[fltsim.0] title=Boeing 737-200 Vasp sim=cf732v2004 model= panel= sound= texture=vasp_oc kb_checklists=Boeing737-400_check kb_reference=Boeing737-400_ref atc_type=Boeing atc_id_enable=1 atc_id=PP-SMC atc_id_color=0xffffffff editable=0 visual_damage=1 ui_manufacturer=Boeing ui_type=737-200 ui_variation=Vasp 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 Vasp painted by Martoni. atc_airline=Vasp [General] atc_type=Boeing atc_model=B732 editable=0 performance=Model by FFX with FDE by Mike Baumann (2003)\n\nEngine's type: P & W JT8D-9A \nWing span: 93 ft\nTotal height 37 ft. \nStatic T\/O Thrust (per engine) 14500 lb. \nMax. range 2645 nm \nMax. T\/O weight 115500 lb. \nCruising altitude 31 - 37000 ft. \nMax. fuel weight 34720 lb. \nCruising speed 420 m.p.h. VMO/MMO 350/.84 \nMax. payload structural 34630 lb.\nCargo capacity 875 cu. ft. \nOverall length 100 ft. 2 in. \nNumber of seats 130\n [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 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.1 induced_drag_scalar = 1.1 elevator_effectiveness = 0.8 aileron_effectiveness = 0.9 rudder_effectiveness = 1.2 pitch_stability = 1.2 roll_stability = 1.0 yaw_stability = 1.2 elevator_trim_effectiveness = 1.1 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.1 [jet_engine] thrust_scalar = 1.2 [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) empty_weight_roll_MOI=1062809.000000 empty_weight_pitch_MOI=1411739.000000 empty_weight_yaw_MOI=1779732.000000 empty_weight_coupled_MOI=1000.000000 [GeneralEngineData] engine_type=1 Engine.0=-1.00,-16.50,-3.50 Engine.1=-1.00, 16.50,-3.50 fuel_flow_scalar=0.80 min_throttle_limit=-0.399902 [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 16.150 rated_N2_rpm= 29920.000 static_thrust= 14500.000 afterburner_available=0 reverser_available=1 [SMOKESYSTEM] smoke.0=-20.00,-3.50,-16.5, SMOKE_JT8D smoke.1=-20.00,-3.50, 16.5, SMOKE_JT8D [airplane_geometry] wing_area= 980.000 wing_span= 93.000 wing_root_chord= 19.800 wing_dihedral= 6.000 wing_incidence= 1.000 wing_twist= 0.802 oswald_efficiency_factor= 0.885 wing_winglets_flag= 0 wing_sweep= 25.000 wing_pos_apex_lon= 15.600 wing_pos_apex_vert= -0.800 htail_area= 408.000 htail_span= 36.000 htail_pos_lon= -37.750 htail_pos_vert= 7.250 htail_dihedral= 7.000 htail_incidence= 1.000 htail_sweep= 30.000 vtail_area= 405.000 vtail_span= 19.912 vtail_sweep= 35.000 vtail_pos_lon= -23.550 vtail_pos_vert= 10.100 elevator_area= 70.500 aileron_area= 26.800 rudder_area= 56.200 elevator_up_limit= 26.100 elevator_down_limit= 26.100 aileron_up_limit= 19.000 aileron_down_limit= 19.000 rudder_limit= 23.500 elevator_trim_limit= 19.000 spoiler_limit= 60.000 spoilerons_available= 1 aileron_to_spoileron_gain=3.000 min_ailerons_for_spoilerons=6.989 min_flaps_for_spoilerons=0.000 [Reference Speeds] flaps_up_stall_speed= 145.000 full_flaps_stall_speed= 115.000 cruise_speed= 509.000 max_indicated_speed=350.000000 max_mach=0.839990 [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 [Flaps.0] type=1 span-outboard= 0.500 extending-time= 15.0 system_type= 1 damaging-speed= 280.000 blowout-speed= 320.000 lift_scalar= 1.200 drag_scalar= 1.100 pitch_scalar= 0.500 flaps-position.0= 0.000 flaps-position.1= 4.999 flaps-position.2= 9.998 flaps-position.3= 14.997 flaps-position.4= 19.996 flaps-position.5= 24.995 flaps-position.6= 29.994 flaps-position.7= 34.993 flaps-position.8= 39.992 [Flaps.1] type=2 span-outboard= 0.800 extending-time= 2.0 system_type= 1 damaging-speed= 280.000 blowout-speed= 320.000 lift_scalar= 1.200 drag_scalar= 1.100 pitch_scalar= 0.200 flaps-position.0=0.000 flaps-position.1=1.000 [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 [pitot_static] vertical_speed_time_constant=999 [exits] number_of_exits = 1 exit_rate.0 = 0.1 [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 [Views] eyepoint=44.70, -1.85, 5.00 [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] elevator=150.000,250.000 aileron= 150.000,250.000 rudder= 150.000,250.000 [direction_indicators] direction_indicator.0=3,0 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center1= 6.00, 0.00, -2.00, 2177.00, 0.00 LeftMain= 2.00, -19.00, -0.20, 1541.00, 0.00 RightMain= 2.00, 19.00, -0.20, 1541.00, 0.00 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=800.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=98 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8.0 use_no_default_pitch=1 use_no_default_bank=1 default_pitch_mode=0 default_bank_mode=0 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain = 1.0 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 0 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [brakes] toe_brakes_scale=0.671407 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=24.637185 flap_limit_idle=0.974028 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
