[fltsim.0]
title=Dornier 328 Welcome Air OE-GBB
sim=d328tp
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Dornier
ui_type=Dornier 328-110
ui_variation=Welcome Air OE-GBB
description=The 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 then a 737. The aircraft is equiped with a full glass cockpit and is certified for cat IIIa landings.
atc_heavy=0
atc_id=OE-GBB
atc_airline=Welcome Air
atc_flight_number=

[fltsim.1]
title=Dornier 328 Welcome Air OE-LIR
sim=d328tp
model=
panel=
sound=
texture=1
checklists=
ui_manufacturer=Dornier
ui_type=Dornier 328-110
ui_variation=Welcome Air OE-LIR
description=The 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 then a 737. The aircraft is equiped with a full glass cockpit and is certified for cat IIIa landings.
atc_heavy=0
atc_id=OE-LIR
atc_airline=Welcome Air
atc_flight_number=

[General]
performance=Max cruise speed:     (TAS)335kt\nCruise altitude:   25000-31000ft\nRange:                900-1000nm\nMTOW:                    30842lb\nMLW:                     29167lb\n\nIFDG Dornier 328-100\nModel:        Robert Versluys\nDynamics:     Robert Versluys\nTextures:     Aviel Nahoum\n              Robert Versluys\n              Kristiaan Duivesteijn\nBeta-Tester:  Karl Klatt\nPlease read the docs for our repaint and distribution policies.
atc_type=DORNIER
atc_model=DO328
editable=1

[flight_tuning]
cruise_lift_scalar=1.0parasite_drag_scalar=0.9induced_drag_scalar=1.0elevator_effectiveness=1.0aileron_effectiveness=1.0rudder_effectiveness=1.0pitch_stability=2.0roll_stability=1.0yaw_stability=1.0elevator_trim_effectiveness=1.0aileron_trim_effectiveness=0.8
rudder_trim_effectiveness=1.0

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=-1.500, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=23286.000
empty_weight_roll_MOI=284432.000
empty_weight_pitch_MOI=232022.000
empty_weight_yaw_MOI=296220.000
empty_weight_coupled_MOI=1300.000
max_gross_weight=30881.120
CG_forward_limit=0.000
CG_aft_limit=1.000

[fuel]
LeftMain=0.000, -10.000, 3.500, 566.800, 0.000
RightMain=0.000, 10.000, 3.500, 566.800, 0.000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=585.000

wing_span=85.000

wing_root_chord=7.000

wing_dihedral=2.500

wing_incidence=1.000

wing_twist=-3.000

oswald_efficiency_factor=0.700

wing_winglets_flag=0

wing_sweep=3.000

wing_pos_apex_lon=-25.000

wing_pos_apex_vert=0.000
htail_span=17.167
htail_pos_lon=-24.583
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=0.000
vtail_area=42.000
vtail_span=7.389
vtail_sweep=0.000
vtail_pos_lon=-20.500
vtail_pos_vert=4.083
elevator_area=39.000
aileron_area=31.080
rudder_area=42.600
elevator_up_limit=13.178
elevator_down_limit=13.178
aileron_up_limit=17.762
aileron_down_limit=17.762
rudder_limit=23.491
elevator_trim_limit=11.459
spoiler_limit=59.989
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000
htail_area=67.000


[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=1.000, 23.000, 0.000, -5.750, 1500.000, 0.000, 0.714, 35.000, 0.272, 2.500, 0.900, 7.000, 5.000, 0.000, 120.000, 1202.542
point.1=1.000, -2.917, -6.583, -5.917, 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=1.000, -2.917, 6.583, -5.917, 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=0.000
static_cg_height=5.507

[GeneralEngineData]
engine_type=5
Engine.0=-25.250, -11.667, 1.000
Engine.1=-25.250, 11.667, 1.000
fuel_flow_scalar=0.500

[TurbineEngineData]
fuel_flow_gain=0.022
inlet_area=1.000
rated_N2_rpm=29920.000
static_thrust=200.000
afterburner_available=0

[propeller]
propeller_type=0
propeller_diameter=11.100
propeller_blades=6
propeller_moi=77.000
beta_max=45.000
beta_min=10.000
min_gov_rpm=25000.000
prop_tc=0.004
gear_reduction_ratio=13.000
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=700.000
beta_feather=85.000
power_absorbed_cf=0.900
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=1.000
minimum_reverse_beta=-20.000

[turboprop_engine]
maximum_torque=8568.000

[Reference Speeds]
flaps_up_stall_speed=100.000
full_flaps_stall_speed=75.600
cruise_speed=230.000

[keyboard_response]
elevator=30.000000,120.000000
aileron=120.000000,1000.000000
rudder=150.000000,180.000000

[Views]
eyepoint=19.838829,-1.704499,2.499077

[autopilot]
autopilot_available=1
flight_director_available=1
autothrottle_available=0
default_vertical_speed=1000.000000
pitch_takeoff_ga=8.000000
use_no_default_bank=1

[direction_indicators]
direction_indicator.0=3,0

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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit

[forcefeedback]
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=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 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

[Radios]
// Radio Type=available, 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

[Flaps.0]
type=1
span-outboard=0.500
extending-time=5.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=13.331, 0.000
flaps-position.2=26.662, 0.000
flaps-position.3=39.992, 0.000