[fltsim.0]
title=Boeing 747-400 Air France
sim=747-400F-GE-CF6-80C2B5F
model=
panel=
sound=
texture=AF
atc_airline=Air France
atc_flight_number=7280
atc_heavy=1
atc_id=F-GISG
atc_parking_types=GATE, RAMP
atc_parking_code=AF
ui_manufacturer=Boeing
ui_type=747-400
ui_typerole=Commercial Airliner
ui_createdby=Project Opensky
ui_variation=Air France New Livery
description=Project Opensky - 747-400\nVersion 2006.9.6-FSX\n\nModel Designers\n   Chang Yeon, Vincent Cho\n   Simon Ng  \n\nFlight Dynamics Designer\n   Warren C. Daniel\n   Brandon D. Henry\n\nTechnical Resource\n   Shigeo Kitaguchi\n\nAir France New Livery \n Daniel Alamilla \n\nTest Pilots\n   Project Opensky Members\n-----\nCrew: 9 \nPassengers: 416\nCrew Station: 4 seats, 2 rest bunks\nLavatory: 10\nGalley: 4\n\nEngines: GE CF6-80C2B15F2\nTO Thrust: 62,100 lb x 4\n\nTypical Cruise Speed \n   @ FL350: M.84\n\nFor proper operation, see B747\nmanual at: www.projectopensky.com \n\nBoeing 747 de la compañía de bandera francesa que presenta sus nuevos colores en el año 2009 con ligeras variaciones con respecto a la antigua imagen,que está incorporando paulatinamente a su flota mas moderna de 777 principalmente.Avion con registro ficticio ,pues se desconoce si Air France aplicara la nueva imagen a sus 747


[General]
performance=Cargo\nAft Bulk: 520 ft3 (9,720 lb)  \nLower Deck Aft: 2800 ft3 (57,500 lb)\nLower Deck Fwd: 2800 ft3 (61,000 lb)\nMain Deck: 21,117 ft3 (load dependant)\n\nDimensions\nSpan 211 ft 5 in (213 ft -- fueled)\nLength 231 ft 10 in\nHeight 63 ft 5 in\n\nMax Fuel Cap.: 53,644 US Gal.\nMax Gross Taxi Weight: 877,000 lb\nMax Gross TOW: 875,000 lb\nMLW: 666,000 lb\nMZFW: 610,000 lb\nOEW: 363,473 lb\n\nWheels\/Brakes: BF Goodrich\/Carbon Brakes\nNoise Compliance: Stage III\nApproach Category: CAT IIIB
atc_type=BOEING AIRCRAFT
atc_model=B744
editable=0
Category=airplane

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

[WEIGHT_AND_BALANCE]
reference_datum_position     =    97.0, 0, 0
empty_weight_CG_position     =  -107.0, 0, 0

max_number_of_stations = 8

station_load.0 =    "4500,  -150.0,  0.0,   0.0,  Aft Bulk - Payload" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 =    "15000, -150.0,  0.0,   0.0,  LD aft - Payload"   // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 =    "90000,  -40.0,  0.0,   0.0,  LD fwd - Payload"   // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 =    "55000,-107.0,  0.0,   0.0,  Main Dk  - Payload" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 =    "1600,   -50.0,  0.0,  20.0,  Upper Dk - Payload" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

empty_weight= 364473.000
max_gross_weight= 913000.000

// Moments of Inertia
empty_weight_roll_MOI=  37018662.500
empty_weight_pitch_MOI= 46713121.500
empty_weight_yaw_MOI=   70309608.000
empty_weight_coupled_MOI= 0.000
                 
[fuel]
Center1   =  -97.000,   0.0, -4.0, 17153.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2   = -290.500,   0.0,  6.0,  3298.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  = -102.000, -35.0, -4.0, 12538.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux   = -108.500, -52.0, -3.0,  5761.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -102.000,  35.0, -4.0, 12538.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux  = -108.500,  52.0, -3.0,  5761.0, 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=1                 

[airplane_geometry]
wing_area=              5650.000
wing_span=               211.000
wing_root_chord=          23.000
wing_dihedral=             6.998
wing_incidence=            2.000
wing_twist=               -0.994
oswald_efficiency_factor=  0.830
wing_winglets_flag=            1
wing_sweep=               37.500
wing_pos_apex_lon=       -55.100
wing_pos_apex_vert=        0.000
htail_area=             1470.000
htail_span=               72.750
htail_pos_lon=          -213.000
htail_pos_vert=           10.000
htail_incidence=           0.000
htail_sweep=              37.500
vtail_area=             1060.000
vtail_span=               37.121
vtail_sweep=              45.000
vtail_pos_lon=          -200.500
vtail_pos_vert=           20.083
elevator_area=           326.800
aileron_area=            225.200
rudder_area=             229.900
elevator_up_limit=        24.000
elevator_down_limit=      18.000
aileron_up_limit=         20.000
aileron_down_limit=       20.000
rudder_limit=             30.000
elevator_trim_limit=      24.000
spoiler_limit=            45.000
spoilerons_available=          0
aileron_to_spoileron_gain=     0
min_ailerons_for_spoilerons=   0
min_flaps_for_spoilerons=      0
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    = 150.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 126.0                 //Knots True (KTAS)
cruise_speed            = 495.0                 //Knots True (KTAS)
max_indicated_speed=350.000000
max_mach=0.900000

[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 25                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 5                                    // degrees
flaps-position.2 = 10                                   // degrees
flaps-position.3 = 15                                   // degrees
flaps-position.4 = 20                                   // degrees
flaps-position.5 = 25                                   // degrees
flaps-position.6 = 30                                   // degrees
damaging-speed   = 200                                  // KIAS
blowout-speed    = 250                                  // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.45
system_type = 1                                         //Hydraulic

[flaps.1]
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 = 5                                    // degrees
flaps-position.2 = 10                                   // degrees
flaps-position.3 = 15                                   // degrees
flaps-position.4 = 20                                   // degrees
flaps-position.5 = 25                                   // degrees
flaps-position.6 = 30                                   // degrees
damaging-speed   = 200                                  // KIAS
blowout-speed    = 250                                  // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.45
system_type = 1                                         //Hydraulic

[flaps.2]
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 12                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 10.0                                 // degrees
flaps-position.2 = 20.0                                 // degrees
flaps-position.3 = 20.0                                 // degrees
flaps-position.4 = 20.0                                 // degrees
flaps-position.5 = 20.0                                 // degrees
flaps-position.6 = 20.0                                 // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.45
system_type = 1                                         //Hydraulic

[flaps.3]
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 12                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 20.0                                 // degrees
flaps-position.2 = 20.0                                 // degrees
flaps-position.3 = 20.0                                 // degrees
flaps-position.4 = 20.0                                 // degrees
flaps-position.5 = 20.0                                 // degrees
flaps-position.6 = 20.0                                 // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.45
system_type = 1                                         //Hydraulic

[flaps.4]
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.2                                  // 0.0 .. 1.0
extending-time   = 12                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 20.0                                 // degrees
flaps-position.2 = 20.0                                 // degrees
flaps-position.3 = 20.0                                 // degrees
flaps-position.4 = 20.0                                 // degrees
flaps-position.5 = 20.0                                 // degrees
flaps-position.6 = 20.0                                 // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.28
drag_scalar = 0.40
pitch_scalar= 0.45
system_type = 1                                         //Hydraulic


[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.25
aileron_effectiveness  = 0.75
rudder_effectiveness   = 0.75
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 0.75
aileron_trim_effectiveness  = 0.65
rudder_trim_effectiveness   = 0.65


[GeneralEngineData]
engine_type= 1
Engine.0= -105.600, -69.500,  0.000
Engine.1=  -75.600, -39.167, -7.000
Engine.2=  -75.600,  39.167, -7.000
Engine.3= -105.600,  69.500,  0.000
fuel_flow_scalar= 0.9676
min_throttle_limit=-0.319946


[TurbineEngineData]
bypass_ratio=4.970
fuel_flow_gain=0.002000
inlet_area=40.68
rated_N2_rpm=29920.000000
static_thrust= 62100.000
afterburner_available= 0
reverser_available= 1

[jet_engine]
thrust_scalar = 1.0


[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=105.000000
pitch_takeoff_ga=8.000000
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=0.300000
max_pitch_velocity_lo_alt_breakpoint= 7000.000000
max_pitch_velocity_hi_alt_breakpoint=24000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.03000
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=1.000000


[contact_points]

        //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)

point.0 = 1.000,  -30.333,    0.000, -14.050, 2181.102, 0.000, 5.812,  70.000, 0.400, 1.200, 0.550, 11.000, 11.000, 0.000, 0.000, 0.000
point.1 = 1.000, -109.583,  -18.000, -13.833, 2574.803, 1.000, 5.812,   0.000, 0.602, 0.500, 0.551, 14.900, 14.900, 2.000, 0.000, 0.000
point.2 = 1.000, -109.583,   18.000, -13.833, 2574.803, 2.000, 5.812,   0.000, 0.602, 0.500, 0.551, 17.100, 17.100, 3.000, 0.000, 0.000
point.3 = 2.000, -146.000, -102.900,   7.000,  787.402, 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, -146.000,  102.900,   7.000,  787.402, 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, -189.667,    0.000,  -2.000,  787.402, 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,   -9.167,    0.000,  -5.750,  787.402, 0.000, 0.000,   0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 4.000, 0.000, 0.000
point.7 = 2.000, -229.667,    0.000,  55.500,  787.402, 0.000, 0.000,   0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 8.000, 0.000, 0.000
point.8 = 2.000, -106.400,  -69.500,  -5.000,  787.402, 0.000, 0.000,   0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000, 0.000, 0.000
point.9 = 2.000,  -76.300,  -39.167,  -9.000,  787.402, 0.000, 0.000,   0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000, 0.000, 0.000
point.10= 2.000,  -76.300,   39.167,  -9.000,  787.402, 0.000, 0.000,   0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000, 0.000, 0.000
point.11= 2.000, -106.400,   69.500,  -5.000,  787.402, 0.000, 0.000,   0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000, 0.000, 0.000
point.12= 2.000,    0.000,    0.000,   0.000,  787.402, 0.000, 0.000,   0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 4.000, 0.000, 0.000

static_pitch= 1.000
static_cg_height= 13.625
gear_system_type=0

// Nose gear
//point.0= 1.000, -30.333, -1.500, -15.833, 1181.102, 0.000, 2.000, 70.000, 1.859, 2.500, 0.518, 9.000, 11.000, 0.000, 240.000, 280.000
//point.1= 1.000, -30.333,  1.500, -15.833, 1181.102, 0.000, 2.000, 70.000, 1.859, 2.500, 0.518, 9.000, 11.000, 0.000, 240.000, 280.000
//
// Main Wing Gear (left)
//point.2= 1.000,  -104.583, -18.000, -16.133, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000
//point.3= 1.000,  -104.583, -14.000, -16.133, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000
//point.4= 1.000,   -99.583, -18.000, -16.133, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000
//point.5= 1.000,   -99.583, -14.000, -16.133, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000
//
// Main Wing Gear (right)
//point.6= 1.000,  -104.583, 18.000, -16.133, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000
//point.7= 1.000,  -104.583, 14.000, -16.133, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000
//point.8= 1.000,   -99.583, 18.000, -16.133, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000
//point.9= 1.000,   -99.583, 14.000, -16.133, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000

// Main Center Gear (left)
//point.10= 1.000, -115.583, -8.000, -16.133, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000
//point.11= 1.000, -115.583, -4.000, -16.133, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000
//point.12= 1.000, -109.583, -8.000, -16.133, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000
//point.13= 1.000, -109.583, -4.000, -16.133, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000
//
// Main Center Gear (right)
//point.14= 1.000, -115.583,  8.000, -16.133, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000
//point.15= 1.000, -115.583,  4.000, -16.133, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000
//point.16= 1.000, -109.583,  8.000, -16.133, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000
//point.17= 1.000, -109.583,  4.000, -16.133, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000
//
//Scrape points
//point.18 = 2.000, -146.000, -102.900,  7.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 5.000, 0.000, 0.000
//point.19 = 2.000, -146.000,  102.900,  7.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 6.000, 0.000, 0.000
//point.20 = 2.000, -189.667,   0.000,  -2.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000, 0.000, 0.000
//point.21 = 2.000,   -9.167,   0.000,  -5.750,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 4.000, 0.000, 0.000
//point.22 = 2.000, -229.667,   0.000,  55.500,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 8.000, 0.000, 0.000
//point.23 = 2.000, -106.400, -69.500,  -5.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000, 0.000, 0.000
//point.24 = 2.000,  -76.300, -39.167,  -9.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000, 0.000, 0.000
//point.25 = 2.000,  -76.300,  39.167,  -9.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000, 0.000, 0.000
//point.26 = 2.000, -106.400,  69.500,  -5.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 9.000, 0.000, 0.000
//point.27 = 2.000,    0.000,   0.000,   0.000,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000,  0.000,  0.000, 4.000, 0.000, 0.000
//
//static_pitch= -1.000
//static_cg_height= 13.625
//gear_system_type=0

[TailHook]    // For opening cargo door.
tailhook_length=1                               ;(feet)
tailhook_position = 0.0, 0.0, 0.0            ;(feet) longitudinal, lateral, vertical positions from datum

[folding_wings]  // For opening main deck cargo door.
wing_fold_system_type = 4                       ;0=None
fold_rates = 0.05,0.05                          ;Percent per second
cable_force_adjust = 1.0

[Views]
eyepoint=-14.000, -2.000, 14.800    // Longitude, Latitude and Vertical position from Reference Point, (FEET)

[electrical]
//                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 1, 0 ,  1.0
gear_motor         = 0, 5 , 17.0
avionics_bus       = 0, 0 ,  1.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 0 ,  1.0
additional_system  = 0, 0 ,  1.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 7, 0 , 99.0
gear_motor         = 4, 0 ,  1.0
fuel_pump          = 0, 0 ,  1.0
fuel_transfer_pump = 0, 0 ,  1.0
starter1           = 0, 20, 17.0
starter2           = 0, 0 ,  1.0
light_nav          = 0, 0 ,  1.0
light_beacon       = 0, 0 ,  1.0
light_landing      = 0, 0 ,  1.0
light_taxi         = 0, 0 ,  1.0
light_strobe       = 0, 0 ,  1.0
light_panel        = 0, 7 , 99.0
light_recognition  = 0, 0 ,  1.0
light_wing         = 0, 0 ,  1.0
marker_beacon      = 0, 0 ,  1.0
standby_vacuum     = 0, 0 ,  1.0
auto_brakes        = 0, 0 ,  1.0
hydraulic_pump     = 0, 0 ,  1.0
propeller_device   = 0, 0 ,  1.0


[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

[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

[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, 200
aileron  = 100, 200
rudder   = 100, 200

[exits]
number_of_exits = 4
// SP
//exit.0 = 0.10,  -43.00, -9.0,  0.0, 0 //Main Pax Door, L1 Door, Main level
//exit.1 = 0.12,  -58.00,  7.0, -7.0, 1 //Fwd Lower Right Cargo Door
//exit.2 = 0.12, -128.00,  7.0, -7.0, 1 //Aft Lower Right Cargo Door

// -100, -200, -300, -400
//number_of_exits = 6
//exit.0 = 0.10,  -54.00, -9.0,  0.0, 0 //Main Pax Door, L1 Door, Main level - Reserved for Cargo models
//exit.1 = 0.10,  -72.00, -9.0,  0.0, 0 //Main Pax Door, L2 Door, Main level
//exit.2 = 0.12,  -54.00,  7.0, -7.0, 1 //Fwd Lower Right Cargo Door
//exit.3 = 0.12, -156.00,  7.0, -7.0, 1 //Aft Lower Right Cargo Door
//exit.4 = 0.12, -156.00, -7.0,  0.0  1 //Main Deck, Large Cargo Door, Aft, Left Side - Reserved for Cargo models
//exit.5 = 0.12, -167.00,  7.0,  7.0  0 //Lower Air Stair - Reserved for VC-25A

exit.0 = 0.10,  -54.00, -9.0,  0.0, 0 //Main Pax Door, L1 Door, Main level - Reserved for Cargo models
exit.1 = 0.12,  -54.00,  7.0, -7.0, 1 //Fwd Lower Right Cargo Door
exit.2 = 0.10,  -72.00, -9.0,  0.0, 0 //Main Pax Door, L2 Door, Main level
exit.3 = 0.12, -167.00,  7.0,  7.0  1 //Lower Air Stair - Reserved for VC-25A


[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

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

[SMOKESYSTEM]
//Aileron tip vortecies
smoke.0=0, -127.167, -86.167, Opensky_vortex
smoke.1=0, -127.167,  86.167, Opensky_vortex
//Wing condensation
smoke.2=0, -105.917, -39.167, Opensky_conden
smoke.3=0, -105.917,  39.167, Opensky_conden

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo                   
light.0 = 1,   -32.200,    0.600,  19.100,  Opensky_beacon ,
light.1 = 1,   -83.500,    0.000,  -7.080,  Opensky_beacon ,
light.2 = 3, -219.700,   -0.250,   12.300, Opensky_nav_yellow ,
light.3 = 3, -219.700,    0.250,   12.300, Opensky_nav_yellow ,
light.4 = 2, -218.900,    0.000,   11.450, fx_strobeh ,
light.5 = 3,  -13.850,    0.000,   14.850, fx_vclighth ,
light.6 = 9, -208.500,   -4.500,   43.750, Opensky_wing_light , // <-----3 previously
light.7 = 9, -208.500,    4.500,   43.750, Opensky_wing_light , // <-----3 previously
light.8= 5,  -79.700,  -29.200,   -2.000, Opensky_nacelle_refl ,
light.9= 5,  -79.700,   29.200,   -2.000, Opensky_nacelle_refl ,
light.10= 5,  -46.500,  -11.700,    0.000, Opensky_nacelle_refl ,
light.11= 5,  -46.500,   11.700,    0.000, Opensky_nacelle_refl ,
light.12= 5,  -40.500,  -13.700,    1.900, Opensky_nacelle_refl ,
light.13= 5,  -40.500,   13.700,    1.900, Opensky_nacelle_refl ,
light.14= 5,  -14.333,    0.000,   -2.000, Opensky_nacelle_refl ,
light.15= 3,  -18.300,   -6.500,    6.000, Opensky_nacelle_refl ,
light.16= 3,  -52.610,   -4.500,    6.000, Opensky_nacelle_refl ,
light.17= 3, -144.510,    0.000,   -3.000, Opensky_wing_light ,


//================================================================
//New for FSX
//================================================================
Category=airplane


[CameraDefinition.0]
Title = "Right Wing View"
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 = 0.65
ShowWeather = Yes
InitialXyz = 3.2, 1.8, -5
InitialPbh = 5, 0, 100
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum


[CameraDefinition.1]
Title = "Left Wing View"
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 = 0.65
ShowWeather = Yes
InitialXyz = -3.2, 1.8, -5
InitialPbh = 5, 0, 260
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum


[CameraDefinition.2]
Title = "Main Landing Gear"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the Main Landing Gear
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = FALSE
InitialZoom = .45
ShowWeather = Yes
InitialXyz = 0, -5.0, 15.0
InitialPbh = -10, 0, 180
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum


[CameraDefinition.3]
Title = "Pushback Tug"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = Walking with the pushback tug
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .50
ShowWeather = Yes
InitialXyz = 3.0, -2.0, 42.0
InitialPbh = -8, 0, 190
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect= No
ClipMode=Minimum


[CameraDefinition.4]
Title = "Air stair view"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking at the air stair
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .50
ShowWeather = Yes
InitialXyz =  -13.0, -2, 10.00
InitialPbh = -10, 0, 55
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 = 0.75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=True
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.0, -0.0, 0.0
InitialPbh=0, 0, 0


[CameraDefinition.002]
Title = "Center Pedistal"
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 = 0.50
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = No
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.5, 0.0, 0.0
InitialPbh=80, 0, 0


[CameraDefinition.003]
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 = 0.45
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.5, 0.0, 0.0
InitialPbh=-40.0, 0, 0


[CameraDefinition.004]
Title = "Flight Engineer Panel"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.50
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.7, 0.0, -1.5
InitialPbh=5.0, 0, 90.0


[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
structural_deice_type=0


[deice_system]
structural_deice_type=1     //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots


[brakes] 
//================================================================
//New for FSX
//================================================================
parking_brake = 1         // Parking brake available
toe_brakes_scale = 0.9155 //Brake scalar
auto_brakes = 5
hydraulic_system_scalar = 1  //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure


[stall_warning]
//================================================================
//New for FSX
//================================================================
type=2
stick_shaker=1


[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=1,1,1,1
normal_pressure=3000.000000


[attitude_indicators]
attitude_indicator.0=1


[turn_indicators]
turn_indicator.0=1,0

[GPWS]
max_warning_height         =  1000
sink_rate_fpm              = -3800
excessive_sink_rate_fpm    = -5500
climbout_sink_rate_fpm     = -1000
flap_and_gear_sink_rate_fpm= -1400