[fltsim.0]
title=Dornier Do228
sim=Dornier228
model=
panel=
sound=
texture=
panel_alias=beech_king_air_350\panel
sound_alias=beech_king_air_350\sound
kb_checklists=
kb_reference=
atc_id=ZS-IAD
ui_manufacturer=Dornier
ui_type=Do228
ui_variation=Independent Airlines
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=Independent
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=0.000, 0.000, 0.000, 0.000
[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=0.505
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=1.111
propeller_type= 0
propeller_diameter= 8.960
propeller_blades= 4
propeller_moi= 24.000
beta_max= 60.000
beta_min= 13.000
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=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, 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= 60.000
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
