[fltsim.0]
title=FSP Advanced Products MD-11 Delta old colors
sim=md11
model=vc
panel=
sound=
texture=DAL
atc_id=DAL
atc_airline=Delta
atc_flight_number=591
ui_manufacturer=McDonnell-Douglas/Boeing
ui_type=McDonnell Douglas  MD-11
ui_variation=Delta with VC
description=Overland Co.,Ltd. Products --- McDonnell Douglas MD-11\n\nL1 L2 Cabin Door      [Shift+E] then [1]\nCargo Door                [Shift+E] then [2]\nL4/R4 Cabin Door          Wing Fold/Extend



[General]
visual_damage=0 // 0=off, 1=on
atc_type=MD
atc_model=MD11
editable=0
performance=Cruise Speed\t 473kt\nMaximum Range\t6,821 nm\nService Ceiling\t32,400 ft\nMax Takeoff Weight\t602,555 lb\nSeating\t\t270 to 405\nCargo Capacity\t3,552 CU ft\n


[WEIGHT_AND_BALANCE]
max_gross_weight=602555                      // (pounds)
empty_weight=286965                          // (pounds)

reference_datum_position=0, 0, 0             // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0, 0, 0             // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=  2376, 0, 0, 1.75, Crew
station_load.1= 17300, 0, 0, 1.75, Cargo
station_load.2=  3168, 0, 0, 0.00, Farst
station_load.3=  7524, 0, 0, 0.00, Business
station_load.4= 26136, 0, 0, 0.00, Economy

;Moments of Inertia
empty_weight_pitch_MOI= 8000000
empty_weight_roll_MOI= 15500000
empty_weight_yaw_MOI=  12300000
empty_weight_coupled_MOI=0.0

[flight_tuning]
cruise_lift_scalar=1.1
parasite_drag_scalar=1.16
induced_drag_scalar=1.200
elevator_effectiveness=1.08
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                                //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0= 10.2, -26.6, -8.4                  //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-87.5,   0.0, 14.4                  //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2= 10.2,  26.6, -8.4                  //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1                           //Scalar for fuel flow efficiency
min_throttle_limit=-0.250000

[TurbineEngineData]
fuel_flow_gain=0.00200                        //Gain on fuel flow
inlet_area=76.0                               //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=1.00

[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, 75.42, 0.00, -15.50, 1181.1, 0, 2.220, 70.0, 1.43, 2.0, 0.8235, 7.0, 8.0, 0, 185.0, 250.0 //nose
point.1=1, -7.50, -18.00, -15.80, 1574.8, 1, 2.520, 0.0, 1.15, 2.8, 0.8470, 8.1, 10.1, 2, 185.0, 250.0 //left main
point.2=1, -7.50, 18.00, -15.80, 1574.8, 2, 2.520, 0.0, 1.15, 2.8, 0.8470, 8.1, 10.1, 3, 185.0, 250.0 //right main
point.3=1, -7.75, 0.00, -15.60, 1574.8, 0, 2.520, 0.0, 1.55, 2.8, 0.8470, 8.1, 10.1, 0, 185.0, 250.0 //center main

point.4=2, -14.17, -84.80, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 //left wing
point.5=2, -14.17, 84.80, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 //right wing
point.6=2, -83.33, 0.00, 2.50, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 
point.7=2, 96.67, 0.00, -3.75, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 //aft fuselage scrape

static_pitch=-0.16
static_cg_height=14.8
gear_system_type=0

[Views]
eyepoint=91.8, -1.55, 5.6,

[flaps.0]
type=1                                    	 // 1 - tail, 2 - lead
span-outboard=0.2                                // 0.0 .. 1.0
extending-time=25                                // seconds
flaps-position.0=0                               // degrees
flaps-position.1=0                               // degrees
flaps-position.2=15                               // degrees
flaps-position.3=22                              // degrees
flaps-position.4=25                              // degrees
flaps-position.5=28                              // degrees
flaps-position.6=35                              // degrees
flaps-position.7=50                              // degrees
damaging-speed=255                               // KIAS
blowout-speed=300                                // KIAS
lift_scalar=0.55
drag_scalar=0.55
pitch_scalar=0.55
system_type=1                                    //Hydraulic

[flaps.1]
type=1                                           // 1 - tail, 2 - lead
span-outboard=0.8                                // 0.0 .. 1.0
extending-time=23                                // seconds
flaps-position.0=0                               // degrees
flaps-position.1=0                               // degrees
flaps-position.2=15                               // degrees
flaps-position.3=22                              // degrees
flaps-position.4=25                              // degrees
flaps-position.5=28                              // degrees
flaps-position.6=35                              // degrees
flaps-position.7=50                              // degrees
damaging-speed=255                               // KIAS
blowout-speed=300                                // KIAS
lift_scalar=0.35
drag_scalar=0.35
pitch_scalar=0.35
system_type=1                                    //Hydraulic

[flaps.2]
type=2                                    	// 1 - tail, 2 - lead
span-outboard=0.5                               // 0.0 .. 1.0
extending-time=4                                // seconds
flaps-position.0=0                              // degrees
flaps-position.1=0.5                            // degrees
flaps-position.2=0.5                            // degrees
flaps-position.3=0.5                            // degrees
flaps-position.4=0.5                            // degrees
flaps-position.5=1.0                            // degrees
flaps-position.6=1.0                            // degrees
flaps-position.7=1.0                            // degrees
damaging-speed=260                              // KIAS
blowout-speed=300                               // KIAS
lift_scalar=0.05
drag_scalar=0.05
pitch_scalar=0.05
system_type=1                                   //Hydraulic

[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

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

light.1 = 1, 11.30, 0.00, 12.20, fx_beaconb ,
light.2 = 1, 11.30, 0.00, 12.20, fx_beaconb ,
light.3 = 1, -38.00, 0.00, -8.00, fx_beaconh ,
light.4 = 1, -38.00, 0.00, -8.00, fx_beaconh ,
light.5 = 5, 28.48, 9.94,  1.78, fx_navwhi ,
light.6 = 5, 28.48,-9.94,  1.78, fx_navwhi ,
light.7 = 5, 30.48, 9.36, -1.32, fx_navwhi ,
light.8 = 5, 30.48,-9.36, -1.32, fx_navwhi ,
light.9=  4,  91.30,    -1.15,  1.05, fx_vclighth1,
light.10= 4,  89.80,    -0.15,  4.55, fx_vclight,
light.11= 5,  50.10,   5.65,  1.52, MD80_INSPEC ,   //right wing inspection light
light.11= 5,  50.10,  -5.65,  1.52, MD80_INSPEC ,   //left wing inspection light


[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

[fuel]
Center1=  -14.0,   0.0, -5.0, 9621.2, 3.0     	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2=   11.0,   0.0, -5.0,14727.0, 3.0     	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=  -4.0, -35.0,  0.0, 6107.5, 3.0     	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain= -4.0,  35.0,  0.0, 6107.5, 3.0     	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center3=   21.0,   0.0, -5.0, 1958.0, 3.0     	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2                                   	//Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area=3648.8                	//Square feet
wing_span=169.6                 	//Feet
wing_root_chord=34.0                  	//Feet
wing_dihedral=6.2                   	//Degrees
wing_incidence=1.0                   	//Degrees
wing_twist=0.0                  	//Degrees
oswald_efficiency_factor=0.85           //Measure of lift effeciency of wing
wing_winglets_flag=1                    //Are winglets available?
wing_sweep=34.5                  	//Degrees, wing leading edge
wing_pos_apex_lon=30.2                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=1.0                  //Feet, vertical distance from reference point, positive going up
htail_area=911.0                	//Square feet
htail_span=58.7                  	//Feet
htail_pos_lon=-70.0                	//Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=8.0                   	//Feet, vertical distance from reference point, positive going up
htail_incidence=-1.2                   	//Degrees
htail_sweep=32.0                  	//Degrees, horizontal tail leading edge
vtail_area=623.0                 	//Square feet
vtail_span=30.3                  	//Feet, tip to body
vtail_sweep=35.0                  	//Degrees, vertical tail leading edge
vtail_pos_lon=-62.3                	//Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=12.0                   	//Feet, vertical distance from reference point, positive going up
elevator_area=167.0                 	//Square feet
aileron_area=120.0                  	//Square feet
rudder_area=138.0                 	//Square feet
elevator_up_limit=35.0                  //Degrees
elevator_down_limit=20.0                //Degrees
aileron_up_limit=25.0                  	//Degrees
aileron_down_limit=15.0                 //Degrees
rudder_limit=25.0                  	//Degrees
elevator_trim_limit=20.0                //Degrees
spoiler_limit=50.0                  	//Degrees
spoilerons_available=1                  //Spoilerons Available?
aileron_to_spoileron_gain=3             //Aileron to spoileron gain
min_ailerons_for_spoilerons=10          //Degrees
min_flaps_for_spoilerons=0              //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed=150.0              //Knots True (KTAS)
full_flaps_stall_speed=120.0            //Knots True (KTAS)
cruise_speed=322.0                 	//Knots True (KTAS)
max_indicated_speed=473.000000
max_mach=0.880000

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1500.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
use_no_default_pitch = 1 		// 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 		// 0 = Default to Wing Leveler mode, 1 = No default bank mode.
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


[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

[brakes]
toe_brakes_scale=0.489926		; brakes_scale 0 to none 1 to hard
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=2

[turn_indicators]
turn_indicator.0=1,0

[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.12,0.11                          ;Percent per second

[TailHook]
tailhook_length=4                             ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.0