[fltsim.0] title=Dornier 228 Cosmic Air sim=Dornier228 model= panel= sound= texture= kb_checklists=Do228_CHECK kb_reference=kneeboard_keys ui_manufacturer=Dornier ui_type=228 ui_variation=Cosmic Air atc_id= atc_heavy=0 atc_airline=Cosmic Air atc_flight_number=107 description=The Super-Rugged Dornier 228 can operate virtually anywhere with STOL capabilities and fits the Nepalese Himalays perfect. With many in service, Cosmic Air has been Nepal's one of the oldest Private Airlines operating the Do228. Origional by Bjorn Buchner. Repainted by Yeatin Giri. [General] atc_type=DORNIER atc_model=D228 performance=Engine Model : Garrett TPE 331-5A-252 D or Garrett TPE 331-10 \nTakeoff Power : 2 x 776shp\nMax Take Off Weight : 6,400 kg \nMax. range : 750 km \nService ceiling : 27000ft\nMax. speed : 434km\/h\nPassengers : 19\nCrew : 2\ [WEIGHT_AND_BALANCE] max_gross_weight=14175.000 empty_weight=8248.000 reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=4.000, 0.000, 3.000 max_number_of_stations=50 ;Moments of Inertia empty_weight_pitch_MOI=30000.000 empty_weight_roll_MOI=18200.000 empty_weight_yaw_MOI=36500.000 empty_weight_coupled_MOI=0.000 CG_forward_limit=0.000 CG_aft_limit=1.000 station_load.0=0.000000,0.000000,0.000000,0.000000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=0.510 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.500 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type=5 Engine.0=8.560, -8.590, 4.600 Engine.1=8.560, 8.590, 4.600 fuel_flow_scalar=1.000 min_throttle_limit=-0.250000 [propeller] thrust_scalar=1.000 propeller_type=0 propeller_diameter=8.960 propeller_blades=4 propeller_moi=24.000 beta_max=60.000 beta_min=3.000 min_gov_rpm=25520.000 prop_tc=0.004 gear_reduction_ratio=17.600 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=200.000 beta_feather=80.000 power_absorbed_cf=0.900 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=1.000 minimum_reverse_beta=-14.000 [TurbineEngineData] fuel_flow_gain=0.011 inlet_area=1.000 rated_N2_rpm=41000.000 static_thrust=158.000 afterburner_available=0 [turboprop_engine] power_scalar=1.000 maximum_torque=1981.000 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [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 //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, 22.700, 0.000, -4.470, 1181.000, 0.000, 0.610, 39.900, 0.159, 5.000, 0.952, 4.800, 4.800, 0.000, 0.000, 0.000 point.1=1.000, 2.450, -4.910, -4.480, 1574.000, 1.000, 1.070, 0.000, 0.642, 2.500, 0.815, 4.500, 5.200, 2.000, 0.000, 0.000 point.2=1.000, 2.450, 4.910, -4.480, 1574.000, 2.000, 1.070, 0.000, 0.642, 2.500, 0.815, 4.800, 4.900, 3.000, 0.000, 0.000 point.3=2.000, -6.138, 0.000, -1.380, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=0.000 static_cg_height=4.800 point.4=2.000, -21.480, 0.000, 1.530, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.5=2.000, 24.550, 0.000, -1.530, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.6=2.000, 2.790, 2.000, 2.460, 787.400, 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, 0.560, 27.620, 5.530, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.8=2.000, 0.560, -27.620, 5.530, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.9=2.000, 2.790, -2.000, 2.460, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 gear_system_type=0 [Views] eyepoint=17.5, -1.39, 3.6 [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 5=landing light.0=2, 1.1, 27.9, 4.9, fx_strobe.fx , light.1=2, 1.1, -27.9, 4.9, fx_strobe.fx , light.2=2, 1.1, 27.9, 4.9, fx_strobeh.fx , light.3=2, 1.1, -27.9, 4.9, fx_strobeh.fx , light.4=2, -22, 0.00, 12.28, fx_beaconh , light.5=2, -22, 0.00, 12.28, fx_beacon , light.6=2, -6, 0.00, -1.5, fx_beaconh , light.7=2, -6.1, 0.00, -1.5, Do_BCNL.fx , light.8=4, 15, 0.00, 2.5, Do_NAVR.fx , light.9 = 5, 22.00, 11.30, -9.61, Dowing.fx , light.10 = 5, 22.00, -11.30, -9.61, Dowing.fx , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [Smokesystem] smoke.0= -0.5, 0.0, -6.00, fx_smoke_turbprop.fx smoke.1= -0.5, 0.0, 6.00, fx_smoke_turbprop.fx [fuel] LeftMain=4.950, -4.950, 5.280, 210.000, 0.000 LeftAux=4.950, -13.200, 5.280, 94.500, 0.000 RightMain=4.950, 4.950, 5.280, 210.000, 0.000 RightAux=4.950, 13.200, 5.280, 94.500, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=344.000 wing_span=55.800 wing_root_chord=7.670 wing_dihedral=0.000 wing_incidence=1.000 wing_twist=-1.500 oswald_efficiency_factor=0.700 wing_winglets_flag=0 wing_sweep=4.000 wing_pos_apex_lon=7.670 wing_pos_apex_vert=5.530 htail_area=98.880 htail_span=21.480 htail_pos_lon=-22.400 htail_pos_vert=3.070 htail_incidence=0.500 htail_sweep=0.000 vtail_area=63.670 vtail_span=7.980 vtail_sweep=40.000 vtail_pos_lon=-18.410 vtail_pos_vert=4.600 elevator_area=17.000 aileron_area=13.500 rudder_area=7.300 elevator_up_limit=17.000 elevator_down_limit=15.000 aileron_up_limit=18.000 aileron_down_limit=18.000 rudder_limit=30.000 elevator_trim_limit=15.000 spoiler_limit=0.000 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 [Reference Speeds] flaps_up_stall_speed=80.000 full_flaps_stall_speed=60.000 cruise_speed=234.300 max_indicated_speed=259.000000 max_mach=0.579980 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1500.0 autothrottle_available=0 pitch_takeoff_ga=8.000 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [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 [Flaps.0] type=1 span-outboard=0.750 extending-time=5.000 system_type=1 damaging-speed=120.000 blowout-speed=200.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=7.000 flaps-position.0=0.000, 0.000 flaps-position.1=10.000, 0.000 flaps-position.2=25.000, 0.000 flaps-position.3=40.000, 0.000 [brakes] toe_brakes_scale=1.000000 parking_brake=1 [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=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0