[fltsim.0]
title=Shorts 360 American Eagle
sim=shorts360
model=
panel=
sound=
texture=AA
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=N381MQ
ui_manufacturer=Shorts
ui_type=360
ui_variation=American Eagle
description=Shorts 360 N381MQ American Eagle-Original Model by Mike Stone-Repaint by Aaron Marsh-nitrain@optonline.net
atc_heavy=0
atc_airline=Eagle Flight
atc_flight_number=001
[General]
atc_type=
atc_model=sh36
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 = 27100.000
empty_weight = 17350.000
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 = 70000.000
empty_weight_roll_MOI = 75000.000
empty_weight_yaw_MOI = 120000.000
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 =1.000
aileron_effectiveness =1.000
rudder_effectiveness =1.000
pitch_stability =2.002
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.503
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 5
Engine.0 = 5.000, -11.000, 3.000
Engine.1 = 5.000, 11.000, 3.000
fuel_flow_scalar = 1.000
min_throttle_limit=-0.250000
[propeller]
thrust_scalar =1.000
propeller_type = 0
propeller_diameter = 11.000
propeller_blades = 5
propeller_moi = 58.000
beta_max = 45.000
beta_min = 15.000
min_gov_rpm = 2000.000
prop_tc = 0.004
gear_reduction_ratio = 18.000
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 = 80.000
power_absorbed_cf = 0.900
defeathering_accumulators_available= 0
prop_reverse_available = 1
minimum_on_ground_beta = 1.000
minimum_reverse_beta = -14.000
[TurbineEngineData]
fuel_flow_gain = 0.011
inlet_area = 2.000
rated_N2_rpm = 29920.000
static_thrust = 100.000
afterburner_available= 0
[turboprop_engine]
power_scalar =1.000
maximum_torque = 4500.000
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, 21.000, 0.000, -7.800, 1500.000, 0.000, 1.000, 40.000, 0.150, 2.500, 0.900, 3.000, 3.000, 0.000, 0.000, 0.000
point.1= 1.000, -2.000, -7.500, -8.400, 1800.000, 1.000, 1.600, 0.000, 0.500, 2.500, 0.800, 3.000, 3.000, 2.000, 0.000, 0.000
point.2= 1.000, -2.000, 7.500, -8.400, 1800.000, 2.000, 1.600, 0.000, 0.500, 2.500, 0.800, 3.000, 3.000, 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 = 8.000
gear_system_type=0
[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, 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, 1.70, -37.45, 6.11, fx_navred ,
light.1 = 3, 1.70, 37.45, 6.11, fx_navgre ,
light.2 = 3, -41.11, 0.00, 3.42, fx_navwhi ,
light.3 = 2, 1.93, -37.34, 6.11, fx_strobe ,
light.4 = 2, 1.93, 37.34, 6.11, fx_strobe ,
light.5 = 1, -10.43, 0.00, -5.48, fx_beacon ,
light.6 = 2, -0.33, 0.00, 5.52, fx_beacon ,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = 0.000, -16.000, 0.000, 288.000, 0.000
LeftAux = 0.000, -6.000, -1.500, 79.500, 0.000
RightMain = 0.000, 16.000, 0.000, 288.000, 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
electric_pump=0
[airplane_geometry]
wing_area = 450.000
wing_span = 75.000
wing_root_chord = 6.000
wing_dihedral = 3.000
wing_incidence = 1.000
wing_twist = -1.000
oswald_efficiency_factor= 0.900
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 2.500
wing_pos_apex_vert = 5.000
htail_area = 143.000
htail_span = 26.000
htail_pos_lon = -36.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 0.000
vtail_area = 110.000
vtail_span = 14.000
vtail_sweep = 25.000
vtail_pos_lon = -33.000
vtail_pos_vert = 4.000
elevator_area = 50.000
aileron_area = 24.000
rudder_area = 26.000
elevator_up_limit = 15.000
elevator_down_limit = 15.000
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 30.000
elevator_trim_limit = 15.000
spoiler_limit = 0.000
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 = 90.000
full_flaps_stall_speed = 75.000
cruise_speed = 216.000
max_indicated_speed=259.000000
max_mach=0.579980
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 0
pitch_takeoff_ga=8.000000
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
[TailHook]
tailhook_length=4
tailhook_position=-15.0, 0.0, -1.0
cable_force_adjust=1
[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= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 30.000, 0.000
[brakes]
toe_brakes_scale=1.000000
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
