[fltsim.0]
title=Dornier 328-110 Horizon
sim=d328tp
model=
panel=
sound=
texture=QX
checklists=
ui_manufacturer=Dornier
ui_type=Do 328-110
ui_variation=Horizon
description=Horizon Air "Wings of the great Northwest" had 10 of these and was the North American rollout airline, but in less than 5 years they were removed from the fleet due lack of parts, and other MTX issues. Passengers & Pilots loved them, but ground crews found them a nightmare. \nOriginal desing by Robert Versluys. \nRepaint by Alejandro Hurtado
atc_id=N355PH
atc_airline=Horizon
atc_parking_types=GATE
atc_parking_codes=QX2
[General]
performance=Max cruise speed: 400kts\nRange with 32pax: 900nm\nTakeoff field: 3570ft
atc_type=Dornier
atc_model=DO328
editable=0
[WEIGHT_AND_BALANCE]
empty_weight = 19665 // (pounds)
reference_datum_position = 0.000000,0.000000,0.000000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0.000000,0.000000,0.000000 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations =50
station_load.0 =0.000000,0.000000,0.000000,0.000000
station_load.1 = 275, 0, 0, 0.0 //Pilots
station_load.2 = 3372, 0, 0, 0.0 //Payload
;Moments of Inertia
empty_weight_roll_MOI = 205716
empty_weight_pitch_MOI = 231761
empty_weight_yaw_MOI = 330944
empty_weight_coupled_MOI = 1300
max_gross_weight=34968.000000
[fuel]
LeftMain=0.000000,-14.500000,-1.00000,566.800000,0.000000
RightMain=0.000000,14.500000,-1.00000,566.800000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=1
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type=5
Engine.0=11.250000,-7.833333,5.000000
Engine.1=11.250000,7.833333,5.000000
fuel_flow_scalar=0.870000
min_throttle_limit=-0.250000
[TurbineEngineData]
fuel_flow_gain=0.011000
inlet_area=1.10000
rated_N2_rpm=27000.000000
static_thrust=510.000000
afterburner_available=0
[propeller]
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter = 11.1 //Propeller Diameter, (feet)
propeller_blades = 6 //Number of propeller blades
propeller_moi = 237 //Propeller moment of inertia
beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min = 12 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm = 5000 //Miminum governed RPM
prop_tc = 0.001 //Prop time-constant
gear_reduction_ratio = 16.69 //Propeller gear reduction ratio
fixed_pitch_beta = 0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit = 80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available = 1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available = 1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather = 700 //Minimum RPM for prop feathering
beta_feather = 90 //Feathering pitch angle (degrees)
power_absorbed_cf = 0.9 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available = 1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta = 0.5 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta = -40.0 //Minimum pitch angle in reverse, (degrees)
[turboprop_engine]
maximum_torque=9236
power_scalar = 1.0 //Scalar on Turboprop power
[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, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 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]
//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)
point.0=1, 22.72, 0.00, -6.159, 1500, 0, 0.714, 80, 0.272, 0.572, 0.9, 7.0, 5.0, 0, 120, 250
point.1=1, -1.917, -5.604, -6.256, 1574.803, 1.000, 1.014, 0.000, 0.272, 2.500, 0.581, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1, -1.917, 5.604, -6.256, 1574.803, 2.000, 1.014, 0.000, 0.272, 2.500, 0.581, 5.000, 5.000, 3.000, 0.000, 0.000
point.3=2.000, -0.500, -42.667, 3.833, 1574.803, 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, -0.500, 42.667, 3.833, 1574.803, 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, -20.333, 0.000, 0.000, 1574.803, 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, 24.083, 0.000, 0.000, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=0.000000
static_cg_height=5.506865
gear_system_type=0
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 15.0 //Flap angle that activates warning at idle
flap_limit_power = 30.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[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, 1
Adf.1=1
Transponder.1=1
Marker.1=1
[exits]
number_of_exits= 2
exit_rate.0= 0.25 ;Percent per second
exit_rate.1= 0.35 ;Percent per second
[folding_wings]
wing_fold_system_type= 4 ;0=None
fold_rates= 200.00,200.00 ;Percent per second
[TailHook]
tailhook_length= 1 ;(feet)
tailhook_position= -15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust= 1.0
[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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1=2, -42.19, 0.00, 2.953, fx_strobeh ,
light.2=1, -1.932, 0.00, -4.662, fx_beaconb ,
light.3=1, 4.232, 0.00, 5.84, fx_beaconh,
electric_pump=0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[airplane_geometry]
wing_area=722.000000
wing_span=70.333333
wing_root_chord=10.250000
wing_dihedral=2.999268
wing_incidence=-0.494385
wing_twist=-0.999756
oswald_efficiency_factor=1.666504
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=245.000000
htail_span=26.666667
htail_pos_lon=-37.333333
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=253.000000
vtail_span=18.135600
vtail_sweep=0.000000
vtail_pos_lon=-35.833333
vtail_pos_vert=5.833333
elevator_area=16.985000
aileron_area=13.477000
rudder_area=7.275000
elevator_up_limit=16.999658
elevator_down_limit=15.498508
aileron_up_limit=18.002334
aileron_down_limit=18.002334
rudder_limit=30.000070
elevator_trim_limit=15.000035
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=12,0.000000
flaps-position.2=20,0.000000
flaps-position.3=32,0.000000
[Reference Speeds]
flaps_up_stall_speed = 96.0 //Knots True (KTAS)
full_flaps_stall_speed = 76.8 //Knots True (KTAS)
cruise_speed = 330.0 //Knots True (KTAS)
max_mach = 0.59
max_indicated_speed = 270 //Red line (KIAS)
[autopilot]
use_no_default_pitch=1
use_no_default_bank=1
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 500.0
autothrottle_available= 1
pitch_takeoff_ga=8.0
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=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
default_pitch_mode=0
default_bank_mode=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
[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
[stall_warning]
type=2
