[fltsim.0]
title=L40 Meta Sokol_0
sim=L40_Meta_Sokol
model=
panel=
sound=
texture=
checklists=
description=L-40 is a sports and touring plane , manufakturer by ORLIÈAN in Czechoslovakia 1957-1959,
first flight 29 March 1956, exported to 16 countries, single-engine low-wing cantilever monoplane of a metal construction,
retractable inverted tricycle gear ,the plane had four seats with twin controls in front.
atc_id_color=0000000000
visual_damage=0
ui_manufacturer=ORLICAN
[fltsim.1]
title=L40 Meta Sokol_1
sim=L40_Meta_Sokol
model=
panel=
sound=
texture=1
checklists=
description=L-40 is a sports and touring plane , manufakturer by ORLIÈAN in Czechoslovakia 1957-1959,
first flight 29 March 1956, exported to 16 countries, single-engine low-wing cantilever monoplane of a metal construction,
retractable inverted tricycle gear ,the plane had four seats with twin controls in front.
atc_id_color=0000000000
visual_damage=0
ui_manufacturer=ORLICAN
[fltsim.2]
title=L40 Meta Sokol_2
sim=L40_Meta_Sokol
model=
panel=
sound=
texture=2
checklists=
description=L-40 is a sports and touring plane , manufakturer by ORLIÈAN in Czechoslovakia 1957-1959,
first flight 29 March 1956, exported to 16 countries, single-engine low-wing cantilever monoplane of a metal construction,
retractable inverted tricycle gear ,the plane had four seats with twin controls in front.
atc_id_color=0000000000
visual_damage=0
ui_manufacturer=ORLICAN
[General]
atc_type=Metasokol
atc_model=
editable=0
performance= Maximum Speed 250 km/h\ Cruise
Speed 190 km/h \permissible overload: speed 225km/h +3.57, -1.55\speed 250km/h +2.65, -0\maximum speed for eject flaps and
gear 145 km/h\ Engine M332, M332A, M332AK 103kW 140 hp\Propeller is metal,two blade with electrical adjustment VJ1.410/1850\
Maximum Range 1100 km \Service Ceiling\6000m 18000ft \Fuel Capacity 2x55 L \Empty Weight 530 kg\Maximum Gross Weight 950 kg\
Length 7.54 m\Wingspan 10.058 m\Height 2.52 m
Category=airplane
[CameraDefinition.0]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0, 2.0, -3.9
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Nose"
Guid = {8A1987D0-09B6-7E48-B4E1-62C5DBE2A720}
Description =Looking back from the nose of the engine toward the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .3
ShowWeather = Yes
InitialXyz = 0, 1.1, 4.0
InitialPbh = 20, 0, 180
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
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 = 8, 0.3, 1
InitialPbh = 0, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[CameraDefinition.3]
Title = "Left Wing"
Guid = {7a91803e-898b-435a-8391-725be6a48203}
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 = -8, 0.3, 1
InitialPbh = 0, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[CameraDefinition.4]
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 = 0.75
SmoothZoomTime = 1.1
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.5, 0.05, -0.2
InitialPbh=0, 0, 0
[CameraDefinition.5]
Title = "Thrust lever"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.2
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.2, -0.5, 0
InitialPbh=9, 0, 22
[CameraDefinition.6]
Title = "Light Switches"
Guid = {195EAB58-9E4A-3E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.3
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0, -0.5, 0
InitialPbh=0, 0, -5
[weight_and_balance]
max_gross_weight = 2555
empty_weight = 1855
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -0.7, 0, 0
empty_weight_pitch_MOI = 1400
empty_weight_roll_MOI = 1400
empty_weight_yaw_MOI =2555
empty_weight_coupled_MOI = 0.0
max_number_of_stations = 5
station_load.0 = "170, -3.1, -1.5, 0.0, Pilot"
station_load.1 = "170, -3.1, 1.5, 0.0, Front Passenger"
station_load.2 = "100, -6.1, -1.5, 0.0, Rear Passenger"
station_load.3 = "100, -6.1, 1.5, 0.0, Rear Passenger"
station_load.4 = "33, -8.5, 0.0, 0.0, Baggage"
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.2
engine.0 = 2.1, 0.0,-0.5
min_throttle_limit=0.000000
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
[Views]
eyepoint = -0.95, -.838, 2.0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -0.95, -20.10, -0.10, fx_navred ,
light.1 = 3, -0.95, 20.10, -0.10, fx_navgre ,
light.2 = 7, -0.90, -20.10, -0.10, fx_recog ,
light.3 = 7, -0.90, 20.10, -0.10, fx_recog ,
light.4 = 1, -16.75, 0.00, 8.20, fx_beacon ,
light.5 = 4, 0.00, 0.00, 1.25, fx_vclight,
light.6 = 2, -0.75, -20.10, -0.10, fx_strobe ,
light.7 = 2, -0.75, 20.10, -0.10, fx_strobe ,
light.8 = 3, -20.10, 0.00, 1.55, fx_navwhi,
light.9 = 5, 3.00, -4.00, -2.0, fx_Shockwave_landing_light // Shockwave light
light.10 = 5, 3.00, 4.00, -2.0, fx_Shockwave_landing_light // Shockwave light
light.11 = 3, 3.00, -4.00, -2.0, fx_navwhi,
light.12 = 3, 3.00, 4.00, -2.0, fx_navwhi,
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 2
LeftMain = -4.1, -7.9, -0.8, 47.5, 3
RightMain = -4.1, 7.9, -0.8, 47.5, 3
electric_pump=0
[contact_points]
static_pitch = 5.0
static_cg_height = 5.0
max_number_of_points = 9
point.0 = 1, -5.60, 0, -4.30, 1181.1, 0, 0.523, 35.00, 0.296, 2.5, 0.794, 3.5, 3.5, 0, 165, 165
point.1 = 1, 1.85,-3.732, -5.00, 1574.8, 1, 0.73, 0, 0.286, 2.5, 0.808, 5.2, 5.2 2, 165, 165
point.2 = 1, 1.85, 3.732, -5.00, 1574.8, 2, 0.73, 0, 0.286, 2.5, 0.808, 5.2, 5.2, 3, 165, 165
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
gear_system_type=0
[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000
[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[airplane_geometry]
//ACM_AREAW1// 0,0,0,1.5543,0.6111,0.6111,0,1.4766,1.2224,1.2224
//ACM_AREAW2// 0,1.3990,1.8337,1.8337,0,1.3213,2.4451,2.4451,0,1.2434
//ACM_AREAW3// 3.0564,3.0564,0,1.1657,3.6677,3.6677,0,1.0880,4.2789,4.2789
//ACM_AREAW4// 0,1.0104,4.8902,4.8902,0,0.9326,5.5015,5.5015,0,0.8549
//ACM_AREAH1// 0,0,0,1.1987,0.1997,0.1997,0,1.1389,0.3995,0.3995
//ACM_AREAH2// 0,1.0788,0.5993,0.5993,0,1.0190,0.7991,0.7991,0,0.9591
//ACM_AREAH3// 0.9990,0.9990,0,0.8991,1.1987,1.1987,0,0.8392,1.3985,1.3985
//ACM_AREAH4// 0,0.7792,1.5985,1.5985,0,0.7192,1.7983,1.7983,0,0.6593
//ACM_AREAV1// 0,0,0,1.0972,0.1218,0.1218,0,1.0094,0.2437,0.2437
//ACM_AREAV2// 0,0.9217,0.3657,0.3657,0,0.8338,0.4875,0.4875,0,0.7461
//ACM_AREAV3// 0.6096,0.6096,0,0.6582,0.7315,0.7315,0,0.5705,0.8533,0.8533
//ACM_AREAV4// 0,0.4828,0.9753,0.9753,0,0.3950,1.0972,1.0972,0,0.3072
//ACM_CAREAW1// 2.7507,2.7507,0.7771,1.0880,3.0564,3.0564,0.7771,1.0724,3.3620,3.3620
//ACM_CAREAW2// 0.7771,1.0570,3.6677,3.6677,0.7771,1.0414,3.9734,3.9734,0.7771,1.0259
//ACM_CAREAW3// 4.2789,4.2789,0.7771,1.0104,4.5845,4.5845,0.7771,0.9947,4.8902,4.8902
//ACM_CAREAW4// 0.7771,0.9793,5.1958,5.1958,0.7771,0.9636,5.5015,5.5015,0.7771,0.9481
//ACM_CAREAH1// 0,0,0.5993,1.1987,0.1997,0.1997,0.5993,1.1689,0.3995,0.3995
//ACM_CAREAH2// 0.5993,1.1389,0.5993,0.5993,0.5993,1.1088,0.7991,0.7991,0.5993,1.0788
//ACM_CAREAH3// 0.9990,0.9990,0.5993,1.0490,1.1987,1.1987,0.5993,1.0190,1.3985,1.3985
//ACM_CAREAH4// 0.5993,0.9890,1.5985,1.5985,0.5993,0.9591,1.7983,1.7983,0.5993,0.9290
//ACM_CAREAV1// 0,0,0.2743,0.8228,0.1218,0.1218,0.2743,0.7789,0.2437,0.2437
//ACM_CAREAV2// 0.2743,0.7350,0.3657,0.3657,0.2743,0.6912,0.4875,0.4875,0.2743,0.6473
//ACM_CAREAV3// 0.6096,0.6096,0.2743,0.6035,0.7315,0.7315,0.2743,0.5595,0.8533,0.8533
//ACM_CAREAV4// 0.2743,0.5156,0.9753,0.9753,0.2743,0.4717,1.0972,1.0972,0.2743,0.4278
wing_area = 175.0
wing_span = 36.1
wing_root_chord = 5.1
wing_dihedral = 5.5
wing_incidence = 2.5
wing_twist = -1.5
oswald_efficiency_factor = 0.6
wing_winglets_flag = 0
wing_sweep = 0.0
wing_pos_apex_lon = -2.6
wing_pos_apex_vert = 0.0
htail_area = 34.0
htail_span = 11.8
htail_pos_lon = -18.6
htail_pos_vert = 0.0
htail_incidence = 1.0
htail_sweep = 0.0
vtail_area = 10.0
vtail_span = 3.6
vtail_sweep = 0.0
vtail_pos_lon = -16.5
vtail_pos_vert = 1.5
elevator_area = 16.6
aileron_area = 18.3
rudder_area = 6.7
elevator_up_limit = 28.0
elevator_down_limit = 21.0
aileron_up_limit = 20.0
aileron_down_limit = 15.0
rudder_limit = 24.0
elevator_trim_limit = 19.5
spoiler_limit = 90.0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
auto_spoiler_available=0
spoiler_extension_time=0.250000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
[SMOKESYSTEM]
smoke.0=-10.00, -0.70, 0.0, fx_smoke_w
[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=1.0
induced_drag_scalar=1.0
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=1.0
[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=4 //Number of cylinders
max_rated_rpm=2550 //Max rated RPM
max_rated_hp=185 //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=1 //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=1.0 //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=1050 //Miminum governed RPM
prop_tc=0.0 //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=1 //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)
[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 = 0.95 //Brake scalar
[hydraulic_system]
normal_pressure = 0.0 //PSI
[Views]
eyepoint=-4.354, -.884, 1.385
[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 = 15 // degrees, KIAS
flaps-position.2 = 30 // degrees, KIAS
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 3 //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
[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
[Reference Speeds]
flaps_up_stall_speed=66.0 //Knots True (KTAS)
full_flaps_stall_speed=52.8 //Knots True (KTAS)
cruise_speed=180.0 //Knots True (KTAS)
max_indicated_speed = 195 //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
[stall_warning]
type=2
stick_shaker=0
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=4.900000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0
