[fltsim.0] title=Boeing 737-100 (NASA) sim=Boeing 737-100 model= panel= sound= texture= kb_checklists=Check kb_reference=Specs ui_manufacturer=Boeing ui_type=737-100 ui_variation=NASA description=One should hardly be surprised that the world's most prolific manufacturer of commercial aircraft is also the producer of the world's most popular jetliner. The 737 became the best-selling commercial jetliner worldwide when orders for it hit 1,831 in June 1987 (surpassing Boeing's own 727 as the previous champ). However, it wasn't always that way. In the first few years of production, there were so few orders that Boeing considered canceling the program. They didn't, and the airplane has more than proven itself in over three decades of service. The Boeing 737-100 is one of the early variants and is painted in NASA colors. atc_heavy=0 atc_id=N515NA atc_airline=Navigator atc_flight_number= [General] performance=Wing Span: 28.35m (93ft 0in)\nOverall Length: 28.67m (94ft 0in)\nTail Height: 11.29m (37ft)\nPassengers: 115 (Single class) \nOperating empty: 25,878kg (57,000lb)\nMax takeoff: 49,940kg (110,000lb)\nEngines: 2 x Pratt & Whitney JT8D7 turbofans\nMaximum thrust: 62.3kN (14,000lb) \nMaximum Range 1540 nm\nSpeed: Cruise 430 kt\n Maximum 509 kt @ 33000 ft \nCeiling: 35000 ft\n\nDesigner: Vasco Ferreira\nDate: 30 May 2004\nE-mail: paulif@yebo.co.za\n atc_type=BOEING AIRCRAFT atc_model=B721 [ground_reaction] main_gear_static_compression=1.0 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=0.8 // (feet), The distance the center gear strut is compressed when at rest on the ground main_gear_damping_ratio=0.9 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio=0.9 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [pitot_static] vertical_speed_time_constant=100 //Increasing this value will cause a more instantaneous reaction in the VSI [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=0.850 induced_drag_scalar=1.000 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 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 2 , 0 gear_motor=0, 2 , 0 autopilot=0, 2 , 0 avionics_bus=0, 2 , 0 avionics=0, 2 , 0 pitot_heat=0, 2 , 0 additional_system=0, 2 , 0 marker_beacon=0, 2 , 0 gear_warning=0, 2 , 0 fuel_pump=0, 2 , 0 starter1=0, 2 , 0 starter2=0, 2 , 0 starter3=0, 2 , 0 starter4=0, 2 , 0 light_nav=0, 2 , 0 light_beacon=0, 2 , 0 light_landing=0, 2 , 0 light_taxi=0, 2 , 0 light_strobe=0, 2 , 0 light_panel=0, 2 , 0 prop_sync=0, 2 , 0 auto_feather=0, 2 , 0 auto_brakes=0, 2 , 0 standby_vacuum=0, 2 , 0 hydralic pump=0, 2 , 0 fuel_transfer_pump=0, 2 , 0 propeller_deice=0, 2 , 0 propeller_deice=0, 2 , 0 light rocognition=0, 2 , 0 light_wing=0, 2 , 0 light_logo=0, 2 , 0 [WEIGHT_AND_BALANCE] empty_weight= 57000.000 reference_datum_position= 0.000, 0.000, 0.000 max_number_of_stations= 50 station_load.0="170, 46.2, -2.0, 4.3, Pilot" station_load.1="170, 46.2, 2.0, 4.3, Co-pilot" station_load.2="680, 0.0, 0.0, 3.5, Cabin crew" station_load.3="680, 36.4, 0.0, 3.5, Row 1 (x4)" station_load.4="680, 33.6, 0.0, 3.5, Row 2 (x4)" station_load.5="680, 30.8, 0.0, 3.5, Row 3 (x4)" station_load.6="680, 28.0, 0.0, 3.5, Row 4 (x4)" station_load.7="680, 25.2, 0.0, 3.5, Row 5 (x4)" station_load.8="680, 22.1, 0.0, 3.5, Row 6 (x4)" station_load.9="1020, 19.6, 0.0, 3.5, Row 7 (x6)" station_load.10="1020, 16.8, 0.0, 3.5, Row 8 (x6)" station_load.11="1020, 14.0, 0.0, 3.5, Row 9 (x6)" station_load.12="1020, 11.2, 0.0, 3.5, Row 10 (x6)" station_load.13="1020, 8.4, 0.0, 3.5, Row 11 (x6)" station_load.14="1020, 5.6, 0.0, 3.5, Row 12 (x6)" station_load.15="1020, 2.8, 0.0, 3.5, Row 13 (x6)" station_load.16="1020, 0.0, 0.0, 3.5, Row 14 (x6)" station_load.17="1020, -2.8, 0.0, 3.5, Row 15 (x6)" station_load.18="1020, -5.6, 0.0, 3.5, Row 16 (x6)" station_load.19="1020, -8.4, 0.0, 3.5, Row 17 (x6)" station_load.20="1020, -11.2, 0.0, 3.5, Row 18 (x6)" station_load.21="1020, -14.0, 0.0, 3.5, Row 19 (x6)" station_load.22="680, -16.8, 0.0, 3.5, Row 20 (x4)" station_load.23="340, -19.6, 0.0, 3.5, Row 21 (x2)" station_load.24="3000, 0.0, 0.0, 0.0, Baggage for" station_load.25="5000, -10.0, 0.0, 0.0, Baggage aft" empty_weight_CG_position= 0.000, 0.000, 0.000 empty_weight_pitch_MOI= 1615138.000 empty_weight_roll_MOI= 728430.000 empty_weight_yaw_MOI= 1733867.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 110000.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] Center1= 0.000, 0.000, 0.000, 1600.000, 0.000 LeftMain= -3.000, -19.000, 0.000, 800.000, 0.000 RightMain= -3.000, 19.000, 0.000, 800.000, 0.000 fuel_type=2.0 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area= 980.000 wing_span= 93.000 wing_root_chord= 15.500 wing_dihedral= 6.000 wing_incidence= 2.000 wing_twist= 0.000 oswald_efficiency_factor= 0.800 wing_winglets_flag= 0 wing_sweep= 25.000 wing_pos_apex_lon= 6.000 wing_pos_apex_vert= 0.000 htail_area= 408.000 htail_span= 41.750 htail_pos_lon= -41.670 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 305.000 vtail_span= 19.910 vtail_sweep= 0.000 vtail_pos_lon= -35.830 vtail_pos_vert= 20.670 elevator_area= 70.500 aileron_area= 26.800 rudder_area= 56.200 elevator_up_limit= 26.000 elevator_down_limit= 20.600 aileron_up_limit= 19.480 aileron_down_limit= 14.900 rudder_limit= 23.500 elevator_trim_limit= 19.500 spoiler_limit= 60.020 spoilerons_available= 0 aileron_to_spoileron_gain= 2.000 min_ailerons_for_spoilerons= 6.000 min_flaps_for_spoilerons= 0.000 [contact_points] max_number_of_points=10 point.0= 1.000, 37.000, 0.000, -6.000, 1181.100, 0.000, 1.640, 56.700, 0.800, 2.500, 0.900, 6.000, 6.000, 0.000, 220.000, 250.000 point.1= 1.000, -3.160, -9.400, -6.700, 1574.800, 1.000, 1.640, 0.000, 1.000, 2.500, 0.900, 7.900, 7.900, 2.000, 220.000, 250.000 point.2= 1.000, -3.160, 9.400, -6.700, 1574.800, 2.000, 1.640, 0.000, 1.000, 2.500, 0.900, 8.100, 8.100, 3.000, 220.000, 250.000 point.3= 2.000, -14.167, -47.333, 0.000, 787.402, 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, -14.167, 47.333, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -54.000, 0.000, 2.833, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 42.667, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= -0.800 static_cg_height= 5.800 gear_system_type=0 [GeneralEngineData] engine_type= 1 Engine.0= 4.750, -16.083, -2.500 Engine.1= 4.750, 16.083, -2.500 fuel_flow_scalar= 1.2487081 min_throttle_limit=-0.249939 [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 19.600 rated_N2_rpm= 29920.000 static_thrust= 16000.000 afterburner_available= 0 reverser_available= 1 [Reference Speeds] flaps_up_stall_speed= 142.000 full_flaps_stall_speed= 113.600 cruise_speed= 430.000 max_indicated_speed=350.000000 max_mach=0.8500 [keyboard_response] elevator=80.0,110.0 aileron=180.0,250.0 rudder=180.0,300.0 [Views] eyepoint=37.998790,-0.986815,6.946153 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1500.000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=1 autothrottle_max_rpm=110.00 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=0.000000 [direction_indicators] direction_indicator.0=3,0 [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 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -6.00, -40.20, 4.51, fx_navredm light.1=3, -6.00, 40.20, 4.51, fx_navgrem light.2=2, -4.90, -40.20, 4.45, fx_strobeh light.3=2, -4.90, 40.20, 4.45, fx_strobeh light.4=3, -36.10, 0.0, 7.62, fx_navwhih light.7=1, 19.30, 0.00, -1.00, fx_beaconb light.8=1, 10.00, 0.00, 10.51, fx_beaconb [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=250 ; in microseconds [brakes] toe_brakes_scale=0.610370 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 [jet_engine] thrust_scalar=1.000 [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= 1.000 drag_scalar= 1.000 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= 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