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hier die PSS aircraft.cfg für die POSKY 747!!!


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:D hallo es geht :rolleyes: die POSKY 747 fliegt ganz normal, alle Leistungsdaten stimmen...das FMC muckt auch nicht auf..sollte doch noch ein Fehler sein einfach ne Mail schreiben! Viel Spaß!

 

hier die .cfg:

 

[fltsim.0]

title=Project Opensky - Boeing 747-400 BA CIVS

sim=747-400-RR-RB-211-524HT

model=

panel=

sound=

texture=

checklists=

 

atc_airline=SPEEDBIRD

atc_flight_number=092

 

ui_manufacturer=Boeing

ui_type=747-400

ui_variation=British Airways 'Whale Rider'

visual_damage=1

 

atc_heavy=1

atc_id=G-BNLO

 

description=Project Opensky \nBoeing 747-400\nVersion 2002.5.6C\Ready for PSS Panel\nEngine Type RR RB-211-524HT\n\n747-400 Commercial Version\aircraft cfg by activa@tiscali.de 2003

 

[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: 58,000 lb x 4\n\nMax Fuel Cap.: 57,065 US Gal.\nMaxTOW: 870,000 lbs\nMLW: 630,000 lbs\nZFW: 545,965 lbs\nOEW: 407,107 lbs\n\nMax Range: 7305 mi \nTypical Cruise Speed \n @ FL350: M.85

 

atc_type=BOEING AIRCRAFT

atc_model=B744

editable=0

 

[pitot_static]

vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI

 

[electrical]

//BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)

autopilot = 0, 5 , 17.0

avionics_bus = 0, 10, 17.0

avionics = 1, 5 , 17.0

gear_warning = 0, 2 , 17.0

fuel_pump = 0, 5 , 17.0

light_nav = 0, 5 , 17.0

light_beacon = 0, 5 , 17.0

light_landing = 0, 5 , 17.0

light_taxi = 0, 5 , 17.0

light_strobe = 0, 5 , 17.0

light_panel = 0, 5 , 17.0

 

pitot_heat = 0, 15, 17.0

additional_system = 0, 20, 17.0

marker_beacon = 1, 2, 17.0

starter1 = 0, 20, 17.0

starter2 = 0, 20, 17.0

starter3 = 0, 20, 17.0

starter4 = 0, 20, 17.0

auto_brakes = 0, 15, 17.0

hydraulic_pump = 0, 2, 17.0

fuel_transfer_pump = 0, 5, 17.0

 

max_battery_voltage = 28.0

generator_alternator_voltage = 28.0

max_generator_alternator_amps= 60.0

electric_always_available = 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, 1

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

 

[forcefeedback]

gear_bump_nose_magnitude=200 ; 0 - 10000

gear_bump_nose_direction=18000 ; 0 - 35999 degrees

gear_bump_nose_duration=250000 ; in microseconds

gear_bump_left_magnitude=500 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; in microseconds

gear_bump_right_magnitude=500 ; 0 - 10000

gear_bump_right_direction=00500 ; 0 - 35999 degrees

gear_bump_right_duration=250000 ; in microseconds

ground_bumps_magnitude1=50 ; 0 - 10000

ground_bumps_angle1=08900 ; 0 - 35999 degrees

ground_bumps_intercept1=3.0

ground_bumps_slope1=0.20

ground_bumps_magnitude2=50 ; 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

 

 

[sMOKESYSTEM]

smoke.0=80,-50,-90.0, fx_contrail_s.fx

smoke.1=80,-50, 90.0, fx_contrail_s.fx

 

[WEIGHT_AND_BALANCE]

empty_weight = 397000 // (pounds)

 

reference_datum_position = 0.0, 0, 0

empty_weight_CG_position = 5.0, 0, 0

 

station_load.0 = 0450, 81.00, 0.0, 0.0 //Weight Crew (lbs) LEAVE

station_load.1 = 4000, 29.00, 0.0, 0.0 //Weight Galleys(lbs) LEAVE

station_load.2 = 10000, 58.00, 0.0, 0.0 //Weight Baggage 1 (lbs) Baggage A |

station_load.3 = 5000, 4.00, 0.0, 0.0 //Weight Baggage 2 (lbs) CARGO |--Max 60,000 lb

station_load.4 = 10000, -50.00, 0.0, 0.0 //Weight Baggage 3 (lbs) Baggage B |

station_load.5 = 8640, 58.00, 0.0, 0.0 //Weight Psgr Sect OA (lbs) First ---- |--180 lb PER PASSANGER

station_load.6 = 18720, 80.00, 0.0, 0.0 //Weight Psgr Sect OB (lbs) Business |

station_load.7 = 23400, 48.00, 0.0, 0.0 //Weight Psgr Sect OC (lbs) Economy A |--MAX 412 Passengers

station_load.8 = 23400, -83.00, 0.0, 0.0 //Weight Psgr Sect OD (lbs) Economy B |

 

//TOTAL ZFW = 500610

empty_weight_roll_MOI=18200000.000000

empty_weight_pitch_MOI=33100000.000000

empty_weight_yaw_MOI=39700000.000000

empty_weight_coupled_MOI=0.000000

max_gross_weight= 892365.689

 

[pitot_static]

vertical_speed_time_constant=999

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=70

 

[General]

performance=Flight Dynamic file by Johan Dees\nFS2002 Version 3.5\n\n\n

atc_type=Boeing

atc_model=B744

editable=0

 

[fuel]

Center1=0.000000,0.000000,-4.000000,20731.000000,3.000000

LeftMain=-5.000000,-35.000000,0.000000,18870.000000,3.000000

RightMain=-5.000000,35.000000,0.000000,18870.000000,3.000000

fuel_type=2.000000

number_of_tank_selectors=1

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=48.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=5.000002,0.000000

flaps-position.2=10.000004,0.000000

flaps-position.3=15.000006,0.000000

flaps-position.4=20.000009,0.000000

flaps-position.5=25.000011,0.000000

flaps-position.6=30.000013,0.000000

 

[GeneralEngineData]

engine_type=1

Engine.0=-24.000000,-68.333333,-4.500000

Engine.1=-2.500000,-38.333333,-2.500000

Engine.2=-2.500000,38.333333,-2.500000

Engine.3=-24.000000,68.333333,-4.500000

fuel_flow_scalar=1.000000

 

[Reference Speeds]

flaps_up_stall_speed=200.000000

full_flaps_stall_speed=160.000000

cruise_speed=593.555189

 

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=350.000000,250.000000

 

[Views]

eyepoint=86.801284,-2.499077,16.160700

 

[GeneralEngineData]

engine_type=1

Engine.0=-24.000000,-68.333333,-4.500000

Engine.1=-2.500000,-38.333333,-2.500000

Engine.2=-2.500000,38.333333,-2.500000

Engine.3=-24.000000,68.333333,-4.500000

fuel_flow_scalar=1.3

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

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.

 

[direction_indicators]

direction_indicator.0=3,0

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[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, 67.333, 0.000, -13.850, 2181.102, 0.000, 5.812, 78.480, 0.859, 0.500, 0.518, 11.000, 11.000, 0.000, 0.000, 0.000

point.1 = 1.000, -12.583, -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, -12.583, 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, -49.000, -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, -49.000, 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, -92.667, 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, 88.167, 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,-132.667, 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, -14.917, -69.500, -7.000, 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, 14.917, -39.167, -11.000, 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, 14.917, 39.167, -11.000, 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, -14.917, 69.500, -7.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000

static_pitch= -1.000

static_cg_height= 13.125

 

// Nose gear

//point.0= 1.000, 67.333, -1.500, -15.333, 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, 67.333, 1.500, -15.333, 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, -7.583, -18.000, -17.133, 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, -7.583, -14.000, -17.133, 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, -2.583, -18.000, -17.133, 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, -2.583, -14.000, -17.133, 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, -7.583, 18.000, -17.133, 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, -7.583, 14.000, -17.133, 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, -2.583, 18.000, -17.133, 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, -2.583, 14.000, -17.133, 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, -18.583, -8.000, -17.133, 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, -18.583, -4.000, -17.133, 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, -12.583, -8.000, -17.133, 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, -12.583, -4.000, -17.133, 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, -18.583, 8.000, -17.133, 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, -18.583, 4.000, -17.133, 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, -12.583, 8.000, -17.133, 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, -12.583, 4.000, -17.133, 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, -49.000, -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, -49.000, 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 -92.667, 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, 88.167, 0.000, -3.750, 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, -132.667, 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, -14.917, -69.500, -7.000, 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, 14.917, -39.167, -11.000, 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, 14.917, 39.167, -11.000, 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, -14.917, 69.500, -7.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000

//

//static_pitch= -1.000

//static_cg_height= 13.625

 

[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

 

[flight_tuning]

cruise_lift_scalar = 1.0

parasite_drag_scalar = 1.0

induced_drag_scalar = 1.0

elevator_effectiveness = 1.0

aileron_effectiveness = 1.0

rudder_effectiveness = 1.0

pitch_stability = 1.0

roll_stability = 1.0

yaw_stability = 1.0

elevator_trim_effectiveness = 1.0

aileron_trim_effectiveness = 1.0

rudder_trim_effectiveness = 1.0

 

 

[TurbineEngineData]

fuel_flow_gain=0.001900

inlet_area=98.000000

rated_N2_rpm=29920.000000

static_thrust=56750.000000

afterburner_available=0

reverser_available=1

 

[airplane_geometry]

wing_area=5650.000000

wing_span=210.833333

wing_root_chord=26.833333

wing_dihedral=7.800293

wing_incidence=0.999756

wing_twist=0.802002

oswald_efficiency_factor=0.828610

wing_winglets_flag=65281

wing_sweep=0.000000

wing_pos_apex_lon=0.000000

wing_pos_apex_vert=0.000000

htail_area=1470.000000

htail_span=73.166667

htail_pos_lon=-190.000000

htail_pos_vert=0.000000

htail_incidence=0.000000

htail_sweep=0.000000

vtail_area=830.000000

vtail_span=32.848135

vtail_sweep=0.000000

vtail_pos_lon=-190.000000

vtail_pos_vert=5.833333

elevator_area=350.000000

aileron_area=222.000000

rudder_area=247.000000

elevator_up_limit=30.000013

elevator_down_limit=30.000013

aileron_up_limit=30.000013

aileron_down_limit=30.000013

rudder_limit=33.231552

elevator_trim_limit=30.000013

spoiler_limit=70.000030

spoilerons_available=0

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.969466

min_flaps_for_spoilerons=0.000000

 

[sMOKESYSTEM]

//Aileron tip vortecies

smoke.0=0, -30.167, -86.167, Opensky_vortex

smoke.1=0, -30.167, 86.167, Opensky_vortex

//Wing condensation

smoke.2=0, -08.917, -39.167, Opensky_conden

smoke.3=0, -08.917, 39.167, Opensky_conden

 

[LIGHTS]

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

light.0 = 1, 65.200, 0.600, 19.100, Opensky_beacon ,

light.1 = 1, 13.500, 0.000, -7.080, Opensky_beacon ,

light.2 = 2, -49.000, -102.900, 13.150, fx_strobeh ,

light.3 = 2, -49.000, 102.900, 13.150, fx_strobeh ,

light.4 = 3, -122.700, -0.250, 12.300, Opensky_nav_yellow ,

light.5 = 3, -122.700, 0.250, 12.300, Opensky_nav_yellow ,

light.6 = 2, -121.900, 0.000, 11.450, fx_strobeh ,

light.7 = 3, 84.850, 0.000, 14.850, fx_vclighth ,

light.8 = 3, -111.500, -4.500, 43.750, Opensky_wing_light ,

light.9 = 3, -111.500, 4.500, 43.750, Opensky_wing_light ,

light.10= 5, 18.700, -29.200, -2.000, Opensky_nacelle_refl ,

light.11= 5, 18.700, 29.200, -2.000, Opensky_nacelle_refl ,

light.12= 5, 51.500, -11.700, 0.000, Opensky_nacelle_refl ,

light.13= 5, 51.500, 11.700, 0.000, Opensky_nacelle_refl ,

light.14= 5, 57.500, -13.700, 1.900, Opensky_nacelle_refl ,

light.15= 5, 57.500, 13.700, 1.900, Opensky_nacelle_refl ,

light.16= 5, 83.333, 0.000, -2.000, Opensky_nacelle_refl ,

light.17= 3, 72.300, -6.500, 6.000, Opensky_nacelle_refl ,

light.18= 3, 45.610, -4.500, 6.000, Opensky_nacelle_refl ,

light.19= 3, -47.510, 0.000, -3.000, Opensky_wing_light ,

Geschrieben

:D die Angaben über die Gewichte werden vom Flusi selbst verändert, weil der Load Editor ist natürlich auch nutzbar!

 

Gruß

 

:p

Geschrieben

Heyyyy!!!!!

 

 

 

 

 

 

Was sollen.........

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

denn immer diese.............

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

langen Einträge hier :confused: :confused: :confused:

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Kleiner Scherz :D:D:D:D:D

 

Danke für das Posten der CFG, werde es gleich mal in meinem Hangar ändern, dann klappt es auch mit der Nachbarin. ;)

 

Schönen Gruß

 

Stefan

Geschrieben

:eek: Hi Stefan,

 

und schon getestet? Funktioniert es? Bitte um kurze Nachricht :p

 

Gruß

 

K.A.

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Gast
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