[fltsim.0] title=FlightFX 727-200 Northwest sim=727200 model= panel= sound= texture= atc_id= atc_heavy=0 atc_flight_number=722 atc_airline=NORTHWEST ui_manufacturer=Boeing ui_type=727-200 ui_variation=Northwest description=One of the most successful commercial jet airliners ever designed. Production totaled 1,831 aircraft between the early 1960's and 1984.\nOriginal model: Kevin Trinkle,Gary Carlson\nModifications and GMax design: Erick Cantu, Jonathan Stewart, FDE by Mike Baumann visual_damage=1 [General] performance=wingspan\s 108ft\nlength\s 153ft 2in\ntail height\s 34ft\ngross taxi weight\s 191,000 lbs\nthrust\s (PWJT8D-17R) 17,400lbs ea (x3)\ncruise speed\s 570-605 mph\ncruise alt\s 30,000-40,000ft\nrange\s 1500-2500nm\npassengers\s 148-189\nfuel load\s 9,806 gallons atc_type=BOEING AIRCRAFT atc_model=B722 [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= 1.000 pitch_stability= 1.200 roll_stability= 1.200 yaw_stability= 1.200 parasite_drag_scalar= 1.200 induced_drag_scalar= 1.200 elevator_effectiveness= 1.100 aileron_effectiveness= 1.000 rudder_effectiveness= 1.000 elevator_trim_effectiveness= 1.100 aileron_trim_effectiveness= 1.000 rudder_trim_effectiveness= 1.000 [jet_engine] thrust_scalar=1.100 [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=66 station_load.0= 1000, 59.00, 3.00, 5.50 station_load.1= 320, 59.00, -3.00, 5.50 station_load.2= 500, 56.26, 3.00, 5.50 station_load.3= 320, 56.26, -3.00, 5.50 station_load.4= 500, 53.52, 3.00, 5.50 station_load.5= 320, 53.52, -3.00, 5.50 station_load.6= 320, 50.78, -3.00, 5.50 station_load.7= 320, 48.04, 3.00, 5.50 station_load.8= 320, 48.04, -3.00, 5.50 station_load.9= 4500, 47.00, 0.00, 0.00 station_load.10= 320, 45.30, 3.00, 5.50 station_load.11= 320, 45.30, -3.00, 5.50 station_load.12= 480, 42.56, -3.00, 5.50 station_load.13= 480, 42.56, 3.00, 5.50 station_load.14= 480, 39.82, -3.00, 5.50 station_load.15= 480, 39.82, 3.00, 5.50 station_load.16= 4500, 39.00, 0.00, 0.00 station_load.17= 480, 37.08, -3.00, 5.50 station_load.18= 480, 37.08, 3.00, 5.50 station_load.19= 480, 34.34, -3.00, 5.50 station_load.20= 480, 34.34, 3.00, 5.50 station_load.21= 480, 31.60, -3.00, 5.50 station_load.22= 480, 31.60, 3.00, 5.50 station_load.23= 480, 28.86, -3.00, 5.50 station_load.24= 480, 18.86, 3.00, 5.50 station_load.25= 480, 26.12, -3.00, 5.50 station_load.26= 480, 26.12, 3.00, 5.50 station_load.27= 480, 23.38, -3.00, 5.50 station_load.28= 480, 23.38, 3.00, 5.50 ststion_load.29= 480, 20.64, -3.00, 5.50 station_load.30= 480, 20.64, 3.00, 5.50 station_load.31= 480, 17.90, -3.00, 5.50 station_load.32= 480, 17.90, 3.00, 5.50 station_load.33= 480, 15.16, -3.00, 5.50 station_load.34= 480, 15.16, 3.00, 5.50 station_load.35= 480, 12.42, -3.00, 5.50 station_load.36= 480, 12.42, 3.00, 5.50 station_load.37= 480, 9.68, -3.00, 5.50 station_load.38= 480, 2.68, 3.00, 5.50 station_load.39= 480, 6.94, -3.00, 5.50 station_load.40= 480, 6.94, 3.00, 5.50 station_load.41= 480, 4.20, -3.00, 5.50 station_load.42= 480, 4.20, 3.00, 5.50 station_load.43= 480, 1.46, -3.00, 5.50 station_load.44= 480, 1.46, 3.00, 5.50 station_load.45= 480, -1.28, -3.00, 5.50 station_load.46= 480, -1.28, 3.00, 5.50 station_load.47= 480, -4.02, -3.00, 5.50 station_load.48= 480, -4.02, 3.00, 5.50 station_load.49= 480, -6.76, -3.00, 5.50 station_load.50= 480, -6.76, 3.00, 5.50 station_load.51= 480, -9.50, -3.00, 5.50 station_load.52= 480, -9.50, 3.00, 5.50 station_load.53= 480, -12.24, -3.00, 5.50 station_load.54= 480, -12.24, 3.00, 5.50 station_load.55= 12000, -16.00, 0.00, 0.00 station_load.56= 480, -14.98, -3.00, 5.50 station_load.57= 500, -14.98, 3.00, 5.50 station_load.58= 320, -17.72, -3.00, 5.50 station_load.59= 480, -20.46, -3.00, 5.50 station_load.60= 500, -20.46, 3.00, 5.50 station_load.61= 480, -23.20, -3.00, 5.50 station_load.62= 500, -23.20, 3.00, 5.50 station_load.63= 3300, -35.00, -9.30, 5.00 station_load.64= 3300, -54.00, 0.00, 5.60 station_load.65= 3300, -35.00, 9.30, 5.00 empty_weight= 121407.000 empty_weight_roll_MOI= 3054404.000 empty_weight_pitch_MOI= 5231321.000 empty_weight_yaw_MOI= 5419140.000 empty_weight_coupled_MOI= 1500.000 max_gross_weight= 175609.998 //MTOW=210000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [GeneralEngineData] engine_type= 1 Engine.0= -35.00, -9.30, 5.00 Engine.1= -54.50, 0.00, 5.60 Engine.2= -35.00, 9.30, 5.00 fuel_flow_scalar= 0.900 [SMOKESYSTEM] smoke.0= 5.00, -50.00, -9.30, fx_hjg_707 smoke.1= 5.60, -60.50, 0.00, fx_hjg_707 smoke.2= 5.00, -50.00, 9.30, fx_hjg_707 [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 20.912 rated_N2_rpm= 29920.000 static_thrust= 17400.000 afterburner_available= 0 reverser_available= 1 [airplane_geometry] wing_area= 1620.000 wing_span= 108.000 wing_root_chord= 15.250 wing_dihedral= 2.999 wing_incidence= 2.000 wing_twist= -1.000 oswald_efficiency_factor=10.422 wing_winglets_flag= 1 wing_sweep= 28.000 wing_pos_apex_lon= 21.200 wing_pos_apex_vert= 0.100 htail_area= 491.000 htail_span= 40.750 htail_pos_lon= -58.350 htail_pos_vert= 24.000 htail_incidence= 1.000 htail_sweep= 30.000 vtail_area= 422.000 vtail_span= 23.422 vtail_sweep= 42.000 vtail_pos_lon= -43.800 vtail_pos_vert= 16.000 elevator_area= 117.750 aileron_area= 64.800 rudder_area= 71.740 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 23.491 elevator_trim_limit= 19.481 spoiler_limit= 59.989 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 = 144.000 full_flaps_stall_speed = 115.200 cruise_speed = 605.000 //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] point.0=1.000, 65.000, 0.000, -7.100, 1181.100, 0.000, 1.323, 78.000, 0.300, 2.300, 0.700, 4.200, 4.200, 0.000, 200.0, 280.0 //ngear point.1=1.000, -2.250, -9.670, -8.100, 1574.803, 1.000, 2.000, 0.000, 0.400, 2.500, 0.600, 6.900, 6.900, 2.000, 200.0, 280.0 //lgear point.2=1.000, -2.250, 9.670, -8.100, 1574.803, 2.000, 2.000, 0.000, 0.400, 2.500, 0.600, 7.200, 7.200, 3.000, 200.0, 280.0 //rgear point.3=2.000, -23.900, -55.850, -0.583, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //lwing point.4=2.000, -23.900, 55.850, -0.583, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //rwing point.5=2.000, 81.300, 0.000, 1.900, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //nose point.6=2.000, -81.000, 0.000, 23.800, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //tail point.7=2.000, -35.200, 0.000, -3.150, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //thook static_pitch= -0.900 static_cg_height= 7.800 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 12.000 system_type= 1 damaging-speed= 280.000 blowout-speed= 320.000 lift_scalar= 1.300 drag_scalar= 1.100 pitch_scalar= 1.000 flaps-position.0=0.000 flaps-position.1=2.000 flaps-position.2=5.000 flaps-position.3=15.000 flaps-position.4=20.000 flaps-position.5=25.000 flaps-position.6=30.000 flaps-position.7=40.000 [Flaps.1] type= 2 span-outboard= 0.800 extending-time= 5.000 system_type= 1 damaging-speed= 280.000 blowout-speed= 320.000 lift_scalar= 1.200 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000 flaps-position.1= 1.000 flaps-position.2= 1.500 flaps-position.3= 2.000 [electrical] //BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 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_heat = 0, 15, 17.0 additional_system = 0, 20, 17.0 marker_beacon = 1, 2, 17.0 starter1 = 0, 20, 17.0 starter2 = 0, 20, 17.0 starter3 = 0, 20, 17.0 auto_brakes = 0, 15, 17.0 hydraulic_pump = 0, 2, 17.0 fuel_transfer_pump = 0, 5, 17.0 max_battery_voltage = 28.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps= 60.0 electric_always_available = 1 [pitot_static] vertical_speed_time_constant=999 [exits] number_of_exits=1 exit_rate.0=0.2 [Views] eyepoint= 72.50, -2.00, 6.15 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0= 3, -16.70, -55.50, 0.75, MD80_NAVR , light.1= 3, -17.50, -55.85, 0.75, MD80_NAVR , light.2= 2, -15.60, -55.45, 0.70, MD80_STROBE , light.3= 3, -23.90, -55.75, 0.55, MD80_INSPEC2 , light.4= 3, -16.70, 55.50, 0.75, MD80_NAVG , light.5= 3, -17.50, 55.85, 0.75, MD80_NAVG , light.6= 2, -15.58, 55.47, 0.70, MD80_STROBE , light.7= 3, -23.90, 55.75, 0.55, MD80_INSPEC2 , light.8= 3, -81.00, 0.00, 23.80, fx_navwhi , light.9= 2, -81.00, 0.00, 23.80, MD80_STROBE , light.10= 5, 24.75, -6.55, 3.30, MD80_INSPEC2 , light.11= 5, 24.75, 6.55, 3.30, MD80_INSPEC2 , light.12= 4, 72.60, -1.80, 6.35, fx_vclight , light.13= 4, 72.60, 1.80, 6.35, fx_vclight , light.14= 5, 4.80, -40.00, 8.40, fx_fxwing2.fx , light.15= 5, 4.80, 40.00, 8.40, fx_fxwing2.fx , light.16= 1, 12.50, 0.00, -3.85, MD80_BCNL , light.17= 1, 40.00, 0.00, 11.35, MD80_BCNU , [keyboard_response] elevator=150.000000, 250.000000 aileron= 150.000000, 250.000000 rudder= 150.000000, 250.000000 [direction_indicators] direction_indicator.0=3,0 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) //9806 US gallons (31000 L) standard for 208000 lbs. Center1= 8.00, 0.00, -1.50, 4530.00, 30.00 LeftMain= 1.00, -19.00, -0.20, 2638.00, 28.00 RightMain= 1.00, 19.00, -0.20, 2638.00, 28.00 fuel_type= 2.000 number_of_tank_selectors= 1 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 800 autothrottle_available= 1 autothrottle_arming_required= 1 autothrottle_max_rpm= 99 autothrottle_takeoff_ga= 1 pitch_takeoff_ga= 8.00 autoland_available= 0 use_no_default_pitch= 1 use_no_default_bank= 1 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1= 1 Com.1= 1, 0 Com.2= 1, 0 Nav.1= 1, 0, 1 Nav.2= 1, 0, 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