[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 V2.3 max_gross_weight = 150000 empty_weight = 74170 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 4, 0, 0 empty_weight_pitch_MOI = 2572439 empty_weight_roll_MOI = 2262183 empty_weight_yaw_MOI = 3337024 empty_weight_coupled_MOI = 0 max_number_of_stations = 9 station_load.0 = "170.0, 41.0, -1.5, 0.0, Pilot" station_load.1 = "170.0, 41.0, 1.5, 0.0, Co-Pilot" station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" station_load.3 = "1360.0, 25.5, 0.0, 0.0, First Class" station_load.4 = "8160.0, 11.0, 0.0, 0.0, Coach 3-10" station_load.5 = "8160.0, -10.0, 0.0, 0.0, Coach 11-18" station_load.6 = "7140.0, -30.5, 0.0, 0.0, Coach 19-25" station_load.7 = "10000.0, 20.5, 0.0, 0.0, Forward Baggage" station_load.8 = "4000.0, -27.5, 0.0, 0.0, Aft Baggage" [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 = 3, 8.55, 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 engine.0 = 4.75, -16.1, -4.5 engine.1 = 4.75, 16.1, -4.5 min_throttle_limit=-0.550000 max_contrail_temperature=-30 [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 electric_pump=0 [contact_points] static_pitch = -0.6 static_cg_height = 7 max_number_of_points = 7 point.0 = 1, 39, 0, -6.7365, 1181.1, 0, 1.442, 55.92, 0.3, 2.5, 0.5, 4, 4, 0, 220, 250 point.1 = 1, -7.1286, -10, -7.899, 1574.8, 1, 1.442, 0, 1, 2.5, 0.9, 6.9, 6.9, 2, 220, 250 point.2 = 1, -7.1286, 10, -7.899, 1574.8, 2, 1.442, 0, 1, 2.5, 0.9, 7.1, 7.1, 3, 220, 250 point.3 = 2, -14.17, -47.33, 4, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -14.17, 47.33, 4, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -52.1668, 0, 5.187, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 43.9872, 0, 0.7861, 787.4, 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 = 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// 0,0,0,6.4583,1.6044,1.6044,0.8891,7.0247,3.2088,3.2088 //ACM_AREAW2// 1.7783,7.5911,4.8133,4.8133,2.6679,8.1576,6.4176,6.4176,3.5573,8.7241 //ACM_AREAW3// 8.0221,8.0221,4.4467,9.2903,9.6266,9.6266,5.3361,9.8570,11.2306,11.2306 //ACM_AREAW4// 6.2252,10.4231,12.8353,12.8353,7.1146,10.9898,14.4399,14.4399,8.0038,11.5563 //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// 0,0,0,6.5012,0.7221,0.7221,0.6061,6.5872,1.4447,1.4447 //ACM_AREAV2// 1.2122,6.6732,2.1670,2.1670,1.8184,6.7593,2.8894,2.8894,2.4244,6.8453 //ACM_AREAV3// 3.6117,3.6117,3.0306,6.9313,4.3340,4.3340,3.6368,7.0173,5.0566,5.0566 //ACM_AREAV4// 4.2430,7.1036,5.7789,5.7789,4.8491,7.1894,6.5012,6.5012,5.4552,7.2754 //ACM_CAREAW1// 7.2199,7.2199,7.2312,8.5228,8.0221,8.0221,7.6757,8.9027,8.8240,8.8240 //ACM_CAREAW2// 8.1204,9.2831,9.6266,9.6266,8.5649,9.6632,10.4287,10.4287,9.0100,10.0431 //ACM_CAREAW3// 11.2306,11.2306,9.4546,10.4231,12.0332,12.0332,9.8992,10.8035,12.8353,12.8353 //ACM_CAREAW4// 10.3437,11.1836,13.6372,13.6372,10.7887,11.5635,14.4399,14.4399,11.2333,11.9434 //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// 0,0,1.6253,4.8758,0.7221,0.7221,2.2314,5.2220,1.4447,1.4447 //ACM_CAREAV2// 2.8375,5.5682,2.1670,2.1670,3.4437,5.9141,2.8894,2.8894,4.0499,6.2603 //ACM_CAREAV3// 3.6117,3.6117,4.6560,6.6064,4.3340,4.3340,5.2621,6.9524,5.0566,5.0566 //ACM_CAREAV4// 5.8681,7.2986,5.7789,5.7789,6.4745,7.6447,6.5012,6.5012,7.0805,7.9906 wing_area = 1856 wing_span = 94.75 wing_root_chord = 21.18 wing_dihedral = 6.19 wing_incidence = 1.0 wing_twist = -0.5 oswald_efficiency_factor = 0.75 wing_winglets_flag = 0 wing_sweep = 29 wing_pos_apex_lon = 13.23 wing_pos_apex_vert = 0 htail_area = 338.0 htail_span = 41.70 htail_pos_lon = -42.97 htail_pos_vert = 0 htail_incidence = 0.0 htail_sweep = 30 vtail_area = 291 vtail_span = 21.33 vtail_sweep = 40 vtail_pos_lon = -35.02 vtail_pos_vert = 8.08 elevator_area = 70.5 aileron_area = 26.9 rudder_area = 56.2 elevator_up_limit = 22.5 elevator_down_limit = 19.5 aileron_up_limit = 20.0 aileron_down_limit = 20.0 rudder_limit = 26.0 elevator_trim_limit = 20.0 spoiler_limit = 60.0 aileron_to_spoileron_gain = 3 min_ailerons_for_spoilerons = 10 min_flaps_for_spoilerons = 0 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, 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=1.2 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 [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=19.6 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=23500 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=1.0 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 5.0 //Flap angle that activates warning at idle flap_limit_power = 25.5 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.2 //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=43.7, -1.31, 3.7 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] //Trailing Edge Flaps type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 20 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 1 // degrees flaps-position.2 = 2 // degrees flaps-position.3 = 5 // degrees flaps-position.4 = 10 // degrees flaps-position.5 = 15 // degrees flaps-position.6 = 25 // degrees flaps-position.7 = 30 // degrees flaps-position.8 = 40 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.1 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.1] //Inboard Leading Edge Flaps type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 2 // seconds flaps-position.0 = 0 // flaps-position.4 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.1 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.2] //Outboard Leading Edge Slat type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 3 // seconds flaps-position.0 = 0 // flaps-position.3 = 0.5 // flaps-position.4 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.1 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [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 [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=0,0 [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 ; 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=12.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=25.0 gs_integrator_control=0.53 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [Reference Speeds] flaps_up_stall_speed=122.0 //Knots True (KTAS) full_flaps_stall_speed=113.0 //Knots True (KTAS) cruise_speed=477.0 //Knots True (KTAS) max_mach = 0.87 max_indicated_speed = 340 //Red line (KIAS) [stall_warning] type=2 [fltsim.0] title=AAV B732 AeroGal sim=aia_737_200 model= panel= sound= texture=AeroGal atc_id= atc_airline=AeroGal atc_flight_number=557 ui_manufacturer=AI Aardvark ui_type=Boeing 737-200 ui_variation=AeroGal description=AI Aardvark 737-200 atc_id_color=0000000000 visual_damage=0
