[fltsim.0] title=Mistubishi MU-2B Paint 1 sim=MU2BJ model= panel= sound= texture=pax1 kb_checklists= kb_reference= atc_id=N337MU ui_manufacturer=Mitsubishi ui_type=MU-2B-36J ui_variation=white with stripes description=In 1956 Mitsubishi Heavy Industries of Japan decide to build a turbine-powered business airplane with the two goals -- high cruise speed with short, rough-field capability in mind. Large flaps needed to extend across the entire trailing edge of the small wing, leaving no room for ailerons, Mitsubishi's solution was to install spoilers for roll control. The MU-2 fuselage is round because that is the optimum way to design a pressure vessel. Tip tanks were necessary because the small wing did not have enough internal volume to contain the required fuel.\n\nIn meeting the primary design goals, Mitsubishi encountered some unintended fallout. The airplane did what people said they wanted an airplane to do, but it looked different and didn't handle like an ordinary airplane.\n\nThe safety record of the MU-2 has not been good but there has been no pattern of crashes. What remains of Mitsubishis production run is still flying the skies efficiently and, provided the pilots are well trained, safely. visual_damage=1 atc_heavy=0 atc_airline= atc_flight_number= [fltsim.1] title=Mistubishi MU-2B Paint 2 sim=MU2BJ model=3blade panel= sound= texture=pax2 kb_checklists= kb_reference= atc_id=N235MU ui_manufacturer=Mitsubishi ui_type=MU-2B-35J ui_variation=white and blue description=The Mistsubishi MU-2 is a high wing, high economy, light turboprop that was produced from the middle of the 1960's to the early period of the 1980's. The Mistsubishi MU-2 has a unique reputation of being fast, comfortable and unavoidably dangerous. The aircraft has no ailerons, and an over sensitive trim, and full span flaps on its short, 37 foot wing that offers an interesting if not challenging flight experience for new and seasoned pilots alike. Flying this aircraft like a normal turboprop has resulted in over 95% of MU-2 crashes, so care and technique is a must when flying this unpredictable , yet somewhat stable airplane. visual_damage=1 atc_heavy=0 atc_airline= atc_flight_number= [fltsim.2] title=Mistubishi MU-2B Cargo sim=MU2BJ model=cargo panel= sound= texture=cargo1 kb_checklists= kb_reference= atc_id=ZU-SMU ui_manufacturer=Mitsubishi ui_type=MU-2B-35J Cargo Conversion ui_variation=Springbok Aviation (fictional) description=In 1956 Mitsubishi Heavy Industries of Japan decide to build a turbine-powered business airplane with the two goals -- high cruise speed with short, rough-field capability in mind. Large flaps needed to extend across the entire trailing edge of the small wing, leaving no room for ailerons, Mitsubishi's solution was to install spoilers for roll control. The MU-2 fuselage is round because that is the optimum way to design a pressure vessel. Tip tanks were necessary because the small wing did not have enough internal volume to contain the required fuel.\n\nIn meeting the primary design goals, Mitsubishi encountered some unintended fallout. The airplane did what people said they wanted an airplane to do, but it looked different and didn't handle like an ordinary airplane.\n\nThe safety record of the MU-2 has not been good but there has been no pattern of crashes. What remains of Mitsubishis production run is still flying the skies efficiently and, provided the pilots are well trained, safely. visual_damage=1 atc_airline=Springbok [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
