// WARNING NEVER TAKE OFF "FREEWARE_(C)_TDS_01AUG2014" from title=
// If you do those , wings will be gone and other unexpected things will happen.
// Title must be under 127 character since FSX will cause error when exceed.
//
// +A ... Option Antenna
// +D ... Option Decal
// +T ... Option type
// 
// Number after Above is Hex and checks at Bit
//0 = 0000
//1 = 0001
//2 = 0010
//3 = 0011
//4 = 0100
//5 = 0101
//6 = 0110
//7 = 0111
//8 = 1000
//9 = 1001
//A = 1010
//B = 1011
//C = 1100
//D = 1101
//E = 1110
//F = 1111
// 
// Model by Hiroshi Igami
// FDE Version W18 2.2.2016 By Nicholas Wilkinson with help from Erick Cantu and Luiz Perina
// FDE 727-100 TAY651 QF W
// Textures by Kyle Schurb and Carlos Eduardo Salas
// Effects by David Biggar

[fltsim.0]
title=FREEWARE_(C)_TDS_01AUG2014 _721_JT8D-217--EW +D00 +TBF40 UPS 727-108c
sim=TdsB721-TAY651
model=
panel=
sound=
texture=ups
kb_checklists=
kb_reference=

atc_id=N936UP
atc_airline=UPS
atc_flight_number=936
atc_heavy=0
atc_parking_types=GATE, RAMP, CARGO
atc_parking_code=PDT

ui_manufacturer=TDS
ui_type=727-100F TAY651 
ui_variation=UPS
visual_damage=1
description="The Boeing 727 is a midsized, narrow-body three-engined jet aircraft built by Boeing Commercial Airplanes from the early 1960s to 1984. It can carry 149 to 189 passengers and later models can fly up to 2,700 nautical miles (5,000 km) nonstop. Intended for short and medium-length flights, the 727 can use relatively short runways at smaller airports. It has three Pratt & Whitney JT8D (although some have been re-engined with the Rolls-Royce Tay) engines below the T-tail, one on each side of the rear fuselage with a center engine that connects through an S-duct to an inlet at the base of the fin. The 727 is Boeing's only trijet aircraft. Model by Hiroshi Igami. FDE Version W09 7/19/2014 By Nicholas Wilkinson with help from Erick Cantu (with permission) and Luiz Perina. Textures by Kyle Schurb and Carlos Eduardo Salas. Repaints by Pedro Rodriguez, Paul Winn and Danny Cummings. Effects by David Biggar. Sounds by Christoffer Petersen (RR TAY), Adam Murphy and Jesse Casserly (JT8D-9). VC by Thomas Ruth." 

[General]
atc_type=BOEING
atc_model=B727
editable=1
performance=
category=airplane

[pitot_static]
vertical_speed_time_constant = 999  
pitot_heat=1.000000

[WEIGHT_AND_BALANCE]
max_gross_weight =170000
empty_weight = 80602
reference_datum_position     =  0.0,  0.0,  0.0
empty_weight_CG_position     = -0.0, -0.0, -0.0 

max_number_of_stations =8

//Seating Capacity First 10, Coach 109; 190 lbs per pax

// Moments of Inertia
empty_weight_pitch_MOI  =2310355
empty_weight_roll_MOI   = 598970
empty_weight_yaw_MOI    =3052955
empty_weight_coupled_MOI =     0
CG_forward_limit= 0
CG_aft_limit= 1

station_load.0= 0, 36.84,  0.00, 0.00, Container 1 2
station_load.1= 6333, 21.66,  0.00, 0.00, Container 3 4
station_load.2= 6333,  6.49,  0.00, 0.00, Container 5 6
station_load.3= 6333, -8.67,  0.00, 0.00, Container 7 8
station_load.4= 1583, 21.98,  0.00, 0.00, Fwd Cargo
station_load.5= 1583, -8.67, 0.00, 0.00, Aft Cargo

[flight_tuning]
cruise_lift_scalar     =1.0
parasite_drag_scalar   =1.0
induced_drag_scalar    =1.0
elevator_effectiveness =1.0
aileron_effectiveness  =1.0
rudder_effectiveness   =1.0
pitch_stability        =1.0
roll_stability         =1.0
yaw_stability          =1.0

elevator_trim_effectiveness =0.55
aileron_trim_effectiveness  =1.0
rudder_trim_effectiveness   =1.0

[GeneralEngineData]
engine_type =1
Engine.0 =-25.600, -9.028, 3.300
Engine.1 =-40.416,  0.000, 2.900
Engine.2 =-25.600,  9.028, 3.300
fuel_flow_scalar =1.2
min_throttle_limit =-0.10                    
max_contrail_temperature = -30                  

[TurbineEngineData]
bypass_ratio = 3.07
fuel_flow_gain =0.001
inlet_area =9.0
rated_N2_rpm =12136
static_thrust =15400                  
afterburner_available =0
reverser_available =1

[jet_engine]
thrust_scalar =1

[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, 5,  17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2,  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


[contact_points]

max_number_of_points =7

static_pitch= -0.500
static_cg_height= 10.0
gear_system_type=1 
tailwheel_lock=0

point.0= 1, 50.187,  -0.000,  -8.756, 1600, 0, 1.319, 75.000, 0.350, 3.500, 0.650, 9.000, 9.000, 0, 240.0, 325.0
point.1= 1, -4.304,  -7.900, -10.925, 1575, 1, 2.080,  0.000, 1.000, 1.500, 0.650, 9.000, 8.100, 6, 240.0, 325.0
point.2= 1, -4.304,   7.900, -10.925, 1575, 2, 2.080,  0.000, 1.000, 1.500, 0.650, 9.000, 8.100, 7, 240.0, 325.0
point.3= 2, -4.265,   0.000,   0.000, 727,  0, 0.000,  0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.4= 2, -25.495,-56.322,  -2.729, 727,  0, 0.000,  0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.5= 2, -24.954,  0.000,  -4.967, 727,  0, 0.000,  0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.6= 2, -25.495, 56.322,  -2.729, 727,  0, 0.000,  0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4


[gear_warning_system]
gear_warning_available =0  
pct_throttle_limit = 0.10000 
flap_limit_idle    = 5.00000 
flap_limit_power   =25.50000


[brakes]
parking_brake =1  
toe_brakes_scale = 0.65
auto_brakes=1			
hydraulic_system_scalar=0.0		
differential_braking_scale=0.0	


[hydraulic_system]
normal_pressure =3000
electric_pumps  = 0
engine_map      = 1,1,0,0


[Views]
eyepoint= 47.829, -1.66, 5.451


[Radios]
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, 6=taxi, 7=recognition, 8=wing, 9=logo 
light.0 = 8,   5.59, -30.23, 2.39, tdsb8_wing_light
light.1 = 8,   5.59,  30.23, 2.39, tdsb8_wing_light
light.2 = 6, 54.179,   0.00,-1.96, tdsnose_gearwell


[keyboard_response]      
elevator = 100, 200   
aileron  = 100, 200
rudder   = 100, 200


[direction_indicators]
direction_indicator.0=3,0


[attitude_indicators]

attitude_indicator.0 = 2 


[turn_indicators]
turn_indicator.0=0,0

[exits]
number_of_exits = 4
exit_rate.0 = 0.1
exit_rate.1 = 0.12
exit_rate.2 = 0.12
exit_rate.3 = 0.12

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
touchdown=fx_tchdwn, 1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=96.8
pitch_takeoff_ga=0
use_no_default_pitch =1
use_no_default_bank =1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=0.3
max_pitch_velocity_lo_alt_breakpoint=7000
max_pitch_velocity_hi_alt_breakpoint=24000
max_bank=32
max_bank_acceleration=1.2
max_bank_velocity=1.5
max_throttle_rate=0.028
nav_proportional_control=9
nav_integrator_control=0.25
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain=1


[fuel]
Center1      = -0.000,   0.000, -3.930, 4120.000, 0.000
LeftMain     = -0.000, -32.800, -0.820, 1780.000, 0.000
RightMain    = -0.000,  32.800, -0.820, 1780.000, 0.000
fuel_type =2
number_of_tank_selectors =3                    
electric_pump=0
fuel_dump_rate=0.02
anemometer_pump=0
manual_pump=0
engine_driven_pump=0


[airplane_geometry]
wing_area               =1720
wing_span               =108
wing_root_chord         =25
wing_dihedral           =2
wing_incidence          =0
wing_twist              =-0.3
oswald_efficiency_factor=0.771
wing_winglets_flag      =1
wing_sweep              =35
wing_pos_apex_lon       =19.224
wing_pos_apex_vert      =0.0
htail_area              =376
htail_span              =35.9
htail_pos_lon           =-61.18
htail_pos_vert          =21.52
htail_incidence         =0
htail_sweep             =40
vtail_area              =350
vtail_span              =15
vtail_sweep             =45
vtail_pos_lon           =-48.00
vtail_pos_vert          =3.94
elevator_area           =95
aileron_area            =55
rudder_area             =40
elevator_up_limit       =28
elevator_down_limit     =20
aileron_up_limit        =15
aileron_down_limit      =20
rudder_limit            =25
elevator_trim_limit     =20
spoiler_limit           =60
spoilerons_available    =1
aileron_to_spoileron_gain =1
min_ailerons_for_spoilerons=1
min_flaps_for_spoilerons  =0.0
spoiler_extension_time=2
spoiler_handle_available=1
auto_spoiler_available=1
positive_g_limit_flaps_up=3.7
negative_g_limit_flaps_up=-2.96
positive_g_limit_flaps_down=2.59
negative_g_limit_flaps_down=-2.22

[Reference Speeds]
flaps_up_stall_speed    = 142
full_flaps_stall_speed  = 113
max_indicated_speed     =575
cruise_speed=250
max_mach=0.9

[forcefeedback]
gear_bump_nose_magnitude=6000  
gear_bump_nose_direction=18000          
gear_bump_nose_duration=250000          
gear_bump_left_magnitude=6000         
gear_bump_left_direction=35500        
gear_bump_left_duration=250000       
gear_bump_right_magnitude=6000         
gear_bump_right_direction=500       
gear_bump_right_duration=250000       
ground_bumps_magnitude1=3250        
ground_bumps_angle1=8900            
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750      
ground_bumps_angle2=9100            
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000               
crash_direction1=1000            
crash_magnitude2=10000            
crash_direction2=9000          
crash_period2=75000               
crash_duration2=2500000        
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111


[stall_warning]
type=2
stick_shaker=1

[flaps.0]
type= 1
system_type=1
span-outboard= 0.5                            
extending-time= 30                             
damaging-speed=280.0                              
blowout-speed=320.0                               
flaps-position.0=0                                                            
flaps-position.1=1                                 
flaps-position.2=2                                 
flaps-position.3=5                               
flaps-position.4=15                       
flaps-position.5=20                    
flaps-position.6=25                       
flaps-position.7=30                         
flaps-position.8=40                        
lift_scalar=1
drag_scalar=
pitch_scalar=1


[flaps.1]      
type= 2      
system_type=1   
span-outboard= 1                       
extending-time= 10                  
damaging-speed=280                         
blowout-speed=320                          
flaps-position.0=0                                                            
flaps-position.1=0                                 
flaps-position.2=5                               
flaps-position.3=5                       
flaps-position.4=5                    
flaps-position.5=5                       
flaps-position.6=5                         
flaps-position.7=5                                             
flaps-position.8=5                        
lift_scalar=1
drag_scalar=1
pitch_scalar=1

[flaps.2]      
type= 2      
system_type=1   
span-outboard= 1                       
extending-time= 10                  
damaging-speed=280                         
blowout-speed=320                          
flaps-position.0=0                                                            
flaps-position.1=1                                 
flaps-position.2=1                               
flaps-position.3=1                       
flaps-position.4=1                    
flaps-position.5=1                       
flaps-position.6=1                         
flaps-position.7=1                                             
flaps-position.8=1                        
lift_scalar=1
drag_scalar=1
pitch_scalar=1

[smokesystem]
smoke.0=-24.78, 8.40, 3.33, db72smoke
smoke.1=-24.78, -8.40, 3.33, db72smoke
smoke.2=-40.60, 0.00, 2.53, db72smoke


[GPWS]
max_warning_height=0
sink_rate_fpm=-1500
excessive_sink_rate_fpm=-2000
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-100

[pneumatic_system]
max_pressure=18
bleed_air_scalar=0.15

[deice_system]
structural_deice_type=0

[vacuum_system]
max_pressure=5.15
vacuum_type=0
electric_backup_pressure=0
engine_map=1, 1, 1, 0