[fltsim.0] title=Boeing 727-200 cargo sim=b727 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=TC-CGU atc_airline=Efes atc_flight_number=293 ui_manufacturer=Boeing ui_type=727-200 ui_variation=Ephesus visual_damage=1 description=Paint by Arslan "vaccaro" Türegün\n40 years old and still flying, the venerable 727 far surpassed Boeing's most optimistic sales forecasts. 1831 were built, with many still in service today. Noisy and inefficient by today's standards, it set new standards for comfort and reliability in its day. atc_heavy=0 [General] atc_type=BOEING AIRCRAFT atc_model=B727 editable=1 performance=Max speed: 598 mph\nRange: 2,728 mi\nCeiling: 33,000 ft.\nEmpty weight: 99,370\nLoaded: 190,090\nPassengers: 145 typical [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] max_gross_weight = 209000.000 empty_weight = 100000.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 0.000 max_number_of_stations = 50 station_load.0 = 20000.000, 0.000, 0.000, 0.000 ;Moments of Inertia empty_weight_pitch_MOI = 5600000.000 empty_weight_roll_MOI = 1400000.000 empty_weight_yaw_MOI = 4000000.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.000 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 [GeneralEngineData] engine_type = 1 Engine.0 = -45.000, -9.000, 4.000 Engine.1 = -45.000, 9.000, 4.000 fuel_flow_scalar = 1.000 Engine.2= -60.000, 0.000, 3.000 [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 18.000 rated_N2_rpm = 29920.000 static_thrust = 16000.000 afterburner_available = 0 reverser_available = 1 [jet_engine] thrust_scalar =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, 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] point.0= 1.000, 40.000, 0.000, -7.500, 1181.100, 0.000, 1.442, 55.920, 0.800, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000 point.1= 1.000, -7.750, -8.580, -8.900, 1574.800, 1.000, 1.442, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000 point.2= 1.000, -7.750, 8.580, -8.900, 1574.800, 2.000, 1.442, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000 point.3= 2.000, -14.170, -47.330, 0.000, 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, 0.000, 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= 2.000, -54.000, 0.000, 2.830, 787.400, 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, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 max_number_of_points = 21 static_pitch= -1.000 static_cg_height= 7.500 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -22.89, -53.20, 0.85, fx_navredm , light.1 = 3, -22.89, 53.20, 0.85, fx_navgrem , light.2 = 3, -80.73, 0.00, 23.16, fx_navwhih , light.3 = 2, -24.00, -53.53, 0.85, fx_strobeh , light.4 = 2, -24.00, 53.53, 0.85, fx_strobeh , light.5 = 2, 3.36, 0.00, -4.21, fx_beaconb , light.6 = 1, 29.96, 0.00, 9.15, fx_beaconh , light.7 = 4, 60.87, 0.00, 6.39, fx_vclight , light.8 = 5, 66.0, 0.00, -7.00, newll, [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; use_no_default_bank = 1 use_no_default_pitch = 1 [fuel] Center1 = 0.000, 0.000, 0.000, 3800.000, 0.000 LeftMain = -3.000, -19.000, 0.000, 2500.000, 0.000 RightMain = -3.000, 19.000, 0.000, 2500.000, 0.000 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 [airplane_geometry] wing_area = 1400.000 wing_span = 108.000 wing_root_chord = 25.000 wing_dihedral = 2.000 wing_incidence = 1.000 wing_twist = -0.500 oswald_efficiency_factor= 0.750 wing_winglets_flag = 0 wing_sweep = 35.000 wing_pos_apex_lon = 12.000 wing_pos_apex_vert = 0.000 htail_area = 350.000 htail_span = 35.000 htail_pos_lon = -60.000 htail_pos_vert = 24.000 htail_incidence = 0.000 htail_sweep = 30.000 vtail_area = 440.000 vtail_span = 20.000 vtail_sweep = 35.000 vtail_pos_lon = -45.000 vtail_pos_vert = 8.000 elevator_area = 45.000 aileron_area = 25.000 rudder_area = 59.000 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 = 140.000 full_flaps_stall_speed = 110.000 cruise_speed = 515.000 [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 [Flaps.0] type= 1 span-outboard= 0.400 extending-time= 8.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.500 drag_scalar= 0.500 pitch_scalar= 0.250 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= 1 span-outboard= 0.400 extending-time= 8.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.500 drag_scalar= 0.500 pitch_scalar= 0.250 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.2] type= 2 span-outboard= 0.800 extending-time= 4.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 4.000 drag_scalar= 0.400 pitch_scalar= 0.200 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.000, 0.000 flaps-position.2= 0.000, 0.000 flaps-position.3= 1.000, 0.000 [Flaps.3] type= 2 span-outboard= 0.800 extending-time= 4.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.500 drag_scalar= 0.500 pitch_scalar= 0.250 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.000, 0.000 flaps-position.2= 0.000, 0.000 flaps-position.3= 1.000, 0.000