[fltsim.0]
title=Beechcraft Duke B60 N263Z
sim=Beech_Duke_B60
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=N263Z
ui_manufacturer=Beechcraft
ui_type=Duke
ui_variation=B60
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twim turbogarged Avco Lycoming piston engines.
[fltsim.1]
title=Beechcraft Duke BE60 N362QC
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N362QC
kb_checklists=
kb_reference=
atc_id=N362QC
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N362QC
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twin turbocharged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.2]
title=Beechcraft Duke BE60 N725YG
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N725YG
kb_checklists=
kb_reference=
atc_id=N725YG
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N725YG
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twim turbogarged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.3]
title=Beechcraft Duke BE60 N7079D
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N7079D
kb_checklists=
kb_reference=
atc_id=N7079D
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N7079D
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twim turbogarged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.4]
title=Beechcraft Duke BE60 N322RJ
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N322RJ
kb_checklists=
kb_reference=
atc_id=N322RJ
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N322RJ
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twim turbogarged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.5]
title=Beechcraft Duke BE60 N81215
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N81215
kb_checklists=
kb_reference=
atc_id=N81215
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N81215
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twim turbocharged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.6]
title=Beechcraft Duke BE60 N3669D
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N3669D
kb_checklists=
kb_reference=
atc_id=N3669D
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N3669D
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twim turbogarged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.7]
title=Beechcraft Duke BE60 N953EA
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N953EA
kb_checklists=
kb_reference=
atc_id=N953EA
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N953EA
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twim turbocharged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.8]
title=Beechcraft Duke BE60 N707ND
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N707ND
kb_checklists=
kb_reference=
atc_id=N707ND
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N707ND
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twim turbogarged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.9]
title=Beechcraft Duke BE60 N6008S
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N6008S
kb_checklists=
kb_reference=
atc_id=N6008S
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N6008S
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twim turbogarged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.10]
title=Beechcraft Duke BE60 N538SC
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N538SC
kb_checklists=
kb_reference=
atc_id=N538SC
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N538SC
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twim turbogarged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.11]
title=Beechcraft Duke BE60 N495EC
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N495EC
kb_checklists=
kb_reference=
atc_id=N495EC
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N495EC
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twim turbogarged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.12]
title=Beechcraft Duke BE60 N420JG Jaguar Edition
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N420JG
kb_checklists=
kb_reference=
atc_id=N420JG
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N420JG
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twin turbocharged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.13]
title=Beechcraft Duke BE60 N380PC
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N380PC
kb_checklists=
kb_reference=
atc_id=N380PC
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N380PC
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twin turbocharged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.14]
title=Beechcraft Duke BE60 N265D
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N265D
kb_checklists=
kb_reference=
atc_id=N265D
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N265D
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twin turbocharged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.15]
title=Beechcraft Duke BE60 N14VP
sim=Beech_Duke_B60
model=
panel=
sound=
texture=N14VP
kb_checklists=
kb_reference=
atc_id=N14VP
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=N14VP
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twin turbocharged Avco Lycoming piston engines.Model & master textures by Paul Craig
[fltsim.16]
title=Beechcraft Duke BE60 C-GUYD
sim=Beech_Duke_B60
model=
panel=
sound=
texture=C-GUYD
kb_checklists=
kb_reference=
atc_id=C-GUYD
ui_manufacturer=Beechcraft
ui_type=Duke BE60
ui_variation=C-GUYD
description=The B60 Beechcraft Duke is a 6 seat pressurised cabin class aircraft providing good performance from it's twim turbogarged Avco Lycoming piston engines.Model & master textures by Paul Craig
[General]
atc_type=BEECH
atc_model=BE60
editable=0
performance="Maximum Speed\n248 kts 460 km\/hr\n\nCruise Speed\n233 kts \t 431 km\/hr\nRange: 1227 nm 2274Km\n\nEngine\nAvco Lycoming TIO-541-E1C4 Turbocharged six-cylinder 380 hp. \n\nPropeller\nThree-Bladed, Constant Speed Hartzell.\n\nService Ceiling\n30,000 ft 9,144 m\n\nFuel Capacity\n232 gal 279 US gal 1055 L\n\nEmpty Weight\n4,500 lb 2,041 kg\n\nMaximum Gross Weight\n7,000 lb\t 3,175 kg\n\nUseful Load\n2,500 lb\t 1,133 kg\n\nLength\n33 ft, 10 in 10.31 m\n\nWingspan\n39 ft, 3 in\t 11.97 m\n\nHeight\n12 ft, 4 in 3.76 m\n\nSeating\nUp to 6"
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 7000 // (pounds)
empty_weight = 4500 // (pounds)
reference_datum_position = 6.96, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -6.06, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 20
station_load.0 = 170, 5.0, -2.0, 0.0, Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, 5.0, 2.0, 0.0, Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 0, -2.1, -2.0, 0.0, Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 0, -2.1, 2.0, 0.0, Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 170, -5.3, -2.0, 0.0, Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 170, -5.3, 2.0, 0.0, Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 6400
empty_weight_roll_MOI = 3700
empty_weight_yaw_MOI = 6530
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 = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -1.4, -5.3, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -1.4, 5.3, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.05 //Scalar for fuel flow efficiency
min_throttle_limit = 0.0; //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 91.7 //Cubic inches per cylinder
compression_ratio= 8.0 //Compression ratio
number_of_cylinders= 6 //Number of cylinders
max_rated_rpm= 2900.0 //Max rated RPM
max_rated_hp= 380.0 //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= 41.0 //Max design manifold pressure, (inHg)
min_design_mp= 1.0 //Min design manifold pressure, (inHg)
critical_altitude= 17000.0 //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= 0.0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0.0 //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 = 1.0 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.4 //Propeller Diameter, (feet)
propeller_blades= 3 //Number of propeller blades
propeller_moi= 6.9 //Propeller moment of inertia
beta_max= 45.0 //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= 1100.0 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 0.0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80.0 //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= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering
beta_feather= 82.5 //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= 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees)
[contact_points]
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
//GEAR
http://point.0 = 1, 0.82, 0.00, -4.20, 1600, 0, 0.633, 40, 0.42, 2.5, 0.90, 3.0, 3.0, 0, 152, 180
point.1 = 1, -8.04, -4.79, -4.50, 1600, 1, 0.886, 0, 0.50, 2.5, 0.85, 4.1, 4.3, 2, 152, 200
point.2 = 1, -8.04, 4.79, -4.50, 1600, 2, 0.886, 0, 0.50, 2.5, 0.85, 4.3, 4.1, 3, 152, 200
//SCRAPES
point.3= 2, -6.20,-18.91, 0.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4= 2, -6.20, 18.91, 0.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5= 2,-24.04, 0.00, -0.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6= 2, 0.40, 0.00, -1.24, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
static_pitch = 1.56 //Degrees
static_cg_height = 3.43 //Feet
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 = 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 = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.41 // 0.0 .. 1.0
extending-time = 4 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 15 // degrees
flaps-position.2 = 30 // degrees
damaging-speed = 152 // KIAS
blowout-speed = 250 // KIAS
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
;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
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[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
[Views]
eyepoint = -8.213, -0.8612, 2.220 //Longitudinal, Lateral, Vertical (feet)
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -5.95, -19.50, 0.05, fx_navred ,
light.1 = 3, -5.95, 19.50, 0.05, fx_navgre ,
light.2 = 3, -26.90, 0.00, 2.23, fx_navwhi ,
light.3 = 2, -5.65, -19.29, 0.00, fx_strobe ,
light.4 = 2, -5.65, 19.29, 0.00, fx_strobe ,
light.5 = 1, -28.05, 0.00, 8.40, fx_beacon ,
light.6 = 1, -7.68, 1.85, -1.85, fx_beacon ,
light.7 = 4, -7.30, 0.00, 1.50, fx_vclight,
light.8 = 4, -11.50, 0.00, 1.50, fx_vclight,
light.9 = 4, -14.50, 0.00, 1.50, fx_vclight,
[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=1,1 //Turn AND Bank
[fuel]
LeftMain = -8.46, -6.45, 0.0, 116.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -8.46, 6.45, 0.0, 116.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[airplane_geometry]
wing_area = 212.9 //Square feet
wing_span = 37.8 //Feet
wing_root_chord = 5.3 //Feet
wing_dihedral = 6.9 //Degrees
wing_incidence = 1.0 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor= 0.7 //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 = -5.6 //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 = 60.0 //Square feet
htail_span = 15.9 //Feet
htail_pos_lon = -20.1 //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 = 0.5 //Degrees
htail_sweep = 0.0 //Degrees, horizontal tail leading edge
vtail_area = 88.0 //Square feet
vtail_span = 10.7 //Feet, tip to body
vtail_sweep = 0.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -22.9 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 3.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 20.0 //Square feet
aileron_area = 11.3 //Square feet
rudder_area = 10.5 //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=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000
[Reference Speeds]
flaps_up_stall_speed = 81.0 //Knots True (KTAS)
full_flaps_stall_speed = 73.0 //Knots True (KTAS)
cruise_speed = 220.0 //Knots True (KTAS) 45% Power @ FL200
max_indicated_speed = 255.0 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
autothrottle_available= 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
pitch_takeoff_ga=8.000000
[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=1
stick_shaker=0
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=4.900000
engine_map=1,1,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=2