// PREMIER AIRCRAFT DESIGN
// Dornier 328JET, JPB, March 2010
// Model & panel by Jean-Pierre Brisard
// Paint & FD adjustments by Bob May
// All files copyright Premier Aircraft Design 2010
// Do328JET for FSX


[fltsim.0]
title=do328JET ROYAL STAR
sim=do328j
model=pax
panel=169	// Wide screen
//panel=43	// Standard screen
sound=DO
texture=RPC8328
kb_checklists=do328j_check
kb_reference=do328j_ref
atc_airline=regional
atc_flight_number=Do328
atc_parking_types=gate,ramp
atc_parking_codes=ramp
atc_id=RP-C8328
ui_manufacturer=Dornier
ui_type=Do328Jet
ui_variation=ROYAL STAR AVIATION
description=Dornier 328JET Regional commuter\nLength: 69.7 ft\nSpan: 68.8 ft\n Engines: 2 x Pratt & Whitney 306B turbofans, 6,050 lbs 

[General]
atc_type=Dornier
atc_model=328
editable=1
performance=Max cruise speed: 405 kts @ 35,000 ft mph\nRange: 1,200 nm\nCeiling: 35,000 ft\nMax weight: 30840lbs\nPassenger: 30/33
Category=airplane

[WEIGHT_AND_BALANCE]
max_gross_weight =30840.0
empty_weight =15670.00000

reference_datum_position     = 0.00, 0.00, 0.00
empty_weight_CG_position     = -0.000, -0.000, -0.000

max_number_of_stations=4

;Moments of Inertia
empty_weight_pitch_MOI  =110801.64915
empty_weight_roll_MOI   =39664.70845
empty_weight_yaw_MOI    =106202.25687
empty_weight_coupled_MOI=0.00000
CG_forward_limit= 0.00
CG_aft_limit= 1.00
station_load.0= 170, -0.000, -1.350, -4.000, //Captain
station_load.1= 170, -0.000, 1.350, -4.000, //First
station_load.2= 1960, -0.000, -0.000, -4.000, //Passengers
station_load.3= 400, -0.000, -0.000, -4.000, //Baggage

[Views]
//eyepoint=11.5,-1.5,-1.4
eyepoint=18.812,-1.450,-2.750
//eyepoint=16.812,-1.350,-2.450

[flight_tuning]

parasite_drag_scalar   =1.00000
induced_drag_scalar    =1.00000
elevator_effectiveness =1.00000
aileron_effectiveness  =1.00000
rudder_effectiveness   =1.00000
pitch_stability        =1.00000
roll_stability         =1.00000
yaw_stability          =1.00000
elevator_trim_effectiveness =1.50000
aileron_trim_effectiveness  =1.00000
rudder_trim_effectiveness   =1.00000
cruise_lift_scalar=1.00000
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
p_factor_on_yaw=0.00000
torque_on_roll=0.00000
gyro_precession_on_roll=0.00000
gyro_precession_on_yaw=0.00000

[GeneralEngineData]
engine_type =1
Engine.0 =6.500, -8.600, -0.000
Engine.1 =6.500, 8.600, -0.000
fuel_flow_scalar        =0.55000
min_throttle_limit =-0.25000

[TurbineEngineData]
fuel_flow_gain          =0.00250
inlet_area              =1.28950
rated_N2_rpm            =29920.00000
static_thrust           =6050.00000
afterburner_available   =0
reverser_available      =1
//afterburner_throttle_threshold=0.00000
//ThrustSpecificFuelConsumption=0.00000
//AfterBurnThrustSpecificFuelConsumption=0.00000

[jet_engine]
thrust_scalar =1.00000

[Reference Speeds]
flaps_up_stall_speed    = 101.00
full_flaps_stall_speed  = 84.00
cruise_speed            =405.02998
normal_cruise_speed	= 265.00
max_indicated_speed=450.04297
max_mach=0.88000
max_level_speed=330

[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 = 0.000
static_cg_height = 11.000
gear_system_type=0
max_number_of_points=8
tailwheel_lock=0
point.0= 1, 20.948, 0.000, -11.000, 1181, 0, 0.750, 80.000, 0.120, 2.500, 0.826, 5.000, 6.000, 0
point.1= 1, -2.752, -5.268, -11.980, 1574, 1, 0.750, 0.000, 1.242, 2.000, 0.815, 4.500, 5.200, 2, 184.0, 184.0
point.2= 1, -2.752, 5.268, -11.980, 1574, 2, 0.750, 0.000, 1.242, 2.000, 0.815, 4.800, 4.900, 3, 184.0, 184.0
point.3= 2, -2.200, -35.300, 3.200, 2361, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, -2.200, 35.300, 3.200, 2361, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -50.000, 0.000, 0.000, 2361, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2, 23.600, -0.000, -0.500, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.7= 5, 23.600, -0.000, -0.500, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4

[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.0 =4, 20.000000, 0.000000, -3.710000, fx_vclightwhi
light.1 =1, -37.000000, 0.000000, 12.630000, fx_beacon
light.2 =2, -3.100000, -34.920000, 0.133000, fx_strobeh
light.3 =2, -3.100000, 34.920000, 0.133000, fx_strobeh
light.4 =3, -3.100000, -35.000000, 0.133000, fx_navred
light.5 =3, -3.100000, 35.000000, 0.133000, fx_navgre

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[fuel]
LeftMain  = -0.000, -14.500, -1.000, 300.000, 0.000
'LeftAux   = 0.00, -6.00, -1.50,  79.50, 0.00
RightMain = -0.000, 14.500, -1.000, 300.000, 0.000
'RightAux  = 0.00,  6.00, -1.50,  79.50, 0.00
fuel_type =2
number_of_tank_selectors =1                    
electric_pump=0
fuel_dump_rate=0.02000
anemometer_pump=0
manual_pump=0
engine_driven_pump=0

[airplane_geometry]
wing_area               =481.00000
wing_span               =68.80000
wing_root_chord         =7.34084
wing_dihedral           =3.00000
wing_incidence          =0.00000
wing_twist              =0.00000
oswald_efficiency_factor=0.70000
wing_winglets_flag      =0
wing_sweep              =0.00000
wing_pos_apex_lon       =1.74928
wing_pos_apex_vert      =0.00000
htail_area              =84.00000
htail_span              =21.20000
htail_pos_lon           =-49.82634
htail_pos_vert          =11.00000
htail_incidence         =0.00000
htail_sweep             =0.00000
vtail_area              =50.00000
vtail_span              =9.50000
vtail_sweep             =35.00000
vtail_pos_lon           =-47.67937
vtail_pos_vert          =2.50000
elevator_area           =20.00000
aileron_area            =20.00000
rudder_area             =17.00000
elevator_up_limit       =17.00000
elevator_down_limit     =15.50000
aileron_up_limit        =18.00000
aileron_down_limit      =18.00000
rudder_limit            =20.00000
elevator_trim_limit     =15.00000
spoiler_limit           =60.00000
spoilerons_available    =0
aileron_to_spoileron_gain =0.00000
min_ailerons_for_spoilerons =0.00000
min_flaps_for_spoilerons =0.00000
auto_spoiler_available=1
spoiler_extension_time=3.00000
positive_g_limit_flaps_up=3.00000
positive_g_limit_flaps_down=2.10000
negative_g_limit_flaps_up=-2.40000
negative_g_limit_flaps_down=-1.80000
spoiler_handle_available=1
load_safety_factor=1.00000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800 
autothrottle_available=1 
autothrottle_arming_required=0
autothrottle_max_rpm = 110
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8 ;
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=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[forcefeedback]
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[Flaps.0]
type= 1
system_type=0
span-outboard= 0.300
extending-time= 5.0
damaging-speed=250.0
blowout-speed=300.0
flaps-position.0=0.00
flaps-position.1=5.00
flaps-position.2=10.00
flaps-position.3=15.00
flaps-position.4=20.00
lift_scalar=1.80
drag_scalar=1.00
pitch_scalar=1.00

[brakes]
toe_brakes_scale=1.00000
parking_brake=1
auto_brakes=4
hydraulic_system_scalar=0.00000
differential_braking_scale=0.00000

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.09998
flap_limit_power=30.02299
flap_limit_idle=15.01149

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.00000

[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              

[folding_wings]
wing_fold_system_type=4
fold_rates=0.6,0.6

[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

[GPWS]
max_warning_height=0
sink_rate_fpm=-1500
excessive_sink_rate_fpm=-2000
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-100