[fltsim.0] title=Rotorway Exec 162f/mba 2 sim=Rotorway_Exec_162f model= panel= sound= texture= kb_checklists=rotorway_162piston_check kb_reference=rotorway_ref prop_anim_ratio=-.80 atc_id_color=0xc6eff7ff atc_id=459 MT atc_model= ui_manufacturer=RotorWay International ui_type=Pilot PassengerDoors ui_variation=Red and Black description="A REVOLUTION IN TECHNOLOGY Combining a technological breakthrough in powerplant design with refinements to a highly successful, award winning airframe, the new Exec 162F has elevated a tradition into a revolution in helicopter performance." [General] atc_type=Helicopter performance=Cruise Speed \t\n95 kts 110 mph 213 km\/h\n\nEngine\nRI 162F, 162 cu. in. (2659 cc) \n\nMaximum Range\n180 mi 2 hrs. \t \n\nService Ceiling\n10,000 ft m\n\nHovering Ceiling\n5,000 7,000 m\n\nFuel Capacity\n17 U.S. Gallons (64 liters). gal \n\nEmpty Weight\n975 lbs. (442 kg)\n\nMaximum Gross Weight\n1500 lbs. (680 kg)\n\nMaximum Gross Weight (External Loading)\n0 lb 0 kg\n\nLength\t\n22 ft. \t (6.7 meters) m\n\nRotor Span\n25.0 ft\t 7.6 m\n\nHeight\n96 in. \t (2.4 meters) m\n\nSeating \t\n2 \n\nUseful Load\t\n525 lb\t 238 kg\n editable=0 [WEIGHT_AND_BALANCE] max_gross_weight = 1500 // (pounds) empty_weight = 975 // (pounds) reference_datum_position = 8.33, 0.0, 0.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -9.09, 0.0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = "160, -6.0, -0.89, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "160, -6.0, 0.89, 0.0, Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "25, -11.0, 0.0, 0.0, Ballast" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 6000 empty_weight_roll_MOI = 4000 empty_weight_yaw_MOI = 10000 empty_weight_coupled_MOI = 0 [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=skid> //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=3, -2.74, -3.13, -4.23, 1600, 0, 0.00, 0.0, 0.28, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0 point.1=3, -2.74, 3.13, -4.23, 1600, 0, 0.00, 0.0, 0.28, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0 point.2=3, -15.00, -3.13, -4.16, 1600, 0, 0.00, 0.0, 0.28, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0 point.3=3, -15.00, 3.13, -4.16, 1600, 0, 0.00, 0.0, 0.28, 2.5, 0.82, 0.0, 0.0, 7, 0.0, 0.0 point.4=2, -8.50, -11.80, 5.30, 100, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5, 0.0, 0.0 point.5=2, -8.50, 11.80, 5.30, 100, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6, 0.0, 0.0 point.6=2, 3.00, 0.00, 5.30, 100, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4, 0.0, 0.0 point.7=2, -23.00, 0.00, -0.60, 300, 0, 0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9, 0.0, 0.0 static_pitch = 1.4 static_cg_height = 3.58 [brakes] parking_brake = 0 //Parking brake available toe_brakes_scale = 0.0 //Brake scalar [hydraulic_system] normal_pressure = 0.0 //PSI [Views] eyepoint=-6.85, -0.8, 1.035 //(feet) longitudinal, lateral, vertical //eyepoint=-6.50, -0.8, 1.40 //Track IR settings [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -5.35, -1.93, -1.90, fx_navred_rway , light.1 = 3, -5.35, 1.93, -1.90, fx_navgre_rway , light.2 = 3, -23.80, 0.0, 1.25, fx_strobe_rway , light.3 = 1, -13.90, 0.0, 0.85, fx_beacon_rway, light.4 = 5, -1.65, 0.0, -1.35, fx_landing, light.6 = 4, -6.0, 0.0, 1.30, fx_vclighth , [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 1, 1 Nav.2 = 1, 1, 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. //NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque elevator = 100, 180 aileron = 200, 1000 rudder = 200, 1000 [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 = 0 direction_indicator.0=3,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 0 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [fuel] Center1 = -8.33, 0.0, 0.0, 17.0, 0.5 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=1 [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -8.5, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 4.0 //Fuel flow scalar min_throttle_limit = 0.0; //Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 40.5 //Cubic inches per cylinder compression_ratio= 8.5 //Compression ratio number_of_cylinders=4 //Number of cylinders max_rated_rpm= 2700 //Max rated RPM max_rated_hp= 155 //Max rated HP fuel_metering_type= 0 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 1 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque= 0.3 //Starter torque factor turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp= 0 //Max design manifold pressure, (inHg) min_design_mp= 0 //Min design manifold pressure, (inHg) critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture= 1 //Automixture available? 0=FALSE, 1=TRUE auto_ignition= 1 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar= .69 //Scalar on maximum RPM friction idle_rpm_friction_scalar= .50 //Scalar on idle RPM friction [Reference Speeds] cruise_speed = 93.0 //Knots True (KTAS) max_indicated_speed = 130.0 //Red line (KIAS) [autopilot] autopilot_available= 0 flight_director_available= 0 [yaw_string] yaw_string_available=1 [Helicopter] reference_length = 21.58 reference_frontal_area = 17.7 reference_side_area = 44.5 side_aero_center = -12.5 right_trim_scalar = 1.0 correlator_available = 1 governed_pct_rpm_ref = 1.04 governor_pid = 0.4, 0, 0.1, 0, 0.2 rotor_brake_scalar = 1.5 torque_scalar = -1.5 cyclic_roll_control_scalar =2.3 cyclic_pitch_control_scalar =2.4 pedal_control_scalar =.50 collective_on_rotor_torque_scalar = 0.37 [fuselage_aerodynamics] drag_force_cf = 0.55 side_drag_force_cf = 10.0 pitch_damp_cf = -5.0 roll_damp_cf = -5.0 yaw_damp_cf = -0.1 yaw_stability_cf = 0.19 [MainRotor] Position = -8.33, 0, 4.61 //Longitudinal, Lateral, Vertical feet from datum Radius = 12.5 //feet max_disc_angle = 5.0 RatedRpm = 520 Number_of_blades = 2 Weight_per_blade = 21.0 Weight_to_moi_factor = 0.56 inflow_vel_reference = 32.0 [SecondaryRotor] Position = -22.8, .660, .850 //Longitudinal, Lateral, Vertical feet from datum TailRotor = 1 Radius = 2.09375 //feet [exits] number_of_exits=3 exit_rate.0=0.2 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks startup =fx_engstrt_RWay landrotorwash=fx_rtr_lnd_RWay waterrotorwash=fx_rtr_wtr_RWay windshield_rain_effect_available=1 [SMOKESYSTEM] //?,long,lat from ref datum