[fltsim.0]
title=Project Opensky - Alitalia 700th Embraer 145LR Airstair
sim=OSERJ145lr
model=asvc
panel=vc
sound=
texture=

atc_heavy=0
atc_airline=Alitalia
atc_flight_number=700
atc_parking_types=RAMP, GATE
atc_parking_code=

ui_manufacturer=Project Opensky
ui_type=ERJ-145LR
ui_variation=Alitalia 700th (Airstair)
visual_damage=1
atc_id=I-EXML
description=Project Opensky \nEmbraer Regional Jet - 145\nVersion 2007.9.1\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\nMaster Texture & Scheme Designer\n   Samy Fay\n\nTest Pilots\n   Project Opensky Members



[General]
atc_type=EMBRAER
atc_model=E145
performance=Passengers: 48\nCrew: 2+1 \n\nTotal Cargo Volume: 325 cu ft \n\nDimensions:\nSpan 65 ft 9 in\nLength 98 ft 0 in\nHeight 22 ft 2 in\n\nEngines: RR AE3007A1\nTO Thrust Rating: 7,580 lb\n\nMax Fuel Cap.: 11,435 lb\nMaxTOW: 48,502 lb\nMZFW: 39,463 lb\n\nTypical Cruise Speed @ FL350: \nM.78 - Normal Cruise\nM.80 - High Speed Cruise
editable=0
Category=airplane


[WEIGHT_AND_BALANCE]

//Maximum Ramp Weight		48,700 lb     / 22,090 kg
//Maximum Landing Weight	42,549 lb     / 19,300 kg
//Maximum Zero Fuel Weight	39,463 lb     / 17,900 kg
//Basic Operating Weight	27,758 lb     / 12,591 kg
//Maximum Payload		      12,755 lb     /  5,786 kg
//Maximum Fuel*			11,435 lb     /  5,187 kg
//*Fuel Density                 6.76 lb/gal /   .803 kg/l


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 = 12,755 lbs
// Maximum Payload per Opensky =  9,651 lbs
// Seating Configuration - Option 4 - Max PAX = 48
station_load.0 =   75,	 13.124, 0.000000, 3.000000, Wardrobe
station_load.1 =  320,	 13.124, 0.000000, 3.000000, Galley1
station_load.2 =  160,	 13.124, 0.000000, 3.000000, Galley2
station_load.3 = 2380,	 13.124, 0.000000, 3.000000, Std Economy Fwd // 14 PAX      
station_load.4 = 5440,	  0.000, 0.000000, 3.000000, Std Economy Aft // 32 PAX
station_load.5 = 1276,	-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= 48700.000
empty_weight= 26707.000 
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,   39.531,   0.000,  -7.900, 1300.000, 0, 0.812,  70.000, 0.550,  0.500,  0.250, 	10.000,	14.000, 0.000, 250.000, 280.000 // Nose gear
point.1 = 1,   -7.969,  -6.705,  -9.000, 1600.000, 1, 1.250,  0.000,  0.800,  1.500,  0.350, 	13.000, 15.000, 2.000, 250.000, 280.000 // Left main gear
point.2 = 1,   -7.969,   6.705,  -9.000, 1600.000, 2, 1.250,  0.000,  0.800,  1.500,  0.350, 	13.000, 15.000, 3.000, 250.000, 280.000 // Right main gear

// Scrape Points
// Fuselage
point.3 = 2,   39.531,   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,  -58.469,   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,  -50.669,   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,  -58.000, -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,  -58.000,  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,    1.243,   0.000,    4.245, 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  =2.500
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       =   0         //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              = -48.844
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              = -27.000
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= -20.000, -6.750, 2.800
Engine.1= -20.000,  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= 7580.000
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 = .75
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]
LeftMain   =-1.800000,-6.750000,-1.500000,846.000000,0.000000
RightMain  =-1.800000, 6.750000,-1.500000,846.000000,0.000000
fuel_type  =2.000000
number_of_tank_selectors=1
electric_pump=0