[fltsim.0]
title=Boeing 767-300ER UPS
sim=UP767300
model=
panel=
sound=
texture=
checklists=

atc_airline=UPS
atc_id=N330UP
atc_flight_number=6195
atc_heavy=1

ui_manufacturer=Boeing
ui_type=767-300ER
ui_variation=UPS
visual_damage=1

description=Project Opensky Boeing 767-34AF\nUPS Boeing 767300ER N330UP\nserial no.27756 delivered 10\/ago\/01\nModel Designers\n   Mitsushi Yutaka\n   Hiroshi Igami \n\nUPS, United Parcel Service Textures by\n   Kevin Sparkuhl\n\nFlight Dynamics Designer\n   Warren C. Daniel ver4.6\n\nTechnical Advisors\n   Nick Peterson\n   Simon Ng\n\nTest Pilots\n   Project Opensky Members\n\nMaximun Range: 1,737 nautical miles (3,910 km) \n\nTypical city pairs: \n   Louisville-Ontario\n   Miami-Bogota-Campinas\n   Miami-Caracas-Campinas\n   Campinas-Buenos Aires

[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

[General]
performance=Passengers\n10F\/36C\/150Y total=196\n\nCargo\nLD-2 containers aft \nTotal lower hold volume: 3,770 cu ft \n\nDimensions\nSpan 156 ft 1 in\nLength 180 ft 3 in\nHeight 52 ft \n\nEngines: GE CF6-80C2B6F\nTO Thrust Rating: 56,430 lb\n\nMax Fuel Cap.: 24,140 gal\nMaxTOW: 412,000 lb\nZFW: 260,000 lb\n\nTypical Cruise Speed \n  @ FL350: M.80

atc_type=BOEING AIRCRAFT
atc_model=B763

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


[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= 295000.000
empty_weight_roll_MOI= 4378085.000
empty_weight_pitch_MOI= 7971735.000
empty_weight_yaw_MOI= 12879901.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 456737.995
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar     =1.000
parasite_drag_scalar   =1.451
induced_drag_scalar    =1.451
elevator_effectiveness =1.000
aileron_effectiveness  =1.000
rudder_effectiveness   =1.201
pitch_stability        =1.000
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[fuel]
Center1= 0.000, 0.000, 0.000, 11896.000, 3.000
LeftMain= 0.000, -5.000, 0.000, 6122.000, 3.000
RightMain= 0.000, 5.000, 0.000, 6122.000, 3.000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 3050.000
wing_span= 156.083
wing_root_chord= 20.000
wing_dihedral= 6.498
wing_incidence= -1.000
wing_twist= 1.000
oswald_efficiency_factor= 0.653
wing_winglets_flag= 0
wing_sweep= 31.500
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 733.000
htail_span= 53.750
htail_pos_lon= -91.667
htail_pos_vert= 0.000
htail_incidence= 1.994
htail_sweep= 45.000
vtail_area= 325.000
vtail_span= 20.555
vtail_sweep= 35.000
vtail_pos_lon= -87.500
vtail_pos_vert= 5.000
elevator_area= 60.000
aileron_area= 20.000
rudder_area= 56.200
elevator_up_limit= 31.513
elevator_down_limit= 10.313
aileron_up_limit= 24.000
aileron_down_limit= 18.000
rudder_limit= 32.000
elevator_trim_limit= 18.335
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

        //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)


[contact_points]

point.0= 1.000, 70.500, 0.000, -9.750, 1181.102, 0.000, 2.000, 70.000, 0.500, 0.500, 0.750, 9.000, 9.000, 0.000, 0.000, 0.000
point.1= 1.000, -9.000, -15.250, -9.500, 1574.803, 1.000, 2.000, 0.000, 0.500, 0.500, 0.920, 11.900, 11.900, 2.000, 0.000, 0.000
point.2= 1.000, -9.000, 15.250, -9.500, 1574.803, 2.000, 2.000, 0.000, 0.500, 0.500, 0.920, 11.900, 11.900, 3.000, 0.000, 0.000
point.3= 2.000, 0.000, -78.000, 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, 0.000, 78.000, 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, -60.000, 0.000, 0.000, 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, 78.000, 0.000, 0.000, 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, 0.000, 78.000, 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, 36.000, 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= -1.000
static_cg_height= 9.600

//
//Nose Gear
//point.0= 1.000, 70.500, -1.500, -10.500, 1181.102, 0.000, 2.000, 70.000, 1.000, 2.500, 0.518, 9.000, 9.000, 0.000, 280.000, 300.000
//point.1= 1.000, 70.500,  1.500, -10.500, 1181.102, 0.000, 2.000, 70.000, 1.000, 2.500, 0.518, 9.000, 9.000, 0.000, 280.000, 300.000
//
//Left Main Gear
//point.2= 1.000, -9.000, -15.250, -10.000, 1574.803, 1.000, 2.000, 0.000, 1.000, 2.500, 0.551, 11.900, 11.900, 2.000, 280.000, 300.000
//point.3= 1.000, -9.000, -12.250, -10.000, 1574.803, 1.000, 2.000, 0.000, 1.000, 2.500, 0.551, 11.900, 11.900, 2.000, 280.000, 300.000
//point.4= 1.000, -4.000, -15.250, -10.000, 1574.803, 1.000, 2.000, 0.000, 1.000, 2.500, 0.551, 11.900, 11.900, 2.000, 280.000, 300.000
//point.5= 1.000, -4.000, -12.250, -10.000, 1574.803, 1.000, 2.000, 0.000, 1.000, 2.500, 0.551, 11.900, 11.900, 2.000, 280.000, 300.000
//
//Right Main Gear
//point.6= 1.000, -9.000,  15.250, -10.000, 1574.803, 2.000, 2.000, 0.000, 1.000, 2.500, 0.551, 13.100, 13.100, 3.000, 280.000, 300.000
//point.7= 1.000, -9.000,  12.250, -10.000, 1574.803, 2.000, 2.000, 0.000, 1.000, 2.500, 0.551, 13.100, 13.100, 3.000, 280.000, 300.000
//point.8= 1.000, -4.000,  15.250, -10.000, 1574.803, 2.000, 2.000, 0.000, 1.000, 2.500, 0.551, 13.100, 13.100, 3.000, 280.000, 300.000
//point.9= 1.000, -4.000,  12.250, -10.000, 1574.803, 2.000, 2.000, 0.000, 1.000, 2.500, 0.551, 13.100, 13.100, 3.000, 280.000, 300.000
//
//Scrape Points
//point.10= 2.000, 0.000, -78.000, 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.11= 2.000, 0.000, 78.000, 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.12= 2.000, -60.000, 0.000, 0.000, 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.13= 2.000, 78.000, 0.000, 0.000, 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.14= 2.000, 0.000, 78.000, 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.15= 2.000, 0.000, 36.000, 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= -1.000
//static_cg_height= 9.600


[GeneralEngineData]
engine_type= 1
Engine.0= 6.000, -26.667, -5.583
Engine.1= 6.000, 26.667, -5.583
fuel_flow_scalar= 0.747

[SMOKESYSTEM]      
smoke.0=90.0,-27.3,-56.0, fx_WingVortex
smoke.1=90.0,-27.3,56.0, fx_WingVortex

[TurbineEngineData]
bypass_ratio=4.970
fuel_flow_gain= 0.002
inlet_area= 33.550
rated_N2_rpm= 29920.000
static_thrust= 60000.000
afterburner_available= 0
reverser_available= 1

[Reference Speeds]
flaps_up_stall_speed= 118.000
full_flaps_stall_speed= 94.400
cruise_speed= 535.341

[keyboard_response]
elevator=100.000000,200.000000
aileron=100.000000,200.000000
rudder=100.000000,200.000000

[Views]
eyepoint=74.997949,-1.768578,8.753178

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=97.000000
pitch_takeoff_ga=8.000000
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


[direction_indicators]
direction_indicator.0=3,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1



[LIGHTS]    
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 
light.1 = 1,  42.5.00,   0.00, 14, fx_beaconh , 
light.2 = 1,  12.5.00,   0.00, -3.8, fx_beaconh , 
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 20.000
system_type= 1
damaging-speed= 200.000
blowout-speed= 250.000
lift_scalar= 0.700
drag_scalar= 0.900
pitch_scalar= 0.900
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 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= 0.800
extending-time= 20.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.300
drag_scalar= 0.100
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
[jet_engine]
thrust_scalar=1.000