//********************************************************* // ALABEO C195 BusinessLiner FSX/P3D // Copyright � Alabeo 2014 - All Rights Reserved //********************************************************* [fltsim.0] title=Alabeo C195 WHITE sim=C195 model= panel= sound= texture= kb_checklists= kb_reference= atc_id= ui_manufacturer="Alabeo" ui_type=C195 BusinessLiner ui_typerole="Single Engine Prop" ui_createdby="Alabeo" ui_variation=WHITE description="BusinessLiner" atc_heavy=0 atc_airline= atc_flight_number= atc_id_color=0000000000 visual_damage=1 [fltsim.1] title=Alabeo C195 N654ER sim=C195 model= panel= sound= texture=1 kb_checklists= kb_reference= atc_id=N654ER ui_manufacturer="Alabeo" ui_type=C195 BusinessLiner ui_typerole="Single Engine Prop" ui_createdby="Alabeo" ui_variation=N654ER description="BusinessLiner" atc_heavy=0 atc_airline= atc_flight_number= atc_id_color=0000000000 visual_damage=1 [fltsim.2] title=Alabeo C195 N784RA sim=C195 model= panel= sound= texture=2 kb_checklists= kb_reference= atc_id=N784RA ui_manufacturer="Alabeo" ui_type=C195 BusinessLiner ui_typerole="Single Engine Prop" ui_createdby="Alabeo" ui_variation=N784RA description="BusinessLiner" atc_heavy=0 atc_airline= atc_flight_number= atc_id_color=0000000000 visual_damage=1 [fltsim.3] title=Alabeo C195 N354MP sim=C195 model= panel= sound= texture=3 kb_checklists= kb_reference= atc_id=N354MP ui_manufacturer="Alabeo" ui_type=C195 BusinessLiner ui_typerole="Single Engine Prop" ui_createdby="Alabeo" ui_variation=N354MP description="BusinessLiner" atc_heavy=0 atc_airline= atc_flight_number= atc_id_color=0000000000 visual_damage=1 [fltsim.4] title=Alabeo C195 N9654H sim=C195 model= panel= sound= texture=4 kb_checklists= kb_reference= atc_id=N9654H ui_manufacturer="Alabeo" ui_type=C195 BusinessLiner ui_typerole="Single Engine Prop" ui_createdby="Alabeo" ui_variation=N9654H description="BusinessLiner" atc_heavy=0 atc_airline= atc_flight_number= atc_id_color=0000000000 visual_damage=1 [fltsim.5] title=Alabeo C195 N683CB sim=C195 model= panel= sound= texture=5 kb_checklists= kb_reference= atc_id=N683CB ui_manufacturer="Alabeo" ui_type=C195 BusinessLiner ui_typerole="Single Engine Prop" ui_createdby="Alabeo" ui_variation=N683CB description="BusinessLiner" atc_heavy=0 atc_airline= atc_flight_number= atc_id_color=0000000000 visual_damage=1 [fltsim.6] title=Alabeo C195 NI62MP sim=C195 model= panel= sound= texture=6 kb_checklists= kb_reference= atc_id=NI62MP ui_manufacturer="Alabeo" ui_type=C195 BusinessLiner ui_typerole="Single Engine Prop" ui_createdby="Alabeo" ui_variation=NI62MP description="BusinessLiner" atc_heavy=0 atc_airline= atc_flight_number= atc_id_color=0000000000 visual_damage=1 [General] atc_type=Cessna atc_model=C195 editable=0 performance="Maximum Speed\t\n161 kts\t185 mph\t298 kmh\n\nCruise Speed\t\n148 kts\t170 mph\t274 kmh\n\nEngine\t\nJacobs R-755 Radial Engine\t300 hp\n\nPropeller\t\nHamilton Standard, 2 Bladed, constant speed\n\nMaximum Range\t\n695 nm\t800 sm\t1287 km\n\nService Ceiling\t\n18300 ft\t\t5578 m\n\nFuel Capacity\t\n75 U.S. gal\t284 L\n\nEmpty Weight\t\n2100 lb\t953 kg\n\nMaximum Gross Weight\t\n3350 lb\t1520 kg\n\nUseful Load\t\n1250 lb\t567 kg\n\nLength\t\n27,33 ft\t8,33 m\n\nWingspan\t\n36,16 ft\t11,02 m\n\nHeight\t\n7,17 ft\t2,18 m\n\nSeating\t\n5" Category = airplane [WEIGHT_AND_BALANCE] max_gross_weight = 3350 // (pounds) empty_weight = 2100 // (pounds) ;Moments of Inertia empty_weight_pitch_MOI = 2000 empty_weight_roll_MOI = 2000 empty_weight_yaw_MOI = 2700 empty_weight_coupled_MOI = 0 reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 6 station_load.0 = 185, 0, 0, 0 //Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 0, 0, 0, 0 station_load.2 = 0, -1, -0.5, 0 station_load.3 = 0, -1, 0.0, 0 station_load.4 = 0, -1, 0.5, 0 station_load.5 = 0, -2, 0.0, 0 station_name.0 = "pilot" station_name.1 = "fwd pax" station_name.2 = "left pax" station_name.3 = "mid pax" station_name.4 = "right pax" station_name.5 = "bag 220lbs" [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.5 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 0.1 p_factor_on_yaw = 0.5 torque_on_roll = 0.5 hi_alpha_on_roll = 0.5 hi_alpha_on_yaw = 0.5 gyro_precession_on_yaw = 0.5 gyro_precession_on_pitch = 0.5 [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 7, 0, -0.5 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 0.9 //Fuel flow scalar min_throttle_limit = 0 //Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar = 1 //Piston power scalar cylinder_displacement= 70 //Cubic inches per cylinder compression_ratio= 8.1 //Compression ratio number_of_cylinders=9 //Number of cylinders max_rated_rpm= 2200 //Max rated RPM max_rated_hp= 300 //Max rated HP fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque= 1 //Starter torque factor turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp= 0 //Max design manifold pressure, (inHg) min_design_mp= 0 //Min design manifold pressure, (inHg) critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar= 1 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar= 1 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar= 1 //Scalar on maximum RPM friction idle_rpm_friction_scalar= 1 //Scalar on idle RPM friction detonation_onset = 36 [propeller] thrust_scalar = 1 //Propeller thrust scalar propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 7.6 //Propeller Diameter, (feet) propeller_blades= 2 //Number of propeller blades propeller_moi= 10.9 //Propeller moment of inertia beta_max= 40 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 15 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 1000 //Miminum governed RPM prop_tc= 0.1 //Prop time-constant gear_reduction_ratio= 1 //Propeller gear reduction ratio fixed_pitch_beta= 20 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit= 80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available= 0 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available= 0 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available= 0 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather= 0 //Minimum RPM for prop feathering beta_feather= 0 //Feathering pitch angle (degrees) power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta= 0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= 0 //Minimum pitch angle in reverse, (degrees) //0 Class //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 [contact_points] point.0= 1, -18.4, 0.0, -0.65, 1500, 0, 0.5, 60, 0.09, 2.5, 0.7, 0, 0, 0, 0.0, 0.0 point.1= 1, 2.25, -3.8, -5.45, 1500, 1, 1.2, 0, 0.28, 2.0, 0.8, 0, 0, 2, 0.0, 0.0 point.2= 1, 2.25, 3.8, -5.45, 1500, 2, 1.2, 0, 0.28, 2.0, 0.8, 0, 0, 3, 0.0, 0.0 point.3= 2, 2.0, -15.0, 3.70, 1500, 0, 0.0, 0, 0.00, 0.0, 0.0, 0, 0, 5, 0.0, 0.0 point.4= 2, 2.0, 15.0, 3.70, 1500, 0, 0.0, 0, 0.00, 0.0, 0.0, 0, 0, 6, 0.0, 0.0 point.5= 2, -1.5, -13.5, -1.00, 1500, 0, 0.0, 0, 0.00, 0.0, 0.0, 0, 0, 5, 0.0, 0.0 point.6= 2, -1.5, 13.5, -1.00, 1500, 0, 0.0, 0, 0.00, 0.0, 0.0, 0, 0, 6, 0.0, 0.0 point.7= 2, -3.0, -12.0, -1.50, 1500, 0, 0.0, 0, 0.00, 0.0, 0.0, 0, 0, 5, 0.0, 0.0 point.8= 2, -3.0, 12.0, -1.50, 1500, 0, 0.0, 0, 0.00, 0.0, 0.0, 0, 0, 6, 0.0, 0.0 point.9= 2, -12.5, 0.0, 5.50, 1500, 0, 0.0, 0, 0.00, 0.0, 0.0, 0, 0, 9, 0.0, 0.0 point.10= 2, 5, 0.0, 0.00, 1500, 0, 0.0, 0, 0.00, 0.0, 0.0, 0, 0, 4, 0.0, 0.0 static_pitch = 12.5 static_cg_height = 4.5 tailwheel_lock= 0 [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.7 //Brake scalar differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected auto_brakes = 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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 4, 1.2, 0.0, 0.5, fx_vclightalaccnc [hydraulic_system] normal_pressure = 0.0 //PSI [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 = 0 Transponder.1 = 1 Marker.1 = 1 [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=0,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=1,0 [vacuum_system] max_pressure=5.15 //PSI vacuum_type=1 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi engine_map=1 [pneumatic_system] max_pressure=0.000000 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] Leftmain = 0, -3, 2, 38, 1 Rightmain = 0, 3, 2, 38, 1 fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 218 wing_span = 36 wing_root_chord = 7 wing_dihedral = 0 wing_incidence = 0 //Degrees wing_twist = 0 //Degrees oswald_efficiency_factor= 1 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 1 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 1 //Feet, vertical distance from reference point, positive going up htail_area = 16 //Square feet htail_span = 10 //Feet htail_pos_lon = -12 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 1.5 //Feet, vertical distance from reference point, positive going up htail_incidence = 0 //Degrees htail_sweep = 33 //Degrees, horizontal tail leading edge vtail_area = 9 //Square feet vtail_span = 5 //Feet, tip to body vtail_sweep = 27 //Degrees, vertical tail leading edge vtail_pos_lon = -12 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 3 //Feet, vertical distance from reference point, positive going up elevator_area = 15 //Square feet aileron_area = 17 //Square feet rudder_area = 10 //Square feet elevator_up_limit = 28 elevator_down_limit = 17 aileron_up_limit = 25 aileron_down_limit = 25 rudder_limit = 21 elevator_trim_limit = 9 spoiler_limit = 0 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 auto_spoiler_available = 0 positive_g_limit_flaps_up=4.4 positive_g_limit_flaps_down=3.9 negative_g_limit_flaps_up=-2.0 negative_g_limit_flaps_down=-1.7 load_safety_factir=1.5 [flaps.0] type=1 span-outboard= 0.4 extending-time= 7 flaps-position.0= 0 flaps-position.1= 45 damaging-speed= 130 blowout-speed= 140 lift_scalar= 1 drag_scalar= 1 pitch_scalar= 1 system_type= 2 [Reference Speeds] flaps_up_stall_speed = 54 //Knots True (KTAS) full_flaps_stall_speed = 53 //Knots True (KTAS) cruise_speed = 120 //Knots True (KTAS) max_indicated_speed = 205 //Red line (KIAS) [stall_warning] type=2 stick_shaker=0 [deice_system] structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots [exits] number_of_exits = 4 exit.0 = 0.4 // (0=Main 1=Emergency) exit.1 = 0.4 // (0=Main 1=Emergency) [autopilot] autopilot_available= 0 flight_director_available= 0 [forcefeedback] ground_bumps_magnitude1=3000 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=4.0 ground_bumps_slope1=0.25 ground_bumps_magnitude2=350 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=0.7 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 [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. elevatpor = 140, 240 aileron = 200, 1000 rudder = 200, 1000 [Views] eyepoint = 0.75, -1.05, 1.50 [CameraDefinition.001] Title = "Right Seat" Guid = {195EAB58-9E4A-1E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = Yes SnapPbhAdjust = Swivel SnapPbhReturn = False PanPbhAdjust = Swivel PanPbhReturn = False Track = None ShowAxis = YES AllowZoom = TRUE InitialZoom = 0.45 SmoothZoomTime = 2.0 ZoomPanScalar = 0.5 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.55, 0, -0.2 InitialPbh=13, 0, 340 [CameraDefinition.002] Title = "Panel" 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 = 0.5 SmoothZoomTime = 2.0 ZoomPanScalar = 1 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.26, -0.27, -0.1 InitialPbh=0, 0.0, 0.0 [CameraDefinition.003] Title = "Passenger" Guid = {0456199A-99D4-11DC-B263-66CC55D89593} Origin = Virtual Cockpit MomentumEffect = Yes SnapPbhAdjust = Swivel SnapPbhReturn = False PanPbhAdjust = Swivel PanPbhReturn = False Track = None ShowAxis = YES AllowZoom = TRUE InitialZoom = 0.40 SmoothZoomTime = 2.0 ZoomPanScalar = 0.4 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.5, 0.03, -0.82 InitialPbh=8, 0, 337 [CameraDefinition.0] Title = angle view 1 Guid = {B0CA7E72-F3D9-F748-8BF5-108D197B2469} Description = angle view 1 Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = 1.5, 0.3, -4.2 InitialPbh = 5, 0, 359 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.1] Title = angle view 2 Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59} Description = angle view 2 Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.64 ShowWeather = Yes InitialXyz = 2.7, 0.4, 7.0 InitialPbh = 5, 0, 205 XyzAdjust = TRUE Category=Aircraft ClipMode=Minimum MomentumEffect=TRUE [CameraDefinition.2] Title = angle view 3 Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED} Description = angle view 3 Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.60 ShowWeather = Yes InitialXyz = -6.45, -0.29, -0.27 InitialPbh = 0, 0, 72 XyzAdjust = TRUE Category=Aircraft ClipMode=Minimum [CameraDefinition.3] Title = "angle view 4" Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A} Description = angle view 4 Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.64 ShowWeather = Yes InitialXyz = -2.6, 0.7, -8.4 InitialPbh = 10, 0, 5 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.4] Title = "angle view 5" Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de} Description = angle view 5 Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.45 ShowWeather = Yes InitialXyz = -6.7, 0.3, 0.5 InitialPbh = 8, 0, 100 XyzAdjust = TRUE Category=Aircraft ClipMode=Minimum [CameraDefinition.5] Title = "angle view 6" Guid = {7a91803e-898b-435a-8391-725be6a48203} Description = angle view 6 Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.40 ShowWeather = Yes InitialXyz = 3.5, 2.2, -6.3 InitialPbh = 25, 0, 320 XyzAdjust = TRUE Category=Aircraft ClipMode=Minimum MomentumEffect=TRUE [CameraDefinition.6] Title = "angle view 7" Guid = {8A1987D0-09B6-7E48-B4E1-62C5DBE2A720} Description =angle view 7 Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom =0.49 ShowWeather = Yes InitialXyz = -0, 1.1, 5.2 InitialPbh = 15, 0, 180 XyzAdjust = TRUE Category=Aircraft MomentumEffect=FALSE ClipMode=Minimum [CameraDefinition.7] Title = "angle view 8" Guid = {8A1987D0-09B6-7E48-B4E1-62C5DBE2A721} Description =angle view 8 Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom =0.70 ShowWeather = Yes InitialXyz = -10, 2.1, 5.2 InitialPbh = 14, 0, 122 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.8] Title = "angle view 9" Guid = {bbc3f178-c1bd-41e6-a714-a87a7e2256b6} Description =angle view 9 Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom =0.35 ShowWeather = Yes InitialXyz = -3.2, -0.35, 2.8 InitialPbh = -3, 0, 135 XyzAdjust = TRUE Category=Aircraft MomentumEffect=FALSE ClipMode=Minimum