///////////////////////////////////////////////////////
// //
// Dornier 228-212 //
// //
// //
// //
// //
// Model & panel by Jean-Pierre Brisard //
// Paint by Bob May //
// Technical advice by Joe Zerilli //
// Photoreal panel and gauges by JP Langer et al //
// //
// All files copyright Premier Aircraft Design 2008 //
// //
///////////////////////////////////////////////////////
// 09/15/2008 Modified [Radios] section
// 09/17/2008 Modified contact points (nose wheel no more go in the runway when braking)
// 09/18/2008 Modified [Fuel] section (2200 lbs + 200 lbs per wing)
// 09/20/2008 Modified number_of_tank_selectors = 2 (instead of 1)
// 10/03/2008 Modified [Flaps] section according flaps angles of the flight manual
// 10/20/2008 Modified gear and flaps limit speeds
[fltsim.0]
title=do228_212_Air_Guadeloupe JPL
sim=do228_bg02
model=
panel=jpl
sound=
texture=guadeloupe
kb_checklists=do228_check_12
kb_reference=do228_ref
atc_id=F-OGPI
ui_manufacturer=Dornier
ui_type=Do 228-212
ui_variation=Air Guadeloupe JPL
description=Dornier 228-212 Regional turboprop commuter/utility aircraft\nLength: 54.3 ft\nSpan: 55.7 ft\n Engines: 2 Garrett TPE 331-5 turbines 750 SHP
[fltsim.1]
title=do228_212_Air_Caraibes JPL
sim=do228_bg02
model=
panel=jpl
sound=
texture=caraibes
kb_checklists=do228_check_12
kb_reference=do228_ref
atc_id=F-OHQK
ui_manufacturer=Dornier
ui_type=Do 228-212
ui_variation=Air Caraibes JPL
description=Dornier 228-212 Regional turboprop commuter/utility aircraft\nLength: 54.3 ft\nSpan: 55.7 ft\n Engines: 2 Garrett TPE 331-5 turbines 750 SHP
//-------------------------------------------------------------------------------------------------------------------------------------
[General]
atc_type=Dornier
atc_model=d28
editable=1
performance=Max cruise speed: 260 mph\nRange: 540-1460 nm\nCeiling: 28,000 ft\nMax weight: 13,000 lbs\nPassenger: 19
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 14110.00
empty_weight = 7183.00
reference_datum_position = 0.00, 0.00, 0.00
empty_weight_CG_position = 0.00, 0.00, 0.00
max_number_of_stations=12
station_load.0=170.0, 9.0, -1.35, 0.000 // Pilot - Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170.0, 9.0, 1.35, 0.000 // Co-Pilot
station_load.2=170.0, 5.5, -2.00, 0.000 // Passenger
station_load.3=170.0, 5.5, 2.00, 0.000 // Passenger
station_load.4=170.0, 5.5, 2.00, 0.000 // Passenger
station_load.5=170.0, 5.5, -2.00, 0.000 // Passenger
station_load.6=170.0, 0.00, 2.00, 0.000 // Passenger
station_load.7=170.0, 0.00, -2.00, 0.000 // Passenger
station_load.8=170.0, -2.5, -2.00, 0.000 // Passenger
station_load.9=170.0, -2.5, 2.00, 0.000 // Passenger
station_load.10=000.0, -2.5, 2.0, 0.000 // Passenger
station_load.11=000.0, -2.5, -2.00, 0.000 // Passenger
station_load.12=220.00,-8.00, 000.0,000.0//Luggage
;Moments of Inertia
empty_weight_pitch_MOI = 80000.00
empty_weight_roll_MOI = 36000.00
empty_weight_yaw_MOI = 75000.00
empty_weight_coupled_MOI= 0.00
CG_forward_limit= 0.00
CG_aft_limit= 1.00
station_load.0=0.00,0.00,0.00,0.00
[flight_tuning]
parasite_drag_scalar =0.50 //0.90
induced_drag_scalar =0.50 //1.00
elevator_effectiveness =1.00
aileron_effectiveness =1.00
rudder_effectiveness =1.00
pitch_stability =1.00
roll_stability =1.00
yaw_stability =1.00
elevator_trim_effectiveness =1.00
aileron_trim_effectiveness =1.00
rudder_trim_effectiveness =1.00
[GeneralEngineData]
engine_type = 5
Engine.0 = 6.50, -8.60, 0.60
Engine.1 = 6.50, 8.60, 0.60
fuel_flow_scalar = 0.70
min_throttle_limit=-0.250
[propeller]
thrust_scalar =1.00
propeller_type = 0
propeller_diameter = 8.60
propeller_blades = 4
propeller_moi = 5 // 22.00
beta_max = 45.00
beta_min = 0
min_gov_rpm = 40060
prop_tc = 0.004
gear_reduction_ratio = 26.2287 //17.6 // 11.60
fixed_pitch_beta = 0.00
low_speed_theory_limit = 80.00
prop_sync_available = 1
prop_deice_available = 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather = 700.00
beta_feather = 79.30
power_absorbed_cf = 0.90
defeathering_accumulators_available= 0
prop_reverse_available = 1
minimum_on_ground_beta = 1.00
minimum_reverse_beta = -14.00
[TurbineEngineData]
fuel_flow_gain = 0.1 //0.05 //0.011
inlet_area = 1.00
rated_N2_rpm = 30000// 42147 //41730
static_thrust = 150 // 250.00
afterburner_available= 0
[turboprop_engine]
power_scalar =1.00
maximum_torque =3270.0 // 4270.00
max_rpm_mechanical_efficiency_scalar=1.00
idle_rpm_mechanical_efficiency_scalar=1.00
max_rpm_friction_scalar=1.00
idle_rpm_friction_scalar=1.00
[Reference Speeds]
flaps_up_stall_speed = 101.00
full_flaps_stall_speed = 84.00
cruise_speed = 215.00 //knots indicated airspeed @ 9,000 ft
normal_cruise_speed = 215.00
max_indicated_speed=259.00
max_mach=0.579980
max_level_speed=300
[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
[contact_points]
//Classes...What type of point 0=Unused or Ignore
// 1=Wheel
// 2=Scrape point
// 4=Float
// 5=Float Rudder
//0 Class
//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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal
//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)
static_pitch = 0
static_cg_height = 8.1
tailwheel_lock = 0
gear_system_type = 1 //Hydraulic
max_number_of_points = 8
point.0 = 1, 18.47, 0, -8.6, 1181, 0, 0.75, 39.9, 0.096, 2.5, 0.9516, 4.8, 4.8, 0, 184, 184
point.1 = 1.000,-2.320,-4.64,-9.06,1574, 1, 0.75, 0.0, 0.642, 2.5, 0.8152, 4.5, 5.2, 2, 184.0, 184.0
point.2 = 1.000,-2.320,4.64,-9.06,1574, 2, 0.75, 0.0, 0.642, 2.5, 0.8152, 4.8, 4.9, 3, 184.0, 184.0
point.3 = 2.000,-2.200,-29.300,3.200,2360.907127,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,5.000,0.000,0.000
point.4 = 2.000,-2.200,29.300,3.200,2360.907127,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,6.000,0.000,0.000
point.5 = 2.000,-35.000,0.000,11.000,2360.907127,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,9.000,0.000,0.000
point.6 = 2.000,23.600,-0.000,-0.500,1574.803150,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,4.000,0.000,0.000
point.7 = 5.000,23.600,-0.000,-0.500,1574.803150,0.000,0.000,0.000,0.000,0.000,0.000,0.000,0.000,4.000,0.000,0.000
[Views]
//eyepoint=13.267,-0.619,2.607
//eyepoint=13.104,-0.815,2.77
//eyepoint=13.00,-1.000,0.607
//eyepoint=11.0,-1.5,-1.9
eyepoint=11.5,-1.5,-1.4
[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.
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.0 = 3, -4.10, -27.4, -0.05, fx_navred ,
light.1 = 3, -4.10, 27.4, -0.05, fx_navgre ,
'light.2 = 3, -35.00, 0.00, 11.00, fx_navwhi ,
light.3 = 2, -4.35, -27.4, -0.35, fx_strobe ,
light.4 = 2, -4.35, 27.4, -0.35, fx_strobe ,
light.5 = 1, -28.00, 0.00, 7.5,fx_beaconh ,
light.6 = 1, 7.10, 0.00, -6.10, fx_beaconh ,
light.7 = 4, 12.50, -1.00, -2.10, fx_vclightwhi ,
light.8= 4, 12.50, 1.00, -2.10, fx_vclightwhi ,
light.9 = 4, 9.50, 0.00, -2.10, fx_vclightwhi ,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = 0.00, -6.00, -1.50, 30.00, 0.00
LeftAux = 0.00,-14.50, -1.00, 328.00, 0.00
RightMain = 0.00, 6.00, -1.50, 30.00, 0.00
RightAux = 0.00, 14.50, -1.00, 328.00, 0.00
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=2
[airplane_geometry]
wing_area = 310.00
wing_span = 58.00
wing_root_chord = 6.60
wing_dihedral = 6.00
wing_incidence = 1.00
wing_twist = -1.50
oswald_efficiency_factor= 0.70
wing_winglets_flag = 1
wing_sweep = 3.00
wing_pos_apex_lon = 2.00
wing_pos_apex_vert = -1.00
htail_area = 76.00
htail_span = 18.20
htail_pos_lon = -27.50
htail_pos_vert = 11.00
htail_incidence = 0.00
htail_sweep = 20.00
vtail_area = 50.00
vtail_span = 6.50
vtail_sweep = 35.00
vtail_pos_lon = -23.50
vtail_pos_vert = 4.50
elevator_area = 14.00
aileron_area = 13.00
rudder_area = 17.00
elevator_up_limit = 17.00
elevator_down_limit = 15.50
aileron_up_limit = 18.00
aileron_down_limit = 18.00
rudder_limit = 30.00
elevator_trim_limit = 15.00
spoiler_limit = 0.00
spoilerons_available = 0
aileron_to_spoileron_gain = 0.00
min_ailerons_for_spoilerons = 0.00
min_flaps_for_spoilerons = 0.00
auto_spoiler_available=0
spoiler_extension_time=0.000000
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
use_no_default_pitch=1
use_no_default_bank=1
autothrottle_available= 0
pitch_takeoff_ga=8.00
max_pitch=10.00
max_pitch_acceleration=1.00
max_pitch_velocity_lo_alt=2.00
max_pitch_velocity_hi_alt=1.50
max_pitch_velocity_lo_alt_breakpoint=20000.00
max_pitch_velocity_hi_alt_breakpoint=28000.00
max_bank=25.00
max_bank_acceleration=1.80
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.250
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.520
gs_integrator_control=0.260
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.00
default_pitch_mode=0
default_bank_mode=0
[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= 0.30
extending-time= 5.00
system_type= 0
damaging-speed= 250.00
blowout-speed= 300.00
flaps-position.0= 0.00, 0.00
flaps-position.1= 5.00, 160.00
flaps-position.2=20.00, 130.00
flaps-position.3=30.00, 130.00
drag_scalar=1.30
lift_scalar=1.20
[Flaps.1]
type= 1
span-outboard= 0.30
extending-time= 5.00
system_type= 0
damaging-speed= 250.00
blowout-speed= 300.00
flaps-position.0= 0.00, 0.00
flaps-position.1= 5.00, 160.00
flaps-position.2=20.00, 130.00
flaps-position.3=30.00, 130.00
drag_scalar=1.30
lift_scalar=1.20
[brakes]
toe_brakes_scale=1.00
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=3000.00
[stall_warning]
type=1
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[exits]
number_of_exits=2
exit_rate.0=0.2 ;Percent per second
exit_rate.1=0.5
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=2
