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Posky B747-400V4 Help

Featured Replies

Hi guys! For some reason the nose gear as seen below is not fully touch the ground. Also when I move the bose gear is bumping up and down none stop.

 

 

 

 

[fltsim.0]

title=Project Opensky - Boeing 747-400 AIR FRANCE

sim=747-400-GE-CF6-80C2B1

model=

panel=

sound=

texture=AFR

checklists=

atc_airline=Air France

atc_flight_number=295

atc_parking_types=GATE, RAMP

atc_parking_code=ANZ

ui_manufacturer=Project Opensky

ui_type=747-400

ui_variation=AIR FRANCE

visual_damage=1

atc_heavy=157

atc_id=157

description=Project Opensky \nBoeing 747-400\nVersion 2006.9.7-FSX\n\nEngine Type GE CF6-80C2B1\n\n747-400 Commercial Version\n\nModel Designer\n Hiroshi Igami \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: GE CF6-80C2B1\nTO Thrust: 54,750 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 = -100.0, 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= 650.000//225.200

rudder_area= 229.900

elevator_up_limit= 24.000

elevator_down_limit= 18.000

aileron_up_limit= 40.000//20.000

aileron_down_limit= 40.000//20.000

rudder_limit= 30.000

elevator_trim_limit= 24.000//24.000

spoiler_limit= 45.000

spoilerons_available= 1

aileron_to_spoileron_gain= 1

min_ailerons_for_spoilerons= 5.0

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=365.000000

max_mach=0.920000

[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 = 1.50

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= 54750.000

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, -18.000, 0.000, -15.250, 5181.102, 0.000, 2.042, 70.000, 0.600, 0.650, 0.950, 11.000, 11.000, 0.000, 240.000, 280.000 // Nose Gear

point.1 = 1.000, -110.583, -6.350, -15.403, 3574.803, 1.000, 1.917, 0.000, 1.620, 1.150, 0.741, 12.900, 14.900, 2.000, 240.000, 280.000 // Main Center Gear - Left

point.2 = 1.000, -110.583, 6.350, -15.403, 3574.803, 2.000, 1.917, 0.000, 1.620, 1.150, 0.741, 13.100, 15.400, 3.000, 240.000, 280.000 // Main Center Gear - Right

point.3 = 1.000, -102.083, -18.000, -15.403, 3574.803, 0.000, 1.917, 0.000, 1.620, 1.150, 0.741, 12.900, 14.900, 2.000, 240.000, 280.000 // Main Wing Gear - Left

point.4 = 1.000, -102.083, 18.000, -15.403, 3574.803, 0.000, 1.917, 0.000, 1.620, 1.150, 0.741, 13.100, 15.400, 3.000, 240.000, 280.000 // Main Wing Gear - Right

point.5 = 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.6 = 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.7 = 2.000, -175.667, 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 // Tail Scrape Point

point.8 = 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.9 = 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.10= 2.000, -108.400, -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 // Engine Scrape Point

point.11= 2.000, -80.300, -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 // Engine Scrape Point

point.12= 2.000, -80.300, 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 // Engine Scrape Point

point.13= 2.000, -108.400, 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 // Engine Scrape Point

point.14= 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= 12.500

gear_system_type=0

 

// Nose gear

//point.0= 1.000, -20.333, -1.500, -13.750, 2181.102, 0.000, 2.000, 70.000, 0.300, 0.500, 0.880, 11.000, 11.000, 0.000, 240.000, 280.000

//point.1= 1.000, -20.333, 1.500, -13.750, 2181.102, 0.000, 2.000, 70.000, 0.300, 0.500, 0.880, 11.000, 11.000, 0.000, 240.000, 280.000

//

// Main Wing Gear (left)

//point.2= 1.000, -104.583, -18.000, -16.533, 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, -16.533, 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, -16.533, 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, -16.533, 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, -16.533, 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, -16.533, 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, -16.533, 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, -16.533, 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, -16.533, 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, -16.533, 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, -16.533, 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, -16.533, 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, -16.533, 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, -16.533, 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, -16.533, 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, -16.533, 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= 0.000

//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=-32.500, -2.000, 11.100 // 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, 5 , 17.0

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

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]

light.0 = 3, -219.700, -0.250, 12.300, Opensky_nav_yellow ,

light.1 = 3, -219.700, 0.250, 12.300, Opensky_nav_yellow ,

light.2 = 2, -218.900, 0.000, 11.19, fx_strobeh ,

light.3 = 4, -32.350, 0.000, 11.100, fx_vclighth ,//Type changed and

light.4 = 1, -35.100, 0.600, 19.100, fx_beaconh ,

light.5 = 1, -83.500, 0.600, -7.080, Opensky_beacon ,

light.6 = 9, -208.500, -4.500, 43.750, Opensky_wing_light , // <-----3

light.7 = 9, -208.500, 4.500, 43.750, Opensky_wing_light , // <-----3

light.8= 5, -46.500, -11.700, 0.000, Opensky_nacelle_refl ,

light.9= 5, -46.500, 11.700, 0.000, Opensky_nacelle_refl ,

light.10= 5, -79.700, -29.200, -2.000, Opensky_nacelle_refl ,

light.11= 5, -79.700, 29.200, -2.000, Opensky_nacelle_refl ,

light.12= 5, -46.500, -11.700, 0.000, Opensky_nacelle_refl ,

light.13= 5, -46.500, 11.700, 0.000, Opensky_nacelle_refl ,

light.14= 5, -40.500, -13.700, 1.900, Opensky_nacelle_refl ,

light.15= 5, -40.500, 13.700, 1.900, Opensky_nacelle_refl ,

light.16= 5, -14.333, 0.000, -2.000, Opensky_nacelle_refl ,

light.4= 4, -80.22, 0.00, -11.05, fx_vclighth,

light.5= 3, -18.300, -6.500, 6.000, Opensky_nacelle_refl ,

light.6= 3, -52.610, -4.500, 6.000, Opensky_nacelle_refl ,

light.7= 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

 

[CameraDefinition.201]

Title=EZdok Aircraft Universal camera

Guid={D8D67955-2E9B-4e75-9D8B-8EFFBBFAC65B}

Description=Universal camera for EZdok cam utility

Origin=Center

SnapPbhAdjust=Swivel

SnapPbhReturn=FALSE

PanPbhAdjust=Swivel

PanPbhReturn=FALSE

Track=None

ShowAxis=FALSE

AllowZoom=TRUE

InitialZoom=0.40

ShowWeather=Yes

InitialXyz=0,0,0

InitialPbh=10, 0, 0

XyzAdjust=TRUE

Category=Aircraft

MomentumEffect=FALSE

ClipMode=Minimum

HotKeySelect=4

Edited by Air France
Image removed as it exceeds 1600W and 400KB max limits.

Anyone one please?

Looks like weight distribution is wrong. Perhaps this link will help - http://www.flightsim.com/vbfs/archive/index.php/t-210814.html.

 

Best regards,

Jim

Jim Young | AVSIM Online! - Simming's Premier Resource!

Member, AVSIM Board of Directors - Serving AVSIM since 2001

Submit News to AVSIM
Important other links: Basic FSX Configuration Guide | AVSIM CTD Guide | AVSIM Prepar3D Guide | Help with AVSIM Site | Signature Rules | Screen Shot Rule | AVSIM Terms of Service (ToS)

I7 8086K  5.0GHz | GTX 1080 TI OC Edition | Dell 34" and 24" Monitors | ASUS Maximus X Hero MB Z370 | Samsung M.2 NVMe 500GB and 1TB | Samsung SSD 500GB x2 | Toshiba HDD 1TB | WDC HDD 1TB | Corsair H115i Pro | 16GB DDR4 3600C17 | Windows 10 

 

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