[fltsim.0]
title=LAM Airlines B767-3YO 
sim=b763-LAM
model=
panel=
sound=
texture=
checklists=PSCIV_B767Full_Checklist
atc_type=Boeing
atc_id_enable=1
atc_id=CS-CEM
editable=0
ui_manufacturer=Boeing
ui_type=767-3YO
ui_variation=LAM Linhas Aereas Mozambique
description=LAM 767-300 ZAMBEZE\nFS2000\/2  Versions\n\n\n\n

[Radios]
Radio type=availeble, stanby, 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


[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



[ground_reaction]
main_gear_static_compression=1.0		// (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=0.8            // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=0.7		// Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=0.5		// Center gear strut damping, 0 = undamped osciallations, 1 = critically damped

[pitot_static]
vertical_speed_time_constant=1		//Increasing this value will cause a more instantaneous reaction in the VSI

[General]
performance=MTOW: 407,000 lbm (184612 kg)\nMLW: 325,600 lbm (147 690 kg)\nPower: 2 x PW 4060 @ 59,750 lbf\nFuel Capacity: 24,050 usg (91 380 L)\nLength: 180 feet, 3 inches (54.9 m)\nWing Span: 156 feet, 1 inches (47.57 m)\nRange: 6,555 miles (10 549 km)\n\nMTOW inital level FL290\nNormal Cruise FL350\nSpeed M 0.80 mach\nStall: 160\/100    Max Cruise: mach .82\nLanding flap 30\/full\nAutoland: beware at 200ft!\nTypical Cruise Speed @ FL350: M.80\n\nAutoland: INOP!

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=248232.000000
empty_weight_roll_MOI=14200000.000000
empty_weight_pitch_MOI=30200000.000000
empty_weight_yaw_MOI=35600000.000000
empty_weight_coupled_MOI=650000.000000

[fuel]
Center1=0.000000,0.000000,-7.000000,11906.000000,3.000000
LeftMain=-9.000000,-30.000000,0.000000,6072.000000,3.000000
RightMain=-9.000000,30.000000,0.000000,6072.000000,3.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=3050.000000
wing_span=156.083333
wing_root_chord=19.500000
wing_dihedral=6.498413
wing_incidence=1.499634
wing_twist=-0.994263
oswald_efficiency_factor=0.816144
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=6.600000
wing_pos_apex_vert=0.000000
htail_area=733.000000
htail_span=53.750000
htail_pos_lon=-91.666667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=325.000000
vtail_span=20.554805
vtail_sweep=0.000000
vtail_pos_lon=-87.500000
vtail_pos_vert=5.000000
elevator_area=60.000000
aileron_area=20.000000
rudder_area=56.200000
elevator_up_limit=30.000013
elevator_down_limit=30.000013
aileron_up_limit=30.000013
aileron_down_limit=30.000013
rudder_limit=30.000013
elevator_trim_limit=20.000009
spoiler_limit=70.000030
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=9.969466
min_flaps_for_spoilerons=0.000000

[contact_points]
point.0=1.000000,69.083333,0.000000,-10.583333,1181.102362,0.000000,3.337899,79.740000,0.800000,2.500000,0.500000,12.000000,12.000000,0.000000,0.000000,0.000000
point.1=1.000000,-8.833333,-13.083333,-11.416667,1574.803150,1.000000,3.337899,0.000000,1.000000,2.500000,0.700000,14.900000,14.900000,2.000000,0.000000,0.000000
point.2=1.000000,-8.833333,13.083333,-11.416667,1574.803150,2.000000,3.337899,0.000000,1.000000,2.500000,0.700000,15.100000,15.100000,3.000000,0.000000,0.000000
point.3=2.000000,-14.166667,-47.333333,19.750000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-14.166667,47.333333,19.750000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-95.833333,0.000000,3.500000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,42.666667,0.000000,-0.083333,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=-0.747070
static_cg_height=10.763417

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=30.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=5.000002,0.000000
flaps-position.2=10.000004,0.000000
flaps-position.3=15.000006,0.000000
flaps-position.4=20.000009,0.000000
flaps-position.5=25.000011,0.000000
flaps-position.6=30.000013,0.000000

[GeneralEngineData]
engine_type=1
Engine.0=2.416667,-26.000000,-6.000000
Engine.1=2.416667,26.000000,-6.000000
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002000
inlet_area=94.000000
rated_N2_rpm=29920.000000
static_thrust=59750.000000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=158.000000
full_flaps_stall_speed=126.400000
cruise_speed=561.192882

[keyboard_response]
elevator=250.000000,300.000000
aileron=250.000000,300.000000
rudder=250.000000,300.000000

[Views]
eyepoint=68.782296,0.000000,9.586204

[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=90.000000
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=3,0