[fltsim.0]
title=Transbrasil B767-283ER PT-TAI circa 1993
sim=767-200ER-PW-JT9D-7A
model=WV
panel=
sound=
texture=
checklists=
atc_airline=Transbrasil
atc_id=TBA
atc_flight_number=702
atc_heavy=1
atc_parking_types=GATE, RAMP
atc_parking_code=
atc_id=PT-TAI
ui_manufacturer=project Opensky
ui_type=767-200
ui_variation=Transbrasil B767-283ER PT-TAI circa 1993
visual_damage=1
description=Project Opensky - Boeing 767-200ER\nVersion 2004.9.9\n\nModel\\VC Designer\n Albert Bouwman \n\nFlight Dynamics\\Sound\\Effects Designer\n Warren C. Daniel\n\nMaster Texture Designer\n Tom Harlaar\n\nTransbrasil Texture Designer\n Ricardo Lin\n\n2D Panel Designer\n Ed Cox\n\nTechnical Advisors\n Nick Peterson\n Simon Ng\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 6,610 nautical miles \n\nModel Information: PT-TAI was delivered on 21\/09\/1993 and returned to lessor on 25\/06\/1999.
[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\n3-class conf: 174\n\nCargo\nTotal lower hold volume: 22 LD2 \n\nDimensions\nSpan 156 ft 1 in\nLength 159 ft 2 in\nHeight 52 ft \n\nEngines: PW JT9D-7R\nTO Thrust Rating: 50,000 lb\n\nMax Fuel Cap.: 16,700 gal\nMaxTOW: 345,000 lb\nTypical ZFW: 209,000 lb\n\nTypical Cruise Speed \n @ FL350: M.78
atc_type=BOEING
atc_model=B767
editable=0
[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
empty_weight = 181350.000
max_gross_weight = 352200.000
max_number_of_stations = 6
// New FS2004 Numbers
// Max Structural Payload Per Boeing - 78,500 lbs
// Max Structural Payload Opensky - 44,500 lbs
// Actual Total PAX - 38,150 lbs
station_load.0 =2550.000000, 45.000000, 0.000000, 0.000000, 1st Class - 15
station_load.1 =6800.000000, 20.000000, 0.000000, 0.000000, Bus Class - 40
station_load.2 =20230.000000, 0.000000, 0.000000, 0.000000, Econ Class -119
// Total Opensky Cargo - 17,350 lbs
station_load.3 =6525.000000, 35.000000, 0.000000, 0.000000, Lwr Dk Cgo Fwd
station_load.4 =6525.000000, -22.000000, 0.000000, 0.000000, Lwr Dk Cgo Aft
station_load.5 =200.000000, -44.000000, 0.000000, 0.000000, Lwr Dk Cgo Bulk
// Moments of Inertia
empty_weight_roll_MOI = 10945212.500
empty_weight_pitch_MOI= 11957602.500
empty_weight_yaw_MOI = 19319851.500
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[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
[fuel] // Max fuel per Boeing - 767-200 = 16,700 US Gallons / 767-200ER = 24,140 US Gallons
Center1 = 0.000, 0.000, 0.000, 7440.000, 3.000
LeftMain = 0.000, -5.000, 0.000, 8350.000, 3.000
RightMain = 0.000, 5.000, 0.000, 8350.000, 3.000
fuel_type = 2.000000
number_of_tank_selectors=1
electric_pump=0
[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= 30.000
wing_pos_apex_vert= 0.000
htail_area= 733.000
htail_span= 53.750
htail_pos_lon= -70.667
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= -66.500
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
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
[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)
//
//=======================================================================================================================================================
//
//FUll Motion, Realistic feel, true footprint contact points
//Nose Gear
//point.0= 1.000, 66.500, -1.500, -16.500, 2181.102, 0.000, 1.541, 65.000, 1.000, 0.920, 0.650, 9.000, 9.000, 0.000, 280.000, 300.000
//point.1= 1.000, 66.500, 1.500, -16.500, 2181.102, 0.000, 1.541, 65.000, 1.000, 0.920, 0.650, 9.000, 9.000, 0.000, 280.000, 300.000
//
//Left Main Gear
//point.2= 1.000, -7.000, -15.250, -16.500, 2574.803, 1.000, 1.916, -13.000, 2.500, 0.850, 0.650, 11.900, 11.900, 2.000, 280.000, 300.000
//point.3= 1.000, -7.000, -12.250, -16.500, 2574.803, 1.000, 1.916, -13.000, 2.500, 0.850, 0.650, 11.900, 11.900, 2.000, 280.000, 300.000
//point.4= 1.000, -2.000, -15.250, -17.500, 2574.803, 1.000, 1.916, 0.000, 3.500, 0.892, 0.650, 11.900, 11.900, 2.000, 280.000, 300.000
//point.5= 1.000, -2.000, -12.250, -17.500, 2574.803, 1.000, 1.916, 0.000, 3.500, 0.892, 0.650, 11.900, 11.900, 2.000, 280.000, 300.000
//
//Right Main Gear
//point.6= 1.000, -7.000, 15.250, -16.500, 2574.803, 2.000, 1.916, -13.000, 2.500, 0.850, 0.650, 13.100, 13.100, 3.000, 280.000, 300.000
//point.7= 1.000, -7.000, 12.250, -16.500, 2574.803, 2.000, 1.916, -13.000, 2.500, 0.850, 0.650, 13.100, 13.100, 3.000, 280.000, 300.000
//point.8= 1.000, -2.000, 15.250, -17.500, 2574.803, 2.000, 1.916, 0.000, 3.500, 0.892, 0.650, 13.100, 13.100, 3.000, 280.000, 300.000
//point.9= 1.000, -2.000, 12.250, -17.500, 2574.803, 2.000, 1.916, 0.000, 3.500, 0.892, 0.650, 13.100, 13.100, 3.000, 280.000, 300.000
//
//Scrape Points
//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 // Left wing
//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 // Right wing
//point.12= 2.000, -66.000, 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 // Fuse tail
//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 // Fuse nose
//point.14= 2.000, -46.000, -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 // Fuse aft/lower
//point.15= 2.000, 62.000, -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 // Fuse fwd/lwr
//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 // Engine pod/lwrL
//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 // Engine pod/LwrR
//point.18= 2.000, -66.000, 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 // Top of vert/stab
//point.19= 2.000, 62.000, 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 // Top of fuse/fwd
//point.20= 2.000, 50.000, -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 // Top of fuse/fwd
//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 // Fuse right/fwd
//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 // Fuse right/aft
//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 // Fuse left/fwd
//point.24= 2.000, -74.000, -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 // Horiz stab/left
//point.25= 2.000, -74.000, 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 // Horiz stab/right
//point.26= 2.000, -74.000, 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 // Vert stab/aft
//
//static_pitch= -0.500
//static_cg_height= 14.000
//gear_system_type=0
//
//=======================================================================================================================================================
//
// 3-point, non-realistic feel, non-footprint contact points
//
//point.0 = 1.000, 66.500, 0.000, -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, -4.000, -13.750, -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.2 = 1.000, -4.000, 13.750, -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.3 = 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 // Left wing
//point.4 = 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 // Right wing
//point.5 = 2.000, -66.000, 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 // Fuse tail
//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 // Fuse nose
//point.7 = 2.000, -46.000, -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 // Fuse aft/lower
//point.8 = 2.000, 62.000, -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 // Fuse fwd/lwr
//point.9 = 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 // Engine pod/lwrL
//point.10= 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 // Engine pod/LwrR
//point.11= 2.000, -66.000, 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 // Top of vert/stab
//point.12= 2.000, 62.000, 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 // Top of fuse/fwd
//point.13= 2.000, 50.000, -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 // Top of fuse/fwd
//point.14= 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 // Fuse right/fwd
//point.15= 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 // Fuse right/aft
//point.16= 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 // Fuse left/fwd
//point.17= 2.000, -74.000, -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 // Horiz stab/left
//point.18= 2.000, -74.000, 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 // Horiz stab/right
//point.19= 2.000, -74.000, 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 // Vert stab/aft
//
//static_pitch= -0.500
//static_cg_height= 13.500
//gear_system_type=0
//
//=======================================================================================================================================================
//
// Default with true footprint contact points
//Nose Gear
point.0= 1.000, 66.500, -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, 66.500, 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
//Left Main Gear
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
//Right Main Gear
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
//Scrape Points
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, -66.000, 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, -46.000, -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, 62.000, -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, -66.000, 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, 62.000, 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, 50.000, -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, -74.000, -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, -74.000, 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 // Horiz stab/right
point.26= 2.000, -74.000, 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 // Vert stab/aft
static_pitch= -0.500
static_cg_height= 13.500
gear_system_type=0
//
//=======================================================================================================================================================
//
[GeneralEngineData]
engine_type= 1
Engine.0= 5.500, -26.667, -5.583
Engine.1= 5.500, 26.667, -5.583
fuel_flow_scalar= 0.712
min_throttle_limit=-0.319946
[TurbineEngineData]
bypass_ratio=4.7000
fuel_flow_gain= 0.001
inlet_area= 48.150
rated_N2_rpm= 29920.000
static_thrust= 50000.000
afterburner_available= 0
reverser_available= 1.000
[Reference Speeds]
flaps_up_stall_speed= 118.000
full_flaps_stall_speed= 94.400
cruise_speed= 452.160
max_indicated_speed=340.000000
max_mach=0.860010
[keyboard_response]
elevator=100.000000,200.000000
aileron=100.000000,200.000000
rudder=100.000000,200.000000
[Views]
eyepoint=71.997949,-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=104.70 //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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=Opensky_sparks, 1
touchdown=fx_tchdwn, 1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo
light.1 = 1, 42.000, 0.000, 9.800, Opensky_beacon, // top beacon
light.2 = 1, 12.500, 0.000, -8.700, Opensky_beacon, // bottom beacon
light.3 = 4, 74.000, 0.000, 3.000, Opensky_Boeing_vclight , // Boeing Orange
light.4 = 3, 30.000, 0.000, -4.000, Opensky_nacelle_refl , // front cargo
light.5 = 3, -20.000, 0.000, -4.000, Opensky_nacelle_refl , // rear cargo
light.6 = 3, 73.000, 0.000, 4.000, Opensky_nacelle_refl , // pax door
light.7 = 5, 19.700, 19.000, -4.000, Opensky_nacelle_refl, // nacelle rays from inspection lights
light.8 = 5, 19.700, -19.000, -4.000, Opensky_nacelle_refl, // nacelle rays from inspection lights
light.9 = 5 18.000, 27.000, -4.000, Opensky_wing_light, // wing/LE slat rays from inspection lights
light.10= 5, 18.000, -27.000, -4.000, Opensky_wing_light, // wing/LE slat rays from inspection lights
light.11= 5, 15.500, -45.000, 12.000, Opensky_wing_light, // wing/LE slat rays from inspection lights
light.12= 5, 15.500, 45.000, 12.000, Opensky_wing_light, // wing/LE slat rays from inspection lights
light.13= 5, 32.350, 8.350, -0.250, Opensky_nav_yellow , // flap inspection light
light.14= 5, 32.350, -8.350, -0.250, Opensky_nav_yellow , // flap inspection light
light.15= 5, 28.000, -25.000, 0.000, Opensky_wing_light, // wing/LE slat rays from inspection lights
light.16= 5, 28.000, 25.000, 0.000, Opensky_wing_light, // wing/LE slat rays from inspection lights
light.17= 6, 72.000, 0.000, -8.350, Opensky_wing_light, // gear bay taxi light rays from taxi lights
[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
[jet_engine]
thrust_scalar=1.000
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
[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
