[fltsim.0] title=Dornier 328-110 Lions Air sim=d328tp model= panel= sound= texture= checklists= ui_manufacturer=Dornier ui_type=Dornier 328-110 ui_variation=Lions Air description=The Dornier 328-110 is a high speed regional turboprop, with excelent short field capabilities. The plane first flew on December 6 1991, and was certified in October 1993. The plane can carry 30 to 39 passengers, offering more space per passenger than a 737. The aircraft is equiped with a full glass cockpit and is certified for CAT IIIa landings. atc_id=AEE110 atc_airline=Satena visual_damage=1 [General] performance=Max cruise speed: 270kts\nRange with 32pax: 900nm\nTakeoff field: 3570ft atc_type=Dornier atc_model=DO328 editable=0 [WEIGHT_AND_BALANCE] empty_weight = 19665 // (pounds) reference_datum_position = 0.000000,0.000000,0.000000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0.000000,0.000000,0.000000 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations =50 station_load.0 =0.000000,0.000000,0.000000,0.000000 station_load.1 = 275, 0, 0, 0.0 //Pilots station_load.2 = 3372, 0, 0, 0.0 //Payload ;Moments of Inertia empty_weight_roll_MOI = 205716 empty_weight_pitch_MOI = 231761 empty_weight_yaw_MOI = 330944 empty_weight_coupled_MOI = 1300 max_gross_weight=34968.000000 [fuel] LeftMain=0.000000,-14.500000,-1.00000,566.800000,0.000000 RightMain=0.000000,14.500000,-1.00000,566.800000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=1 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [GeneralEngineData] engine_type=5 Engine.0=11.250000,-7.833333,5.000000 Engine.1=11.250000,7.833333,5.000000 fuel_flow_scalar=0.870000 min_throttle_limit=-0.250000 [SMOKESYSTEM] smoke.0=5.00, 11.250000, 7.833333, fx_smoke_ys11 smoke.1=5.00, 11.250000, -7.833333, fx_smoke_ys11 [TurbineEngineData] fuel_flow_gain=0.011000 inlet_area=1.10000 rated_N2_rpm=27000.000000 static_thrust=510.000000 afterburner_available=0 [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter = 11.1 //Propeller Diameter, (feet) propeller_blades = 6 //Number of propeller blades propeller_moi = 237 //Propeller moment of inertia beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min = 12 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm = 5000 //Miminum governed RPM prop_tc = 0.001 //Prop time-constant gear_reduction_ratio = 16.69 //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= 1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather = 700 //Minimum RPM for prop feathering beta_feather = 90 //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 = 0.5 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta = -40.0 //Minimum pitch angle in reverse, (degrees) [turboprop_engine] maximum_torque=9236 power_scalar =1.0 //Scalar on Turboprop power [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 [contact_points] //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) point.0=1, 22.72, 0.00, -6.159, 1500, 0, 0.714, 80, 0.272, 0.572, 0.9, 7.0, 5.0, 0, 120, 250 point.1=1, -1.917, -5.604, -6.256, 1574.803, 1.000, 1.014, 0.000, 0.272, 2.500, 0.581, 5.000, 5.000, 2.000, 0.000, 0.000 point.2=1, -1.917, 5.604, -6.256, 1574.803, 2.000, 1.014, 0.000, 0.272, 2.500, 0.581, 5.000, 5.000, 3.000, 0.000, 0.000 point.3=2.000, -0.500, -42.667, 3.833, 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, -0.500, 42.667, 3.833, 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, -20.333, 0.000, 0.000, 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, 24.083, 0.000, 0.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=0.000000 static_cg_height=5.506865 gear_system_type=0 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 15.0 //Flap angle that activates warning at idle flap_limit_power = 30.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 1.0 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint = 4.54, -1.20, 3.25 [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, 1 Adf.1=1 Transponder.1=1 Marker.1=1 [exits] number_of_exits= 2 exit_rate.0= 0.25 ;Percent per second exit_rate.1= 0.35 ;Percent per second [folding_wings] wing_fold_system_type= 4 ;0=None fold_rates= 200.00,200.00 ;Percent per second [TailHook] tailhook_length= 1 ;(feet) tailhook_position= -15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust= 1.0 [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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.1=2, -42.19, 0.00, 2.953, fx_strobeh , light.2=1, -1.932, 0.00, -4.662, fx_beaconb , light.3=1, 4.232, 0.00, 5.84, fx_beaconh, electric_pump=0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [airplane_geometry] wing_area=722.000000 wing_span=70.333333 wing_root_chord=10.250000 wing_dihedral=2.999268 wing_incidence=-0.494385 wing_twist=-0.999756 oswald_efficiency_factor=1.666504 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=245.000000 htail_span=26.666667 htail_pos_lon=-37.333333 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=253.000000 vtail_span=18.135600 vtail_sweep=0.000000 vtail_pos_lon=-35.833333 vtail_pos_vert=5.833333 elevator_area=16.985000 aileron_area=13.477000 rudder_area=7.275000 elevator_up_limit=16.999658 elevator_down_limit=15.498508 aileron_up_limit=18.002334 aileron_down_limit=18.002334 rudder_limit=30.000070 elevator_trim_limit=15.000035 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=12,0.000000 flaps-position.2=20,0.000000 flaps-position.3=32,0.000000 [Reference Speeds] flaps_up_stall_speed = 96.0 //Knots True (KTAS) full_flaps_stall_speed = 76.8 //Knots True (KTAS) cruise_speed = 330.0 //Knots True (KTAS) max_mach = 0.59 max_indicated_speed = 270 //Red line (KIAS) [autopilot] use_no_default_pitch=1 use_no_default_bank=1 autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 500.0 autothrottle_available=1 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 default_pitch_mode=0 default_bank_mode=0 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=100.000000 [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 [stall_warning] type=2