[fltsim.0]
title=Beechcraft C90 IAF 501 Mate
sim=AI Beechcraft King Air C90
model=
panel=FSX 2019
sound=
texture=IAF 501 Mate
kb_checklists=
atc_id =4X501
atc_parking_types =Ramp
atc_parking_code =IAF C90
atc_airline=Air Force
atc_flight_number=501
ui_manufacturer = Beech
ui_type =C90
ui_variation =IAF 501 Mate
ui_typerole=World Military
description=This is an upgraded FSX flying model with completely new flying dynamics/new 2D panels and revised interior/exterior textures.All upgrades done by Yiannis Katehis Tsetsas 2019.Original AI model by Henry Tomkiewicz.Flying model conversion by Dee Waldron.
[fltsim.1]
title=Beechcraft C90 501 Gloss
sim=AI Beechcraft King Air C90
model=
panel=FSX 2019
sound=
texture=IAF 501 Gloss
kb_checklists=
atc_id =4X501
atc_parking_types =Ramp
atc_parking_code =IAF C90
atc_airline=Air Force
atc_flight_number=501
ui_manufacturer = Beech
ui_type =C90
ui_variation =IAF 501 Gloss
ui_typerole=World Military
description=This is an upgraded FSX flying model with completely new flying dynamics/new panels and revised interior/exterior textures.All upgrades done by Yiannis Katehis Tsetsas 2019.Original AI model by Henry Tomkiewicz.Flying model conversion by Dee Waldron.
[General]
category=Airplane
editable=0
performance=Velocidad de crucero\t\n315 nudos 363 mph 583 km\/h\n\nMotores\t\nPratt & Whitney PT6A-60A 1.050 CV\n\nAutonomía máxima\t\n1765 mn 2031 m\t 3269 km\n\nTecho de servicio\t\n35000 ft 10668 m\n\nCapacidad de combustible\t\n539 gal. EE.UU. 2040 L\n\nPeso máximo al despegue \n15000 lb\t 6818 kg\n\nLongitud\t\n46,7 ft\t 14,23 m\n\nEnvergadura\t\n57,9 ft\t 17,65 m\n\nAltura\t\n14,3 ft\t 4,36 m\n\nPlazas\t\nHasta 11\n\nCarga útil\t\n5910 lb\t 2681 kg
Category=airplane
[CameraDefinition.0]
Title=Cola
Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description=Vista hacia adelante desde la parte posterior del aparato
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=Ala derecha
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description=Vista desde el extremo del ala derecha hacia la cabina
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=Ala izquierda
Guid={f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description=Vista desde el extremo del ala izquierda hacia la cabina
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=Controles del motor
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
[CameraDefinition.002]
Title = "Cockpit Overview"
Guid = {9B7F3CFD-BF4E-4bd1-B93F-DEBEDC2370D6}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.3
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.35, 0.25, -0.2
InitialPbh=22, 0, 0
[General]
atc_type=Beechcraft
atc_model=BE9L
editable=1
performance="AI Aircraft"
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 16000 // (pounds)
empty_weight = 10000 // (pounds)
reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 2.0, 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=Piloto
station_name.1=Copiloto
station_name.2=Pasajeros
station_name.3=Pasajeros
station_name.4=Pasajeros
station_name.5=Pasajeros
;Moments of Inertia
empty_weight_pitch_MOI = 50000
empty_weight_roll_MOI = 48200
empty_weight_yaw_MOI = 46500
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=3 //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, -4.50, 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=0.3
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=1
[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 = 4.54, -1.20, 3.25
[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, -0.10, -24.80, 1.50, fx_navred ,
light.1 = 3, -0.10, 24.80, 1.50, fx_navgre ,
light.2 = 3, -22.60, 0.00, 2.70, fx_navwhi ,
light.3 = 2, -0.15, -24.95, 1.50, fx_strobeh ,
light.4 = 2, -0.15, 24.95, 1.50, fx_strobeh ,
light.5 = 1, -20.90, 0.00, 10.40, fx_beaconb ,
light.6 = 1, -2.85, 0.00, -1.40, fx_beaconb ,
[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 = 47.2 //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 = 60.0 //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
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.047009
positive_g_limit_flaps_down=2.833333
negative_g_limit_flaps_up=-3.238248
negative_g_limit_flaps_down=-2.428419 //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]
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
[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
