King Air idles too fast??

[ecuber11]

Not sure why but when the default king air idles, it still want to go. Ill have it all the way down and it still is moving like 19 knots IDLED!? Anyone know how to fix this? I moved the props all the way back and it still does this, Help?

[mrzippy]

Make sure in your control settings that throttle sensitivity is max and the null zone setting is zero. At Idle you may have to feather both props-Hold down F2. Make sure your joystick is calibrated and watch out and don't accidentally press F3. I had that problem also. The King-aire is a speedy little turkey!

[slarente]

You can also change the controls to "low idle" (right next to the throttle and propellers controls in the cockpit). It usually solves the problem.

[mallcott]

Not sure why but when the default king air idles, it still want to go. Ill have it all the way down and it still is moving like 19 knots IDLED!? Anyone know how to fix this? I moved the props all the way back and it still does this, Help?

It does, because it does.

[ScatterbrainKid]

A few other FSX planes have the same problem, they always still have a trickle of power when you close your joystick throttle which messes up your landing approach, and after you touch down they don't want to stop rolling unless you stand on the brakes. (seaplanes with the problem will never stop because they have no brakes, so you have to switch off the ignition to kill the engine).
There must be a line in the aircraft config file that needs to be changed, but i can't find one.

[CaptainTower]

I'm sure you could tweak the King Air not to taxi with the throttle pulled all the way off. But then you would not have a King Air 350.

Tim

[Adam24]

A few other FSX planes have the same problem, they always still have a trickle of power when you close your joystick throttle which messes up your landing approach, and after you touch down they don't want to stop rolling unless you stand on the brakes. (seaplanes with the problem will never stop because they have no brakes, so you have to switch off the ignition to kill the engine).
There must be a line in the aircraft config file that needs to be changed, but i can't find one.

Maybe throttle_power_scalar=...? I think there is a line like this, but Im not shore if its exactly like this one

[Schnell14]

19 knots at idle is a tad fast, but from what I read in "real world" pilot reports, almost all turboprops, especially the GA ones, require some braking during taxi. That is because of several design necessities (large props, avoidance of resonance regions, need to prevent combustion shutdowns, etc.) Speed also varies with winds on the taxi heading.

However, Flight Sim's "digital braking" does make for jerky speed control. if the necessity for braking bothers you, you can control the taxi speed in Flight Sim by just changing either the prop pitch or condition lever settings, or both, then readjusting them to the proper settings before takeoff.

Regards,


Schnell

[cmuenier]

It's not mine and I don't remember where I found it

; Localized 09/12/2006 03:16 AM (GMT) 4:4.2.169 aircraft.cfg
[fltsim.0]
title=Beech King Air 350 Paint1
sim=Beech_King_Air_350
model=""
panel=""
sound=""
texture=1
kb_checklists=Beech_King_Air_350_check
kb_reference=Beech_King_Air_350_ref
atc_id_color=0xffffffffff
atc_id=N350KA
ui_manufacturer=Beechcraft
ui_type=King Air 350
ui_variation=Rayures blanches/vertes
ui_typerole=Bimoteur à turbopropulseur
ui_createdby=Microsoft Corporation
description=Le King Air dans toutes ses variantes est un superbe avion de style classique et aux lignes épurées. Les améliorations apportées au fil des années l'ont doté d'un meilleur aérodynamisme, de plus de puissance sous le capot, d'une vitesse accrue, d'une avionique et de systèmes électriques mordernisés, ainsi que d'une cabine luxueuse. Bien que fréquemment utilisé comme avion d'affaires, il est également disponible en configuration cargo.

[fltsim.1]
title=Beech King Air 350 Paint2
sim=Beech_King_Air_350
model=""
panel=""
sound=""
texture=2
kb_checklists=Beech_King_Air_350_check
kb_reference=Beech_King_Air_350_ref
atc_id_color=0xffffffffff
atc_id=N350KA
ui_manufacturer=Beechcraft
ui_type=King Air 350
ui_variation=Rayures blanches/bleues
ui_typerole=Bimoteur à turbopropulseur
ui_createdby=Microsoft Corporation
description=Le King Air dans toutes ses variantes est un superbe avion de style classique et aux lignes épurées. Les améliorations apportées au fil des années l'ont doté d'un meilleur aérodynamisme, de plus de puissance sous le capot, d'une vitesse accrue, d'une avionique et de systèmes électriques mordernisés, ainsi que d'une cabine luxueuse. Bien que fréquemment utilisé comme avion d'affaires, il est également disponible en configuration cargo.

[fltsim.2]
title=Beech King Air 350 Paint3
sim=Beech_King_Air_350
model=""
panel=""
sound=""
texture=3
kb_checklists=Beech_King_Air_350_check
kb_reference=Beech_King_Air_350_ref
atc_id_color=0xffffffffff
atc_id=N350KA
ui_manufacturer=Beechcraft
ui_type=King Air 350
ui_variation=Rayures blanches/bleues et or
ui_typerole=Bimoteur à turbopropulseur
ui_createdby=Microsoft Corporation
description=Le King Air dans toutes ses variantes est un superbe avion de style classique et aux lignes épurées. Les améliorations apportées au fil des années l'ont doté d'un meilleur aérodynamisme, de plus de puissance sous le capot, d'une vitesse accrue, d'une avionique et de systèmes électriques mordernisés, ainsi que d'une cabine luxueuse. Bien que fréquemment utilisé comme avion d'affaires, il est également disponible en configuration cargo.

[fltsim.3]
title=Beech King Air 350
sim=Beech_King_Air_350
model=""
panel=""
sound=""
texture=""
kb_checklists=Beech_King_Air_350_check
kb_reference=Beech_King_Air_350_ref
atc_id_color=0xffffffffff
atc_id=N350KA
ui_manufacturer=Beechcraft
ui_type=King Air 350
ui_variation=Blanc
ui_typerole=Bimoteur à turbopropulseur
ui_createdby=Microsoft Corporation
description=Le King Air dans toutes ses variantes est un superbe avion de style classique et aux lignes épurées. Les améliorations apportées au fil des années l'ont doté d'un meilleur aérodynamisme, de plus de puissance sous le capot, d'une vitesse accrue, d'une avionique et de systèmes électriques mordernisés, ainsi que d'une cabine luxueuse. Bien que fréquemment utilisé comme avion d'affaires, il est également disponible en configuration cargo.

[General]
atc_type=BEECH
atc_model=B350
editable=0
performance=Vitesse de croisière\t\n315 nœuds 363 mph 583 km\/h\n\nMotorisation\t\nPratt & Whitney PT6A-60A 1 050 CV\n\nAutonomie maximale\t\n1 765 nm 2 031 m\t 3 269 km\n\nPlafond pratique\t\n35 000 pieds 10 668 m\n\nCapacité en carburant\t\n539 gal 2 040 l\n\nPoids maximal au décollage \n15 000 livres\t 6 818 kg\n\nLongueur\t\n46,7 pieds\t 14,23 m\n\nEnvergure\t\n57,9 pieds\t 17,65 m\n\nHauteur\t\n14,3 pieds\t 4,36 m\n\nNombre de places\t\njusqu'à 11\n\nCharge utile\t\n5 910 livres\t 2 681 kg
Category=airplane

[CameraDefinition.0]
Title=Empennage
Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description=Vue de l'arrière de l'avion
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.75
ShowWeather=Yes
InitialXyz=0, 3.5, -22.0
InitialPbh=5, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title=Aile droite
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description=Vue de l'extrémité de l'aile droite en regardant le cockpit
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=15, 1.0, 3.0
InitialPbh=6, 0, 270
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum

[CameraDefinition.2]
Title=Aile gauche
Guid={f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description=Vue de l'extrémité de l'aile gauche en regardant le cockpit
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=-15, 1.0, 3.0
InitialPbh=6, 0, 90
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=No
ClipMode=Minimum

[CameraDefinition.001]
Title=Commandes du moteur
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=1.2
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.0, 0.25, -0.2
InitialPbh=48, 0, 27

[WEIGHT_AND_BALANCE]
max_gross_weight=15000 // (pounds)
empty_weight=9090 // (pounds)

reference_datum_position=0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=170, 5.0, -2.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170, 5.0, 2.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=170, -2.1, -2.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=170, -2.1, 2.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=170, -5.3, -2.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5=170, -5.3, 2.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_name.0=Pilote
station_name.1=Copilote
station_name.2=Passager
station_name.3=Passager
station_name.4=Passager
station_name.5=Passager


;Moments of Inertia
empty_weight_pitch_MOI=30000
empty_weight_roll_MOI=18200
empty_weight_yaw_MOI=36500
empty_weight_coupled_MOI=0.0

[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

[GeneralEngineData]
engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-8.3, -4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-8.3, 4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency
min_throttle_limit=-0.25; //Minimum percent throttle. Generally negative for turbine reverser

[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=8.8 //Propeller Diameter, (feet)
propeller_blades=4 //Number of propeller blades
propeller_moi=24 //Propeller moment of inertia
beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15.2 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520 //Miminum governed RPM
prop_tc=0.004 //Prop time-constant
gear_reduction_ratio=17.6 //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=1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700 //Minimum RPM for prop feathering
beta_feather=79.3 //Feathering pitch angle (degrees)
power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees)

[TurbineEngineData]
fuel_flow_gain=0.011 //Gain on fuel flow
inlet_area=1.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920 //RPM, second stage compressor rated value
static_thrust=158 //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar=1.0 //Scalar on Turboprop power
maximum_torque=3270 //Maximum torque available (ft-lbs)
PowerSpecificFuelConsumption=0.55 //Brake power specific fuel consumption (turboprop only)


[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 <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)
;/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]
point.0=1, 13.00, 0.00, -4.70, 1181, 0, 0.596, 39.9, 0.296, 2.5, 0.9516, 4.8, 4.8, 0, 184.0, 184.0
point.1=1, -1.67, -8.58, -5.03, 1574, 1, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.5, 5.2, 2, 184.0, 184.0
point.2=1, -1.67, 8.58, -5.03, 1574, 2, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.8, 4.9, 3, 184.0, 184.0
point.3=2, -3.33, -23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -3.33, 23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -22.67, 0.00, 0.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 23.08, 0.00, -1.50, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0

static_pitch=0.2
static_cg_height=4.3
gear_system_type=1 //Hydraulic

[gear_warning_system]
gear_warning_available=1 //Normal
pct_throttle_limit=0.1 //Percent throttle that activates warning
flap_limit_idle=15.0 //Flap angle that activates warning at idle
flap_limit_power=30.0 //Flap angle that activates warning at above idle

[brakes]
parking_brake=1 //Parking brake available
toe_brakes_scale=1.0 //Brake scalar
auto_brakes=0

[hydraulic_system]
normal_pressure=3000.0 //PSI
electric_pumps=0 //no electric pumps
engine_map=1,1,0,0 //pumps on Eng1,2

[Views]
eyepoint=4.3, -1.20, 3.35


[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
flaps-position.1=20 // degrees
flaps-position.2=40 // degrees
damaging-speed=250 // KIAS
blowout-speed=300 // KIAS

[Radios]
;/ Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 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=150, 250
aileron=150, 250
rudder=150, 250

[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=3,0

[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=2 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[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

[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3, 0.56, -28.41, 1.97, fx_navred ,
light.1=3, 0.56, 28.41, 1.97, fx_navgre ,
light.2=3, -31.20, 0.00, 9.75, fx_navwhi ,
light.3=2, 0.89, -28.48, 1.87, fx_strobe ,
light.4=2, 0.89, 28.48, 1.87, fx_strobe ,
light.5=1, -26.30, 0.00, 9.89, fx_beacon ,
light.6=2, -4.55, 0.00, -1.85, fx_strobe ,
light.7=4, 4.91, 0.00, 1.64, fx_vclight,


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

[fuel]
LeftMain=0.0, -14.5, -1.0, 190.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux=0.0, -6.0, -1.5, 79.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=0.0, 14.5, -1.0, 190.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=0.0, 6.0, -1.5, 79.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=1


[airplane_geometry]
wing_area=310.0 //Square feet
wing_span=57.2 //Feet
wing_root_chord=5.4 //Feet
wing_dihedral=6.0 //Degrees
wing_incidence=1.0 //Degrees
wing_twist=-1.5 //Degrees
oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing
wing_winglets_flag=1 //Are winglets available?
wing_sweep=1.0 //Degrees, wing leading edge
wing_pos_apex_lon=2.1 //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=67.0 //Square feet
htail_span=17.2 //Feet
htail_pos_lon=-22.6 //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=0.5 //Degrees
htail_sweep=20.0 //Degrees, horizontal tail leading edge
vtail_area=42.0 //Square feet
vtail_span=7.4 //Feet, tip to body
vtail_sweep=40.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-20.5 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=4.1 //Feet, vertical distance from reference point, positive going up
elevator_area=17.0 //Square feet
aileron_area=13.5 //Square feet
rudder_area=7.3 //Square feet
elevator_up_limit=17.0 //Degrees
elevator_down_limit=15.5 //Degrees
aileron_up_limit=18.0 //Degrees
aileron_down_limit=18.0 //Degrees
rudder_limit=30.0 //Degrees
elevator_trim_limit=15.0 //Degrees
spoiler_limit=0.0 //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
positive_g_limit_flaps_up=3.0 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down=2.0 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up=-2.0 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down=-2.0 //Design G load tolerance (negative, flaps down)
load_safety_factor=1.5 //Design G load safety factor

[Reference Speeds]
flaps_up_stall_speed=96.0 //Knots True (KTAS)
full_flaps_stall_speed=76.8 //Knots True (KTAS)
cruise_speed=300.0 //Knots True (KTAS)
max_mach=0.58
max_indicated_speed=263 //Red line (KIAS)

[autopilot]
use_no_default_bank=1
use_no_default_pitch=1
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
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=1.0
default_pitch_mode=0
default_bank_mode=0

[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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

[deice_system]
structural_deice_type=2 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots

[Schnell14]

Posted by Error (Mine)