[fltsim.0]
title=Boeing 757-300  CON
sim=b757-300
model=
panel=
sound=
texture=CON
kb_checklists=
kb_reference=
atc_id=573CON
atc_airline=Continental
atc_flight_number=4334
ui_manufacturer=Boeing
ui_type=757-300 
ui_variation=Continental
description=Boeing 757-300 
atc_heavy=1
atc_parking_types=GATE
atc_parking_codes=CON
visual_damage=0


[General]
atc_type=BOEING AIRCRAFT
atc_model=B753
performance=Cruise Speed\t.80 - .84 Mach\nNever Exceed         .86 Mach\nMaximum Range\t3,485 nm\nMTOW                    217,500 lb\nSeating\t\t243 to 279\nCargo Capacity\t2,382 CU ft\n

[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 = 271000.000
empty_weight = 142000.000

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 = 0.000, 0.000, 0.000, 0.000
station_load.0 =170.000000, 78.000000, -1.500000, 0.000000, Pilot           
station_load.1 =170.000000, 78.000000, 1.500000, 0.000000, Co-Pilot        
station_load.2 =510.000000, 0.000000, 0.000000, 0.000000, Crew            
station_load.3 =2720.000000, 58.000000, 0.000000, 0.000000, First Class     
station_load.4 =11900.000000, 35.000000, 0.000000, 0.000000, Coach           
station_load.5 =17000.000000, -18.000000, 0.000000, 0.000000, Coach           
station_load.6 =6103.000000, 30.000000, 0.000000, 0.000000, Forward Baggage 
station_load.7 =6503.000000, -30.000000, 0.000000, 0.000000, Aft Baggage     

;Moments of Inertia
empty_weight_pitch_MOI  = 5523317.000
empty_weight_roll_MOI   = 1169473.000
empty_weight_yaw_MOI    = 4193728.000
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        =1.402
roll_stability         =1.202
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 = 23.510, 21.740, -4.590
Engine.1 = 23.510, -21.740, -4.590
fuel_flow_scalar = 1.000
min_throttle_limit=-0.349976

[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 50.000
rated_N2_rpm = 29920.000
static_thrust = 43500.000
afterburner_available = 0
reverser_available = 1.000

[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, 73.400, 0.000, -11.850, 1181.102, 0.000, 1.256, 60.000, 0.239, 2.500, 1.933, 4.000, 4.000, 0.000, 0.000, 0.000
point.1= 1.000, -1.670, -12.000, -13.450, 1574.803, 1.000, 1.630, 0.000, 1.972, 2.500, 0.498, 6.000, 6.000, 2.000, 0.000, 0.000
point.2= 1.000, -1.670, 12.000, -13.450, 1574.803, 2.000, 1.630, 0.000, 1.972, 2.500, 0.498, 6.000, 6.000, 3.000, 0.000, 0.000
point.3= 2.000, -77.310, 0.000, 32.190, 3200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.4= 2.000, 92.640, 0.000, -0.800, 3200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.5= 2.000, 83.940, 0.000, 5.170, 3200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
point.6= 2.000, 10.820, -62.610, 3.900, 3200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.7= 2.000, -10.820, 62.610, 3.900, 3200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000

max_number_of_points = 21

static_pitch= 0.100
static_cg_height= 11.500
gear_system_type=0

[Views]
eyepoint=83.8, -1.65, 4.40   //(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

[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 = 98
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8;
use_no_default_bank=1
use_no_default_pitch=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=1.000000
autothrottle_takeoff_ga=1

[fuel]
Center1= 0.000, 0.000, 0.000, 3490.000, 0.000
LeftMain= 7.380, -15.000, 0.000, 4000.000, 0.000
RightMain= 7.380, 15.000, 0.000, 4000.000, 0.000
fuel_type=2.0
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area               = 1994.000 
wing_span               = 124.100    
wing_root_chord         = 26.890  
wing_dihedral           = 5.000 
wing_incidence          = 0.520 
wing_twist              = 0.500 
oswald_efficiency_factor= 0.750 
wing_winglets_flag      = 0  
wing_sweep              = 30.000  
wing_pos_apex_lon       = 24.730  
wing_pos_apex_vert      = 0.000  
htail_area              = 541.950 
htail_span              = 50.440   
htail_pos_lon           = -58.580 
htail_pos_vert          = 3.600  
htail_incidence         = 0.000
htail_sweep             = 35.000  
vtail_area              = 369.940  
vtail_span              = 23.610  
vtail_sweep             = 45.000
vtail_pos_lon           = -54.610
vtail_pos_vert          = 8.980
elevator_area           = 134.760
aileron_area            = 46.380  
rudder_area             = 124.960 
elevator_up_limit       = 22.500 
evator_down_limit     = 19.50
aileron_up_limit        = 24.000
aileron_down_limit      = 20.000
rudder_limit            = 32.000
elevator_trim_limit     = 20.000
spoiler_limit           = 45.000
spoilerons_available    = 1
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000
elevator_down_limit= 20.626

[Reference Speeds]
flaps_up_stall_speed    = 142.000
full_flaps_stall_speed  = 110.000
cruise_speed            = 490.000
max_indicated_speed=350.000000
max_mach=0.860010

[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

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3,  -9.80, 62.35,  4.23, fx_navgre ,
light.1 = 3, -9.50, 62.35,  4.23, fx_navgre ,
light.2 = 3, -9.80, -62.35, 4.23, fx_navred ,
light.3 = 3, -9.50, -62.35, 4.23, fx_navred ,
light.4 = 2, -12.2, -62.65,  4.23, fx_strobeh ,
light.5 = 2, -12.2,  62.65,  4.23, fx_strobeh ,
light.6 = 3, -15.3, -62.4,   4.13, fx_navwhi ,
light.7 = 3, -15.3,  62.4,   4.13, fx_navwhi, 
light.8 =  1, 56.13, 0.0, 9.59,   fx_beaconh ,  
light.9 =1, 31.73, 0.0,-4.03,   fx_beaconh , 
light.10 = 4,  82, -2.1, 5.9 ,  fx_vclighth ,
light.11 = 4,  82, 2.1, 5.9 , fx_vclighth ,

//light.12= 2, -82.14, 0.000, 06.77, fx_navwhi ,       

[folding_wings]  // #3 door on 3 door version, #4 door on 4 door version.
wing_fold_system_type = 4                  
fold_rates = 0.4,0.4                       
cable_force_adjust = 1.0




[brakes]
toe_brakes_scale=0.88
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.097656
flap_limit_power=25.996227
flap_limit_idle=5.918312

[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


[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= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
[Flaps.1]
type= 2
span-outboard= 0.400
extending-time= 20.000
system_type= 0
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= 10.000, 0.000
[Flaps.2]
type= 2
span-outboard= 0.700
extending-time= 30.000
system_type= 0
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= 5.000, 0.000
flaps-position.2= 10.000, 0.000