[fltsim.0]
JABIndex=1
title=ATR42-500 LG AIRLINES
sim=atr42 500
model=
panel=
sound=
texture=1
checklists=
kb_checklists=checklist
description=ATR42-500
ui_manufacturer=ATR
ui_type=42 500
ui_variation=ATR Lg Airlines
atc_heavy=0
atc_id=OLG9
atc_airline=Lg Airlines
atc_flight_number=

[WEIGHT_AND_BALANCE]
reference_datum_position=000, 0, 6.800
empty_weight_CG_position=000, 0.000, -8.000
max_number_of_stations=50

station_load.0=0.000000,0.000000,0.000000,0.000000

empty_weight=32832.000
empty_weight_roll_MOI=260000.000
empty_weight_pitch_MOI=302000.000
empty_weight_yaw_MOI=470000.000
empty_weight_coupled_MOI=1400.000
max_gross_weight=36817.000
CG_forward_limit=0.000
CG_aft_limit=1.000

[fuel]
LeftMain=0.000, -14.500, -5.000, 299.000, 0.000
RightMain=0.000, 14.500, -5.000, 299.000, 0.000
fuel_type=2.000
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area=870.000
wing_span=88.750
wing_root_chord=8.830
wing_dihedral=1.500
wing_incidence=1.500
wing_twist=-1.500
oswald_efficiency_factor=0.800
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=-1.500
wing_pos_apex_vert=-8.0
htail_area=120.000
htail_span=23.917
htail_pos_lon=-36.000
htail_pos_vert=9.000
htail_incidence=0.500
htail_sweep=0.000
vtail_area=150.000
vtail_span=14.000
vtail_sweep=5.000
vtail_pos_lon=-36.000
vtail_pos_vert=9.000
elevator_area=40.000
aileron_area=35.920
rudder_area=69.530
elevator_up_limit=17.502
elevator_down_limit=10.626
aileron_up_limit=15.481
aileron_down_limit=10.897
rudder_limit=23.491
elevator_trim_limit=5.000
spoiler_limit=59.989
spoilerons_available=1
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=10.000
min_flaps_for_spoilerons=0.000

//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)
[contact_points]
point.0=1.000, 35.000, 0.000, -13.3000, 1574.803, 0.100, 0.518, 80.0, 0.150, 3.100, 0.900, 8.000, 8.000, 0.000, 0.000, 0.000
point.1=1.000, -2.0, -7.200, -13.800, 1574.803, 1.000, 0.718, 0.000, 0.283, 1.500, 0.970, 9.000, 9.000, 2.000, 0.000, 0.000
point.2=1.000, -2.0, 7.200, -13.800, 1574.803, 2.000, 0.718, 0.000, 0.283, 1.500, 0.970, 10.000, 10.000, 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, -5.833, 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, -10.833, 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=6.400
gear_system_type=0

[GeneralEngineData]
engine_type=5
Engine.0=5.900, -13.000, -8.000
Engine.1=5.900, 13.000, -8.000
fuel_flow_scalar=1.000
min_throttle_limit=-0.229980

[TurbineEngineData]
fuel_flow_gain=0.015
inlet_area=1.000
rated_N2_rpm=21400.000
static_thrust=195.000
afterburner_available=0

[propeller]
propeller_type=0
propeller_diameter=13.600
propeller_blades=6
propeller_moi=580.000
beta_max=45.000
beta_min=12.000
min_gov_rpm=16000.000
prop_tc=0.0004
gear_reduction_ratio=17.600
fixed_pitch_beta=0.000
low_speed_theory_limit=80.000
prop_sync_available=0
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=00.000
beta_feather=86.000
power_absorbed_cf=0.900
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=1.000
minimum_reverse_beta=-14.000
thrust_scalar=1.208

[turboprop_engine]
maximum_torque=10366.000
power_scalar=1.000
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[Reference Speeds]
flaps_up_stall_speed=102.000
full_flaps_stall_speed=81.600
cruise_speed=304.798
max_indicated_speed=331.195313
max_mach=0.650000

[keyboard_response]
elevator=30.000, 50.000
aileron=60.000, 250.000
rudder=70.000, 100.000

[Views]
eyepoint=30, -1.5, -4.6

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit            
light.0=3, 5.30, -38.98, -1.00,  fx_navred ,
light.1=3, 5.30,  38.98, -1.00,  fx_navgre ,
light.2=3, -37.30,   0.00, -4.00,  fx_navwhi ,
light.3=2, 5.25, -38.98, -1.00,  fx_strobe ,
light.4=2, 5.25,  38.98, -1.00,  fx_strobe ,
light.5=1, -32.50,   0.00, 11.80,  fx_beacon ,
light.6=1, 7.00,   0.00, -12.00,  fx_beacon ,
light.7=4,  15,   0.00, 2,  fx_vclight,
light.8=4,  31.5,   -2.0, -5.5,  fx_vclight,
light.9=4,  31.5,   2.0, -5.5,  fx_vclight,

[General]
performance=Wing span 24.57 m \nOverall length 22.70 m \nTotal height 7.59 m \nMax. T/O weight 18600 kg \nMax. fuel weight 4500 kg \nCruising altitude 2000 - 7600 m \nCapacity payload 5750 kg \nCruising speed 472 km./h \nEngines (2) PW 127E \nMax. Power/Eng. 2400 hp \n 
atc_type=ATR
atc_model=ATR42

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1500.000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000
pitch_takeoff_ga=8.000
vertical_speed_hold_available=1
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[direction_indicators]
direction_indicator.0=3,0

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=0.858
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=0.4
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[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

[Flaps.0]
type=1
span-outboard=0.500
extending-time=10.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=0.200
flaps-position.0=0.000, 0.000
flaps-position.1=9.998, 0.000
flaps-position.2=19.996, 0.000
flaps-position.3=29.994, 0.000
flaps-position.4=39.992, 0.000

[brakes]
toe_brakes_scale=1.969543
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=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
