[fltsim.0] title=Boeing 737-200 Vaspex sim=cf732v2004 model= panel= sound= texture=vaspex kb_checklists=Boeing737-400_check kb_reference=Boeing737-400_ref atc_type=Boeing atc_id_enable=1 atc_id=PP-SMB atc_id_color=0xffffffff editable=0 visual_damage=1 ui_manufacturer=Boeing ui_type=737-200 ui_variation=Vaspex description="The Boeing 737-200 is the most successful commercial jet airliner ever built. A total of 1,114 were built between 1967 and 1988\n2x JT8D-17R's at 16,400 lbs thrust\nFS2004 FDE v1.00 for FFX\/SGA Models\n Copyright: March 2004 Charles Fox" - Boeing 737-200 FAB painted by Martoni. atc_airline=Vaspex [General] atc_type=BOEING atc_model=B732 editable=0 performance="Cruise Speed \n440 kts 507 mph 907 km\/h\n\nEngines \nJT8D-17A\n\nMaximum Range \n1,950 nm 2,2900 mi 3,660 km\n\nService Ceiling \n37, 000 ft 11,000 m\n\nFuel Capacity \n5,160 U.S. gal 19,505 L\n\nEmpty Weight-Standard \n65,431 lb 29,740 kg\n\nMaximum Gross Weight\n95,000 lb 43,180 kg\n\nLength \n93 ft 36.45 m\n\nWingspan \n94 ft, 9 in 25.9 m\n\nHeight \n37 ft 11.23 m\n\nSeating \nSeats 107 to 118\n\nCargo Capacity \n1,373 ft3 38.93 m3\n\n" [pitot_static] vertical_speed_time_constant=50 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] max_gross_weight=117500 // (pounds) empty_weight=95000 // (pounds) reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=3.826, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0="170.0, 41.0, -1.5, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1="170.0, 41.0, 1.5, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2="0.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3="0.0, 25.5, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4="0.0, 11.0, 0.0, 0.0, Coach 3-10" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5="0.0, -10.0, 0.0, 0.0, Coach 11-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6="0.0, -30.5, 0.0, 0.0, Coach 19-25" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7="0.0, 20.5, 0.0, 0.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8="0.0, -27.5, 0.0, 0.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=2329283 empty_weight_roll_MOI=2940012 empty_weight_yaw_MOI=2429385 empty_weight_coupled_MOI=0 [flight_tuning] cruise_lift_scalar=1.0000 parasite_drag_scalar=0.7519 induced_drag_scalar=0.8231 elevator_effectiveness=1.0000 aileron_effectiveness=1.0000 rudder_effectiveness=1.0000 pitch_stability=0.8000 roll_stability=1.0000 yaw_stability=1.0000 elevator_trim_effectiveness=1.0000 aileron_trim_effectiveness=1.0000 rudder_trim_effectiveness=1.0000 [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-9.858,-16.242,-8.107 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-9.858, 16.242,-8.107 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=2.1508 //Scalar for fuel flow efficiency min_throttle_limit=-0.989868 //Minimum percent throttle. Generally negative for turbine reverser max_contrail_temperature=-30 //Temperature (deg C) below which contrails may appear [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=9.852 //Square Feet, engine nacelle inlet area rated_N2_rpm=26500 //RPM, second stage compressor rated value static_thrust=16500 //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 [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, 5, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 2, 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) point.0=1, 36.48, 0.00,-8.05, 1181.10, 0, 2.25, 78.0, 0.50, 1.00, 0.75, 6.00, 6.00, 0, 000, 280 //nose gear point.1=1, 0.85, -8.95,-9.70, 1574.80, 1, 3.33, 0.0, 1.00, 2.50, 0.75, 6.00, 6.00, 2, 000, 280 //left gear point.2=1, 0.85, 8.95,-9.70, 1574.80, 2, 3.33, 0.0, 1.00, 2.50, 0.75, 6.00, 6.00, 3, 000, 280 //right gear point.3=2,-11.00,-48.50, 1.90, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5, 000, 000 //left wing point.4=2,-11.00, 48.50, 1.90, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 6. 000, 000 //right wing point.5=2,-52.00, 0.00, 7.25, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 9. 000, 000 //tail (set for hstab tips which extend beyond fslge) point.6=2, 53.25, 0.00, 1.25, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4. 000, 000 //nose point.7=2,-32.00, 0.00,-0.50, 1574.80, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 000, 000 //aft fuselage scrape max_number_of_points=21 static_pitch=-0.50 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=8.7 //feet, altitude of CG when at rest on the ground gear_system_type=0 //Hydraulic [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=0.625629 //Brake scalar [hydraulic_system] normal_pressure=3000.0 //PSI electric_pumps=1 //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=30 // 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=280 // KIAS blowout-speed=320 // KIAS lift_scalar=0.8 drag_scalar=0.6 pitch_scalar=0.8 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=20 // seconds flaps-position.0=0 // flaps-position.1=1.0 // damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=1.0 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=20 // seconds flaps-position.0=0 // flaps-position.1=0.5 // flaps-position.4=1.0 // damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=1.0 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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 =3, -11.70, -48.30, 3.10, fx_navred , light.1 =3, -11.70, 48.30, 3.10, fx_navgre , light.2 =4, -15.60, -47.70, 3.00, fx_navwhi , light.3 =4, -15.60, 47.70, 3.00, fx_navwhi , light.4 =2, -12.80, -48.40, 3.10, fx_strobe , light.5 =2, -12.80, 48.40, 3.10, fx_strobe , light.6 =4, -51.55, 0.00, 7.70, fx_navwhi , light.7 =3, -51.55, 0.00, 7.70, fx_strobe , light.8 =1, 7.80, 0.00, 10.50, fx_beacon , light.9 =1, 6.80, 0.00, -3.20, fx_beaconb , light.10 =4, 43.10, -1.50, 6.00, fx_vclight , [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 [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 [TailHook] tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=0.7 [folding_wings] wing_fold_system_type=4 fold_rates=0.12,0.11 [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 [SMOKESYSTEM] smoke.0=-20.00,-3.50,-16.5, SMOKE_JT8D smoke.1=-20.00,-3.50, 16.5, SMOKE_JT8D [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=500 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=96.6 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=30.0 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 se_no_default_pitch=1 use_no_default_bank=1 yaw_damper_gain=0.4 default_bank_mode=0 [fuel] Center1=7.909, 0.00, -3.051, 2303.70, 0.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=3.075, -17.16, -0.469, 1428.15, 0.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=3.075, 17.16, -0.469, 1428.15, 0.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=1098.0 //Square feet wing_span=93.00 //Feet wing_root_chord=19.927 //Feet wing_dihedral=6.0 //Degrees wing_incidence=1.0 //Degrees wing_twist=0.802 //Degrees oswald_efficiency_factor=0.885 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=25.0 //Degrees, wing leading edge wing_pos_apex_lon=19.551 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=-3.873 //Feet, vertical distance from reference point, positive going up htail_area=312.046 //Square feet htail_span=36.00 //Feet htail_pos_lon=-31.733 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=7.112 //Feet, vertical distance from reference point, positive going up htail_incidence=-5.20 //Degrees htail_sweep=30.0 //Degrees, horizontal tail leading edge vtail_area=224.0 //Square feet vtail_span=37.008 //Feet, tip to body vtail_sweep=35.0 //Degrees, vertical tail leading edge vtail_pos_lon=-25.959 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=8.872 //Feet, vertical distance from reference point, positive going up elevator_area=70.504 //Square feet aileron_area=24.596 //Square feet rudder_area=56.188 //Square feet elevator_up_limit=26.1 //Degrees elevator_down_limit=26.1 //Degrees aileron_up_limit=27.000 //Degrees aileron_down_limit=17.00 //Degrees rudder_limit=25.0 //Degrees elevator_trim_limit=20.0 //Degrees spoiler_limit=60.0 //Degrees spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=3 //Aileron to spoileron gain min_ailerons_for_spoilerons=13.5 //Degrees min_flaps_for_spoilerons=0.0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=142.0 //Knots True (KTAS) full_flaps_stall_speed=113.0 //Knots True (KTAS) cruise_speed=440.0 //Knots True (KTAS) max_mach=0.82 max_indicated_speed=340 //Red line (KIAS) [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 [stall_warning] type=2 [contact_points] //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) point.0=1, 38.000, 0.000, -6.950, 1574.800, 0.000000, 1.370, 53.640, 0.208, 2.500, 0.639, 5.000, 5.000, 0.000, 0.000, 250.000 point.1=1,-1.800, -10.200, -8.800, 1574.800, 1.000000, 1.370, 0.000, 1.000, 2.500, 1.200, 5.000, 5.000, 2.000, 0.000, 250.000 point.2=1,-1.800, 10.200, -8.800, 1574.800, 2.000000, 1.370, 0.000, 1.000, 2.500, 1.200, 5.000, 5.000, 3.000, 0.000, 250.000 point.3=2,0.000000,-46.500000,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2,0.000000,46.500000,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2,-54.166667,0.000000,2.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2,45.750000,0.000000,-2.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=0.126343 static_cg_height=8.8 gear_system_type=0
