//Premier Aircraft Design
//Copyright 2008
//Barry Blaisdell, Jean-Pierre Brisard, Bob May
//Model for FSX

[fltsim.0]
title=MD11F_X_UPS
sim=MD-11F
sound=x
model=
panel=cargo-x
texture=ups
kb_checklists=MD-11F_check
kb_reference=MD-11F_ref
atc_id=N270UP
atc_airline=UPS
atc_flight_number=188
atc_heavy=1
ui_manufacturer=McDonnell-Douglas/Boeing
ui_type=MD-11F
ui_variation=Cargo UPS
ui_typerole=Commercial Airliner
ui_createdby=Premier Aircraft design
visual_damage=0
description=McDonnell-Douglas/Boeing MD-11F\nMedium/Long Range Freighter\nThe MD-11 is a modernised, slightly stretched and re-engined development of the DC-10 trijet.

Category = airplane


[General]
atc_type=McDonnell Douglas
atc_model=MD11
performance=Power: 3 Pratt&Whitney PW4462 Turbofans @ 62,000lbs Thrust ea\nCruise Speed\tMach .82@FL310\nMaximum Range\t7,000 nm\nService Ceiling\t45,000 ft\nMax Takeoff Weight\t602,500 lb
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 = 0.9
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 = 1.0
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 = -3.6, -1.8, -11
InitialPbh = 0, 0, 18
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, 9.0, -80.0
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 = 0.75
ShowWeather = Yes
InitialXyz = 30.8, 1.6, 4.0
InitialPbh = 6, 0, 280
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 = 0.75
ShowWeather = Yes
InitialXyz = -30.8, 1.6, 4.0
InitialPbh = 6, 0, 80
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 = .5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.35, 0.0, 0.0
InitialPbh=2, 0, 0

[CameraDefinition.002]
Title = "Radio Stack"
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 = 1.1
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.66, 0.1, 0.15
InitialPbh=33, 0, 0

[CameraDefinition.003]
Title = "Engine Controls"
Guid = {195EAB58-9E4A-3E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.85
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.35, 0.1, 0.05
InitialPbh=31, 0.0, 0.0

[General]
atc_type=McDonnellDouglas
atc_model=MD11
performance=Power: 3 Pratt&Whitney PW4462 Turbofans @ 62,000lbs Thrust ea\nCruise Speed\tMach .82@FL310\nMaximum Range\t7,000 nm\nService Ceiling\t45,000 ft\nMax Takeoff Weight\t602,500 lb
Category=airplane



[flight_tuning]
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.2//1.000 
induced_drag_scalar=1.2//1.000 
elevator_effectiveness=1.000 
aileron_effectiveness=1.100 
rudder_effectiveness=1.100 
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 

[Views]
eyepoint=93.10, -2.8, 6.90

[weight_and_balance]
max_gross_weight = 630500
empty_weight = 249500
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 12540000
empty_weight_roll_MOI = 6800000
empty_weight_yaw_MOI = 14500000
empty_weight_coupled_MOI = 0.0000
max_number_of_stations = 10

station_load.0 = 170.0, 94.5, -2.50, 5.000, Pilot // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170.0, 94.5, 2.50,  5.000, Co-Pilot
station_load.2 = 170.0, 91.5, -4.00, 5.000, Flt Crew
station_load.3 = 170.0, 91.5, 4.00,  5.000, Flt Crew
station_load.4 = 170.0, 92.0, 0.00,  5.000, Flt Crew
station_load.5 = 35000, 52.0, 0.00, 0.000, Forward Pax
station_load.6 = 35000, 0.00, 0.00, 0.000, Ctr Pax
station_load.7 = 30000, -10.00, 0, 0, Aft Pax
station_load.8=  1000, -22.00, 0, 0, Aft Ballast

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -34.300,-78.800, 2.500, fx_navredh ,
light.1=3, -34.300, 78.800, 2.500, fx_navgreh ,
light.2=2, -43.800,-79.000, 2.400, fx_strobeh ,
light.3=2, -43.800, 79.000, 2.400, fx_strobeh ,
light.4=1, 22.00,   0.00,  13.0, fx_beaconb ,
light.5=1, -22.00,   0.00, -8.10, fx_beaconb ,
light.6=4, 95.00,   -1.50,  5.00, fx_vclightwhi ,
light.7=4, 95.00,   1.50,  5.00, fx_vclightwhi ,
light.8=4, 95.50,   0.00,  3.50, fx_vclightwhi ,

[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

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

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second

[autopilot]
use_no_default_pitch=1
use_no_default_bank=1
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;
max_pitch=8.0
max_pitch_acceleration=1.0
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=20.0
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 =1.0
default_pitch_mode=0
default_bank_mode=0


[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

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1 =0, 0, -6, 9600, 0
LeftMain =-13, -45.0, 1.00, 14000, 0
RightMain =-13, 45.0, 1.00, 14000, 0
fuel_type =2
number_of_tank_selectors =1
electric_pump=1


//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, 74.720, 0.000, -16.0, 1200.000, 0.000, 1.500, 50.000, 0.800, 2.500, 0.800, 4.000, 4.000, 0.000, 0.000, 0.000
point.1=1.000, -9.467, -17.57, -16.5, 1600.000, 1.000, 2.000, 0.000, 1.800, 2.500, 0.800, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1.000, -9.467, 17.57, -16.5, 1600.000, 2.000, 2.000, 0.000, 1.800, 2.500, 0.800, 5.000, 5.000, 3.000, 0.000, 0.000
point.3=2.000, -48.000, -87.000, 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, -48.000, 87.000, 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, -90.50, 0.000, 4.000, 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, 102.600, 0.000, 2.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7=5.000, -30.900,  0.000, -7.300, 1600, 0.000, 0.000, 50.000, 0.000,  0.000, 1.000, 1.100, 1.500,0.000, 0.000, 0.000
static_pitch=0.000
static_cg_height=16.000
gear_system_type=0

[keyboard_response]
elevator =150.000000, 250.000000
aileron =150.000000, 250.000000
rudder =150.000000, 250.000000

[airplane_geometry]
wing_area =3650.000
wing_span =169.5
wing_root_chord =35.0
wing_dihedral =4.0
wing_incidence =2
wing_twist =0
oswald_efficiency_factor =0.85
wing_winglets_flag =1
wing_sweep =35.000000
wing_pos_apex_lon =29.000000
wing_pos_apex_vert =-3.000000
htail_area =900.000000
htail_span =59
htail_pos_lon =-64.000
htail_pos_vert =10.000000
htail_incidence =1.000000
htail_sweep =32.000000
vtail_area =605.000000
vtail_span =32.00000
vtail_sweep =35.000000
vtail_pos_lon =-58.0000
vtail_pos_vert =11.0000
elevator_area =228.65
aileron_area =147.431000
rudder_area =105.600000
elevator_up_limit =37.6
elevator_down_limit =27.1
aileron_up_limit =20
aileron_down_limit =20
rudder_limit =23
elevator_trim_limit =12
spoiler_limit =60
aileron_to_spoileron_gain =2.050000
min_ailerons_for_spoilerons =6
min_flaps_for_spoilerons =1.000000
spoilerons_available =1
auto_spoiler_available=1
spoiler_extension_time=1.000000
positive_g_limit_flaps_up=4.005342
positive_g_limit_flaps_down=2.990385
negative_g_limit_flaps_up=-2.990385
negative_g_limit_flaps_down=-1.997863

[electrical]
max_battery_voltage =24
generator_alternator_voltage =28
max_generator_alternator_amps =190
flap_motor =0, 5, 17
gear_motor =0, 5, 17
autopilot =0, 5, 10
avionics_bus =0, 10, 15
avionics =1, 5, 15
pitot_heat =0, 15, 10
additional_system =0, 20, 10
marker_beacon =1, 2, 2
gear_warning =0, 2, 2
fuel_pump =0, 5, 15
starter1 =0, 20, 15
starter2 =0, 20, 15
starter3 =0, 20, 15
light_nav =0, 5, 12
light_beacon =0, 5, 10
light_landing =0, 5, 10
light_taxi =0, 5, 10
light_strobe =0, 5, 10
light_panel =0, 5, 10
hydraulic_pump =0, 2, 10
fuel_transfer_pump =0, 5, 10
light_recognition =0, 5, 10
light_wing =0, 5, 10
light_logo =0, 5, 10
electric_always_available =1

[Flaps.0]
span-outboard=0.500000
extending-time=12
system_type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=1.000000,0.000000
flaps-position.2=6.000000,0.000000
flaps-position.3=21.00000,0.000000
flaps-position.4=28.00000,0.000000
flaps-position.5=35.00000,0.000000
flaps-position.6=50.00000,0.000000
lift_scalar =1.30
drag_scalar =1.50
pitch_scalar=1.00
type=1

[flaps.1]    
type =2                                    
span-outboard =0.8                                 
extending-time =3                                  
flaps-position.0 =0
flaps-position.1 =1.0                                  
lift_scalar =1.10
drag_scalar =1.50
pitch_scalar=1.00
system_type =1                                                              

[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type =1
fuel_flow_scalar =0.810
engine.0 =14.25, -27, -7.0,
engine.1 =14.25, 27, -7.0,
engine.2 =-72, 0, 17.6,
min_throttle_limit=-0.100

[TurbineEngineData]
fuel_flow_gain =0.001                 //Gain on fuel flow
inlet_area =24.0                              //Square Feet, engine nacelle inlet area
rated_N2_rpm =29920                            //RPM, second stage compressor rated value
static_thrust =60000                           //Lbs, max rated static thrust at Sea Level
afterburner_available =0                       //Afterburner available?
reverser_available =1                          //Thrust reverser available?

[jet_engine]
thrust_scalar =1.10//1.2

[Reference Speeds]
flaps_up_stall_speed    =150.0                 //Knots True (KTAS)
full_flaps_stall_speed  =120.0                 //Knots True (KTAS)
cruise_speed            =320.0                 //Knots True (KTAS)
max_mach                =0.85
max_indicated_speed     =325                   //Red line (KIAS)

[direction_indicators]
direction_indicator.0=3,0 

[pitot_static]
vertical_speed_time_constant=100
pitot_heat=1.000000

[brakes]
toe_brakes_scale=0.800
parking_brake=1
auto_brakes=4

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.783101
flap_limit_idle=22.918312

[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,0
normal_pressure=3000.000000
[stall_warning]
type=1
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[TailHook]
tailhook_length=1                              ;(feet)
tailhook_position = 92.395, 2.694, 6.225           ;(feet) longitudinal,lateral, vertical positions from datum
cable_force_adjust = 1.0

[folding_wings]
wing_fold_system_type=4
fold_rates=1.5,1.5

[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1

[pneumatic_system]
max_pressure=5.000000
bleed_air_scalar=0.000000

[deice_system]
structural_deice_type=0