//aia FS9 update

[fltsim.0]
title=AIA EMB120 Air Moldova NC 
sim=aia_emb_120
model=reflective
panel=
sound=
texture=MLD-Air Moldova Emb120 AIR MOLDOVA
kb_checklists=
kb_reference=
atc_id=N71GL
atc_airline=AIR MOLDOVA
atc_flight_number=899
ui_manufacturer=AI Aardvark
ui_type=Embraer EMB-120
ui_variation=AIR MOLDOVA
description=AI Aardvark EMB-120 
atc_id_color=0000000000
visual_damage=0
atc_parking_codes=MLD
atc_parking_types=RAMP,GATE


[General]
atc_type=EMBRAER 
atc_model=E120 
editable=0 
performance="Cruise Speed\t\n315 kts            363 mph          583 km\/h\n\nEngines\t\nPratt & Whitney PT6A-60A    1,050 shp\n\nMaximum Range\t\n1,765 nm          2,031 m\t   3,269 km\n\nService Ceiling\t\n35,000 ft         10,668 m\n\nFuel Capacity\t\n539 U.S. gal      2,040 L\n\nMaximum Takeoff Weight \n15,000 lb\t          6,818 kg\n\nLength\t\n46.7 ft\t           14.23 m\n\nWingspan\t\n57.9 ft\t           17.65 m\n\nHeight\t\n14.3 ft\t           4.36 m\n\nSeating\t\nUp to 11\n\nUseful Load\t\n5,910 lb\t           2,681 kg" 

[weight_and_balance]

// ACM V2.3
max_gross_weight = 15000
empty_weight = 9090
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 3, 0, -.5
empty_weight_pitch_MOI = 50000
empty_weight_roll_MOI = 36200
empty_weight_yaw_MOI = 36500
empty_weight_coupled_MOI = 0
max_number_of_stations = 6

station_load.0 = 0, 10.4, -2, 0
station_load.1 = "170,  5.0,  2.0, 0.0, Co-Pilot"
station_load.2 = "170, -2.1, -2.0, 0.0, Passenger"
station_load.3 = "170, -2.1,  2.0, 0.0, Passenger"
station_load.4 = "170, -5.3, -2.0, 0.0, Passenger"
station_load.5 = "170, -5.3,  2.0, 0.0, Passenger"


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2.7, -31.48, 2.48, fx_navred
light.1 = 3, 2.70, 31.48, 2.48, fx_navgre
light.2 = 3, -34.67, 0.01, 14.01, fx_navwhi
light.3 = 2, 2.86, -31.29, 2.46, fx_strobe
light.4 = 2, 2.86, 31.29, 2.46, fx_strobe
light.5 = 1, -0.03, 0.01, 6.27, fx_beacon
light.6 = 1, 2.98, 0, -1.91, fx_beacon

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.0
engine.0 = 5.77, -10.81, 1.19, 
engine.1 = 5.77, 10.81, 1.19, 
min_throttle_limit=-0.150000

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

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1

LeftMain = 0, -14.5, -1, 190, 0
LeftAux = 0, -6, -1.5, 79.5, 0
RightMain = 0, 14.5, -1, 190, 0
RightAux = 0, 6, -1.5, 79.5, 0
electric_pump=0


[contact_points]
static_pitch = -0.6
static_cg_height = 5.35
max_number_of_points = 7

point.0 = 1, 25.6686, 0, -5.3755, 1181, 0, 0.596, 39.9, 0.296, 2.5, 0.9516, 4.8, 4.8, 0, 184, 184
point.1 = 1, -0.6458, -11, -5.6547, 1574, 1, 0.596, 0, 0.3, 2.5, 0.8152, 4.5, 5.2, 2, 184, 184
point.2 = 1, -0.6458, 11, -5.6547, 1574, 2, 0.596, 0, 0.3, 2.5, 0.8152, 4.8, 4.9, 3, 184, 184
point.3 = 2, -0.6559, -32.4787, 2.4014, 787, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -0.6559, 32.4787, 2.4014, 787, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -30.1391, 0, 3.9616, 787, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 29.9752, 0, -0.3843, 787, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
gear_system_type=0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0,0,0,1.6459,0.9685,0.9685,0.0168,1.5805,1.9371,1.9371
//ACM_AREAW2// 0.0337,1.5151,2.9056,2.9056,0.0507,1.4496,3.8743,3.8743,0.0675,1.3842
//ACM_AREAW3// 4.8428,4.8428,0.0844,1.3188,5.8115,5.8115,0.1014,1.2534,6.7800,6.7800
//ACM_AREAW4// 0.1182,1.1880,7.7486,7.7486,0.1351,1.1227,8.7172,8.7172,0.1520,1.0573
//ACM_AREAH1// 0,0,0,1.7474,0.2912,0.2912,0.1059,1.7661,0.5824,0.5824
//ACM_AREAH2// 0.2119,1.7847,0.8737,0.8737,0.3179,1.8034,1.1649,1.1649,0.4239,1.8220
//ACM_AREAH3// 1.4562,1.4562,0.5299,1.8406,1.7474,1.7474,0.6359,1.8593,2.0387,2.0387
//ACM_AREAH4// 0.7419,1.8779,2.3299,2.3299,0.8479,1.8964,2.6212,2.6212,0.9539,1.9151
//ACM_AREAV1// 0,0,0,2.2555,0.2506,0.2506,0.2101,2.2853,0.5012,0.5012
//ACM_AREAV2// 0.4205,2.3152,0.7518,0.7518,0.6308,2.3450,1.0024,1.0024,0.8410,2.3749
//ACM_AREAV3// 1.2530,1.2530,1.0513,2.4047,1.5036,1.5036,1.2617,2.4346,1.7541,1.7541
//ACM_AREAV4// 1.4720,2.4644,2.0048,2.0048,1.6822,2.4942,2.2555,2.2555,1.8926,2.5241
//ACM_CAREAW1// 4.3586,4.3586,0.8989,1.2281,4.8428,4.8428,0.9074,1.2201,5.3271,5.3271
//ACM_CAREAW2// 0.9158,1.2122,5.8115,5.8115,0.9243,1.2042,6.2958,6.2958,0.9327,1.1962
//ACM_CAREAW3// 6.7800,6.7800,0.9412,1.1880,7.2644,7.2644,0.9496,1.1800,7.7486,7.7486
//ACM_CAREAW4// 0.9581,1.1720,8.2328,8.2328,0.9666,1.1641,8.7172,8.7172,0.9750,1.1561
//ACM_CAREAH1// 0,0,0.8737,1.7474,0.2912,0.2912,0.9797,1.8098,0.5824,0.5824
//ACM_CAREAH2// 1.0857,1.8720,0.8737,0.8737,1.1916,1.9343,1.1649,1.1649,1.2977,1.9967
//ACM_CAREAH3// 1.4562,1.4562,1.4036,2.0590,1.7474,1.7474,1.5097,2.1214,2.0387,2.0387
//ACM_CAREAH4// 1.6158,2.1837,2.3299,2.3299,1.7217,2.2460,2.6212,2.6212,1.8278,2.3083
//ACM_CAREAV1// 0,0,0.5637,1.6915,0.2506,0.2506,0.7741,1.8116,0.5012,0.5012
//ACM_CAREAV2// 0.9843,1.9316,0.7518,0.7518,1.1947,2.0518,1.0024,1.0024,1.4049,2.1719
//ACM_CAREAV3// 1.2530,1.2530,1.6153,2.2918,1.5036,1.5036,1.8256,2.4119,1.7541,1.7541
//ACM_CAREAV4// 2.0359,2.5320,2.0048,2.0048,2.2460,2.6521,2.2555,2.2555,2.4563,2.7722
wing_area = 310.0
wing_span = 57.2
wing_root_chord = 5.4
wing_dihedral = 6.0
wing_incidence = 1.0
wing_twist = -1.5
oswald_efficiency_factor = 0.7
wing_winglets_flag = 1
wing_sweep = 1.0
wing_pos_apex_lon = 2.1
wing_pos_apex_vert = 0.0
htail_area = 67.0
htail_span = 17.2
htail_pos_lon = -22.6
htail_pos_vert = 0.0
htail_incidence = 0.5
htail_sweep = 20.0
vtail_area = 42.0
vtail_span = 7.4
vtail_sweep = 40.0
vtail_pos_lon = -20.5
vtail_pos_vert = 4.1
elevator_area = 17.0
aileron_area = 13.5
rudder_area = 7.3
elevator_up_limit = 17.0
elevator_down_limit = 15.5
aileron_up_limit = 18.0
aileron_down_limit = 18.0
rudder_limit = 30.0
elevator_trim_limit = 15.0
spoiler_limit = 60.0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17

[flight_tuning]
cruise_lift_scalar=.8 
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 

[propeller]
thrust_scalar=1.0                   //Propeller thrust scalar
propeller_type=0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=8.8                   //Propeller Diameter, (feet)
propeller_blades=4                     //Number of propeller blades
propeller_moi=24                    //Propeller moment of inertia
beta_max=45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15.2                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520                 //Miminum governed RPM
prop_tc=0.004                 //Prop time-constant
gear_reduction_ratio=17.6                  //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=79.3                  //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=1.0                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0                 //Minimum pitch angle in reverse, (degrees)

[TurbineEngineData]
fuel_flow_gain=0.011                 //Gain on fuel flow
inlet_area=1.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                 //RPM, second stage compressor rated value
static_thrust=158                   //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar=1.0                   //Scalar on Turboprop power
maximum_torque=3270                  //Maximum torque available (ft-lbs)

[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 = 0.5  //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 

[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 5                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 20                                   // degrees
flaps-position.2 = 40                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS

[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 

[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
[Reference Speeds]
flaps_up_stall_speed=106.0                  //Knots True (KTAS)
full_flaps_stall_speed=96.8                  //Knots True (KTAS)
cruise_speed=300.0                 //Knots True (KTAS)
max_mach                = 0.58
max_indicated_speed     = 263                   //Red line (KIAS)

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800.0 
autothrottle_available=0 
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

[stall_warning]
type=2