[fltsim.0]
title=Southwest 727-227 Adv
sim=727200
model=
panel=
sound=
texture=
atc_id=N564PE
atc_heavy=0
atc_flight_number=456
atc_airline=
ui_manufacturer=Boeing
ui_type=727-227 Adv
ui_variation=Southwest Airlines
description=Repaint by: Capt. Wes Archibald - Model by: FFX
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
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=0
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
min_throttle_limit=-0.499939
[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)
max_indicated_speed=597.656250
max_mach=0.839990
//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
gear_system_type=0
[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= 1.00, -19.00, -0.20, -1.50, 2638.00, 280.00
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
electric_pump=0
[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
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
[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
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
