[fltsim.0]
title=AIA 737-200 Star Air
sim=aia_737_200
model=no_refl
panel=
sound=
texture=star
atc_id=PK-ALN
atc_airline=Star Air
atc_flight_number=
ui_manufacturer=Boeing
ui_type=737-200
ui_variation=Star Air
description=AI Aardvark 737-200 Star Air registration PK-ALN "Nandina". Repaint by Rinaldi Hanafi 
atc_id_color=0000000000
visual_damage=0

[General]
atc_type=BOEING AIRCRAFT 
atc_model=B732 
editable=1 
visual_damage=1
performance=Only experienced AI pilots should attempt to fly this aircraft. 

[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI

[weight_and_balance]

// ACM V2.0
max_gross_weight = 120000
empty_weight = 100792
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -2, 0, 0
empty_weight_pitch_MOI = 8072439
empty_weight_roll_MOI = 2262183
empty_weight_yaw_MOI = 3337024
empty_weight_coupled_MOI = 0
max_number_of_stations = 2

station_load.0 = 0, 22.98, 0, 3.00
station_load.1 = 10000, 43.55, 0, 1.63


[lights]

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

light.0 = 3, -14.46, -46.48, 3.5, fx_navred
light.1 = 3, -14.46, 46.48, 3.5, fx_navgre
light.2 = 2, -14.20, -46.37, 3.5, fx_strobe
light.3 = 2, -14.2, 46.37, 3.5, fx_strobe
light.4 = 2, 9.58, 0, -3.18, fx_beacon
light.5 = 1, 4.7, 0, 9.89, fx_beacon
light.6 = 3, -19.05, 46.76, 3.5, fx_navwhi
light.7 = 3, -19.05, -46.76, 3.5, fx_navwhi
light.8 = 3, -52.80, 0, 7.32, fx_navwhi

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.000
engine.0 = 4.750, -16.100, -2.500
engine.1 = 4.750, 16.100, -2.500

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

[fuel]

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

fuel_type = 2
number_of_tank_selectors = 1

Center1 = 0, 0, 0, 2313, 0
LeftMain = -3, -19, 0, 1500, 0
RightMain = -3, 19, 0, 1500, 0


[contact_points]
static_pitch = -0.5
static_cg_height = 6.9
max_number_of_points = 7

point.0 = 1, 42.6512, 0, -6.6816, 5000, 0, 1.2, 55.92, 0.3, 2.5, 0.9, 4, 4, 0, 0, 0
point.1 = 1, -8.3593, -8.9561, -7.6262, 5000, 1, 1.442, 0, 1, 2.5, 0.9, 6.9, 6.9, 2, 0, 0
point.2 = 1, -8.3593, 8.9561, -7.6262, 5000, 2, 1.442, 0, 1, 2.5, 0.9, 7.1, 7.1, 3, 0, 0
point.3 = 2.000, -14.170, -47.330, 3.578, 787.400, 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, -14.170, 47.330, 3.578, 787.400, 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, 44.6712, 0, 1.7802, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.6 = 2, -51.7798, 0, 4.7323, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 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 = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
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

[airplane_geometry]
//ACM_AREAW1// 0,0,0,5.4864,1.6044,1.6044,0.7480,5.9601,3.2088,3.2088
//ACM_AREAW2// 1.4960,6.4340,4.8133,4.8133,2.2444,6.9078,6.4176,6.4176,2.9925,7.3817
//ACM_AREAW3// 8.0221,8.0221,3.7407,7.8555,9.6266,9.6266,4.4889,8.3294,11.2306,11.2306
//ACM_AREAW4// 5.2371,8.8030,12.8353,12.8353,5.9850,9.2770,14.4399,14.4399,6.7333,9.7509
//ACM_AREAH1// 0,0,0,4.2367,0.7059,0.7059,0.4074,4.4324,1.4119,1.4119
//ACM_AREAH2// 0.8151,4.6283,2.1182,2.1182,1.2230,4.8242,2.8243,2.8243,1.6303,5.0198
//ACM_AREAH3// 3.5306,3.5306,2.0383,5.2157,4.2367,4.2367,2.4460,5.4116,4.9428,4.9428
//ACM_AREAH4// 2.8536,5.6076,5.6489,5.6489,3.2613,5.8034,6.3550,6.3550,3.6691,5.9993
//ACM_AREAV1// 0,0,0,6.0960,0.6772,0.6772,0.4742,6.0823,1.3545,1.3545
//ACM_AREAV2// 0.9484,6.0689,2.0320,2.0320,1.4227,6.0556,2.7093,2.7093,1.8969,6.0423
//ACM_AREAV3// 3.3866,3.3866,2.3712,6.0289,4.0640,4.0640,2.8454,6.0155,4.7413,4.7413
//ACM_AREAV4// 3.3199,6.0019,5.4186,5.4186,3.7941,5.9885,6.0960,6.0960,4.2684,5.9752
//ACM_CAREAW1// 7.2199,7.2199,6.1097,7.2069,8.0221,8.0221,6.4839,7.5264,8.8240,8.8240
//ACM_CAREAW2// 6.8579,7.8456,9.6266,9.6266,7.2321,8.1646,10.4287,10.4287,7.6062,8.4840
//ACM_CAREAW3// 11.2306,11.2306,7.9801,8.8030,12.0332,12.0332,8.3542,9.1224,12.8353,12.8353
//ACM_CAREAW4// 8.7284,9.4413,13.6372,13.6372,9.1021,9.7608,14.4399,14.4399,9.4764,10.0801
//ACM_CAREAH1// 0,0,2.1182,4.2367,0.7059,0.7059,2.5260,4.5384,1.4119,1.4119
//ACM_CAREAH2// 2.9337,4.8400,2.1182,2.1182,3.3413,5.1420,2.8243,2.8243,3.7490,5.4436
//ACM_CAREAH3// 3.5306,3.5306,4.1567,5.7455,4.2367,4.2367,4.5644,6.0472,4.9428,4.9428
//ACM_CAREAH4// 4.9720,6.3488,5.6489,5.6489,5.3797,6.6508,6.3550,6.3550,5.7873,6.9524
//ACM_CAREAV1// 0,0,1.5240,4.5720,0.6772,0.6772,1.9982,4.8024,1.3545,1.3545
//ACM_CAREAV2// 2.4725,5.0328,2.0320,2.0320,2.9467,5.2631,2.7093,2.7093,3.4210,5.4937
//ACM_CAREAV3// 3.3866,3.3866,3.8952,5.7241,4.0640,4.0640,4.3695,5.9545,4.7413,4.7413
//ACM_CAREAV4// 4.8439,6.1848,5.4186,5.4186,5.3179,6.4154,6.0960,6.0960,5.7923,6.6458
wing_area = 1137.000
wing_span = 94.750
wing_root_chord = 18.000
wing_dihedral = 6.200
wing_incidence = 1.000
wing_twist = -0.500
oswald_efficiency_factor = 0.750
wing_winglets_flag = 0
wing_sweep = 25.000
wing_pos_apex_lon = 8.000
wing_pos_apex_vert = 0.000
htail_area = 338.000
htail_span = 41.700
htail_pos_lon = -35.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 30.000
vtail_area = 224.000
vtail_span = 20.000
vtail_sweep = 35.000
vtail_pos_lon = -35.800
vtail_pos_vert = 5.800
elevator_area = 70.500
aileron_area = 26.900
rudder_area = 56.200
elevator_up_limit = 22.500
elevator_down_limit = 19.500
aileron_up_limit = 20.000
aileron_down_limit = 20.000
rudder_limit = 26.000
elevator_trim_limit = 20.000
spoiler_limit = 60.000
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 1

[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, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 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=.950 
parasite_drag_scalar=0.550 
induced_drag_scalar=0.550 
elevator_effectiveness=1.000 
aileron_effectiveness=1.000 
rudder_effectiveness=1.000 
pitch_stability=1.000 
roll_stability=1.000 
yaw_stability=1.000 
elevator_trim_effectiveness=1.000 
aileron_trim_effectiveness=1.000 
rudder_trim_effectiveness=1.000 

[TurbineEngineData]
fuel_flow_gain=0.002 
inlet_area=19.600 
rated_N2_rpm=29920.000 
static_thrust=24000.000 
afterburner_available=0 
reverser_available=1 

[jet_engine]
thrust_scalar=1.00 

[Views]
eyepoint=43.7, -1.31, 3.55   //(feet) longitudinal, lateral, vertical distance from reference datum

[Radios]
// Radio Type=availiable, 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 

[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 

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800 
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8 ;

[Reference Speeds]
flaps_up_stall_speed=142.000 
full_flaps_stall_speed=113.000 
cruise_speed=477.000 

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 20.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.50
drag_scalar= 1.100
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 5.000, 0.000
flaps-position.4= 10.000, 0.000
flaps-position.5= 15.000, 0.000
flaps-position.6= 25.000, 0.000
flaps-position.7= 30.000, 0.000
flaps-position.8= 40.000, 0.000

[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 2.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 0.000, 0.000
flaps-position.3= 0.500, 0.000
flaps-position.4= 1.000, 0.000

[Flaps.2]
type= 2
span-outboard= 0.800
extending-time= 3.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.500, 0.000
flaps-position.2= 1.000, 0.000