[fltsim.0]
title=b727   
sim=b727
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=N72720
atc_airline=American Airlines
atc_flight_number=A9286
ui_manufacturer=Boeing
ui_type="727-200"
ui_variation="American Airlines"
description=The 727-100 had been in service barely a year when Boeing began serious consideration of a stretched, greater capacity development.This resulted in the 727-200, which Boeing announced it was developing in August 1965. The 727-200 was essentially a minimum change development of the 100, the only major change being the 6.10m (20ft) fuselage stretch, which increased maximum seating to 189 passengers. The 727-200's stretch consisted of two 3.05m (10ft) plugs, one forward and one rear of the wing. Otherwise the 727-100 and 200 shared common engines, fuel tank capacity and the same maximum takeoff weight.The first flight of the 727-200 occurred on July 27 1967, with certification granted in late November that year. The -200 was placed into service by launch customer Northeast Airlines (this airline was later acquired by Delta) the following month, by which time total 727 orders for both models had exceeded 500.The 727-200 helped broaden the sales appeal of the 727 considerably and snared significant sales.



[fltsim.1]
title=b727  Paint1
sim=b727 
model=
panel=
sound=
texture=1
kb_checklists=
kb_reference=
atc_id=N2812W
atc_airline=Viasa
atc_flight_number=A9265
ui_manufacturer=Boeing
ui_type="727-200"
ui_variation="Viasa"
description=The 727-100 had been in service barely a year when Boeing began serious consideration of a stretched, greater capacity development.This resulted in the 727-200, which Boeing announced it was developing in August 1965. The 727-200 was essentially a minimum change development of the 100, the only major change being the 6.10m (20ft) fuselage stretch, which increased maximum seating to 189 passengers. The 727-200's stretch consisted of two 3.05m (10ft) plugs, one forward and one rear of the wing. Otherwise the 727-100 and 200 shared common engines, fuel tank capacity and the same maximum takeoff weight.The first flight of the 727-200 occurred on July 27 1967, with certification granted in late November that year. The -200 was placed into service by launch customer Northeast Airlines (this airline was later acquired by Delta) the following month, by which time total 727 orders for both models had exceeded 500.The 727-200 helped broaden the sales appeal of the 727 considerably and snared significant sales.





[fltsim.2]
title=b727  Paint2
sim=b727 
model=
panel=
sound=
texture=2
kb_checklists=
kb_reference=
atc_id=N2812W
atc_airline=Northwest
atc_flight_number=A9265
ui_manufacturer=Boeing
ui_type="727-200"
ui_variation="Northwest"
description=The 727-200 had been in service barely a year when Boeing began serious consideration of a stretched, greater capacity development.This resulted in the 727-200, which Boeing announced it was developing in August 1965. The 727-200 was essentially a minimum change development of the 100, the only major change being the 6.10m (20ft) fuselage stretch, which increased maximum seating to 189 passengers. The 727-200's stretch consisted of two 3.05m (10ft) plugs, one forward and one rear of the wing. Otherwise the 727-100 and 200 shared common engines, fuel tank capacity and the same maximum takeoff weight.The first flight of the 727-200 occurred on July 27 1967, with certification granted in late November that year. The -200 was placed into service by launch customer Northeast Airlines (this airline was later acquired by Delta) the following month, by which time total 727 orders for both models had exceeded 500.The 727-200 helped broaden the sales appeal of the 727 considerably and snared significant sales. 


[fltsim.3]
title=b727  Paint3
sim=b727 
model=
panel=
sound=
texture=3
kb_checklists=
kb_reference=
atc_id=N2812W
atc_airline=Lufthansa
atc_flight_number=2184
ui_manufacturer=Boeing
ui_type="727-200"
ui_variation="Lufthansa"
description=The 727-200 had been in service barely a year when Boeing began serious consideration of a stretched, greater capacity development.This resulted in the 727-200, which Boeing announced it was developing in August 1965. The 727-200 was essentially a minimum change development of the 100, the only major change being the 6.10m (20ft) fuselage stretch, which increased maximum seating to 189 passengers. The 727-200's stretch consisted of two 3.05m (10ft) plugs, one forward and one rear of the wing. Otherwise the 727-100 and 200 shared common engines, fuel tank capacity and the same maximum takeoff weight.The first flight of the 727-200 occurred on July 27 1967, with certification granted in late November that year. The -200 was placed into service by launch customer Northeast Airlines (this airline was later acquired by Delta) the following month, by which time total 727 orders for both models had exceeded 500.The 727-200 helped broaden the sales appeal of the 727 considerably and snared significant sales. 




[fltsim.4]
title=b727   Paint4
sim=b727
model=
panel=
sound=
texture=4
kb_checklists=
kb_reference=
atc_id=N72720
atc_airline=Northwest
atc_flight_number=2184
ui_manufacturer=Boeing
ui_type="727-200"
ui_variation="Northwest"
description=The 727-100 had been in service barely a year when Boeing began serious consideration of a stretched, greater capacity development.This resulted in the 727-200, which Boeing announced it was developing in August 1965. The 727-200 was essentially a minimum change development of the 100, the only major change being the 6.10m (20ft) fuselage stretch, which increased maximum seating to 189 passengers. The 727-200's stretch consisted of two 3.05m (10ft) plugs, one forward and one rear of the wing. Otherwise the 727-100 and 200 shared common engines, fuel tank capacity and the same maximum takeoff weight.The first flight of the 727-200 occurred on July 27 1967, with certification granted in late November that year. The -200 was placed into service by launch customer Northeast Airlines (this airline was later acquired by Delta) the following month, by which time total 727 orders for both models had exceeded 500.The 727-200 helped broaden the sales appeal of the 727 considerably and snared significant sales.














Category = airplane

[CameraDefinition.0]
Title = "Right Side Window"
Guid = {54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC}
Description = View of the right wing from the passenger cabin
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.8
ShowWeather = Yes
InitialXyz = 3.2, 1.8, -5
InitialPbh = 5, 0, 100
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title = "Left Side Window"
Guid = {0ae3f864-da10-4e5a-977c-b9bba47d6f7a}
Description = View of the left wing from the passenger cabin
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.8
ShowWeather = Yes
InitialXyz = -3.2, 1.8, -5
InitialPbh = 5, 0, 260
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title = "Landing Gear"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the landing gear and left wing inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .52
ShowWeather = Yes
InitialXyz = -3.3, -1.8, -11
InitialPbh = 0, 0, 17
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.3]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0, 6.5, -55.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.4]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 30.8, 1.6, 4.0
InitialPbh = 6, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.5]
Title = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -30.8, 1.6, 4.0
InitialPbh = 6, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum

[CameraDefinition.001]
Title = "Right Seat"
Guid = {8ff6c134-098d-409f-baec-caba3f683f98}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 0.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.50, 0.0, 0.0
InitialPbh=2, 0, 0

[CameraDefinition.002]
Title = "Center Console"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.9
SmoothZoomTime = 2.0
ZoomPanScalar = 2.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.45, 0.30, -0.15
InitialPbh=84.2, 0, 0

[CameraDefinition.003]
Title = "Engine Controls"
Guid = {a5741a54-ea6d-4580-9709-c99161e38a83}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.9
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.45, 0.10, 0.35
InitialPbh=85.0, 0, 0

[CameraDefinition.004]
Title = "Overhead Panel"
Guid = {4ca337db-ae88-4c5f-96ea-ddebbd2a86fe}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.7
SmoothZoomTime = 2.0
ZoomPanScalar = 1.15
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.47, -0.62, -0.4
InitialPbh=-58.0, 0, 0









[General]
atc_type=BOEING
atc_model=B722
editable=0
performance=Cruise Speed:  FL280-390\nMaximum Range: 1,810 nm\nService Ceiling: 39,000 ft\nEmpty Weight: 97,770 lbs\nFuel Weight: 54,203 lbs (8,090 US Gal) \nMax Takeoff Weight: 190,500 lbs\nMax Landing Weight: 161,000 lbs\nVmo\/Mmo: 375kts\/M0.91\n                  ( <FL100\/>FL100\/Mach)\nClimb:           250kts\/300kts\/M0.76\nMax Cruise:  250kts\/350kts\/M0.82\nDescent:       250kts\/280kts\/M0.77
Category=airplane

[pitot_static]
vertical_speed_time_constant=50
pitot_heat=1.000000

[WEIGHT_AND_BALANCE]
max_gross_weight=190500
empty_weight=97770

reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=1.826, 0.000, 1.908

max_number_of_stations=8

station_load.0=    "190.0,   68.170, -1.206,  4.683, Pilot"              
station_load.1 =   "190.0,   68.170,  1.206,  4.683, First Officer"
station_load.2 =   "190.0,   64.527,  0.000,  4.683, Flt Engineer"         
station_load.3 =   "260.0,   60.191, -1.895,  4.683, 2-Flt Attendant"        
station_load.4 ="33150.0,  16.652,  0.000,  4.683, 170-Coach Pax"        
station_load.5 =    "260.0, -28.794,  0.000,  4.683, 2-Flt Attendant"     
station_load.6 =   "1187.2,  33.998,  0.000, -0.347, Forward Cargo"
station_load.7=    "1362.8, -16.826,  0.000, -0.347, Aft Cargo"

;Moments of Inertia
empty_weight_pitch_MOI=10000000
empty_weight_roll_MOI=5000000
empty_weight_yaw_MOI=9300000
empty_weight_coupled_MOI=0

[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 = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[GeneralEngineData]
engine_type=1
Engine.0=-43.018, -8.958, 5.551
Engine.1 =-60.711,  0.000, 5.030
Engine.2=-43.018, 8.958, 5.551
fuel_flow_scalar=1.941
min_throttle_limit=-0.500
max_contrail_temperature=-30

[SMOKESYSTEM]
smoke.0=5.551, -58.018,-8.958, smoke_jt8d                
smoke.1=5.030, -75.711, 0.000, smoke_jt8d
smoke.2=5.551, -58.018, 8.958, smoke_jt8d

[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=9.852
rated_N2_rpm=12250.000
static_thrust=17400.000
afterburner_available=0
reverser_available=1

[jet_engine]
thrust_scalar=1.000

[electrical]
max_battery_voltage=28
generator_alternator_voltage=28
max_generator_alternator_amps=60
engine_generator_map=1,1,1
electric_always_available=1
autopilot=0, 5, 17
avionics_bus=0, 10, 17
avionics=1, 5, 17
pitot_heat=0, 15, 17
additional_system=0, 20, 17
marker_beacon=1, 2, 17
gear_warning=0, 2, 17
fuel_pump=0, 5, 17
starter1=0, 20, 17
starter2=0, 20, 17
starter3=0, 20, 17
light_nav=0, 5, 17
light_beacon=0, 5, 17
light_landing=0, 5, 17
light_taxi=0, 5, 17
light_strobe=0, 5, 17
light_panel=0, 5, 17
auto_brakes=0, 15, 17
hydraulic_pump=0, 2, 17
fuel_transfer_pump=0, 5, 17

        //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, 60.648, 0.000, -7.800, 1056.000, 0.000, 1.333, 50.000, 0.500, 3.500, 0.750, 8.000, 8.000, 0.000, 0.000, 270.000
point.1=1.000, -2.602, -9.375, -8.350, 1320.000, 1.000, 2.083, 0.000, 0.500, 4.500, 0.990, 8.200, 8.200, 2.000, 0.000, 270.000
point.2=1.000, -2.602, 9.375, -8.350, 1320.000, 2.000, 2.083, 0.000, 0.500, 4.500, 0.990, 8.200, 8.200, 3.000, 0.000, 270.000
point.3=2.000, 63.140, 0.000, -2.775, 60.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.4=2.000, 0.000, 0.000, -3.469, 60.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.5=2.000, -35.386, 0.000, -1.387, 60.000, 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, -21.189, -52.715, 0.688, 60.000, 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, -21.189, 52.715, 0.688, 60.000, 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=8

static_pitch=-1.110
static_cg_height=8.300
gear_system_type=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.050
flap_limit_idle=15.5
flap_limit_power=25.5

[brakes]
parking_brake=1
toe_brakes_scale=0.550
auto_brakes=4

[hydraulic_system]
normal_pressure=3000.0
electric_pumps=0
engine_map=1,1,1,0

[Views]
eyepoint=68.170, -1.206, 5.898

[Flaps.0]  //Sets initial trailing drag, lift, and visuals
type=1
span-outboard=0.800
extending-time=30.000
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
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=0.500
drag_scalar=0.200
pitch_scalar=0.000
system_type=1

[Flaps.1]  //Adjusts trailing drag factors
type=1
span-outboard=0.800
extending-time=30.000
flaps-position.0=0.000
flaps-position.1=4.435
flaps-position.2=2.779
flaps-position.3=10.623
flaps-position.4=25.389
flaps-position.5=48.874
flaps-position.6=91.302
flaps-position.7=185.320
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=0.000
drag_scalar=0.200
pitch_scalar=0.000
system_type=1

[Flaps.2]  //Adjusts trailing lift factors
type=1
span-outboard=0.800
extending-time=30.000
lift_scalar=0.800
drag_scalar=0.000
pitch_scalar=0.000
flaps-position.0=0.000
flaps-position.1=5.900
flaps-position.2=5.750
flaps-position.3=4.783
flaps-position.4=8.762
flaps-position.5=11.003
flaps-position.6=14.831
flaps-position.7=22.851
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=0.500
drag_scalar=0.000
pitch_scalar=0.000
system_type=1

[Flaps.3]  //Sets leading visual graphics
type=2
span-outboard=0.800
extending-time=6.000
flaps-position.0=0.000, 0.000
flaps-position.1=1.000, 0.000
flaps-position.2=2.000, 0.000
damaging-speed=250.000
blowout-speed=300.000
lift_scalar=0.000
drag_scalar=0.000
pitch_scalar=0.000
system_type=1


[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=1, 8.00,  0.00, -3.65, fx_beaconb ,
light.1=1, 27.70, 0.00, 11.40, fx_beaconh,
light.2=2, -30.00, -60.01,  2.30, fx_strobeh ,
light.3=2, -30.00,  60.00,  2.30, fx_strobeh ,
light.4=2, -96.70, 0.00, 24.60, fx_strobe ,
light.5=3, -96.70, 0.00, 24.60, fx_navwhi ,
light.6=3, -30.00, -60.1, 2.30, fx_navredm ,
light.7=3, -30.00, 60.0,  2.30, fx_navgrem
//light.8=4,  68.60, 2.00, 4.50, fx_vclighth ,
light.9=4, 68.60,-0.50, 4.50, fx_vclighth ,
light.10=4, 64.60,-2.50, 5.50, fx_vclight ,
//light.11=4, 64.60, 2.00, 5.50, fx_vclight , 











[keyboard_response]      
elevator=150, 250   
aileron=150, 250
rudder=150, 250

[direction_indicators]
direction_indicator.0=2

[attitude_indicators]
attitude_indicator.0=2 

[turn_indicators]
turn_indicator.0=1,0

[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
visual_damage=1
//windshield_rain_effect_available = 1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=100
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm=99
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8
max_pitch=10.0
max_pitch_acceleration=1.5
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=1.00
default_pitch_mode=0
default_bank_mode=0

[fuel]  //8090 US Gallons Total
Center1=10.851, 0.000, -0.520, 4530.000, 0.000
LeftMain=5.685, -16.710, 0.000, 1780.000, 0.000
RightMain=5.685, 16.710, 0.000, 1780.000, 0.000
fuel_type=2
number_of_tank_selectors=1                    
electric_pump=0

[airplane_geometry]
wing_area=1650.000
wing_span=108.000
wing_root_chord=25.151
wing_dihedral=3.000
wing_incidence=2.000
wing_twist=-0.500
oswald_efficiency_factor=0.800
wing_winglets_flag=0
wing_sweep=32.000
wing_pos_apex_lon=24.118
wing_pos_apex_vert=0.867
htail_area=376.000
htail_span=35.761
htail_pos_lon=-55.471
htail_pos_vert=24.284
htail_incidence=0.000
htail_sweep=42.000
vtail_area=290.000
vtail_span=15.092
vtail_sweep=57.000
vtail_pos_lon=-32.784
vtail_pos_vert=10.755
elevator_area=107.996
aileron_area=67.404
rudder_area=66.171
elevator_up_limit=27.000
elevator_down_limit=17.000
aileron_up_limit=17.000
aileron_down_limit=17.000
rudder_limit=25.000
elevator_trim_limit=9.500
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
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000

[Reference Speeds]
flaps_up_stall_speed=146.000
full_flaps_stall_speed=122.000
cruise_speed=488.000
max_mach=0.910
max_indicated_speed=375.000

[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

[stall_warning]
type=2
stick_shaker=1
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0