[fltsim.0]
title=Boeing 767-201ER Piedmont 'Pride of Piedmont' (N603P) - No Wing Views
sim=767-200ER-GE-CF6-80A
model=NOWV
panel=
sound=
texture=PAI_N603P
checklists=
atc_airline=Piedmont
atc_flight_number=5
atc_heavy=1
atc_parking_types=GATE
atc_parking_code=USA,PAI
atc_id=N603P
ui_manufacturer=Boeing-Project Opensky
ui_type=767-201ER
ui_variation=Piedmont 'Pride of Piedmont' (N603P) (No Wing Views)
visual_damage=1
description=Project Opensky - Boeing 767-201ER\nVersion 2004.8.0\n Piedmont 'Pride of Piedmont' (N603P) repaint by\n Jeffrey S. Bryner\nModel\\VC Designer\n Albert Bouwman \n\nFlight Dynamics\\Sound\\Effects Designer\n Warren C. Daniel\n\nMaster Texture Designer\n Tom Harlaar\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
[fltsim.1]
title=Boeing 767-201ER Piedmont 'Pride of Piedmont' (N603P) - Wing Views
sim=767-200ER-GE-CF6-80A
model=WV
panel=
sound=
texture=PAI_N603P
checklists=
atc_airline=Piedmont
atc_flight_number=5
atc_heavy=1
atc_parking_types=GATE
atc_parking_code=USA,PAI
atc_id=N603P
ui_manufacturer=Boeing-Project Opensky
ui_type=767-201ER
ui_variation=Piedmont 'Pride of Piedmont' (N603P) (Wing Views)
visual_damage=1
description=Project Opensky - Boeing 767-201ER\nVersion 2004.8.0\n Piedmont 'Pride of Piedmont' (N603P) repaint by\n Jeffrey S. Bryner\nModel\\VC Designer\n Albert Bouwman \n\nFlight Dynamics\\Sound\\Effects Designer\n Warren C. Daniel\n\nMaster Texture Designer\n Tom Harlaar\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
[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: 181 \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: GE CF6-80A2\nTO Thrust Rating: 50,000 lb\n\nMax Fuel Cap.: 16,700 gal\nMaxTOW: 345,000 lb\nZFW: 209,000 lb\n\nTypical Cruise Speed \n @ FL350: M.80
atc_type=BOEING AIRCRAFT
atc_model=B762
[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 = 181610.000
max_gross_weight = 409000.000
max_number_of_stations = 6
// New FS2004 Numbers
// Max Structural Payload Per Boeing - 73,350 lbs
// Max Structural Payload Opensky - 46,249 lbs
// Actual Total PAX - 31,675 lbs
station_load.0 = "3150, 20.0, 0.0, 0.0, 1st Class - 18 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "5250, 40.0, 0.0, 0.0, Bus Class - 30 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "23275, 0.0, 0.0, 0.0, Econ Class -133 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
// Total Opensky Cargo - 14,574 lbs
station_load.3 = "6787, 45.0, 0.0, 0.0, Lwr Dk Cgo Fwd" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "6787, -50.0, 0.0, 0.0, Lwr Dk Cgo Aft" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "1000, -70.0, 0.0, 0.0, Lwr Dk Cgo Bulk" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
// Moments of Inertia
empty_weight_roll_MOI= 4378085.000
empty_weight_pitch_MOI= 7971735.000
empty_weight_yaw_MOI= 12879901.000
empty_weight_coupled_MOI= 0.000
[flight_tuning]
cruise_lift_scalar = 1.00
parasite_drag_scalar = 0.773
induced_drag_scalar = 0.963
elevator_effectiveness = 1.00
aileron_effectiveness = 1.00
rudder_effectiveness = 1.20
pitch_stability = 1.00
roll_stability = 1.00
yaw_stability = 1.00
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[fuel] // Max fuel per Boeing - 24,140 lb
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
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 // 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= 13.500
gear_system_type=0
//
//=======================================================================================================================================================
//
[GeneralEngineData]
engine_type= 1
Engine.0= 6.000, -26.667, -5.583
Engine.1= 6.000, 26.667, -5.583
fuel_flow_scalar=1.08
min_throttle_limit=-0.319946
[TurbineEngineData]
bypass_ratio=4.7000
fuel_flow_gain= 0.001
inlet_area= 40.69
rated_N2_rpm= 29920.000
static_thrust= 50000.000
afterburner_available= 0
reverser_available= 1
[Reference Speeds]
flaps_up_stall_speed= 118.000
full_flaps_stall_speed= 94.400
cruise_speed= 535.341
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=68.997949,-1.768578,8.753178
[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=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.
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=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=30.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
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, 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=Opensky_sparks, 1
touchdown=fx_tchdwn, 1
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 30 // seconds
flaps-position.0= 0.000, 0.000
flaps-position.1= 01.000, 0.000
flaps-position.2= 05.000, 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
damaging-speed = 200 // KIAS
blowout-speed = 250 // KIAS
lift_scalar = 0.7
drag_scalar = 0.9
pitch_scalar= 0.5
system_type = 1 //Hydraulic
[flaps.1]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 35 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 20.0 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 0.3
drag_scalar = 0.1
pitch_scalar= 0.1
system_type = 1 //Hydraulic
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1 = 1, 35.500, 0.000, 14.000, Opensky_beacon,
light.2 = 1, 12.500, 0.000, -3.800, Opensky_beacon,
light.3 = 5, 19.700, 19.000, -4.000, Opensky_nacelle_refl,
light.4 = 5, 19.700, -19.000, -4.000, Opensky_nacelle_refl,
light.5 = 5 8.000, 17.000, -10.000, Opensky_wing_light,
light.6 = 5, 19.933, 8.827, -4.368, Opensky_wing_light,
light.7 = 5, 8.000, -17.000, -10.000, Opensky_wing_light,
light.8 = 5, 19.933, -8.827, -4.368, Opensky_wing_light,
[brakes]
toe_brakes_scale=0.396741
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=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 = 0.2 ;Percent per second
exit_rate.1 = 0.1 ;Percent per second
