//PREMIER AIRCRAFT DESIGN
//Copyright 2008
//MU-2 Marquise (FSX) 06.Dec.2008
//DESIGN BY JEAN-PIERRE BRISARD
//FD AND PAINT BY BOB MAY
//TECHNICAL ASSISTANCE BY JOE ZERILLI
//FLIGHT TUNING BY DANNY "CHIEF" CRANCE
//version 1.1M
[fltsim.0]
title=mu2l_N321GM_M
sim=mu2l
model=1
panel=mu2mx
sound=0
texture=n321gm
kb_checklists=MU-2_check
kb_reference=MU-2_ref
atc_id=N321GM
ui_manufacturer=Mitsubishi
ui_type=Marquise
ui_variation=MARQUISE N321GM_M
description=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 first significant change to the airframe came with the stretched MU-2G, first flying January 10, 1969, which featured a 1.91 m (6 ft 3 in) longer fuselage than earlier models; 46 were built before being succeeded by the more powerful MU-2J (108 constructed).
The final stretched-fuselage MU-2 was named the Marquise, and like the Solitaire used 715 shp TPE331 engines.
[fltsim.1]
title=mu2l_N544CB_M
sim=mu2l
model=2
panel=mu2mx
sound=0
texture=N544CB
kb_checklists=MU-2_check
kb_reference=MU-2_ref
atc_id=N544CB
ui_manufacturer=Mitsubishi
ui_type=Marquise
ui_variation=MARQUISE N544CB
description=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 first significant change to the airframe came with the stretched MU-2G, first flying January 10, 1969, which featured a 1.91 m (6 ft 3 in) longer fuselage than earlier models; 46 were built before being succeeded by the more powerful MU-2J (108 constructed).
The final stretched-fuselage MU-2 was named the Marquise, and like the Solitaire used 715 shp TPE331 engines.
[General]
atc_type=MITSU
atc_model=MU2
editable=1
performance=Max speed: 300 mph\nRange: 1200 nm\nCeiling: 29,000\nMax weight: 8930\nPassenger: 6-7 + 2 crew
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 11575
empty_weight = 7650
reference_datum_position = 0.00, 0.00, 0.00
empty_weight_CG_position = -2.20, 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 = 30000
empty_weight_roll_MOI = 18200
empty_weight_yaw_MOI = 36500
empty_weight_coupled_MOI= 0.00
CG_forward_limit= 0.00
CG_aft_limit= 1.00
[flight_tuning]
parasite_drag_scalar =1.00
induced_drag_scalar =1.00
elevator_effectiveness =1.00
aileron_effectiveness =1.00
rudder_effectiveness =1.00
pitch_stability =1.00
roll_stability =1.00
yaw_stability =1.00
elevator_trim_effectiveness =1.00
aileron_trim_effectiveness =1.00
rudder_trim_effectiveness =1.00
[GeneralEngineData]
engine_type =5
Engine.0 =1, -4.60, 0.0
Engine.1 =1, 4.60, 0.0
fuel_flow_scalar =0.51
min_throttle_limit=-0.250
[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=1.200
maximum_torque=3000.000
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
[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, 10.029, 0.000, -6.43, 1281, 0, 0.75, 39.9, 0.142, 2.5, 0.9516, 10.0, 10.0, 0, 184.0, 184.0
point.1=1.000, -4.21, -4.200, -6.53, 1874, 1, 0.75, 0.0, 0.242, 2.5, 0.8152, 14.0, 12.0, 0, 184.0, 184.0
point.2=1.000, -4.21, 4.200, -6.53, 1874, 2, 0.75, 0.0, 0.242, 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 =6.6
gear_system_type=1 //Hydraulic
[Views]
eyepoint=6.122,-1.10,-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, -3.5 , -19.60, -0.5,fx_navred ,
light.1 =3, -3.5, 19.60, -0.5, fx_navgre ,
light.2 =3, -23.4, 0.00, 7.30, fx_navwhi ,
light.3 =2, -3.5, -19.66, -0.50, fx_strobe ,
light.4 =2, -3.5, 19.66, -0.50, fx_strobe ,
light.5 =1, -22.92, 0.00, 7.80,fx_beaconh ,
light.6 =1, 4.50, 0.00, -5.60,fx_beaconh ,
light.7 =4, 7.5, -1.00, -1.10, fx_vclightwhi ,
light.8 =4, 7.5, 1.00, -1.10, 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, 0.0, 160.00, 6.00
LeftAux =0.00, -5.00, 0, 35.0, 0.00
RightAux =0.00, 5.00, 0, 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 =0
wing_pos_apex_vert =0.00
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 =22.00
elevator_down_limit =18.00
aileron_up_limit =22.00
aileron_down_limit =18.00
rudder_limit =30.00
elevator_trim_limit =18.00
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=8.0
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
[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=1.5
lift_scalar=1.00
pitch_scalar=1.00
[Flaps.1]
type=1
span-outboard=0.50
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=1.0
lift_scalar=1.00
pitch_scalar=1.000
[brakes]
toe_brakes_scale=1.0
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=5.150000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=2