[fltsim.0] title=AIA 737-500 CAF sim=aia_737_500 model=no_refl panel= sound= texture=caf checkklists=chk-ref-notes\Boeing_737-500_check kb-checklists=_check kb_reference=_ref kb_notes=_notes atc_id_enable=1 atc_heavy=0 atc_id=157735 atc_airline= atc_flight_number=1 ui_manufacturer=Boeing ui_type=B737-500 ui_variation=CAF 157735 description=Note: For specific aircraft flight instructions, a description, and a history refer to the "Notes" tab of the aircraft's kneeboard. atc_id_color=0000000000 visual_damage=0 [General] atc_type=BOEING atc_model=B735 editable=1 visual_damage=1 performance=Note: For performance and technical data refer to the "Reference" and "Checklist" tabs of the aircraft's kneeboard. [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [weight_and_balance] // ACM V1.0 pl4 max_gross_weight = 120000 empty_weight = 100792 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 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 =50 station_load.0 =0.000000,0.000000,0.000000,0.000000 [flight_tuning] cruise_lift_scalar=.50 parasite_drag_scalar=0.550 induced_drag_scalar=0.550 elevator_effectiveness=1.000 aileron_effectiveness=0.950 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 [GeneralEngineData] engine_type=1 Engine.0=4.750, -16.100, -2.500 Engine.1=4.750, 16.100, -2.500 fuel_flow_scalar=1.000 [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 19.600 rated_N2_rpm= 29920.000 static_thrust= 19000.000 afterburner_available= 0 reverser_available= 1 [jet_engine] thrust_scalar=1.00 [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] static_pitch = -0.5 static_cg_height = 6.9 max_number_of_points = 7 point.0 = 1, 31.6512, 0, -6.6816, 3000, 0, 1.2, 55.92, 0.1, 2.5, 0.9, 4, 4, 0, 0, 0 point.1 = 1, -8.3593, -8.9561, -7.8262, 3000, 1, 1.442, 0, 1, 2.5, 0.9, 6.9, 6.9, 2, 0, 0 point.2 = 1, -8.3591, 8.9561, -7.8262, 3000, 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 [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 [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 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [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 ; [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 [airplane_geometry] 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 spoilerons_available=1 aileron_to_spoileron_gain=3.000 min_ailerons_for_spoilerons=10.000 min_flaps_for_spoilerons=0.000 [Reference Speeds] flaps_up_stall_speed=142.000 full_flaps_stall_speed=113.000 cruise_speed=477.000 [forcefeedback] 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=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 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 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -14.38, -47.67, 3.5, fx_navredm light.1 = 3, -14.38, 47.67, 3.5, fx_navgrem light.2 = 2, -14.06, -47.67, 3.5, fx_strobeh light.3 = 2, -14.06, 47.67, 3.5, fx_strobeh light.4 = 2, 9.58, 0, -3.18, fx_beaconb light.5 = 1, 4.70, 0, 9.89, fx_beaconh light.6 = 3, -18.29, 47.67, 3.5, fx_navwhih light.7 = 3, -18.29, -47.67, 3.5, fx_navwhih light.8 = 3, -52.80, 0, 7.32, fx_navwhi [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= 1.000 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= 1.000 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= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.500, 0.000 flaps-position.2= 1.000, 0.000