[fltsim.0]
title=Thomas Cook Boeing 777-300
sim=777-300-RR-Trent895
model=
panel=
sound=
texture=
checklists=
atc_airline=Thomas Cook
atc_id=FQ777
atc_flight_number=FQ777
atc_heavy=1
ui_manufacturer=Boeing
ui_type=777-300
ui_variation=773 Thomas Cook (RR)
visual_damage=1
description=Project Opensky Boeing 777-300\nVersion 2002.4.2\n\nModel Designers\n Mitsushi Yutaka\n Hiroshi Igami \n\nFlight Dynamics Designer\n Warren C. Daniel\n\nTechnical Resource\n Shigeo Kitaguchi\n Simon Ng\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 5,960 nautical miles (11,030 km) \n\nTypical city pairs: \n Tokyo-Singapore\n Honolulu-Seoul, South Korea\n San Francisco-Tokyo \n\nFor proper operation: See B777 manual at: www.project-opensky.com
[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight= 439100.000
empty_weight_roll_MOI= 8955743.000
empty_weight_pitch_MOI= 22600873.000
empty_weight_yaw_MOI= 22751035.000
empty_weight_coupled_MOI= 1000.000
max_gross_weight= 626799.994
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 2.0
rudder_effectiveness = 2.0
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
[General]
performance=Passengers\n3-class conf: 386 \n2-class conf: 479 \n1-class conf: 550\n\nCargo\n8 96-in x 125-in pallets fwd \n20 LD-3 containers aft \nTotal lower hold volume: 7,552 cu ft \n\nDimensions\nSpan 199 ft 11 in\nLength 242 ft 4 in\nHeight 64 ft 7 in (--max 58 ft 8 in--min)\n\nEngines: RR Trent 895\nTO Thrust Rating: 93,400 lb\n\nMax Fuel Cap.: 45,220 lb (46,309 lb - actual)\nMaxTOW: 660,000 lb\nZFW: 439,100 lb\nMax Range: 5,960 nm \nTypical Cruise Speed @ FL350: M.84
atc_type=BOEING AIRCRAFT
atc_model=B773
editable=0
[pitot_static]
vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI
[fuel]
Center1= 6.000, 0.000, -4.000, 13700.000, 0.000
LeftAux= -2.000, -49.750, 0.000, 9300.000, 0.000
LeftMain= 4.000, -35.000, 0.000, 6200.000, 0.000
RightMain= 4.000, 35.000, 0.000, 6200.000, 0.000
RightAux= -2.000, 49.705, 0.000, 9300.000, 0.000
fuel_type= 2.000
number_of_tank_selectors= 1
[airplane_geometry]
wing_area= 4605.000
wing_span= 199.917
wing_root_chord= 23.000
wing_dihedral= 6.218
wing_incidence= 1.000
wing_twist= -0.500
oswald_efficiency_factor= 0.600
wing_winglets_flag= 0
wing_sweep= 31.5
wing_pos_apex_lon= 25.000
wing_pos_apex_vert= 0.000
htail_area= 1090.000
htail_span= 70.700
htail_pos_lon= -84.5
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 40.000
vtail_area= 573.000
vtail_span= 27.300
vtail_sweep= 35.000
vtail_pos_lon= -92.583
vtail_pos_vert= 5.800
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
spoilerons_available= 0
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 9.969
min_flaps_for_spoilerons= 0.000
[GeneralEngineData]
engine_type= 1
Engine.0= 10.000, -32.583, -10.500
Engine.1= 10.000, 32.583, -10.500
fuel_flow_scalar= 0.6299348
[TurbineEngineData]
bypass_ratio=6.400000
fuel_flow_gain= 0.001
inlet_area= 68.382
rated_N2_rpm= 47872.000
static_thrust= 93400.000
afterburner_available= 0
reverser_available= 1
[Reference Speeds]
flaps_up_stall_speed= 138.000
full_flaps_stall_speed= 110.400
cruise_speed= 485.00
[keyboard_response]
elevator= 100.000, 200.000
aileron= 100.000, 200.000
rudder= 100.000, 200.000
[Views]
eyepoint= 105.188, -1.756, 1.628
[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= 105.000
pitch_takeoff_ga= 8.000
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.
[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 = 0.2 // 0.0 .. 1.0
extending-time = 30 // 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 = 1.00
drag_scalar = 1.00
pitch_scalar= 1.00
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 = 30 // 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 = 1.00
drag_scalar = 1.00
pitch_scalar= 1.00
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 = 35 // 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 = 1.00
drag_scalar = 1.00
pitch_scalar= 1.00
system_type = 1 //Hydraulic
[direction_indicators]
direction_indicator.0=3,0
[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=1.0, 99.833, 0.000, -19.233, 1181.102, 0.000, 5.505, 70.0, 0.552, 2.500, 0.7, 8.000, 9.000 , 0.000,0.000,0.000
point.1=1.0,-6.666667,-18.000000,-19.416667,1574.803150,1.000000,5.505712,-8.0,0.561371,2.500000,1.0,9.900000,11.900000,2.000000,0.000000,0.000000
point.2=1.0,-6.666667,18.000000,-19.416667,1574.803150,2.000000,5.505712,-8.0,0.561371,2.500000,1.0,10.100000,13.100000,3.000000,0.000000,0.000000
point.3=2.0,-14.166667,-99.916667,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.0,-14.166667,99.916667,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.0,-136.417,0.000000,2.500000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.0,105.917,0.000000,-3.750000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
point.7=2.0,14.166667,-99.916667,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,7.000000,0.000000,0.000000
point.8=2.0,0.000000,44.750000,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,8.000000,0.000000,0.000000
static_pitch=0.104370
static_cg_height=17.620275
//Main Nose Gear
//point.0= 1.000, 99.833, 1.500, -20.533, 1181.102, 0.000, 2.000, 70.0, 0.850, 3.000, 0.952, 7.000, 9.000, 0.000, 240.000, 280.000
//point.1= 1.000, 99.833, -1.500, -20.533, 1181.102, 0.000, 2.000, 70.0, 0.850, 3.000, 0.952, 7.000, 9.000, 0.000, 240.000, 280.000
//
//Left Main Gear
//point.2= 1.000,-11.417, -20.291, -16.017, 1574.803, 1.000, 2.000, -8.0, 0.550, 3.000, 0.570, 10.900, 11.900, 2.000, 240.000, 280.000
//point.3= 1.000,-11.417, -15.700, -16.017, 1574.803, 1.000, 2.000, -8.0, 0.550, 3.000, 0.570, 10.900, 11.900, 2.000, 240.000, 280.000
//
//point.4= 1.000, -6.667, -20.291, -19.017, 1574.803, 1.000, 2.000, 0.0, 0.550, 3.000, 0.570, 10.900, 11.900, 2.000, 240.000, 280.000
//point.5= 1.000, -6.667, -15.700, -19.017, 1574.803, 1.000, 2.000, 0.0, 0.550, 3.000, 0.570, 10.900, 11.900, 2.000, 240.000, 280.000
//
//point.6= 1.000, -1.917, -20.291, -19.017, 1574.803, 1.000, 2.000, 8.0, 0.550, 3.000, 0.570, 10.900, 11.900, 2.000, 240.000, 280.000
//point.7= 1.000, -1.917, -15.700, -19.017, 1574.803, 1.000, 2.000, 8.0, 0.550, 2.500, 0.570, 10.900, 11.900, 2.000, 240.000, 280.000
//
//Right Main Gear
//point.8= 1.000, -11.417, 20.291, -16.017, 1574.803, 2.000, 2.000, -8.0, 0.550, 3.000, 0.570, 8.100, 13.100, 3.000, 240.000, 280.000
//point.9= 1.000, -11.417, 15.700, -16.017, 1574.803, 2.000, 2.000, -8.0, 0.550, 3.000, 0.570, 8.100, 13.100, 3.000, 240.000, 280.000
//
//point.10= 1.000, -6.667, 20.291, -19.017, 1574.803, 2.000, 2.000, 0.0, 0.550, 3.000, 0.570, 8.100, 13.100, 3.000, 240.000, 280.000
//point.11= 1.000, -6.667, 15.700, -19.017, 1574.803, 2.000, 2.000, 0.0, 0.550, 3.000, 0.570, 8.100, 13.100, 3.000, 240.000, 280.000
//
//point.12= 1.000, -1.917, 20.291, -19.017, 1574.803, 2.000, 2.000, 8.0, 0.550, 3.000, 0.570, 8.100, 13.100, 3.000, 240.000, 280.000
//point.13= 1.000, -1.917, 15.700, -19.017, 1574.803, 2.000, 2.000, 8.0, 0.550, 3.000, 0.570, 8.100, 13.100, 3.000, 240.000, 280.000
//
//Scrape points
//point.14= 2.000, -14.167, -99.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
//point.15= 2.000, -14.167, 99.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
//point.16= 2.000, -136.417, 0.000, 2.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
//point.17= 2.000, 105.917, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
//point.18= 2.000, 14.167, -99.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
//point.19= 2.000, 0.000, 44.750, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
//
//static_pitch= 0.104
//static_cg_height= 17.900
[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
