[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
