[fltsim.0]
title=Fairchild-Dornier 328-110 Southeast Asian Airlines
sim=d328tp
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Fairchild-Dornier
ui_type=328-110
ui_variation=Southeast Asian Airlines
atc_id=RP-C5328
atc_airline=
atc_flight_number=
description=Information:\nSoutheast Asian Airlines (SEAIR) is the first to operate this kind of aircraft in the Philippine. It is used to carry people to and from key regions of the Philippines wherein larger aircraft could not operate.\n\nHistory/Performance:\nThe Dornier 328-110 is a high speed regional turboprop, with excelent short field capabilities. The plane first flew on December 6 1991, and was certified in October 1993. The plane can carry 30 to 39 passengers, offering more space per passenger than a 737. The aircraft isequiped with a full glass cockpit and is certified for CAT IIIa landings.\n\nOriginal desing by Robert Versluys.\n\n
[General]
performance=Max cruise speed: 400kts\nRange with 32pax: 900nm\nTakeoff field: 3570ft
atc_type=Fairchild-Dornier
atc_model=Do328
editable=1
[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
