
point.8 = 1, -22.6639,   18,      -18.9, 1100, 2, 2.05, 0,  1.9, 1.13289, 0.95,   9.9, 13, 3, 270, 285
point.9 = 1, -17.4028,   18,      -18.9, 1100, 2, 2.05, 0,  1.9, 1.13289, 0.95,   9.9, 13, 3, 270, 285
point.10 = 2, -112.1483, -32.302, 6.1934, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.11 = 2, -112.3419, 32.2605, 6.1525, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.12 = 2, -59.8324, 98.3261, 9.23, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.13 = 2, -59.8324, -98.3261, 9.23, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.14 = 2, -110.6399, 0, 37.3906, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.15 = 2, -110.5517, 0, 1.8579, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.16 = 2, 53.4688, 0, 8.2111, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.17 = 2, 1.9787, 0, -10.6872, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.18 = 2, 46.5784, 0, -10.4012, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.19 = 2, -52.3725, 0, -10.4266, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.20 = 2, -81.4922, 0, -6.4418, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.21 = 2, 14.6689, 32.9365, -13.0471, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.22 = 2, 14.6689, -32.9365, -13.0471, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.23 = 2, 8.4836, 32.9368, -13.9413, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.24 = 2, 8.4836, -32.9368, -13.9413, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.25 = 2, 8.4836, 38.9609, -7.2304, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.26 = 2, 8.4836, -38.9609, -7.2304, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
point.27 = 2, 72.7294, 0, -4.6621, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 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 = 3501.3926
wing_span = 197.30
wing_root_chord = 36.11
wing_dihedral = 7.80
wing_incidence = 5
wing_twist = 6
oswald_efficiency_factor = 0.600
wing_winglets_flag = 1
wing_sweep = 35
wing_pos_apex_lon = 17.41
wing_pos_apex_vert = -6.05
htail_area = 762.19
htail_span = 64.51
htail_pos_lon = -69.36
htail_pos_vert = 1
htail_incidence = -1.5
htail_sweep = 40
vtail_area = 571.87
vtail_span = 31.45
vtail_sweep = 45.5
vtail_pos_lon = -60.13
vtail_pos_vert = 5.78
elevator_area = 254.000
aileron_area = 115.000
rudder_area = 195.29
elevator_up_limit = 32.54
elevator_down_limit = 26.93
aileron_up_limit = 32.20
aileron_down_limit = 16.94
rudder_limit = 32.10
elevator_trim_limit = 20
spoiler_limit = 63
aileron_to_spoileron_gain = 1.5
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 10.000
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 = 1
flap_motor = 0, 5, 17

[flight_tuning]
cruise_lift_scalar=0.5
parasite_drag_scalar=1.0
induced_drag_scalar=1.1 
elevator_effectiveness=1.0 
aileron_effectiveness=3.5
rudder_effectiveness=1.5 
pitch_stability=1. 
roll_stability=0.5 
yaw_stability=1.00 
elevator_trim_effectiveness=0.8 
aileron_trim_effectiveness=0.50 
rudder_trim_effectiveness=0.50 

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

[Reference Speeds]
flaps_up_stall_speed=176.0 
full_flaps_stall_speed=120.00 
cruise_speed=485.00 
max_indicated_speed=360.000000
max_mach=0.89

[Views]
eyepoint=72.50, -1.86, 2.25 

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1000 
autothrottle_available=1 
use_no_default_pitch=			1
use_no_default_bank=			1
pitch_takeoff_ga=18 
autothrottle_arming_required=		1
autothrottle_takeoff_ga=		1
autothrottle_max_rpm=			105.00
default_pitch_mode=0
default_bank_mode=0
max_pitch=				10.00
max_pitch_acceleration=		 	2.00
max_pitch_velocity_lo_alt=		4.00
max_pitch_velocity_hi_alt=		1.50  
max_pitch_velocity_lo_alt_breakpoint=	20000
max_pitch_velocity_hi_alt_breakpoint=	24000
max_bank=				25.00
max_bank_acceleration=			2.0
max_bank_velocity=			3.0
max_throttle_rate=			0.030
nav_proportional_control=		12.00
nav_integrator_control=			0.05
nav_derivative_control=			0.01
nav_integrator_boundary=		0.5
nav_derivative_boundary=		0.35
gs_proportional_control=		15.0 
gs_integrator_control=			0.30
gs_derivative_control=			0.00
gs_integrator_boundary=			0.7
gs_derivative_boundary=			0.00
yaw_damper_gain=			1.00

[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]
type=1
span-outboard=0.800000
extending-time=20
lift_scalar=0.5
drag_scalar=0.3
pitch_scalar=0.5
span-outboard =   0.8
damaging-speed= 260.0
blowout-speed = 280.0
flaps-position.0=0.0,0.000000	
flaps-position.1=0.0,0.000000
flaps-position.2=5,0.000000	
flaps-position.3=15.0,0.000000	
flaps-position.4=20.0,0.000000	
flaps-position.5=25.0,0.000000	
flaps-position.6=30.0,0.000000	
	
[Flaps.1]
type=2
span-outboard=0.800000
extending-time=10.800000
system_type=1
lift_scalar=0.6
drag_scalar=0.3
pitch_scalar=.6
flaps-position.0=0.0,0.000000
flaps-position.1=17.0,0.000000	
flaps-position.2=17.0,0.000000	
flaps-position.3=17.0,0.000000	
flaps-position.4=17.0,0.000000	
flaps-position.5=35.0,0.000000	
flaps-position.6=35.0,0.000000
	
[direction_indicators]
direction_indicator.0=3,0 

[brakes]
toe_brakes_scale=0.580
parking_brake=1

[hydraulic_system]
electric_pumps=1
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

[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 = 0.10                               ;Percent per second


[General]
performance=Passengers\n3-class conf: 300 \n2-class conf: 400 \n1-class conf: 440\n\nCargo\n32 LD-3 containers aft \n600 cubic Ft (17 cubic m)\nTotal lower hold volume: 5,656 cu ft \n\nDimensions\nSpan 199 ft 11 in\nLength 209 ft 1 in\nHeight 64 ft 7 in \n  (--max  58 ft 8 in--min)\n\nEngines: RR Trent 895\nTO Thrust Rating: 93,400 lb\n\nMax Fuel Cap.: 45,220 gal\nMaxTOW: 656,000 lb\nZFW: 429,110 lb\n\nMax Range: 7,695 nm  (14,260 km)\nTypical Cruise Speed \n  @ FL350: M.84
