[fltsim.0]
title=Boeing 747-400 OrientalCay "Hong Kong"
sim=747-400-RR-RB-211-524HT
model=
panel=
sound=
texture=OCAY
checklists=

atc_airline=Cayman
atc_flight_number=228
atc_parking_types=GATE, RAMP
atc_parking_code=CAY

ui_manufacturer=Project Opensky
ui_type=747-400
ui_variation=OrientalCay
ui_typerole=Commercial Airliner
ui_createdby=POSKY
visual_damage=157



atc_heavy=1
atc_id=VH-OJB

description=Project Opensky \nBoeing 747-400\nVersion 2006.9.6-FSX\n\nEngine Type RR RB-211-524HT\n\n747-400 Commercial Version \n\nModel Designer\n   Chang Yeon, Vincent Cho  \n\nFlight Dynamics Designers\n   Warren C. Daniel\n   Brandon D. Henry\n\n   Test Pilots\n   Project Opensky Members\n\nMaximun Range: 7305 nm\n\nFor proper operation: See B747 manual at: \n  www.projectopensky.com

[General]
performance=Passengers\n3-class conf: 524 \n2-class conf: 416 \n1-class conf: N\/A\n\nCargo\nTotal lower hold volume:\n   5,497 ft3 (155.6 m3)  \n\nDimensions\nSpan 211 ft 5 in (213 ft -- fueled)\nLength 231 ft 10 in\nHeight 63 ft 5 in\n\nEngines: RR RB-211-524HT\nTO Thrust: 59,350 lb x 4\n\nMax Fuel Cap.: 57,065 US Gal.\nMaxTOW: 877,000 lbs\nMLW: 630,000 lbs\nMax Payload: 148,716 lbs\nOEW: 394,660 lbs\n\nMax Range: 7305 mi   \nTypical Cruise Speed \n   @ FL350: M.85

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]
empty_weight= 394660.000
max_gross_weight= 877000.000

reference_datum_position     =    97.0, 0, 0
empty_weight_CG_position     =  -107.0, 0, 0

max_number_of_stations = 8

// New FS2004 Numbers
// Max Structural Payload Per Boeing - 148,716 lbs
// Max Structural Payload Opensky    - 148,716 lbs

// Actual Total PAX  - 72,800 lbs
station_load.0 =    "5600,  -20.0,  0.0,   0.0,  1st Class Main Dk  (21 pax)"     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.1 =    "5950,  -70.0,  0.0,   0.0,  Bus Class Main Dk  (35 pax)"     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2 =    "7350,  -50.0,  0.0, 20.00,  Bus Class Upper Dk (42 pax)"     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 =   "53900, -107.0,  0.0,   0.0,  Econ Class Main Dk (322 pax)"    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

// Total Opensky Cargo - 33,500 lbs
station_load.4 =   "15750,  -40.0,  0.0,   0.0,  Lwr Dk Cgo Fwd"                  //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 =   "15750, -150.0,  0.0,   0.0,  Lwr Dk Cgo Aft"                  //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 =    "2000, -170.0,  0.0,   0.0,  Lwr Dk Cgo Bulk"                 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

// 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,  1775.0, 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= -107.600, -69.500,  0.000
Engine.1=  -78.110, -39.167, -7.000
Engine.2=  -78.110,  39.167, -7.000
Engine.3= -107.600,  69.500,  0.000
fuel_flow_scalar= 0.9676
min_throttle_limit=-0.319946

[TurbineEngineData]
bypass_ratio=5.800000
fuel_flow_gain= 0.001
inlet_area= 40.58
rated_N2_rpm= 29992.000
static_thrust= 59350.000
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, -13.533, 2181.102, 0.000, 5.812,  70.000, 0.300, 0.500, 0.880, 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


