by lakevue » Fri Aug 10, 2007 7:03 pm
Yes..checked both "posky" and "All"...no-show. Here is the file you requested....let me know what you think the problem is.
[fltsim.0]
title=Project Opensky Boeing 757-300 Northwest NC Skyteam
sim=B757-300-PW-PW2040
model=
//ADD THE TW0 LETTERS VC AFTER THE MODEL= FOR VC MODEL
panel=
sound=
texture=nwa_nc
kb_checklists=
kb_reference=
atc_id=N597NW
atc_airline=Northwest
atc_flight_number=22
atc_parking_codes=NWA
atc_parking_types=GATE
ui_manufacturer=Project Opensky
ui_type=757-300
ui_variation=Northwest NC w/ Skyteam
description=Project Opensky \nBoeing 757-300\nVersion 2004.8.1\n\nFS2004 Only\n\nEngine Type: PW2040\n\nModel Designers\n Lee Rosario\n Albert Bouwman\n C. Vincent Cho\n Hiroshi Igami\n\nFlight Dynamics Designer\n Warren C. Daniel\n\nMaster Texture Designers\n Jaco du Preez\n Ben Hewitt\n\nTechnical Resource-QC\n Nick Peterson\n Simon Ng\n\nFor proper operation: See B757 manual at: \n www.projectopensky.com
atc_heavy=0
[General]
atc_type=BOEING AIRCRAFT
atc_model=B753
visual_damage=1
editable=0
performance=Passengers\n2-class conf: 243 \n 12 - First\n 231 - Economy\n\nCargo\nFwd lower hold volume: 1,790 cu ft \nAft lower hold volume: 1,312 cu ft\n\nDimensions\nSpan 124 ft 10 in\nLength 178 ft 7 in\nHeight 44 ft 3 in (min)\n 45 ft 1 in (max)\n\nEngines: PW2040\nTO Thrust Rating: 40,900 lb\n\nMax Fuel Cap.: 11,276 gal\nMaxTOW: 272,500 lb\nZFW: 188,000 lb\n\nMax Range: 3,395 nm (6,287 km) \nTypical Cruise Speed \n @ FL350: M.80
TBAirCraftFolderUId=147
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
[airplane_geometry]
wing_area = 1994.000
wing_span = 124.830
wing_root_chord = 26.902
wing_dihedral = 5.000
wing_incidence = 0.500
wing_twist = 1.000
oswald_efficiency_factor= 0.750
wing_winglets_flag = 0
wing_sweep = 24.500
wing_pos_apex_lon = 0.000
wing_pos_apex_vert = 0.000
htail_area =541.949
htail_span = 49.930
htail_pos_lon =-65.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 30.000
vtail_area =369.940
vtail_span = 45.078
vtail_sweep = 35.000
vtail_pos_lon =-58.000
vtail_pos_vert = 5.800
elevator_area =136.000
aileron_area = 48.000
rudder_area =123.000
elevator_up_limit = 24.000
elevator_down_limit = 18.000
aileron_up_limit = 24.000
aileron_down_limit = 18.000
rudder_limit = 32.000
elevator_trim_limit = 16.000
spoiler_limit = 45.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
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
[WEIGHT_AND_BALANCE]
max_gross_weight = 272500.000
empty_weight = 188000.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations =50
station_load.0 =0.000000,0.000000,0.000000,0.000000
;Moments of Inertia
empty_weight_pitch_MOI = 2995645.000
empty_weight_roll_MOI = 1873855.000
empty_weight_yaw_MOI = 5171429.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.500
elevator_effectiveness =1.000
aileron_effectiveness =1.875
rudder_effectiveness =1.000
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 1
Engine.0 = 10.200, -21.250, -3.290
Engine.1 = 10.200, 21.350, -3.290
fuel_flow_scalar = 0.835
min_throttle_limit=-0.319946
[TurbineEngineData]
fuel_flow_gain = 0.002
bypass_ratio=6.00
inlet_area = 33.5757
rated_N2_rpm = 29920.000
static_thrust = 40900.000
afterburner_available = 0
reverser_available = 1
[jet_engine]
thrust_scalar =1.000
[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
autopilot = 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