[fltsim.0]
title=Lancair
sim=Legacy
model=
panel=
sound=
texture=
kb_checklists=Legacy_2000_check
kb_reference=Legacy_2000_ref
atc_id_color=0xffff0000
atc_id=N540L
ui_manufacturer=Lancair
ui_type=Legacy
ui_variation=N540L
description=SEATS 2  conventional\nENGINE: Cont. IO-550-N 310 h.p. @2700 rpm\n PROPELLER: 3 blade, constant speed\n FUEL CAPACITY 66 gal\nLENGTH: 22 ft  -  WINGSPAN 25.5 ft  -  WING AREA 82.5 sq ft\nEMPTY WEIGHT 1500 lbs -  GROSS WEIGHT 2200 lbs\n USEFUL LOAD 700 lbs  -  BAG' CAP 90 lbs\nG LOADING (Utility) +4.4  -2.2 G's\n
SEATS 2 conventional
ENGINE: Cont. IO-550-N 310 h.p. @2700 rpm 
PROPELLER: 3 blade, constant speed
FUEL CAPACITY 66 gal 
LENGTH: 22 ft  -  WINGSPAN 25.5 ft  -  WING AREA 82.5 sq ft
EMPTY WEIGHT 1500 lbs -  GROSS WEIGHT 2200 lbs 
USEFUL LOAD 700 lbs  -  BAGGAGE CAPACITY 90 lbs
G LOADING (Utility) +4.4  -2.2 G's 
300 mph @ sea level.  310 Hp 2700 RPM
Cruise 276 mph @ 8000 75%  power
Vne=272kts
visual_damage=0

[General]
atc_type=EXPERIMENTAL 
atc_model=
editable=0 
performance=FULL THROTTLE 261 kts (300mph) at SLevel and std cnd\n CRUISE  240 kts (276 mph) @ 8,000' at std cnd\nSTALL SPEED (Dirty) Vso 58 kts  -  (clean) 72 kts\nTAKEOFF DISTANCE @ Sea Level 800 ft (gross) -  LANDING ROLL 900 ft\n CROSS WIND LANDING  18 kt (21 mph) Component\nRATE OF CLIMB 3000 fpm solo 2200 fpm @ gross\n SERVICE CEILING 18,000 ft\nFUEL CONSUMPTION (typ) 13.5 - 15 gph\n MAXIMUM RANGE (with reserves @ 8,000') 1042 nm ( 1200 sm) RES //www.lancair.com/html/legacy.htmland SPORT AVIATION, March 2003     
CRUISE  240 kts (276 mph) @ 8,000' at standard conditions
STALL SPEED (Dirty) Vso 58 kts  -  (clean) 72 kts
TAKEOFF DISTANCE @ Sea Level 800 ft (gross) -  LANDING ROLL 900 ft 
CROSS WIND LANDING  18 kt (21 mph) Component
RATE OF CLIMB 3000 fpm solo 2200 fpm @ gross 
SERVICE CEILING 18,000 ft
FUEL CONSUMPTION (typ) 13.5 - 15 gph 
MAXIMUM RANGE (with reserves @ 8,000') 1042 nm ( 1200 sm)
DATA SOURCE - http://www.lancair.com/html/legacy.html
and SPORT AVIATION, March 2003

[fltsim.1]
title=Lancair2
sim=Legacy
model=
panel=tweet
sound=
texture=tweet
kb_checklists=Legacy_2000_check
kb_reference=Legacy_2000_ref
atc_id_color=0xffff0000
atc_id=N18GG
ui_manufacturer=Lancair
ui_type=Legacy
ui_variation=Tweety Bird N18GG
description=SEATS 2  conventional\nENGINE: Cont. IO-550-N 310 h.p. @2700 rpm\n PROPELLER: 3 blade, constant speed\n FUEL CAPACITY 66 gal\nLENGTH: 22 ft  -  WINGSPAN 25.5 ft  -  WING AREA 82.5 sq ft\nEMPTY WEIGHT 1500 lbs -  GROSS WEIGHT 2200 lbs\n USEFUL LOAD 700 lbs  -  BAG' CAP 90 lbs\nG LOADING (Utility) +4.4  -2.2 G's\n
SEATS 2 conventional
ENGINE: Cont. IO-550-N 310 h.p. @2700 rpm 
PROPELLER: 3 blade, constant speed
FUEL CAPACITY 66 gal 
LENGTH: 22 ft  -  WINGSPAN 25.5 ft  -  WING AREA 82.5 sq ft
EMPTY WEIGHT 1500 lbs -  GROSS WEIGHT 2200 lbs 
USEFUL LOAD 700 lbs  -  BAGGAGE CAPACITY 90 lbs
G LOADING (Utility) +4.4  -2.2 G's 
300 mph @ sea level.  310 Hp 2700 RPM
Cruise 276 mph @ 8000 75%  power
Vne=272kts
visual_damage=0

[General]
atc_type=EXPERIMENTAL 
atc_model=
editable=0 
performance=FULL THROTTLE 261 kts (300mph) at SLevel and std cnd\n CRUISE  240 kts (276 mph) @ 8,000' at std cnd\nSTALL SPEED (Dirty) Vso 58 kts  -  (clean) 72 kts\nTAKEOFF DISTANCE @ Sea Level 800 ft (gross) -  LANDING ROLL 900 ft\n CROSS WIND LANDING  18 kt (21 mph) Component\nRATE OF CLIMB 3000 fpm solo 2200 fpm @ gross\n SERVICE CEILING 18,000 ft\nFUEL CONSUMPTION (typ) 13.5 - 15 gph\n MAXIMUM RANGE (with reserves @ 8,000') 1042 nm ( 1200 sm) RES //www.lancair.com/html/legacy.htmland SPORT AVIATION, March 2003     
CRUISE  240 kts (276 mph) @ 8,000' at standard conditions
STALL SPEED (Dirty) Vso 58 kts  -  (clean) 72 kts
TAKEOFF DISTANCE @ Sea Level 800 ft (gross) -  LANDING ROLL 900 ft 
CROSS WIND LANDING  18 kt (21 mph) Component
RATE OF CLIMB 3000 fpm solo 2200 fpm @ gross 
SERVICE CEILING 18,000 ft
FUEL CONSUMPTION (typ) 13.5 - 15 gph 
MAXIMUM RANGE (with reserves @ 8,000') 1042 nm ( 1200 sm)
DATA SOURCE - http://www.lancair.com/html/legacy.html
and SPORT AVIATION, March 2003

[fltsim.2]
title=Lancair3
sim=Legacy
model=
panel=
sound=
texture=N252JT
kb_checklists=Legacy_2000_check
kb_reference=Legacy_2000_ref
atc_id_color=0xffff0000
atc_id=N252JT
ui_manufacturer=Lancair
ui_type=Legacy
ui_variation=N252JT
description=SEATS 2  conventional\nENGINE: Cont. IO-550-N 310 h.p. @2700 rpm\n PROPELLER: 3 blade, constant speed\n FUEL CAPACITY 66 gal\nLENGTH: 22 ft  -  WINGSPAN 25.5 ft  -  WING AREA 82.5 sq ft\nEMPTY WEIGHT 1500 lbs -  GROSS WEIGHT 2200 lbs\n USEFUL LOAD 700 lbs  -  BAG' CAP 90 lbs\nG LOADING (Utility) +4.4  -2.2 G's\n
SEATS 2 conventional
ENGINE: Cont. IO-550-N 310 h.p. @2700 rpm 
PROPELLER: 3 blade, constant speed
FUEL CAPACITY 66 gal 
LENGTH: 22 ft  -  WINGSPAN 25.5 ft  -  WING AREA 82.5 sq ft
EMPTY WEIGHT 1500 lbs -  GROSS WEIGHT 2200 lbs 
USEFUL LOAD 700 lbs  -  BAGGAGE CAPACITY 90 lbs
G LOADING (Utility) +4.4  -2.2 G's 
300 mph @ sea level.  310 Hp 2700 RPM
Cruise 276 mph @ 8000 75%  power
Vne=272kts
visual_damage=0

[General]
atc_type=EXPERIMENTAL 
atc_model=
editable=0 
performance=FULL THROTTLE 261 kts (300mph) at SLevel and std cnd\n CRUISE  240 kts (276 mph) @ 8,000' at std cnd\nSTALL SPEED (Dirty) Vso 58 kts  -  (clean) 72 kts\nTAKEOFF DISTANCE @ Sea Level 800 ft (gross) -  LANDING ROLL 900 ft\n CROSS WIND LANDING  18 kt (21 mph) Component\nRATE OF CLIMB 3000 fpm solo 2200 fpm @ gross\n SERVICE CEILING 18,000 ft\nFUEL CONSUMPTION (typ) 13.5 - 15 gph\n MAXIMUM RANGE (with reserves @ 8,000') 1042 nm ( 1200 sm) RES //www.lancair.com/html/legacy.htmland SPORT AVIATION, March 2003     
CRUISE  240 kts (276 mph) @ 8,000' at standard conditions
STALL SPEED (Dirty) Vso 58 kts  -  (clean) 72 kts
TAKEOFF DISTANCE @ Sea Level 800 ft (gross) -  LANDING ROLL 900 ft 
CROSS WIND LANDING  18 kt (21 mph) Component
RATE OF CLIMB 3000 fpm solo 2200 fpm @ gross 
SERVICE CEILING 18,000 ft
FUEL CONSUMPTION (typ) 13.5 - 15 gph 
MAXIMUM RANGE (with reserves @ 8,000') 1042 nm ( 1200 sm)
DATA SOURCE - http://www.lancair.com/html/legacy.html
and SPORT AVIATION, March 2003
[weight_and_balance]

// ACM V1.0 pl4 i1
max_gross_weight=2200
empty_weight=1500
reference_datum_position=1.8, 0, 0
empty_weight_CG_position=-1.5, 0, 0
empty_weight_roll_MOI=1800.000000
empty_weight_pitch_MOI=3500.000000
empty_weight_yaw_MOI=1400.000000
empty_weight_coupled_MOI=0.000000
max_number_of_stations=1

station_load.0=170, -1.71,0,0
station_load.1=0, 0.0, 0.0, 0
station_load.2=0, 0.0, 0, 0

[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, 10, 17.0 
avionics=1, 5 , 17.0 
pitot_heat=0, 2 , 17.0 
additional_system=0, 20, 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 


[flight_tuning]
cruise_lift_scalar=1.1
parasite_drag_scalar=1.0 // CHANGED AIR FILE FORM 53 TO 30
parasite_drag_scalar=.8
induced_drag_scalar=1.0 //
induced_drag_scalar=.8
elevator_effectiveness=1.0 
aileron_effectiveness=1.0 
rudder_effectiveness=1.0 
pitch_stability=.8
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=.8
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 

[Flaps.0] // 
type=1
span-outboard=0.32 //RES From Ron's Barron
extending-time=5.000
system_type=0
damaging-speed=140.000
blowout-speed=145.000
lift_scalar=1.25
drag_scalar=1.0
pitch_scalar=1.0
system_type=0 // RES  From Ron's Barron
flaps-position.0=0.000, 0.000
flaps-position.1=15.00, 0.000
flaps-position.2=25.00, 0.000

[GeneralEngineData]
engine_type=0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=2.0, 0.0, 0.0                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0                           //Fuel flow scalar
min_throttle_limit=0.000000

[piston_engine]
//CAFE REPORT - RUN UP AGAINST BRAKES STATIC RPM 2662
power_scalar=1.00                              //Piston power scalar
cylinder_displacement=95.8                     //Cubic inches per cylinder  550 CUBIC INCH TOTAL ADJUSTED 4 HP
compression_ratio=8.5                    //Compression ratio from LEGACY TEST REPORT 8.5
number_of_cylinders=6                           //Number of cylinders
max_rated_rpm=2700                             //Max rated RPM   THIS IS MAX RPM - A CONSTANT SPEED PROP WILL LIMIT TO THIS VALUE
max_rated_hp=310                               //Max rated HP  CONTENTIAL IO-550-N 550 cubic inches NA FI
fuel_metering_type=0                           //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type=0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3                  //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=1                   //Automixture available? 0=FALSE, 1=TRUE    A FI current designed engine will have automixture RECORD 507 should not have any impact on the power beings we are auto mixture.
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 WAS1.0 Use .1 for dyno testing
propeller_type=0  //1
propeller_diameter=5.75     //5.75
propeller_blades=2 
propeller_moi=4.900000 
beta_max=40 
beta_min=25 
min_gov_rpm=1400.000000 
prop_tc=0.100000 
gear_reduction_ratio=1.000000 
fixed_pitch_beta=38.920000 
low_speed_theory_limit=80.000000 
prop_sync_available=0 
prop_deice_available=0 
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                        <0=none,1=wheel, 2=scrape, 3=float>
//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)  no impact on the dyanamics of the legacy  only visual and the legacy steers via brakes?  no nose steering on the legacy.
//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 Airspeed limit for retraction     (KIAS)
//15 Airspeed that gear gets damage at (KIAS) 

[contact_points]
static_pitch=1.84021
static_cg_height=3.539863
max_number_of_points=9

//        0   1   2     3     4   5    6    7      8       9    10  11 12 13   14   15

point.0=1, 2.4, 0, -3.9, 1181, 0, 0.523, 40, 0.15, 2.5, 0.808, 3, 3, 0, 176, 220
point.1=1, -2.1917987, -4.56, -3.952, 1574, 1, 0.523, 0, 0.286, 2.5, 0.808, 3, 3, 2, 176, 220
point.2=1, -2.1917987, 4.56, -3.952, 1574, 2, 0.523, 0, 0.286, 2.5, 0.808, 3, 3, 3, 176, 220
point.3=2, 0, -12.9, -1.15, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4=2, 0, 12.9, -1.15, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5=2, -13.842, 0, -1.15, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6=2, 5.7649, 0, -2.5118, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7=2, 0, 0, -2.4, 1574, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0
point.8=2, 0, -13.8, -2.2, 1574, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0

gear_system_type=0

[Views]
eyepoint=-3.9, -.865, 1.45


[Radios]
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 


[SMOKESYSTEM]
smoke.0=0.00, -0.70, 1.40, fx_smoke_w

[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=140, 240 
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 

[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing


light.0=3, -2.77, -13.0, -0.75, Leg_navred
light.1=3, -2.77, 13.0, -0.75, Leg_navgre
light.2=2, -2.9, -13.0, -0.75, Leg_strobeh
light.3=2, -2.9, 13.0, -0.75, Leg_strobeh
light.4=3, -3.81, 0, -1.87, fx_strobe
light.5=4, -3.9500,0.000,2.0, fx_vclLegacy


[EFFECTS]
wake=fx_wake 
water=fx_spray 
dirt=fx_tchdrt 
concrete=fx_sparks 
touchdown=fx_tchdwn_s, 1 

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type=1
number_of_tank_selectors=1

LeftMain=-1.95, -9.9, -1.24, 33.4, 1
RightMain=-1.95, 9.86, -1.24, 33.4, 1
electric_pump=1


[airplane_geometry]
// LEAVING ALL OF THE POSITION VALUES THE SAME FOR NOW 123002 -- ONLY CHANGING AREA AND ANGLES
wing_area=82.6              //Square feet // Legacy Literature
wing_span=25.4               //Feet // Legacy
wing_root_chord=3.3               //Area/Span 
wing_dihedral=3.7                 //Degrees From CAFE REPORT
wing_incidence=1.2             //Degrees From CAFE REPRT
wing_twist=0.0                   //Degrees CAFE REPORT SAYS IT HAS AERO TWIST 
oswald_efficiency_factor=.7                   //Measure of lift effeciency of wing was .6  GUESS BY ME
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=0               //Degrees, wing leading edge 
wing_pos_apex_lon=-0.7       //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=16.16               //Square feet FROM CAFE REPORT
htail_span=8.31              //Feet FROM CAFE REPORT
htail_pos_lon=-13.1                 //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=-.5        //Degrees FROM CAFE REPORT
htail_sweep=6.6                //Degrees, horizontal tail leading edge FROM RHINO DRAWING
vtail_area=10.3               //Square feet FROPM CAFE REPORT 13.9 TOTAL - 3.6 RUDDER
vtail_span=2.8                 //Feet, tip to body FROM RHINO DRAWING
vtail_sweep=47.5                //Degrees, vertical tail leading edge FROM RHINO DRAWING
vtail_pos_lon=-14.3                 //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=6.5               //Square feet 10.0 WAS THE VALUE FOR THE EXTRA  --  3 IS FROM THE RHINO DRAWING
aileron_area=3.65               //Square feet  CAFE REPORT HAS 46.7 X 6.9 ROOT 4.45 AT TIP  3.65 FT TOTAL FOR BOTH  -- EXTRA HAS 18.4
rudder_area=3.6         //Square feet FROM CAFE REPORT
elevator_up_limit=26.0                  //Degrees
elevator_down_limit=26.0                  //Degrees
aileron_up_limit=23                //Degrees changed from 30 30 april 10 to 23 18
aileron_down_limit=18             //Degrees
rudder_limit=20
elevator_trim_limit=15
//USELESS INFORMATION FOR A GA ARICRAFT
spoiler_limit=80                  //Degrees NO SPOILERS ON THIS ONE
spoilerons_available=0                     //Spoilerons Available? NO
aileron_to_spoileron_gain=0                   //Aileron to spoileron gain NOT AN ISSUE
min_ailerons_for_spoilerons=0                 //Degrees NOT AN ISSUE
min_flaps_for_spoilerons=0                    //Minimum flap handle position when spoilerons activate NOT AN ISSUE
wing_pos_apex_lon=-0.654000

[Reference Speeds]
flaps_up_stall_speed=68                //Knots True (KTAS) CAFE REPORT AT MAX GROSS
full_flaps_stall_speed=56                //Knots True (KTAS) CAFE REPORT AT MAX GROSS
cruise_speed=240         //Knots True (KTAS) LEGACY DATA -- 8K FT
max_indicated_speed=300

[Autopilot]
autopilot_available=1 
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.
flight_director_available=0 
default_vertical_speed=700
autothrottle_available=0 
pitch_takeoff_ga=0.000000 
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
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=0.000000


[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

[brakes]
toe_brakes_scale=0.625019
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.024414
flap_limit_power=1718.873385
flap_limit_idle=0.000000

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0