[fltsim.0]
title=Project Opensky - Embraer Legacy 
sim=OSERJ-Legacy
model=
panel=
sound=
texture=
kb_checklists=OS_ERJ_check
kb_reference=OS_ERJ_ref
atc_heavy=0
atc_airline=Palmetto Express
atc_flight_number=771
atc_parking_types=RAMP, GATE
atc_parking_code=
ui_manufacturer=Project Opensky
ui_createdby="Project Opensky"
ui_typerole="Executive Jet"
ui_type=Legacy 600
ui_variation=Palmetto Express
visual_damage=1
atc_id=N771PE
description=Project Opensky \nEmbraer Legacy\nVersion 2007.9.3\n\nFSX and FS2004 Compatible\n\nEngine Type: Rolls-Royce AE3007\n\nModel Designer\n   Nick Wilkinson - Exterior\n   Jacob Kubique - VC\n\nFlight Dynamics Designer\n   Warren C. Daniel\n   Brandon Henry\n\nTexture Designer \n   Samy Fay (Master texture)\n   Jacob Kubique and Corey Ford (VC)\n\n Scheme painter\n   Samy Fay\n Scheme dedicated to Viviane Desbiens\n\nTest Pilots\n   Project Open Sky Members


[General]
atc_type=EMBRAER
atc_model=E145
performance=Passengers: 8 to 10\nCrew: 2+1 \n\nTotal Cargo Volume: 325 cu ft \n\nDimensions:\nSpan 69 ft 11 in\nLength 98 ft 0 in\nHeight 22 ft 2 in\n\nEngines: RR AE3007\nTO Thrust Rating: 8,736 lb\n\nMax Fuel Cap.: 18,170 lb\nMaxTOW: 49,604 lb\nMZFW: 30,148 lb\n\nTypical Cruise Speed @ FL410: \nM.74 - Normal Cruise\nM.80 - Max Cruise\nRange - 3,250 nm @ M.74
editable=0
Category=airplane


[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= 8

// Maximum Payload per Embraer = 5,126 lbs
// Maximum Payload per Opensky = 1,092 lbs
// Seating Configuration - 2 adults, 2 children
station_load.0 =   35,	 13.124, 0.000000, 3.000000, Wardrobe
station_load.1 =   15,	 13.124, 0.000000, 3.000000, Galley1
station_load.2 =    4,	 13.124, 0.000000, 3.000000, Galley2
station_load.3 =  285,	 13.124, 0.000000, 3.000000, Std Economy Fwd // 2 PAX      
station_load.4 =  137,	  0.000, 0.000000, 3.000000, Std Economy Aft // 2 PAX
station_load.5 =   62,	-34.365, 0.000000, 3.000000, Aft Baggage     

//Moments of Inertia
empty_weight_roll_MOI  =  856479
empty_weight_pitch_MOI =  474924
empty_weight_yaw_MOI   = 2368455
empty_weight_coupled_MOI= 0.000

max_gross_weight= 49758.000
empty_weight= 30148.000 
CG_forward_limit= 0.000
CG_aft_limit= 0.000


[contact_points]

        //0  Class			  (1 = Landing Gear, 2 = Scrape)
        //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 Damage threshold 1 - Max speed
        //15 Damage threshold 2 - Speed damage

// Landing Gear
//	  0    1	 2	   3	   4	   5  6	      7	      8	      9	      10	11	12	13     14       15
point.0 = 1,   32.131,   0.000,  -7.600, 1300.000, 0, 0.812,  76.000, 0.550,  0.500,  0.250, 	 5.000,	7.000, 0.000, 250.000, 280.000 // Nose gear
point.1 = 1,   -7.969,  -6.705,  -8.700, 1600.000, 1, 1.250,  0.000,  0.800,  1.500,  0.350, 	 6.000, 7.500, 2.000, 250.000, 280.000 // Left main gear
point.2 = 1,   -7.969,   6.705,  -8.700, 1600.000, 2, 1.250,  0.000,  0.800,  1.500,  0.350, 	 6.000, 7.500, 3.000, 250.000, 280.000 // Right main gear

// Scrape Points
// Fuselage
point.3 = 2,   33.781,   0.000,  -2.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Nose
point.4 = 2,   31.500,   0.000,  -3.800,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Fuselage bottom fwd
point.5 = 2,    0.000,   0.000,  -6.250,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Fuselage bottom center
point.6 = 2,  -15.000,   0.000,  -3.800,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Fuselage bottom aft

point.7 = 2,   31.500,   0.000,   3.800,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Fuselage top fwd
point.8 = 2,    0.000,   0.000,   3.800,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Fuselage top center
point.9 = 2,  -15.000,   0.000,   3.800,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Fuselage top aft

point.10= 2,   31.500,  -3.800,   0.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Fuselage width fwd lt
point.11= 2,    0.000,   3.800,   0.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Fuselage width fwd rt
point.12= 2,  -15.000,  -3.800,   0.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Fuselage width center lt
point.13= 2,    0.000,   3.800,   0.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Fuselage width center rt
point.14= 2,  -44.235,  -3.800,   0.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Fuselage width aft left
point.15= 2,  -44.235,   3.800,   0.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Fuselage width aft right

point.16= 2,  -15.938,   0.000,   0.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Tailskid aft
point.17= 2,  -52.269,   0.000,   3.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 4,   0.000,   0.000 // Tail-APU

// Tailplane, vert/horiz stabs
point.18= 2,  -52.719,   0.000,  12.200,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 7,   0.000,   0.000 // Vertical stab fwd
point.19= 2,  -44.919,   0.000,  12.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 7,   0.000,   0.000 // Vertical stab aft
point.20= 2,  -52.250, -12.450,  11.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 5,   0.000,   0.000 // Horizontal Stab aft lt
point.21= 2,  -52.250,  12.450,  11.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 6,   0.000,   0.000 // Horizontal Stab aft rt

// Wings
point.22= 2,  -8.500,  -32.950,  -1.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 5,   0.000,   0.000 // Left wingtip fwd
point.23= 2, -11.000,  -32.950,  -1.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 5,   0.000,   0.000 // Left wingtip aft
point.24= 2,  -8.500,   32.950,  -1.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 6,   0.000,   0.000 // Right wingtip fwd
point.25= 2, -11.000,   32.950,  -1.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 6,   0.000,   0.000 // Right wingtip aft
point.26= 2,   0.000,  -13.500,  -2.500,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 5,   0.000,   0.000 // Left wing-mid fwd
point.27= 2,  -7.500,  -13.500,  -2.500,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 5,   0.000,   0.000 // Left wing-mid aft
point.28= 2,   0.000,   13.500,  -2.500,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 6,   0.000,   0.000 // Right wing-mid fwd
point.29= 2,  -7.500,   13.500,  -2.500,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 6,   0.000,   0.000 // Right wing-mid aft

// Engines
point.30= 2, -20.000,   -6.750,   3.900,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 8,   0.000,   0.000 // Left engine bottom
point.31= 2, -20.000,    6.750,   3.900,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 8,   0.000,   0.000 // Right engine bottom
point.32= 2, -14.000,   -6.750,   0.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 8,   0.000,   0.000 // Left engine fwd
point.33= 2, -14.000,    6.750,   0.000,  787.400, 0, 0.000,  0.000,  0.000,  0.000,  0.000,  0.000,  0.000, 8,   0.000,   0.000 // Right engine fwd

max_number_of_points = 34

static_pitch = -1.260
static_cg_height = 7.500
gear_system_type=1           //Hydraulic
emergency_extension_type=2   //None=0,Pump=1,Gravity=2

[LIGHTS]  
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing   
light.1=1,    9.250,   0.000,    4.445, fx_beacon ,
//light.2=1,   -7.000,   0.000,   -6.000, fx_beacon ,



[Views]
eyepoint = 31.4, -1.80, 2.0


[electrical]
max_battery_voltage = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0

                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus       = 0, 5 , 9.5
avionics           = 1, 5 , 9.5
additional_system  = 0, 2 , 9.5
marker_beacon      = 1, 2 , 9.0
fuel_pump          = 0, 5 , 9.0


[flight_tuning]
cruise_lift_scalar     =0.750
parasite_drag_scalar   =1.000
induced_drag_scalar    =1.000
elevator_effectiveness =1.750
aileron_effectiveness  =3.500
rudder_effectiveness   =1.000
pitch_stability        =4.000
roll_stability         =1.000
yaw_stability          =3.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000


[airplane_geometry]
wing_area                  = 551.000
wing_span                  =  68.916     //EMB-145XR
//wing_span                =  65.900     //EMB-145EP/ER/EU/MP/MKL/LR/LU
wing_root_chord            =   7.850
wing_dihedral              =   3.000
wing_incidence             =   6.000
wing_twist                 =   1.000
oswald_efficiency_factor   =   1.000
wing_winglets_flag         =   1         //EMB-145XR
//wing_winglets_flag       =   1         //EMB-145EP/ER/EU/MP/MKL/LR/LU
wing_sweep                 =  24.760
wing_pos_apex_lon          =  12.000
wing_pos_apex_vert         =  -2.500
htail_area                 = 120.600
htail_span                 =  24.900
htail_pos_lon              = -43.094
htail_pos_vert             =  12.848
htail_incidence            =   5.000     //<===========
htail_sweep                =  35.000
vtail_area                 =  77.500
vtail_span                 =  15.716
vtail_sweep                =  42.000
vtail_pos_lon              = -21.250
vtail_pos_vert             =   4.000
elevator_area              =  25.840
aileron_area               =  25.000
rudder_area                =  25.630
elevator_up_limit          =  24.000
elevator_down_limit        =  15.000
aileron_up_limit           =  25.000
aileron_down_limit         =  15.000
rudder_limit               =  15.000
elevator_trim_limit        =  15.000
spoiler_limit              =  30.000
spoilerons_available       =   0
aileron_to_spoileron_gain  =   3.000
min_ailerons_for_spoilerons=   0.700
min_flaps_for_spoilerons   =   0.000
auto_spoiler_available     =   1
spoiler_extension_time     =   2.000
positive_g_limit_flaps_up  =   9.615
positive_g_limit_flaps_down=   2.991
negative_g_limit_flaps_up  =  -5.341
negative_g_limit_flaps_down=  -2.000

[GeneralEngineData]
engine_type= 1
Engine.0= -14.250, -6.750, 2.800
Engine.1= -14.250,  6.750, 2.800
fuel_flow_scalar= 1.200
min_throttle_limit=-0.250000


[TurbineEngineData]
bypass_ratio=5.000 // Overall Pressure Ratio = 18-20:1
fuel_flow_gain= 0.003
inlet_area= 8.0786
rated_N2_rpm= 7376.000
static_thrust= 8736.000
afterburner_available= 0
reverser_available= 1.000


[jet_engine]
thrust_scalar =1.000


[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



[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 400.0


[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2


[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0


[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 2


[altimeters]
altimeter.0 = 1
altimeter.1 = 1


[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0


[vacuum_system]
max_pressure=5.15   //PSI
vacuum_type=2   //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi


[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000


[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0    //Scalar on heat effectiveness, 0 = not available


[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
elevator = 100, 200
aileron  = 100, 200
rudder   = 100, 200


[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0


[deice_system]
structural_deice_type=1     //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots


[exits]
number_of_exits = 2
exit_rate.0 = 0.3                               ;Percent per second
exit_rate.1 = 0.5                               ;Percent per second
exit_rate.2 = 0.8                               ;Percent per second

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


[Reference Speeds]
flaps_up_stall_speed    = 112.000
full_flaps_stall_speed  = 102.000
cruise_speed            = 431.000
max_indicated_speed=340.000000
max_mach=0.82000


[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 0.000
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_takeoff_ga= 1
autothrottle_max_rpm= 95.000
pitch_takeoff_ga= 8.000
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=1.000000
max_pitch_velocity_hi_alt=0.030000
max_pitch_velocity_lo_alt_breakpoint=17000.000000
max_pitch_velocity_hi_alt_breakpoint=24000.000000
max_bank=30.000000
max_throttle_rate=0.100000
nav_proportional_control=25.000000
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=2.000000
max_bank_acceleration=0.800000
max_bank_velocity=3.000000


[forcefeedback]
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds


[brakes]
toe_brakes_scale=0.600000
parking_brake=1
auto_brakes=0
hydraulic_system_scalar = 1  //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure



[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494


[stall_warning]
type=1
stick_shaker=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


[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2


[pitot_static]
pitot_heat=1.000000


[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0


[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000


[deice_system]
structural_deice_type=0


[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 21.000
system_type= 0
damaging-speed= 220.000
blowout-speed= 280.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 9.000, 0.000
flaps-position.2= 18.000, 0.000
flaps-position.3= 22.000, 0.000
flaps-position.4= 45.000, 0.000

[Flaps.1]
type= 1
span-outboard= 0.400
extending-time= 15.000
system_type= 0
damaging-speed= 220.000
blowout-speed= 280.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 9.000, 0.000
flaps-position.2= 18.000, 0.000
flaps-position.3= 22.000, 0.000
flaps-position.4= 45.000, 0.000


[CameraDefinition.0]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .50
ShowWeather = Yes
InitialXyz = 0, 2.3, -20.0
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.45
ShowWeather = Yes
InitialXyz = 10.8, 1.4, -2.0
InitialPbh = 6, 0, 310
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.2]
Title = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.45
ShowWeather = Yes
InitialXyz = -10.8, 1.4, -2.0
InitialPbh = 6, 0, 50
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum

[CameraDefinition.001]
Title = "Radio Stack"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.45, -0.25, -0.1
InitialPbh=14.2, 0, 0

[CameraDefinition.002]
Title = "Engine Controls"
Guid = {195EAB58-9E4A-3E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.1
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.30, 0.09, -0.18
InitialPbh=48.5, 0, 9

[fuel]       // Legacy Fuel, Max fuel = 18,170 lbs, 2,712 gallons
             //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1    = 1.800000, 0.000000,-1.500000,582.400000,0.000000 // Fwd Under Belly Tanks, 3,937 lbs, 582.40 gallons
Center2    =-8.000000, 0.000000,-1.500000,837.350000,0.000000 // Aft Tank, 2,910 lbs, 430.47 gallons
LeftMain   =-1.800000,-6.750000,-1.500000,837.350000,0.000000 // Left Wing Tank, 11,321 lbs, 1674.70 gallons / 2 = 837.35 gallons
RightMain  =-1.800000, 6.750000,-1.500000,837.350000,0.000000 // Left Wing Tank, 11,321 lbs, 1674.70 gallons / 2 = 837.35 gallons 
fuel_type  =2.000000
number_of_tank_selectors=1
electric_pump=0