[fltsim.0]
title=Dornier Do228 Esercito Italiano
sim=Dornier228
model=
panel=
sound=
texture=
panel_alias=
sound_alias=beech_king_air_350\sound
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Dornier
ui_type=D228
ui_variation=EI
description=The rugged Dornier 228 can operate virtually anywhere. The Dornier 228 is a tough, short-field aircraft that's used for passenger service, freight and many sensor platforms. There are almost 250 Dornier 228s in service around the world.
atc_heavy=0
atc_airline=
atc_flight_number=
[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\nAuthor : Björn Büchner (February 2002)\n(bjornbuchner@hotmail.com)\nTextures : Björn Büchner
[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
[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
[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
light.3=2, 1.1, -27.9, 4.9, fx_strobe ,
light.4=2, 1.1, 27.9, 4.9, fx_strobe ,
light.5=1, -22, 0.00, 12.28, fx_beacon ,
light.6=2, -6, 0.00, -1.5, fx_strobe ,
light.7=4, 15, 0.00, 2.5, fx_vclight,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[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
[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
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=0
pitch_takeoff_ga=8.000
[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
