[fltsim.0] title=Project Opensky sim=OSERJ145lr model=as panel= sound= texture= atc_heavy=0 atc_airline=bmi atc_flight_number=2523 atc_parking_types=RAMP, GATE atc_parking_code= ui_manufacturer=Project Opensky ui_type=ERJ-145 ui_variation=Laser visual_damage=1 atc_id=2523 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