//PREMIER AIRCRAFT DESIGN
//Mitsubishi MU-2 Solitaire (FSX version)
//Copyright 2008
//Design by J.P.Brisard
//Textures and FD by Bob May
//Technical assistance by Joe Zerilli



[fltsim.0]
title=mu2s9
sim=mu2s
model=
panel=mu2sx
sound=0
texture=N924PD
kb_checklists=MU-2_check
kb_reference=MU-2_ref
atc_id=N924PD
ui_manufacturer=Mitsubishi
ui_type="MU2 Solitaire"
ui_variation=White/Blue N924PD
description=The Mitsubishi MU-2 is one of postwar Japan's most successful aircraft. It is a high-wing, twin-engine turboprop, and has a pressurized cabin.The final short-fuselage MU-2s produced were known as the Solitaire and were fitted with 665 shp Garrett TPE331-10-501M engines



[General]
atc_type=MITSU
atc_model=MU2
editable=1
performance=Max speed: 330 mph\nRange: 1200 nm\nCeiling: 33,000\nMax weight: 8930\nPassenger: 4 + 2 crew
Category=airplane

[CameraDefinition.0]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
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 = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the 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 = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = View from the left wing tip looking at the 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 = "Engine Controls"
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 = 8930.00
empty_weight = 5430.00

reference_datum_position     = 0.00, 0.00, 0.00
empty_weight_CG_position     = 0.00, 0.00, 0.00

station_load.0 = "170,  1.7, -1.75, -3.0, Pilot"                  //Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, 1.7,  1.75, -3.0, Front Passenger"        //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "350, -3.3,  0.0, -3.0, Payload"                //Payload  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

max_number_of_stations =20

;Moments of Inertia
empty_weight_pitch_MOI  = 80000.00
empty_weight_roll_MOI   = 36000.00
empty_weight_yaw_MOI    = 116000.00
empty_weight_coupled_MOI= 0.00
CG_forward_limit= 0.00
CG_aft_limit= 1.00




[flight_tuning]

parasite_drag_scalar   =1.10
induced_drag_scalar    =1.10
elevator_effectiveness =0.85
aileron_effectiveness  =0.90
rudder_effectiveness   =1.00
pitch_stability        =3.50
roll_stability         =2.00
yaw_stability          =1.50
elevator_trim_effectiveness =1.05
aileron_trim_effectiveness  =0.95
rudder_trim_effectiveness   =1.20

[GeneralEngineData]
engine_type = 5
Engine.0 = 3.50, -9.60, 0.60
Engine.1 = 3.50,  9.60, 0.60
fuel_flow_scalar        = 0.50
min_throttle_limit=-0.250



//[propeller]
//thrust_scalar           =1.00
//propeller_type          = 0
//propeller_diameter      = 8.60
//propeller_blades        = 4
//propeller_moi           = 22.00
//beta_max                = 45.00
//beta_min                = 15.20
//min_gov_rpm             = 25520.00
//prop_tc                 = 0.004
//gear_reduction_ratio    =17.6  // 11.60
//fixed_pitch_beta        = 0.00
//low_speed_theory_limit  = 80.00
//prop_sync_available     = 1
//prop_deice_available    = 1
//prop_feathering_available= 1
//prop_auto_feathering_available= 1
//min_rpm_for_feather     = 700.00
//beta_feather            = 79.30
//power_absorbed_cf       = 0.90
//defeathering_accumulators_available= 0 
//prop_reverse_available  = 1
//minimum_on_ground_beta  = 1.00
//minimum_reverse_beta    = -14.00

[propeller]
thrust_scalar=1.000 
propeller_type=0 
propeller_diameter=8.6 
propeller_blades=4 
propeller_moi=24.000 
beta_max=90.000 
beta_min=6.000 
min_gov_rpm=1114.000 
prop_tc=0.004 
gear_reduction_ratio=17.6 
fixed_pitch_beta=0.000 
low_speed_theory_limit=80.000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=1000.000 
beta_feather=90.000 
power_absorbed_cf=0.900 
defeathering_accumulators_available=1 
prop_reverse_available=1.000 
minimum_on_ground_beta=1.000 
minimum_reverse_beta=-14.000




[TurbineEngineData]
fuel_flow_gain=0.011 
inlet_area=1.000 
rated_N2_rpm=41730.000 
static_thrust=150.000 
afterburner_available=0 

[turboprop_engine]
power_scalar=1.000 
maximum_torque=3200.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=0.800
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=0.800
 
//[TurbineEngineData]
//fuel_flow_gain          = 0.011
//inlet_area              = 1.00
//rated_N2_rpm            = 29920.00
//static_thrust           = 150   // 250.00
//afterburner_available= 0


//[turboprop_engine]
//power_scalar            = 1.35
//maximum_torque          = 4100.00
//max_rpm_mechanical_efficiency_scalar=1.00
//idle_rpm_mechanical_efficiency_scalar=1.00
//max_rpm_friction_scalar=1.00
//idle_rpm_friction_scalar=1.00




[Reference Speeds]
flaps_up_stall_speed    = 82.00
full_flaps_stall_speed  = 75.00
cruise_speed            = 240.00	//knots indicated (IAS) at 20,000 ft.
normal_cruise_speed	= 240.00
max_indicated_speed     =300.00
max_mach=0.579980



[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

[contact_points]
//Classes...What type of point    0=Unused or Ignore
//                                                      1=Wheel
//                                                      2=Scrape point
//                                                      4=Float
//                                                      5=Float Rudder
//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 / Water Rudder Effectiveness  (0=Undamped, 1=Critically Damped) / 1.0 = normal
//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)

point.0=1.000,  8.329, 0.000, -6.20, 1281, 0, 0.75, 39.9, 0.296, 1.5, 0.9516,  10.0, 10.0, 0, 184.0, 184.0
point.1=1.000, -6.41, -7.400, -6.58, 1874, 1, 0.75,  0.0, 0.642, 2.5, 0.8152,  14.0, 12.0, 0, 184.0, 184.0
point.2=1.000, -6.41,  7.400, -6.58, 1874, 2, 0.75,  0.0, 0.642, 2.5, 0.8152,  14.0, 12.0, 0, 184.0, 184.0
point.3=2.000,-2.200,-29.300,3.200,2360.907127,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,5.000,0.000,0.000
point.4=2.000,-2.200,29.300,3.200,2360.907127,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,6.000,0.000,0.000
point.5=2.000,-35.000,0.000,11.000,2360.907127,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,9.000,0.000,0.000
point.6=2.000,23.600,-0.000,-0.500,1574.803150,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,4.000,0.000,0.000
point.7=5.000,23.600,-0.000,-0.500,1574.803150,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,4.000,0.000,0.000


static_pitch =0
static_cg_height = 3.0  //5.9
gear_system_type=1      //Hydraulic

[Views]

eyepoint=2.122,-0.914,-1.1 // 0.681

[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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, -4.5 , -19.66, 0.1,fx_navred ,                      
light.1 = 3, -4.5, 19.66, 0.1, fx_navgre ,
light.2 = 3, -23.4,   0.00,  7.30, fx_navwhi ,
light.3 = 2,  -4.9, -19.66,  0.10, fx_strobe ,
light.4 = 2,  -4.9,  19.66,  0.10, fx_strobe ,
light.5 = 1, -20.92,   0.00, 7.3,fx_beaconh ,
light.6 = 1,-10.530,   0.00, -4.63,fx_beaconh ,
light.7 = 4,  3.0,   -1.00, -2.10,  fx_vclightwhi ,
light.8 = 4,  3.00, 1.00, -2.10,  fx_vclightwhi ,


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

[fuel]

Center1 = 0.00,0.0, -3.0, 160.00, 6.00  
LeftAux   = -3.00, -15.00, -1.50, 35.0, 0.00
RightAux  = -3.00, 15.00, -1.50,  35.0, 0.00
Lefttip=0.0,-20.0,0.0,93,0.0
Righttip=0.0,20.0,0.0,93,0.0
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=1

[airplane_geometry]
wing_area               = 178.00
wing_span               = 39.2
wing_root_chord         = 6.60
wing_dihedral           = 3.00
wing_incidence          = 2.00
wing_twist              = -1.50
oswald_efficiency_factor= 0.70
wing_winglets_flag      = 1
wing_sweep              = 3.00
wing_pos_apex_lon       = 2.00
wing_pos_apex_vert      = -1.00
htail_area              = 76.00
htail_span              = 18.20
htail_pos_lon           = -27.50
htail_pos_vert          = 11.00
htail_incidence         = -1.60
htail_sweep             = 20.00
vtail_area              = 50.00
vtail_span              = 6.50
vtail_sweep             = 35.00
vtail_pos_lon           = -23.50
vtail_pos_vert          = 4.50
elevator_area           = 14.00
aileron_area            = 5.00//13.0
rudder_area             = 17.00
elevator_up_limit       = 17.00
elevator_down_limit     = 15.50
aileron_up_limit        = 10.0//18.00
aileron_down_limit      = 10.0//18.00
rudder_limit            = 30.00
elevator_trim_limit     = 15.00
spoiler_limit           = 00.00
spoilerons_available    = 0
aileron_to_spoileron_gain = 0.00
min_ailerons_for_spoilerons = 0.00
min_flaps_for_spoilerons = 0.00
auto_spoiler_available=0
spoiler_extension_time=0.000000
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

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 0
pitch_takeoff_ga=8.00
max_pitch=10.00
max_pitch_acceleration=1.00
max_pitch_velocity_lo_alt=2.00
max_pitch_velocity_hi_alt=1.50
max_pitch_velocity_lo_alt_breakpoint=20000.00
max_pitch_velocity_hi_alt_breakpoint=28000.00
max_bank=25.00
max_bank_acceleration=1.80
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.250
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.520
gs_integrator_control=0.260
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.00

[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

[Flaps.0]
type= 1
span-outboard= 0.30
extending-time= 12.00
system_type= 0
damaging-speed= 250.00
blowout-speed= 300.00
flaps-position.0= 0.00, 0.00
flaps-position.1= 5.00, 0.00
flaps-position.2=20.00, 0.00
flaps-position.3=40.00, 0.00
drag_scalar=1.150
lift_scalar=1.00
pitch_scalar= 0.900

[Flaps.1]
type= 1
span-outboard= 0.30
extending-time= 12.00
system_type= 0
damaging-speed= 250.00
blowout-speed= 300.00
flaps-position.0= 0.00, 0.00
flaps-position.1= 5.00, 0.00
flaps-position.2=20.00, 0.00
flaps-position.3=40.00, 0.00
drag_scalar=1.150
lift_scalar=1.00
pitch_scalar= 0.900

[brakes]
toe_brakes_scale=1.20
parking_brake= 1.80

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.00

[stall_warning]
type=1
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[exits]
number_of_exits=2
exit_rate.0=0.2                             ;Percent per second
exit_rate.1=0.2              

[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=2