[fltsim.0]
title=McDonnell-Douglas MD-81 Holmfrid Viking
sim=fsx_md81
model=
panel=
sound=
texture=SE-DMD
kb_checklists=
kb_reference=
atc_id=SE-DIP
atc_airline=SCANDINAVIAN
atc_id_color=
atc_flight_number=13
ui_manufacturer=Douglas
ui_type=MD-81
ui_variation=SAS SE-DMD Holmfrid Viking
description=Boeing - McDonnell-Douglas MD-81\n\nModel/VC Designer: Mitsushi Yutaka\nFDE/Sound/Panel/Effect Designer: Warren C. Daniel\nPaint Designer: Peefunk\n\nTypical 2-class: 152\nTypical 1-class: 172\n\nEngines: JT8D-217A\/C\nFuel Flow: 3000 pph per engine\n\nWing span: 107 ft 8 in (32.8 m)\nOverall Length: 147 ft 8 in (45.1 m)\nTail height: 29 ft 6 in (9.05 m)\n\nMTOW: 140,000 lb (63,503 kg)\nOEW: 77,888 lb (35,330 kg)\nPayload: 40,112 lb (18,195 kg)\nZFW: 118,000 lb (53,525 kg)
atc_heavy=0

[fltsim.1]
title=McDonnell-Douglas MD-81 
sim=fsx_md81
model=
panel=
sound=
texture=sas
kb_checklists=
kb_reference=
atc_id=EC-GOM
atc_airline=SCANDINAVIAN
atc_id_color=
atc_flight_number=13
ui_manufacturer=Douglas
ui_type=MD-81
ui_variation=SAS LN-RMT Olav
description=Boeing - McDonnell-Douglas MD-81\n\nModel/VC Designer: Mitsushi Yutaka\nFDE/Sound/Panel/Effect Designer: Warren C. Daniel\nPaint Designer: Peefunk\n\nTypical 2-class: 152\nTypical 1-class: 172\n\nEngines: JT8D-217A\/C\nFuel Flow: 3000 pph per engine\n\nWing span: 107 ft 8 in (32.8 m)\nOverall Length: 147 ft 8 in (45.1 m)\nTail height: 29 ft 6 in (9.05 m)\n\nMTOW: 140,000 lb (63,503 kg)\nOEW: 77,888 lb (35,330 kg)\nPayload: 40,112 lb (18,195 kg)\nZFW: 118,000 lb (53,525 kg)
atc_heavy=0


[General]
atc_type=MCDONNELDOUGLAS
atc_model=MD81
performance=Engines: JT8D-217 @ 20,850lbs each\nMTOW = 147,000 lbs\nMLW = 128,000 lbs (55% fuel)\nZFW = 107,870 lbs\nVmo\/Mmo = 340KIAS\/M0.84\nRange = 2990nm\nCruise = .76 - .80 mach\nMax Alt = 37,000 ft\n(speed book enclosed)\n\n
Category=airplane


[WEIGHT_AND_BALANCE]
max_gross_weight = 140000.000
empty_weight = 77880.000

reference_datum_position     =  77.0, 0, 0      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = -74.0, 0, 0      // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50

station_load.0 =   " 2450,  -69.5,  0.0,   0.0,  First Class-14 pax"     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.1 =   "24150,  -69.5,  0.0,   0.0,  Econ Class-138 pax"     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2 =   " 4504,  -69.5,  0.0,   0.0,  Fwd Cargo"                //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.3 =   " 4504,  -69.5,  0.0,   0.0,  Mid Cargo"                //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.4 =   " 4504,  -69.5,  0.0,   0.0,  Aft Cargo"                //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

;Moments of Inertia
empty_weight_pitch_MOI   = 1320029
empty_weight_roll_MOI    = 1112950
empty_weight_yaw_MOI     = 1415629
empty_weight_coupled_MOI = 0


[flight_tuning]
cruise_lift_scalar     = 1.00
parasite_drag_scalar   = 1.00
induced_drag_scalar    = 1.00
elevator_effectiveness = 1.75
aileron_effectiveness  = 3.50
rudder_effectiveness   = 1.00
pitch_stability        = 1.00
roll_stability         = 1.00
yaw_stability          = 1.00
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 = -103.6, -8.5, 0.6                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -103.6,  8.5, 0.6                    //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar        = 1.016                   //Scalar for fuel flow efficiency
min_throttle_limit=-0.649902


[TurbineEngineData]
bypass_ratio            = 1.740
fuel_flow_gain          = 0.002                 //Gain on fuel flow
inlet_area              = 10.4                  //Square Feet, engine nacelle inlet area
rated_N2_rpm            = 29920                 //RPM, second stage compressor rated value
static_thrust           = 21700                 //Lbs, max rated static thrust at Sea Level
afterburner_available   = 0                     //Afterburner available (Yes=0, No=1)
reverser_available      = 1                     //Thrust reverser available (Yes=0, No=1)


[jet_engine]
thrust_scalar = 1.0


[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
marker_beacon      = 0, 5 , 17.0
standby_vacuum     = 0, 5 , 17.0
auto_brakes        = 0, 5 , 17.0
hydraulic_pump     = 0, 20, 17.0
propeller_device   = 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]
// Nose Gear
point.0 = 1, -7.600, -0.700, -7.300, 3181.000, 0.000, 1.080, 70.000, 1.500, 2.500, 0.530,  7.000,  9.000, 0.000, 280.000, 300.000
point.1 = 1, -7.600,  0.700, -7.300, 3181.000, 0.000, 1.080, 70.000, 1.500, 2.500, 0.530,  7.000,  9.000, 0.000, 280.000, 300.000

// Main Gear - Left
point.2 = 1, -80.100, -9.810, -8.600, 3574.000, 1.000, 1.850,  0.000, 1.850, 3.000, 0.330, 10.000, 13.000, 2.000, 280.000, 300.000 
point.3 = 1, -80.100, -7.010, -8.600, 3574.000, 1.000, 1.850,  0.000, 1.850, 3.000, 0.330, 10.000, 13.000, 2.000, 280.000, 300.000 

// Main Gear - Right
point.4 = 1, -80.100,  7.010, -8.600, 3574.000, 2.000, 1.850,  0.000, 1.850, 3.000, 0.330, 11.000, 12.000, 3.000, 280.000, 300.000
point.5 = 1, -80.100,  9.810, -8.600, 3574.000, 2.000, 1.850,  0.000, 1.850, 3.000, 0.330, 11.000, 12.000, 3.000, 280.000, 300.000

// Scrape Points
point.6 = 2,    0.000,   0.000,  -1.000, 1200, 0, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.0, 5, 220, 280  // Nose
point.7 = 2, -139.210,   0.000,   3.000, 1200, 0, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.0, 6, 220, 280  // Tail Cone
point.8 = 2,  -95.500, -53.600,   3.000, 1200, 0, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.0, 9, 220, 280  // Left Wing Tip
point.9 = 2,  -95.500,  53.600,   3.000, 1200, 0, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.0, 4, 220, 280  // Right Wing Tip
point.10= 2,  -14.410,   0.000,   7.700, 1200, 0, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.0, 4, 220, 280  // Center Top Over Flightdeck
point.11= 2, -131.210,   0.000,  20.600, 1200, 0, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.0, 4, 220, 280  // Top of Center Tailplane
point.12= 2,  -18.830,   0.000,  -4.700, 1200, 0, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.0, 4, 220, 280  // Bottom of Fuselage - Forward
point.13= 2,  -97.300,   0.000,  -5.300, 1200, 0, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.0, 4, 220, 280  // Bottom of Fuselage - Aft

max_number_of_points = 21

static_pitch     = -0.800
static_cg_height =  7.500
gear_system_type=0


[Views]
eyepoint= -12.9, -1.40, 5.0    //(feet) longitudinal, lateral, vertical distance from reference datum


[Flaps.0] 
type= 1                                    
span-outboard= 0.200
extending-time= 20.000                               
system_type= 3
damaging-speed= 260.000
blowout-speed= 300.000
lift_scalar=  1.000
drag_scalar=  2.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 11.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 28.000, 0.000
flaps-position.4= 40.000, 0.000


[Flaps.1]
type= 1
span-outboard= 0.800
extending-time= 23.000
system_type= 3
damaging-speed= 260.000
blowout-speed= 300.000
lift_scalar=  1.000
drag_scalar=  2.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 11.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 28.000, 0.000
flaps-position.4= 40.000, 0.000


[Flaps.2]
type= 2
span-outboard= 0.500
extending-time= 13.000
system_type= 3
damaging-speed= 260.000
blowout-speed= 300.000
lift_scalar=  1.000
drag_scalar=  2.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.500, 0.000
flaps-position.2= 0.500, 0.000
flaps-position.3= 1.000, 0.000
flaps-position.4= 1.000, 0.000


[pitot_static]
vertical_speed_time_constant = 999                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000


[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo 
light.0 = 3, -95.50,  53.60,  0.80, fx_navgre ,
light.1 = 3, -95.50, -53.60,  0.80, fx_navred ,
light.2 = 2, -94.90, -53.60,  0.80, fx_strobeh ,
light.3 = 2, -94.90,  53.60,  0.80, fx_strobeh ,
light.4 = 3, -99.80, -53.70,  0.70, MD81_nav_yellow ,
light.5 = 3, -99.80,  53.70,  0.70, MD81_nav_yellow ,
light.6 = 1, -80.00,   0.00,  8.50, fx_beaconb  ,
light.7 = 1, -85.50,   0.00, -4.30, fx_beaconh  ,
light.8 = 6,   0.00,   0.00, -7.30, MD81-taxi-refl,
light.10 = 4,  -10.70,  2.80,   2.00, fx_vclight,
light.11 = 4,  -10.70,  -2.80,   2.00, fx_vclight,


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


[fuel]
Center1   =  -76.2,   0.0, -6.0,  580.0, 3.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2   =  -78.2,   0.0, -6.0,  580.0, 3.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  =  -78.7, -12.1, -4.0, 2920.0, 3.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain =  -78.7,  12.1, -4.0, 2920.0, 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               = 1209.0                //Square feet
wing_span               = 107.8                 //Feet
wing_root_chord         = 23.1                  //Feet
wing_dihedral           = 3.0                   //Degrees
wing_incidence          = -0.3                  //Degrees
wing_twist              = 0.0                   //Degrees
oswald_efficiency_factor= 0.8                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 24.5                  //Degrees, wing leading edge
wing_pos_apex_lon       = -61.0                 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_area              = 341.0                 //Square feet
htail_span              = 40.0                  //Feet
htail_pos_lon           = -134.0                //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.0                   //Degrees
htail_sweep             = 30.0                  //Degrees, horizontal tail leading edge
vtail_area              = 168.0                 //Square feet
vtail_span              = 14.8                  //Feet, tip to body
vtail_sweep             = 25.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -131.8                //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 10.9                  //Feet, vertical distance from reference point, positive going up
elevator_area           = 105.0                 //Square feet
aileron_area            = 18.0                  //Square feet
rudder_area             = 45.3                  //Square feet
elevator_up_limit       = 25.0                  //Degrees
elevator_down_limit     = 15.0                  //Degrees
aileron_up_limit        = 30.0                  //Degrees
aileron_down_limit      = 25.0                  //Degrees
rudder_limit            = 30.0                  //Degrees
elevator_trim_limit     = 20.00                  //Degrees
spoiler_limit           = 45.0                  //Degrees
spoilerons_available    = 1                     //Spoilerons Available?
aileron_to_spoileron_gain = 20                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10                 //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate
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    = 142.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 113.6                 //Knots True (KTAS)
cruise_speed            = 437.7                 //Knots True (KTAS)
max_indicated_speed=340.000000
max_mach=0.839990


[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= 100.0, 200.0
aileron= 100.0, 200.0
rudder= 100.0, 200.0


[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 800.0
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_max_rpm = 102
autothrottle_takeoff_ga= 1
pitch_takeoff_ga = 0.000;
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=30.000000
max_bank_acceleration=1.800000
max_bank_velocity=6.000000
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


[direction_indicators]
direction_indicator.0=3,0


[Radios] // availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 1
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1

[SMOKESYSTEM]
//JT8D-217/219 SMOKE
smoke.0=0, -103.6, -8.5, MD81_JT8D_engsmoke ,
smoke.1=0, -103.6,  8.5, MD81_JT8D_engsmoke ,


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


[brakes]
toe_brakes_scale=1.000000
parking_brake=1
auto_brakes=4


[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029


[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000


[stall_warning]
type=1
stick_shaker=1


[attitude_indicators]
attitude_indicator.0=1


[turn_indicators]
turn_indicator.0=1,0
[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