[fltsim.0]
title=SIAI-Marchetti SF-260
sim=SIAI-Marchetti SF-260
model=
panel=
sound=
texture=
kb_checklists=
atc_heavy=0
atc_airline=Air Force
atc_flight_number=S21
ui_manufacturer=SIAI-MARCHETTI-AERMACCHI
ui_type=SF-260
ui_typerole="Single Engine Prop"
ui_createdby="G. Quai"
ui_variation="Reparto Sperimentale"
description=The Siai-Marchetti SF.260 is an aircraft marketed as Light attack/aerobatic military trainer. It was designed by (the great) STELIO FRATI. First flight of the prototype on July 15, 1964.
[fltsim.1]
title=SIAI-Marchetti SF-260PAINTAIRCOMBATUSA
sim=SIAI-Marchetti SF-260
model=
panel=
sound=
texture=AIRCOMBATUSA
kb_checklists=
atc_heavy=0
atc_airline=Air Combat
atc_flight_number=S206
ui_manufacturer=SIAI-MARCHETTI-AERMACCHI
ui_type=SF-260
ui_typerole="Single Engine Prop"
ui_createdby="G. Quai"
ui_variation="Air Combat USA"
description=The Siai-Marchetti SF.260 is an aircraft marketed as Light attack/aerobatic military trainer. It was designed by (the great) STELIO FRATI. First flight of the prototype on July 15, 1964.
[General]
atc_type=SF260
atc_model=
editable=0
performance="Maximum Speed\t\n237kts 276mph 441kmh\nEngine\t\nLycoming O-540-E4A5 260hp\t\nPropeller\t\nTwo-bladed constant speed\t\nMaximum Range\t\n1,107nm 1,274sm 2,050km\t\nService Ceiling\t\n19,000ft 5,800m\t\nLength\t\n23.00ft 7.00m\t\nWingspan\t\n26.12ft 8.22m\t\nHeight\t\n8.6 ft 2.6m\t\nSeating\t\n2"
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 3368 // (pounds)
empty_weight = 2189 // (pounds)
reference_datum_position = 3.9, 0, 0.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -3.7, 0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170, -3.1, -1.5, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, -3.1, 1.5, 0.0, flight instructor" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "100, -6.1, -1.5, 0.0, ballast" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "100, -6.1, 1.5, 0.0, Ballast" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "33, -8.5, 0.0, 0.0, Electronic" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 2706
empty_weight_roll_MOI = 2131
empty_weight_yaw_MOI = 3932
empty_weight_coupled_MOI = 0.0
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 0.75
induced_drag_scalar =1.2
elevator_effectiveness =1.1
aileron_effectiveness =1.9
rudder_effectiveness = 1.0
pitch_stability =1.3
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness =1.3
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 2.1, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 90.3 //Cubic inches per cylinder
compression_ratio= 8.0 //Compression ratio
number_of_cylinders=6 //Number of cylinders
max_rated_rpm= 2575 //Max rated RPM
max_rated_hp= 270 //Max rated HP
fuel_metering_type= 0 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 38 //Max design manifold pressure, (inHg)
min_design_mp= 1 //Min design manifold pressure, (inHg)
critical_altitude= 18000 //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= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar =1.2 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.3 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi= 8.0 //Propeller moment of inertia
beta_max= 43 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 15 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1100 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 0 //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= 1 //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)
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
//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, 1.18, 0.0, -3.46, 1181.1, 0, 0.523, 34.00, 0.286, 2.5, 0.794, 3.5, 3.8, 0, 165.0, 165.0
point.1=1, -5.48, -4.5, -3.30, 1574.8, 1, 0.523, 0.00, 0.286, 2.5, 0.808, 4.7, 5.1, 2, 165.0, 165.0
point.2=1, -5.48, 4.5, -3.30, 1574.8, 2, 0.523, 0.00, 0.286, 2.5, 0.808, 5.6, 6.2, 3, 165.0, 165.0
point.3=2, -3.90, -18.0, -0.67, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -3.90 18.0, -0.67, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -20.23, 0.0, 0.83, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, -1.48, 0.0, -2.17, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 4, 0.0, 0.0
point.7=2, -20.23, 0.0, 6.83, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 7, 0.0, 0.0
point.8=2, -4.90, 0.0, -1.83, 1574.8, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 8, 0.0, 0.0
max_number_of_points = 21
static_pitch = 2.9
static_cg_height =3.68
gear_system_type=0 //Electric
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint = -0.75, 0.0, 1.70 // -0.354, 0.0, 1.685
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3,1.00, -13.78, 0.10, fx_navred ,
light.1 = 3,1.00, 13.78, 0.10, fx_navgre ,
light.2 = 7, 0.98, -13.78, 0.10, fx_recog ,
light.3 = 7, 0.98, 13.78, 0.10, fx_recog ,
light.4 = 1, -15.00, 0.00, -0.30, fx_navwhi
light.5 = 4, 0.60,0.40,2.55, fx_vclight,
light.6 = 2,0.96, -13.78, 0.10, fx_strobe ,
light.7 = 2,0.96, 13.78, 0.10, fx_strobe ,
light.8 = 4,0.60,-0.40,2.55, fx_vclight,
[SMOKESYSTEM]
smoke.0=-10.0, 0.0, 0.0, fx_smoke_w
[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.15,0.20 ;Percent per second
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees, KIAS
flaps-position.1 = 8 // degrees, KIAS
flaps-position.2 = 12
flaps-position.3 = 36 // degrees, KIAS
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar =1.1
pitch_scalar= 1.0
system_type = 0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[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
[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, 180
aileron = 200, 1000
rudder = 200, 1000
[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=1,0
[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=1,1 //Turn AND Bank
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -4.1, -7.9, -0.8, 47.5, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -4.1, 7.9, -0.8, 47.5, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 175.0 //Square feet
wing_span = 36.1 //Feet
wing_root_chord = 5.1 //Feet
wing_dihedral = 5.5 //Degrees
wing_incidence = 2.5 //Degrees
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 0.6 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0.0 //Degrees, wing leading edge
wing_pos_apex_lon = -2.6 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 34.0 //Square feet
htail_span = 11.8 //Feet
htail_pos_lon = -18.6 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 1.0 //Degrees
htail_sweep = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 10.0 //Square feet
vtail_span = 3.6 //Feet, tip to body
vtail_sweep = 0.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -16.5 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 1.5 //Feet, vertical distance from reference point, positive going up
elevator_area = 16.6 //Square feet
aileron_area = 18.3 //Square feet
rudder_area = 6.7 //Square feet
elevator_up_limit = 28.0 //Degrees
elevator_down_limit = 21.0 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 15.0 //Degrees
rudder_limit = 24.0 //Degrees
elevator_trim_limit = 19.5 //Degrees
spoiler_limit = 90.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available=0
spoiler_extension_time=0.250
positive_g_limit_flaps_up=4.000
positive_g_limit_flaps_down=2.000
negative_g_limit_flaps_up=-1.500
negative_g_limit_flaps_down=-1.500
[Reference Speeds]
flaps_up_stall_speed = 66.0 //Knots True (KTAS)
full_flaps_stall_speed = 52.8 //Knots True (KTAS)
cruise_speed = 200.0 //Knots True (KTAS)
max_indicated_speed =240 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0
[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
[stall_warning]
type=2
stick_shaker=0
[vacuum_system]
max_pressure=5.150
vacuum_type=1
electric_backup_pressure=4.900
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.00
bleed_air_scalar=1.00
[deice_system]
structural_deice_type=0
[CameraDefinition.0]
Title = "Landing Gear"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the landing gear and left wing inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .52
ShowWeather = Yes
InitialXyz = -3.1, 0.7, -13
InitialPbh = 0, 0, 17
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
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 = 0.7, 2.5, -19.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.2]
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 = 0.5
ShowWeather = Yes
InitialXyz =12.8, 1.6, 0.3
InitialPbh = 6, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[CameraDefinition.3]
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 = 0.5
ShowWeather = Yes
InitialXyz = -12.8, 1.6, 0.3
InitialPbh = 6, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum
[CameraDefinition.4]
Title = "Nose"
Guid = {3208BD74-1898-2743-A507-826C97B75E1B}
Description =Offset from the nose looking back at the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .8
ShowWeather = Yes
InitialXyz = -1.5,0.5,16.0
InitialPbh = 0,0,175
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.001]
Title = "VC Pilot view"
Guid = {8ff6c134-098d-409f-baec-caba3f683f98}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.30, 0.05, -0.25
InitialPbh=9, 0, 0
[CameraDefinition.002]
Title = "VC instructor view"
Guid={4ca337db-ae88-4c5f-96ea-ddebbd2a86fe}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.30, 0.05, -0.15
InitialPbh=7, 0, 0
