[fltsim.0]
title=ATR 72 American Eagle
sim=atr72
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=N431AT
ui_manufacturer=ATR
ui_type=ATR 72
ui_variation=American Eagle
description=ATR 72-500
atc_heavy=0
atc_airline=Eagle Flight
atc_flight_number=651
[General]
atc_type=AEROSPATIALE
atc_model=AT72
editable=1
performance=Max Cruise Speed\t315 kts\nMaximum Range\t1,894 nm\nService Ceiling\t35,000 ft\nMax Gross Weight\t15,000 lb\nSeating\t\tUp to 11\nUseful Load\t5,810 lb\n
[WEIGHT_AND_BALANCE]
max_gross_weight = 48500.000
empty_weight = 28550.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations =50
;Moments of Inertia
empty_weight_pitch_MOI = 720000.000
empty_weight_roll_MOI = 220000.000
empty_weight_yaw_MOI = 460000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0=0.000000,0.000000,0.000000,0.000000
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =0.751
aileron_effectiveness =1.000
rudder_effectiveness =1.000
pitch_stability =2.001
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.508
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 5
Engine.0 = -8.300, -4.800, 0.500
Engine.1 = -8.300, 4.800, 0.500
fuel_flow_scalar = 1.000
[propeller]
thrust_scalar =1.000
propeller_type = 0
propeller_diameter = 11.000
propeller_blades = 6
propeller_moi = 68.000
beta_max = 45.000
beta_min = 15.200
min_gov_rpm = 4000.000
prop_tc = 0.004
gear_reduction_ratio = 17.600
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 = 79.300
power_absorbed_cf = 0.900
defeathering_accumulators_available= 0
prop_reverse_available = 1
minimum_on_ground_beta = 1.000
minimum_reverse_beta = -14.000
[TurbineEngineData]
fuel_flow_gain = 0.011
inlet_area = 1.000
rated_N2_rpm = 29920.000
static_thrust = 450.000
afterburner_available= 0
[turboprop_engine]
power_scalar =1.000
maximum_torque = 9000.000
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
[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
//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, 33.500, 0.000, -6.300, 1181.000, 0.000, 0.596, 40.000, 0.150, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000
point.1= 1.000, -2.000, -6.500, -7.200, 1574.000, 1.000, 0.596, 0.000, 0.400, 2.500, 0.800, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, -2.000, 6.500, -7.200, 1574.000, 2.000, 0.596, 0.000, 0.400, 2.500, 0.800, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -3.330, -23.920, -3.000, 787.000, 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, -3.330, 23.920, -3.000, 787.000, 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, -22.670, 0.000, 0.000, 787.000, 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, 23.080, 0.000, -1.500, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = -1.000
static_cg_height = 6.800
[Views]
eyepoint = 32.85, -1.58, 2.23
[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 = 3, 1.16, -43.66, 5.07, fx_navred ,
light.1 = 3, 1.16, 43.66, 5.07, fx_navgre ,
light.2 = 3, -49.72, 0.00, 2.18, fx_navwhi ,
light.3 = 2, 1.46, -43.56, 5.07, fx_strobe ,
light.4 = 2, 1.46, 43.56, 5.07, fx_strobe ,
light.5 = 1, -45.30, 0.00, 17.71, fx_beacon ,
light.6 = 2, 0.59, 0.00, -5.03, fx_beacon ,
light.7 = 4, 32.71, 0.00, 2.96, fx_vclight,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = 0.000, -20.000, 4.000, 800.000, 0.000
LeftAux = 0.000, -6.000, -1.500, 79.500, 0.000
RightMain = 0.000, 20.000, 4.000, 800.000, 0.000
RightAux = 0.000, 6.000, -1.500, 79.500, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
[airplane_geometry]
wing_area = 656.000
wing_span = 88.000
wing_root_chord = 10.000
wing_dihedral = 0.000
wing_incidence = 0.000
wing_twist = -1.000
oswald_efficiency_factor= 0.800
wing_winglets_flag = 0
wing_sweep = 1.000
wing_pos_apex_lon = 1.000
wing_pos_apex_vert = 5.000
htail_area = 108.000
htail_span = 24.000
htail_pos_lon = -45.000
htail_pos_vert = 15.000
htail_incidence = 0.000
htail_sweep = 5.000
vtail_area = 140.000
vtail_span = 14.000
vtail_sweep = 30.000
vtail_pos_lon = -42.000
vtail_pos_vert = 4.000
elevator_area = 36.000
aileron_area = 23.000
rudder_area = 49.000
elevator_up_limit = 17.000
elevator_down_limit = 15.500
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 30.000
elevator_trim_limit = 15.000
spoiler_limit = 60.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 120.000
full_flaps_stall_speed = 100.000
cruise_speed = 490.000
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
autothrottle_available= 1
pitch_takeoff_ga=8.000000
autothrottle_arming_required=1
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode
use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode
[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
[Flaps.0]
type= 1
span-outboard= 0.300
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 0.500
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 40.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.300
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 0.500
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 20.000, 0.000
flaps-position.2= 40.000, 0.000
