[fltsim.0]
title=Boeing 767-300 Taesa
sim=767-300ER-PW4060
model=WV
panel=
sound=
texture=TEJ
checklists=
atc_airline=TAESA
atc_id=XA-SKY
atc_flight_number=200
atc_heavy=1
atc_parking_types=GATE
atc_parking_code=TEJ
ui_manufacturer=The Boeing Company
ui_type=767-3Y0ER
ui_variation=Taesa Yellow Tail
visual_damage=1
description=Boeing 767-3Y0ER Taesa XA-SKY The Only Boeing 767-300 Propierty of Taesa.

[General]
performance=Passengers\n3-class conf: 218\n2-class conf: 269 \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: RR211-524G/H\nTO Thrust Rating: 59,350 lb\n\nMax Fuel Cap.: 24,140 gal\nMaxTOW: 409,000 lb\nMax ZFW: 295,000 lb\n\nTypical Cruise Speed \n  @ FL350: M.80 
atc_type=BOEING 
atc_model=B763 
editable=0 

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

[weight_and_balance]

// ACM V2.5
max_gross_weight = 409000
empty_weight = 198443
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 11957602.5
empty_weight_roll_MOI = 10945212.5
empty_weight_yaw_MOI = 19319851.5
empty_weight_coupled_MOI = 0
CG_forward_limit = 0.000
CG_aft_limit = 1.000
max_number_of_stations = 6

station_load.0 = 4200.000000, 20.000000, 0.000000, 0.000000, 1st Class - 24
station_load.1 = 8050.000000, 40.000000, 0.000000, 0.000000, Bus Class - 46
station_load.2 = 25900.000000, 0.000000, 0.000000, 0.000000, Econ Class -148
station_load.3 = 8175.000000,  45.000000, 0.000000, 0.000000, Lwr Dk Cgo Fwd
station_load.4 = 8175.000000, -50.000000, 0.000000, 0.000000, Lwr Dk Cgo Aft
station_load.5 = 1000.000000, -70.000000, 0.000000, 0.000000, Lwr Dk Cgo Bulk


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 
light.0 = 1, 48.500, 0.000, 9.800, fx_shockwave_beaconh_l , 
light.1 = 1, 12.500, 0.000, -8.700, fx_shockwave_beaconb_l , 
light.2 = 4, 84.000, 0.000, 3.000, Opensky_Boeing_vclight , 
light.3 = 5 18.000, 27.000, -4.000, Opensky_wing_light, 
light.4 = 5, 18.000, -27.000, -4.000, Opensky_wing_light, light.10 = 5, 15.500, -45.000, 12.000, Opensky_wing_light, 
light.5 = 5, 15.500, 45.000, 12.000, Opensky_wing_light, 
light.6 = 5, 32.350, 8.350, -0.250, Opensky_nav_yellow , 
light.7 = 5, 32.350, -8.350, -0.250, Opensky_nav_yellow , 
light.8 = 5, 28.000, -25.000, 0.000, Opensky_wing_light, 
light.9 = 5, 28.000, 25.000, 0.000, Opensky_wing_light, 
light.10 = 6, 72.000, 0.000, -8.350, Opensky_wing_light, 
light.11 = 8, -10, -25, 0, Rainwash.fx 
light.12 = 8, -10, 25, 0, Rainwash.fx 
light.13 = 5, 28, 9.6, -3.1, fx_shockwave_landing_light_narrow 
light.14 = 5, 28, -9.6, -3.1, fx_shockwave_landing_light_narrow 
light.15 = 6, 77.0, 0, -8, fx_shockwave_landing_light_low 

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 0.7089
min_throttle_limit = -0.319946
engine.0 = 6.000, -26.667, -5.583
engine.1 = 6.000, 26.667, -5.583

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = opensky_sparks, 1
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 = 1
electric_pump = 0

Center1 = 0, 0, 0, 7440, 3
LeftMain = 0, -5, 0, 8350, 3
RightMain = 0, 5, 0, 8350, 3


[contact_points]
static_pitch = -0.5
static_cg_height = 13.5
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 27

point.0 = 1.000, 76.500, -1.500,  -14.750, 2181.102, 0.000, 1.541,  65.000, 0.350, 0.650, 0.850,  9.000,  9.000, 0.000, 280.000, 300.000
point.1 = 1.000, 76.500,  1.500,  -14.750, 2181.102, 0.000, 1.541,  65.000, 0.350, 0.650, 0.850,  9.000,  9.000, 0.000, 280.000, 300.000
point.2 = 1.000, -7.000, -15.250, -14.750, 2574.803, 1.000, 1.916, -13.000, 1.500, 1.200, 0.550, 11.900, 11.900, 2.000, 280.000, 300.000
point.3 = 1.000, -7.000, -12.250, -14.750, 2574.803, 1.000, 1.916, -13.000, 1.500, 1.200, 0.550, 11.900, 11.900, 2.000, 280.000, 300.000
point.4 = 1.000, -2.000, -15.250, -15.750, 2574.803, 1.000, 1.916,   0.000, 1.500, 1.200, 0.550, 11.900, 11.900, 2.000, 280.000, 300.000
point.5 = 1.000, -2.000, -12.250, -15.750, 2574.803, 1.000, 1.916,   0.000, 1.500, 1.200, 0.550, 11.900, 11.900, 2.000, 280.000, 300.000
point.6 = 1.000, -7.000,  15.250, -14.750, 2574.803, 2.000, 1.916, -13.000, 1.500, 1.200, 0.550, 13.100, 13.100, 3.000, 280.000, 300.000
point.7 = 1.000, -7.000,  12.250, -14.750, 2574.803, 2.000, 1.916, -13.000, 1.500, 1.200, 0.550, 13.100, 13.100, 3.000, 280.000, 300.000
point.8 = 1.000, -2.000,  15.250, -15.750, 2574.803, 2.000, 1.916,   0.000, 1.500, 1.200, 0.550, 13.100, 13.100, 3.000, 280.000, 300.000
point.9 = 1.000, -2.000,  12.250, -15.750, 2574.803, 2.000, 1.916,   0.000, 1.500, 1.200, 0.550, 13.100, 13.100, 3.000, 280.000, 300.000
point.10 = 2.000, -15.000, -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, -15.000,  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, -87.000,   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,  88.000,   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, -67.000,  -3.000,  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.15 = 2.000,  72.000,  -3.000,  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.16 = 2.000,   6.000, -27.000, -9.200, 787.402, 0.000, 0.000,   0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 8.000,   0.000,   0.000
point.17 = 2.000,   6.000,  27.000, -9.200, 787.402, 0.000, 0.000,   0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 8.000,   0.000,   0.000
point.18 = 2.000, -87.000,   0.000, 37.000, 787.402, 0.000, 0.000,   0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 8.000,   0.000,   0.000
point.19 = 2.000,  72.000,   9.000,  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.20 = 2.000,  60.000,  -9.000,  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.21 = 2.000,  60.000,   9.000,  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.22 = 2.000, -60.000,  -9.000,  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.23 = 2.000, -60.000,   9.000,  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.24 = 2.000, -95.000, -30.500,  9.000, 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.25 = 2.000, -95.000,  30.500,  9.000, 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.26 = 2.000, -95.000,   0.000, 45.000, 787.402, 0.000, 0.000,   0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000,   0.000,   0.000


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


[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]
//ACM_AREAW1// 0,0,0,6.0960,2.6428,2.6428,1.6196,7.4106,5.2859,5.2859
//ACM_AREAW2// 3.2392,8.7256,7.9288,7.9288,4.8589,10.0403,10.5719,10.5719,6.4784,11.3551
//ACM_AREAW3// 13.2150,13.2150,8.0979,12.6701,15.8578,15.8578,9.7178,13.9849,18.5009,18.5009
//ACM_AREAW4// 11.3374,15.2996,21.1438,21.1438,12.9568,16.6145,23.7870,23.7870,14.5767,17.9295
//ACM_AREAH1// 0,0,0,5.4608,0.9100,0.9100,0.9100,6.0981,1.8201,1.8201
//ACM_AREAH2// 1.8201,6.7350,2.7304,2.7304,2.7304,7.3723,3.6405,3.6405,3.6405,8.0094
//ACM_AREAH3// 4.5507,4.5507,4.5507,8.6464,5.4608,5.4608,5.4608,9.2834,6.3709,6.3709
//ACM_AREAH4// 6.3709,9.9208,7.2813,7.2813,7.2813,10.5579,8.1913,8.1913,8.1913,11.1948
//ACM_AREAV1// 0,0,0,6.2651,0.6959,0.6959,0.4873,6.2512,1.3920,1.3920
//ACM_AREAV2// 0.9746,6.2375,2.0882,2.0882,1.4622,6.2238,2.7843,2.7843,1.9495,6.2100
//ACM_AREAV3// 3.4806,3.4806,2.4370,6.1961,4.1767,4.1767,2.9244,6.1824,4.8729,4.8729
//ACM_AREAV4// 3.4119,6.1687,5.5689,5.5689,3.8993,6.1549,6.2651,6.2651,4.3867,6.1409
//ACM_CAREAW1// 11.8935,11.8935,10.3361,11.5555,13.2150,13.2150,11.1461,12.3044,14.5363,14.5363
//ACM_CAREAW2// 11.9559,13.0530,15.8578,15.8578,12.7658,13.8021,17.1795,17.1795,13.5754,14.5509
//ACM_CAREAW3// 18.5009,18.5009,14.3852,15.2996,19.8225,19.8225,15.1950,16.0487,21.1438,21.1438
//ACM_CAREAW4// 16.0048,16.7975,22.4654,22.4654,16.8148,17.5464,23.7870,23.7870,17.6247,18.2952
//ACM_CAREAH1// 0,0,2.7304,5.4608,0.9100,0.9100,3.6405,6.2346,1.8201,1.8201
//ACM_CAREAH2// 4.5507,7.0082,2.7304,2.7304,5.4608,7.7817,3.6405,3.6405,6.3709,8.5555
//ACM_CAREAH3// 4.5507,4.5507,7.2813,9.3290,5.4608,5.4608,8.1913,10.1028,6.3709,6.3709
//ACM_CAREAH4// 9.1014,10.8762,7.2813,7.2813,10.0116,11.6499,8.1913,8.1913,10.9217,12.4237
//ACM_CAREAV1// 0,0,1.5662,4.6988,0.6959,0.6959,2.0536,4.9355,1.3920,1.3920
//ACM_CAREAV2// 2.5411,5.1725,2.0882,2.0882,3.0285,5.4092,2.7843,2.7843,3.5160,5.6461
//ACM_CAREAV3// 3.4806,3.4806,4.0033,5.8829,4.1767,4.1767,4.4909,6.1198,4.8729,4.8729
//ACM_CAREAV4// 4.9783,6.3565,5.5689,5.5689,5.4657,6.5935,6.2651,6.2651,5.9531,6.8302
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 = 30.000
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 = 0.000
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 = 180.000
aileron_area = 20.000
rudder_area = 56.200
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
aileron_to_spoileron_gain = 0.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[flight_tuning]
cruise_lift_scalar=1.000 
parasite_drag_scalar=1.201 
induced_drag_scalar=1.201 
elevator_effectiveness=1.500 
aileron_effectiveness=0.550 
rudder_effectiveness=0.251 
pitch_stability=1.000 
roll_stability=1.000 
yaw_stability=1.000 
elevator_trim_effectiveness=0.751 
aileron_trim_effectiveness=0.501 
rudder_trim_effectiveness=0.501 

[TurbineEngineData]
bypass_ratio=5.800000
fuel_flow_gain=0.001 
inlet_area=40.58 
rated_N2_rpm=29992.000 
static_thrust=59350.000 
afterburner_available=0 
reverser_available=1.000 

[Reference Speeds]
flaps_up_stall_speed=118.000 
full_flaps_stall_speed=94.400 
cruise_speed=452.16 
max_indicated_speed=340.000000
max_mach=0.860010

[Views]
eyepoint=81.997949,-2.00,4.00 

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=800.000000 
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=110.5000  //Max N1 = 110.50% for RR RB21, 117.50% for GE CF6, 104.70% for JT9D
pitch_takeoff_ga=0.000 
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.
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=0.300000
max_pitch_velocity_lo_alt_breakpoint= 7000.000000
max_pitch_velocity_hi_alt_breakpoint=24000.000000
max_bank=28.000000
max_bank_acceleration=1.200000
max_bank_velocity=1.500000
max_throttle_rate=0.02800
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=1.000000

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 1, 0 
Adf.1=1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
direction_indicator.0=3,0 

[brakes]
toe_brakes_scale=0.43000
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0 = 2 
attitude_indicator.1 = 1 
[turn_indicators]
turn_indicator.0=1,0
[TailHook]    // For opening cargo door.
tailhook_length=1                               ;(feet)
tailhook_position = 0.0, 0.0, 0.0            ;(feet) longitudinal, lateral, vertical positions from datum
[folding_wings]  // For opening main deck cargo door.
wing_fold_system_type = 4                       ;0=None
fold_rates = 0.05,0.05                          ;Percent per second
cable_force_adjust = 1.0
[exits]
number_of_exits = 2
exit_rate.0 = 0.10                               ;Percent per second
exit_rate.1 = 0.09                               ;Percent per second

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 30.000
system_type= 1
damaging-speed= 200.000
blowout-speed= 250.000
lift_scalar= 0.540
drag_scalar= 0.540
pitch_scalar= 0.500
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= 30.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.540
drag_scalar= 0.540
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 5.000, 0.000
flaps-position.3= 5.000, 0.000
flaps-position.4= 5.000, 0.000
flaps-position.5= 20.000, 0.000
flaps-position.6= 20.000, 0.000

[jet_engine]
thrust_scalar=1.000