[fltsim.0]
title=Alitalia 777-200 I-DISA TAORMINA Project Opensky
sim=777-200-GE90-85B
model=
panel=
sound=
texture=
checklists=

atc_airline=alitalia
atc_id=I DISA
atc_flight_number=224
atc_heavy=1

ui_manufacturer=Boeing
ui_type=777-200
ui_variation=ALITALIA
visual_damage=1

description=Project Opensky Boeing 777-200\nVersion 2002.4.2\nREPAINT BY MASSIMO GRASSSI\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: 3,390 nautical miles (5,460 km) \n\nTypical city pairs: \n   NY-San Francisco\n   Denver-Honolulu\n   London-NY\n   Chicago-Honolulu\n   Tokyo-San Francisco\n\nFor proper operation: See B777 manual at: \n  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= 419100.000
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: 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: GE90-85B\nTO Thrust Rating: 85,000 lb\n\nMax Fuel Cap.: 31,000 gal\nMaxTOW: 545,000 lb\nZFW: 419,100 lb\nMax Range: 3,390 nm  (5,460 km)\nTypical Cruise Speed \n  @ FL350: M.84

atc_type=AZTEC
atc_model=B772
editable=1

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


[fuel]
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= 31.500
wing_pos_apex_lon= 25.000
wing_pos_apex_vert= 0.000
htail_area= 1090.000
htail_span= 70.700
htail_pos_lon= -84.500
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= 0.617

[TurbineEngineData]
bypass_ratio=9.000
fuel_flow_gain= 0.001
inlet_area= 82.474
rated_N2_rpm= 29920.000
static_thrust= 85000.000
afterburner_available= 0
reverser_available= 1


[Reference Speeds]
flaps_up_stall_speed= 138.000
full_flaps_stall_speed= 110.400
cruise_speed= 485.000

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

[Views]
eyepoint= 98.502, -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



[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= 1.000, 82.250, 0.000, -19.233, 1181.102, 0.000, 5.505, 70.000, 0.552, 2.500, 0.700, 8.000, 9.000, 0.000, 0.000, 0.000
point.1= 1.000, -6.667, -18.000, -19.417, 1574.803, 1.000, 5.506, -8.000, 0.561, 2.500, 1.000, 9.900, 11.900, 2.000, 0.000, 0.000
point.2= 1.000, -6.667, 18.000, -19.417, 1574.803, 2.000, 5.506, -8.000, 0.561, 2.500, 1.000, 10.100, 13.100, 3.000, 0.000, 0.000
point.3= 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.4= 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.5= 2.000, -120.667, 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.6= 2.000, 88.417, 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.7= 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.8= 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= 17.620

//Main Nose Gear
//point.0= 1.000, 82.250,  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, 82.250, -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, -120.667, 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, 88.417, 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
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 30.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 5.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
[Flaps.1]
type= 2
span-outboard= 0.500
extending-time= 35.000
system_type= 1
damaging-speed= 260.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.500, 0.000
flaps-position.2= 0.500, 0.000
flaps-position.3= 0.500, 0.000
flaps-position.4= 0.500, 0.000
flaps-position.5= 1.000, 0.000
flaps-position.6= 1.000, 0.000