[fltsim.0]
title=Aoba Airlines Mitsubishi MU-2N
sim=MU2BJ
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=JV002A
ui_manufacturer=Mitsubishi
ui_type=MU-2N
ui_variation=Aoba Airlines
description=For use with pilot training flight.
visual_damage=1
atc_heavy=0
atc_airline=Green Air
atc_flight_number=91

[General]
atc_type=MITSUBISHI
atc_model=MU2
editable=1
performance=A total of 740 MU-2's have been built, with that number split about evenly between the original short-fuselage and the long-body airplane. \n\nType: twin-turboprop business aircraft \nPowerplant: two 715-shp (533-kW) Garrett    \n                 TPE331-10-501M turboprops\n\nPerformance: \nMaximum cruising speed 355 mph (571 km\/h) at 16,000 ft (4875 m)\nEconomic cruising speed 355 mph (571 km\/h) at 20,000 ft (8960 m)\nService ceiling 29,400 ft (8960 m)\nRange with maximum fuel and 45-min reserves 1,606 miles (2585 km) \nWeights: empty equipped 7,650 lb (3470 kg)\s maximum take-off 11,575 lb (5250 kg) \n\nDimensions: \nWing span over tiptanks 39 ft 2 in (11.94 m)\nLength 39 ft 5 in (12.01 m)\nHeight 13 ft 8 in (4.17 m)\nWing area 178 sq ft (16.54 m2) \n\nModel and textures by Björn Büchner\nFlight Dynamics by AL Lynch Jr.\n 

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50

station_load.0=168, 8.20, -2.29,-4.26 //PILOT
station_load.1=172, 8.20,  2.29,-4.26 //CO-PILOT

station_load.2=160, 5.57,  -2.29,-4.26 //SEAT 1L
station_load.2=159, 5.57,   2.29,-4.26 //SEAT 1R

station_load.2=120, 1.31,  -2.29,-4.26 //SEAT 2L
station_load.2=135, 1.31,   2.29,-4.26 //SEAT 2R

station_load.2=185, -2.29, -2.29,-4.26 //SEAT 3L
station_load.2=0,   -2.29,  2.29,-4.26 //SEAT 3R

station_load.2=120, -3.00,   2.29,-4.26 //SEAT 4R

//WEIGHT PROGRAMMING BY SIMUBUILD FLIGHT ENGINEERING DEPARTMENT/AL LYNCH JR.  WEIGHT VALUES MAY BE EDITED TO CUSTOM CONFIGURATION

;Inertia Moments
empty_weight=10300.000000
empty_weight_roll_MOI=50000.000000
empty_weight_pitch_MOI=41000.000000
empty_weight_yaw_MOI=60000.000000
empty_weight_coupled_MOI=1300.000000
;2121

[fuel]
LeftAux=    0.0,  -19.5, -0.3,  50.000000,0.000000
LeftMain= -1.64,   -9.8,  0.3,  108.000000,0.000000
Center1=  -1.64,      0,  0.6,  50.000000,0.000000
RightAux=   0.0,   19.5, -0.3,  50.000000,0.000000
RightMain=-1.64,    9.8,  0.3,  108.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=300.000000
wing_span=51.0
wing_root_chord=5.916667
wing_dihedral=5.998535
wing_incidence=0.000000
wing_twist=0.197754
oswald_efficiency_factor=1.907327
wing_winglets_flag=65535
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=100.000000
htail_span=20.000000
htail_pos_lon=-25.000000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=90.000000
vtail_span=10.816654
vtail_sweep=0.000000
vtail_pos_lon=-27.000000
vtail_pos_vert=5.833333
elevator_area=25.000000
aileron_area=12.120000
rudder_area=15.300000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=60
aileron_down_limit=10
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=55
spoilerons_available=1
aileron_to_spoileron_gain=10.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

//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= 1.000, 17.500, 0.000, -7.300, 2000.803, 0.000, 0.602, 60.000, 0.100, 5.000, 0.600, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, -0.917, -2.833, -7.300, 2000.803, 1.000, 0.602, 0.000, 0.274, 2.500, 0.677, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -0.917, 2.833, -7.300, 2000.803, 2.000, 0.602, 0.000, 0.274, 2.500, 0.677, 7.000, 7.000, 3.000, 0.000, 0.000
point.3= 2.000, 2.167, -33.417, 2.417, 1574.803, 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, 2.167, 33.417, 2.417, 1574.803, 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, -26.417, 0.000, 2.500, 1574.803, 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, 14.000, 0.000, -2.500, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 2.000, 16.000, 0.000, -6.000, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.8= 2.000, -0.200, -2.800, -6.000, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.9= 2.000, -0.200, 2.800, -7.000, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.10= 2.000, -15.000, 0.000, -4.600, 2000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= -0.308
static_cg_height= 7.000


[Views]
eyepoint=7.8, -1.20, -1.1

[flaps.0]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.5                                  // 0.0 .. 1.0
extending-time=40                                    // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=20                                   // degrees
flaps-position.2=40                                   // degrees
damaging-speed=180                                  // KIAS
blowout-speed=210                                  // KIAS
lift_scalar=1.5
drag_scalar=2.5
pitch_scalar=-0.1

[GeneralEngineData]
engine_type=5                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-2.3, -5.8, 4.5                      //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-2.3,  5.8, 4.5                      //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.1                   //Scalar for fuel flow efficiency

[propeller]
thrust_scalar=1.0                   //Propeller thrust scalar
propeller_type=0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=7.5                   //Propeller Diameter, (feet)
propeller_blades=3                     //Number of propeller blades
propeller_moi=20                    //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=0                    //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                   //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=0.3                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0                 //Minimum pitch angle in reverse, (degrees)

[TurbineEngineData]
fuel_flow_gain=0.011000
inlet_area=1.000000
rated_N2_rpm=29920.000000
static_thrust=198.000000
afterburner_available=0
reverser_available=0

[turboprop_engine]
power_scalar=1.0                   //Scalar on Turboprop power
maximum_torque=3420                 //Maximum torque available (ft-lbs)

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3, -0.0,  -20.00,  -0.2, fx_navred ,
light.1=3, -0.0,   20.00,  -0.2, fx_navgre ,
light.2=3, -23.5,   0.00,  -0.5, fx_navwhi ,
light.3=1,  8.00,   0.00,  -5.00, fx_beacon ,
light.4=1, -22.00,  0.00,   8.00, fx_beacon ,
light.5=4,   7.8,   0.00,  -2.2, fx_vclight,
light.6=2,  -0.0,  -20.00,  -0.2, fx_strobeh ,
light.7=2,  -0.0,   20.00,  -0.2, fx_strobe ,
;1660

[Reference Speeds]
flaps_up_stall_speed=78.000000
full_flaps_stall_speed=62.400000
cruise_speed=294.398353

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=7.8, -1.20, -1.1

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=3,0

[flight_tuning]
cruise_lift_scalar=1.2
parasite_drag_scalar=1.3
induced_drag_scalar=1.2
elevator_effectiveness=1.5
aileron_effectiveness=1.7
rudder_effectiveness=1.6
pitch_stability=1.5
roll_stability=1.8
yaw_stability=1.5
elevator_trim_effectiveness=5.0
aileron_trim_effectiveness=4.3
rudder_trim_effectiveness=4.2

