[fltsim.0] title=Aerolineas Argentinas Boeing 737-200 sim=aia_737_200 model=reflective panel= sound= texture=ala atc_id=LV-ZSD atc_airline=Aerolineas Argentinas atc_flight_number=1138 ui_manufacturer=AI Planes ui_type=737-200 ui_variation=Aerolinea Argentinas description=AI Aardvark 737-200. Repaint by Rich Rodriguez (smylz@graphic-designer.com) atc_id_color=0000000000 visual_damage=0 [General] atc_type=BOEING 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