28-07-2005, 05:32 PM
Hello
I am looking for someone to do a 747-200F plane as there are none that came with FSP, here is my aircraft config file.
[fltsim.0]
title=EL AL 747-200F
sim=747-200FPW
model=
panel=
sound=
texture=AXL
checklists=
atc_airline=EL AL
atc_flight_number=204
ui_manufacturer=Project Opensky
ui_type=EL AL 747-200 PACK
ui_variation=EL AL CARGO AXL
visual_damage=1
atc_heavy=1
atc_id=4X-AXL
description=Project Opensky - 747-200F\nVersion 2004.1.0\n\nEngine Type PW JT9D7GR4\n\n747-200F Freight Version \n\nModel Designers\n Vincent Cho\n
Yosuke Ube\n\nFlight Dynamics Designer\n Nick Peterson\n Based on original by Warren Daniel\n\nTechnical Resource\n Simon Ng\n Shigeo
Kitaguchi\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 7220 nm\n\nFor proper operation: See B747 manual at: \n http://www.project-opensky.com
[fltsim.1]
title=EL AL 747-200F AXK
sim=747-200FPW
model=
panel=
sound=
texture=AXK
checklists=
atc_airline=EL AL
atc_flight_number=204
ui_manufacturer=Project Opensky
ui_type=EL AL 747-200 PACK
ui_variation=EL AL CARGO AXK
visual_damage=1
atc_heavy=1
atc_id=4X-AXK
description=Project Opensky \nBoeing 747-200F\nVersion 2004.1.1.0\n\nEngine Type PW JT9D-7R4G2\n\n747-200 Freight Version \n\nModel Designer\n
Yosuke Ube\n Vincent Cho\n\nFlight Dynamics Designer\n Nick Peterson, based on original by Warren Daniel\n\nTechnical Resource\n Simon Ng\n
Shigeo Kitaguchi\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 5,650 nm\n\nTypical city pairs: \n Tokyo-Sydney\n Bangkok-Paris\n
Zurich-Johannesburg\n
[fltsim.2]
title=EL AL 747-200F AXF
sim=747-200FPW
model=
panel=
sound=
texture=AXF
checklists=
atc_airline=EL AL
atc_flight_number=204
ui_manufacturer=Project Opensky
ui_type=EL AL 747-200 PACK
ui_variation=EL AL CARGO AXF
visual_damage=1
atc_heavy=1
atc_id=4X-AXF
description=Project Opensky \nBoeing 747-200F\nVersion 2004.1.1.0\n\nEngine Type PW JT9D-7R4G2\n\n747-200 Freight Version \n\nModel Designer\n
Yosuke Ube\n Vincent Cho\n\nFlight Dynamics Designer\n Nick Peterson, based on original by Warren Daniel\n\nTechnical Resource\n Simon Ng\n
Shigeo Kitaguchi\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 5,650 nm\n\nTypical city pairs: \n Tokyo-Sydney\n Bangkok-Paris\n
Zurich-Johannesburg\n
[General]
performance=Cargo\nTotal lower hold volume:\n 5,497 ft3 (155.6 m3)\nTotal Upper Deck volume:\n 18,270 ft3 (522.0 m3) \n\nDimensions\nSpan 195 ft
8 in\nLength 231 ft 10 in\nHeight 63 ft 5 in\n\nEngines: PW JT9D-7R4G2\nTO Thrust: 54,75000 lb x 4\n\nMax Fuel Cap.: 52,410 US Gal.\nMaxTOW: 833,000
lbs\nMLW: 630,000 lbs\nZFW: 460,965 lbs\nOEW: 347,850 lbs\n\nMax Range: 5,650 nm \nTypical Cruise Speed \n @ FL350: M.85
atc_type=BOEING AIRCRAFT
atc_model=B742
editable=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
[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
[pitot_static]
vertical_speed_time_constant=999
[WEIGHT_AND_BALANCE]
reference_datum_position= 88.000, 0.000, 0.000
empty_weight_CG_position= -105.000, 0.000, 0.000
empty_weight=347850
empty_weight_roll_MOI= 18155743.000
empty_weight_pitch_MOI= 17600873.000
empty_weight_yaw_MOI= 19151035.000
empty_weight_coupled_MOI= 0.000
max_gross_weight=833000
max_number_of_stations = 50
station_load.0 = "44600.0, -60.0, 0.0, 0.0, FWD Up Deck"
station_load.1 = "51200.0, -78.00, 0.0,0.0, MID Up Deck"
station_load.2 = "64800.0, -118.0, 0.0, 0.0, Aft Up Deck"
station_load.3 = "45000.0, -58.0, 0.0, 0.0, FWD Belly"
station_load.4 = "35000.0, -120.0, 0.0,0.0, AFT Belly"
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"
[fuel]
Center1 = -88.0, 0.0, -4.0, 19431.0, 3.0
LeftMain =-102.0, -35.0, -4.0, 16660.0, 3.0
LeftAux =-109.5, -52.0, -3.0, 500.0, 3.0
RightMain =-102.0, 35.0, -4.0, 16660.0, 3.0
RightAux =-109.5, 52.0, -3.0, 500.0, 3.0
fuel_type =2.000000
electric_pump=1
number_of_tank_selectors=1
[airplane_geometry]
wing_area= 5500.000
wing_span= 196.000
wing_root_chord= 53.000
wing_dihedral= 3.998
wing_incidence= 3.500
wing_twist= -0.194
oswald_efficiency_factor= 0.730
wing_winglets_flag= 0
wing_sweep= 37.500
wing_pos_apex_lon= -78.000
wing_pos_apex_vert= 0.000
htail_area= 1470.000
htail_span= 72.750
htail_pos_lon= -204.167
htail_pos_vert= 7.000
htail_incidence= 0.000
htail_sweep= 37.500
vtail_area= 1060.000
vtail_span= 37.121
vtail_sweep= 45.000
vtail_pos_lon= -204.500
vtail_pos_vert= 6.083
elevator_area= 326.800
aileron_area= 225.200
rudder_area= 229.900
elevator_up_limit= 20.751
elevator_down_limit= 15.313
aileron_up_limit= 31.513
aileron_down_limit= 31.513
rudder_limit= 17.189
elevator_trim_limit= 19.167
spoiler_limit= 25.783
spoilerons_available= 0
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 11.459
min_flaps_for_spoilerons= 0.000
[contact_points]
point.0= 1.000, -21.333, 0.00, -14.853, 1181.102, 0.000, 2.000, 70.000, 1.129, 1.100, 0.98, 9.000, 11.000,0.000, 240.000, 280.000
point.1= 1.000, -99.583, -16.000, -15.403, 1574.803, 1.000, 2.000, 0.000, 1.62, 1.15, 0.741, 12.900, 14.900, 2.000, 240.000, 280.000
point.2= 1.000, -99.583, 16.000, -15.403, 1574.803, 2.000, 2.000, 0.000, 1.62, 1.15, 0.741, 13.100, 15.400, 3.000, 240.000, 280.000
point.3= 1.000, -109.583, -6.000, -15.403, 1574.803, 1.000, 2.000, 13.000, 1.62, 1.15, 0.741, 13.400, 14.900, 2.000, 240.000, 280.000
point.4= 1.000, -109.583, 6.000, -15.403, 1574.803,2.000, 2.000, 13.000,1.62, 1.15, 0.741, 12.500, 13.500, 3.000, 240.000, 280.000
point.5= 2.000, -102.167, -96.167, 0.000, 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, -102.167, 96.167, 0.000, 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, -220.667, 0.000, 2.500, 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.8= 2.000, 0.0, 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.9= 2.000, -102.167, -96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.10= 2.000, -220.667, 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
static_pitch= -.300
static_cg_height= 13.625
gear_system_type=0
[GeneralEngineData]
engine_type=1
Engine.0=-109.916667,-69.500000,0.000000
Engine.1=-86.916667,-39.166667,-7.000000
Engine.2=-86.916667,39.166667,-7.000000
Engine.3=-109.916667,69.500000,0.000000
fuel_flow_scalar=1.04
min_throttle_limit=-0.399902
[TurbineEngineData]
bypass_ratio=4.970000
fuel_flow_gain=0.002000
inlet_area=37.558941
rated_N2_rpm=29920.000000
static_thrust=54750.000000
afterburner_available=0
reverser_available=1
[Reference Speeds]
flaps_up_stall_speed= 150.000
full_flaps_stall_speed= 126.000
cruise_speed= 524.337
max_indicated_speed=350.000000
max_mach=0.900000
[keyboard_response]
elevator= 100.000, 200.000
aileron= 100.000, 200.000
rudder= 150.000, 250.000
[Views]
eyepoint=-9.000, -2.000, 14.800
[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=14.000000
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Def
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=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
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
[flaps.0]
type = 1 span-outboard = 0.4 extending-time = 25
flaps-position.0 = 0
flaps-position.1 = 5
flaps-position.2 = 10
flaps-position.3 = 15
flaps-position.4 = 20
flaps-position.5 = 25
flaps-position.6 = 30
damaging-speed = 200
blowout-speed = 250
lift_scalar = 1.00
drag_scalar = .67
pitch_scalar= 0.3
system_type = 1
[flaps.1]
type = 1
span-outboard = 0.4
extending-time = 25
flaps-position.0 = 0
flaps-position.1 = 5
flaps-position.2 = 10
flaps-position.3 = 15
flaps-position.4 = 20
flaps-position.5 = 25
flaps-position.6 = 30
damaging-speed = 200
blowout-speed = 250
lift_scalar = 1.00
drag_scalar = .67
pitch_scalar= 0.3
system_type = 1
[flaps.2]
type = 2
span-outboard = 0.8
extending-time = 12
flaps-position.0 = 0
flaps-position.1 = 20.0
damaging-speed = 250
blowout-speed = 300
lift_scalar = 0.67
drag_scalar = .4
pitch_scalar= 0.1
system_type = 1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[direction_indicators]
direction_indicator.0=3,0
[folding_wings] // For opening main deck cargo door.
wing_fold_system_type = 4 ;0=None
fold_rates = 0.070, 0.070 ;Percent per second
cable_force_adjust = 1.0
[exits]
number_of_exits = 2
exit_rate.0 = 0.4
exit_rate.1 = 0.4
[TailHook] // For opening cargo door.
tailhook_length=1 ;(feet)
tailhook_position = 0.0, 0.0, 0.0 fold_rates = .070, .07
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 1, -22.95, 0.600, 19.100, Opensky_beacon ,
light.1 = 1, -74.500, 0.000, -7.080, Opensky_beacon ,
light.2 = 2, -130.00, -95.000, 8.80, fx_strobeh ,
light.3 = 2, -130.00, 95.000, 8.80, fx_strobeh ,
light.4 = 3, -210.700, -0.250, 12.300, Opensky_nav_yellow ,
light.5 = 3, -210.700, 0.250, 12.300, Opensky_nav_yellow ,
light.6 = 2, -210.900, 0.000, 11.450, fx_strobeh ,
light.7 = 3, -4.850, 0.000, 14.850, fx_vclighth ,
light.8 = 3, -199.500, -4.500, 43.750, Opensky_wing_light ,
light.9 = 3, -199.500, 4.500, 43.750,
Opensky_wing_light ,
light.10= 5, -70.700, -29.200, 0.000, Opensky_nacelle_refl ,
light.11= 5, -70.700, 29.200, 0.000, Opensky_nacelle_refl ,
light.12= 5, -37.500, -11.700, 2.000, Opensky_nacelle_refl ,
light.13= 5, -37.500, 11.700, 2.000, Opensky_nacelle_refl ,
light.14= 5, -31.500, -13.700, 3.900, Opensky_nacelle_refl ,
light.15= 5, -31.500, 13.700, 3.900, Opensky_nacelle_refl ,
light.16= 5, -5.333, 0.000, -2.000, Opensky_nacelle_refl ,
light.17= 3, -9.300, -6.500, 6.000, Opensky_nacelle_refl ,
light.18= 3, -43.610, -4.500, 6.000, Opensky_nacelle_refl ,
light.19= 3, -135.510, 0.000, -3.000, Opensky_wing_light ,
[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 = available, 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
[brakes]
toe_brakes_scale=.90555
parking_brake=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
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
I am looking for someone to do a 747-200F plane as there are none that came with FSP, here is my aircraft config file.
[fltsim.0]
title=EL AL 747-200F
sim=747-200FPW
model=
panel=
sound=
texture=AXL
checklists=
atc_airline=EL AL
atc_flight_number=204
ui_manufacturer=Project Opensky
ui_type=EL AL 747-200 PACK
ui_variation=EL AL CARGO AXL
visual_damage=1
atc_heavy=1
atc_id=4X-AXL
description=Project Opensky - 747-200F\nVersion 2004.1.0\n\nEngine Type PW JT9D7GR4\n\n747-200F Freight Version \n\nModel Designers\n Vincent Cho\n
Yosuke Ube\n\nFlight Dynamics Designer\n Nick Peterson\n Based on original by Warren Daniel\n\nTechnical Resource\n Simon Ng\n Shigeo
Kitaguchi\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 7220 nm\n\nFor proper operation: See B747 manual at: \n http://www.project-opensky.com
[fltsim.1]
title=EL AL 747-200F AXK
sim=747-200FPW
model=
panel=
sound=
texture=AXK
checklists=
atc_airline=EL AL
atc_flight_number=204
ui_manufacturer=Project Opensky
ui_type=EL AL 747-200 PACK
ui_variation=EL AL CARGO AXK
visual_damage=1
atc_heavy=1
atc_id=4X-AXK
description=Project Opensky \nBoeing 747-200F\nVersion 2004.1.1.0\n\nEngine Type PW JT9D-7R4G2\n\n747-200 Freight Version \n\nModel Designer\n
Yosuke Ube\n Vincent Cho\n\nFlight Dynamics Designer\n Nick Peterson, based on original by Warren Daniel\n\nTechnical Resource\n Simon Ng\n
Shigeo Kitaguchi\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 5,650 nm\n\nTypical city pairs: \n Tokyo-Sydney\n Bangkok-Paris\n
Zurich-Johannesburg\n
[fltsim.2]
title=EL AL 747-200F AXF
sim=747-200FPW
model=
panel=
sound=
texture=AXF
checklists=
atc_airline=EL AL
atc_flight_number=204
ui_manufacturer=Project Opensky
ui_type=EL AL 747-200 PACK
ui_variation=EL AL CARGO AXF
visual_damage=1
atc_heavy=1
atc_id=4X-AXF
description=Project Opensky \nBoeing 747-200F\nVersion 2004.1.1.0\n\nEngine Type PW JT9D-7R4G2\n\n747-200 Freight Version \n\nModel Designer\n
Yosuke Ube\n Vincent Cho\n\nFlight Dynamics Designer\n Nick Peterson, based on original by Warren Daniel\n\nTechnical Resource\n Simon Ng\n
Shigeo Kitaguchi\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 5,650 nm\n\nTypical city pairs: \n Tokyo-Sydney\n Bangkok-Paris\n
Zurich-Johannesburg\n
[General]
performance=Cargo\nTotal lower hold volume:\n 5,497 ft3 (155.6 m3)\nTotal Upper Deck volume:\n 18,270 ft3 (522.0 m3) \n\nDimensions\nSpan 195 ft
8 in\nLength 231 ft 10 in\nHeight 63 ft 5 in\n\nEngines: PW JT9D-7R4G2\nTO Thrust: 54,75000 lb x 4\n\nMax Fuel Cap.: 52,410 US Gal.\nMaxTOW: 833,000
lbs\nMLW: 630,000 lbs\nZFW: 460,965 lbs\nOEW: 347,850 lbs\n\nMax Range: 5,650 nm \nTypical Cruise Speed \n @ FL350: M.85
atc_type=BOEING AIRCRAFT
atc_model=B742
editable=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
[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
[pitot_static]
vertical_speed_time_constant=999
[WEIGHT_AND_BALANCE]
reference_datum_position= 88.000, 0.000, 0.000
empty_weight_CG_position= -105.000, 0.000, 0.000
empty_weight=347850
empty_weight_roll_MOI= 18155743.000
empty_weight_pitch_MOI= 17600873.000
empty_weight_yaw_MOI= 19151035.000
empty_weight_coupled_MOI= 0.000
max_gross_weight=833000
max_number_of_stations = 50
station_load.0 = "44600.0, -60.0, 0.0, 0.0, FWD Up Deck"
station_load.1 = "51200.0, -78.00, 0.0,0.0, MID Up Deck"
station_load.2 = "64800.0, -118.0, 0.0, 0.0, Aft Up Deck"
station_load.3 = "45000.0, -58.0, 0.0, 0.0, FWD Belly"
station_load.4 = "35000.0, -120.0, 0.0,0.0, AFT Belly"
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"
[fuel]
Center1 = -88.0, 0.0, -4.0, 19431.0, 3.0
LeftMain =-102.0, -35.0, -4.0, 16660.0, 3.0
LeftAux =-109.5, -52.0, -3.0, 500.0, 3.0
RightMain =-102.0, 35.0, -4.0, 16660.0, 3.0
RightAux =-109.5, 52.0, -3.0, 500.0, 3.0
fuel_type =2.000000
electric_pump=1
number_of_tank_selectors=1
[airplane_geometry]
wing_area= 5500.000
wing_span= 196.000
wing_root_chord= 53.000
wing_dihedral= 3.998
wing_incidence= 3.500
wing_twist= -0.194
oswald_efficiency_factor= 0.730
wing_winglets_flag= 0
wing_sweep= 37.500
wing_pos_apex_lon= -78.000
wing_pos_apex_vert= 0.000
htail_area= 1470.000
htail_span= 72.750
htail_pos_lon= -204.167
htail_pos_vert= 7.000
htail_incidence= 0.000
htail_sweep= 37.500
vtail_area= 1060.000
vtail_span= 37.121
vtail_sweep= 45.000
vtail_pos_lon= -204.500
vtail_pos_vert= 6.083
elevator_area= 326.800
aileron_area= 225.200
rudder_area= 229.900
elevator_up_limit= 20.751
elevator_down_limit= 15.313
aileron_up_limit= 31.513
aileron_down_limit= 31.513
rudder_limit= 17.189
elevator_trim_limit= 19.167
spoiler_limit= 25.783
spoilerons_available= 0
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 11.459
min_flaps_for_spoilerons= 0.000
[contact_points]
point.0= 1.000, -21.333, 0.00, -14.853, 1181.102, 0.000, 2.000, 70.000, 1.129, 1.100, 0.98, 9.000, 11.000,0.000, 240.000, 280.000
point.1= 1.000, -99.583, -16.000, -15.403, 1574.803, 1.000, 2.000, 0.000, 1.62, 1.15, 0.741, 12.900, 14.900, 2.000, 240.000, 280.000
point.2= 1.000, -99.583, 16.000, -15.403, 1574.803, 2.000, 2.000, 0.000, 1.62, 1.15, 0.741, 13.100, 15.400, 3.000, 240.000, 280.000
point.3= 1.000, -109.583, -6.000, -15.403, 1574.803, 1.000, 2.000, 13.000, 1.62, 1.15, 0.741, 13.400, 14.900, 2.000, 240.000, 280.000
point.4= 1.000, -109.583, 6.000, -15.403, 1574.803,2.000, 2.000, 13.000,1.62, 1.15, 0.741, 12.500, 13.500, 3.000, 240.000, 280.000
point.5= 2.000, -102.167, -96.167, 0.000, 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, -102.167, 96.167, 0.000, 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, -220.667, 0.000, 2.500, 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.8= 2.000, 0.0, 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.9= 2.000, -102.167, -96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.10= 2.000, -220.667, 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
static_pitch= -.300
static_cg_height= 13.625
gear_system_type=0
[GeneralEngineData]
engine_type=1
Engine.0=-109.916667,-69.500000,0.000000
Engine.1=-86.916667,-39.166667,-7.000000
Engine.2=-86.916667,39.166667,-7.000000
Engine.3=-109.916667,69.500000,0.000000
fuel_flow_scalar=1.04
min_throttle_limit=-0.399902
[TurbineEngineData]
bypass_ratio=4.970000
fuel_flow_gain=0.002000
inlet_area=37.558941
rated_N2_rpm=29920.000000
static_thrust=54750.000000
afterburner_available=0
reverser_available=1
[Reference Speeds]
flaps_up_stall_speed= 150.000
full_flaps_stall_speed= 126.000
cruise_speed= 524.337
max_indicated_speed=350.000000
max_mach=0.900000
[keyboard_response]
elevator= 100.000, 200.000
aileron= 100.000, 200.000
rudder= 150.000, 250.000
[Views]
eyepoint=-9.000, -2.000, 14.800
[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=14.000000
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Def
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=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
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
[flaps.0]
type = 1 span-outboard = 0.4 extending-time = 25
flaps-position.0 = 0
flaps-position.1 = 5
flaps-position.2 = 10
flaps-position.3 = 15
flaps-position.4 = 20
flaps-position.5 = 25
flaps-position.6 = 30
damaging-speed = 200
blowout-speed = 250
lift_scalar = 1.00
drag_scalar = .67
pitch_scalar= 0.3
system_type = 1
[flaps.1]
type = 1
span-outboard = 0.4
extending-time = 25
flaps-position.0 = 0
flaps-position.1 = 5
flaps-position.2 = 10
flaps-position.3 = 15
flaps-position.4 = 20
flaps-position.5 = 25
flaps-position.6 = 30
damaging-speed = 200
blowout-speed = 250
lift_scalar = 1.00
drag_scalar = .67
pitch_scalar= 0.3
system_type = 1
[flaps.2]
type = 2
span-outboard = 0.8
extending-time = 12
flaps-position.0 = 0
flaps-position.1 = 20.0
damaging-speed = 250
blowout-speed = 300
lift_scalar = 0.67
drag_scalar = .4
pitch_scalar= 0.1
system_type = 1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[direction_indicators]
direction_indicator.0=3,0
[folding_wings] // For opening main deck cargo door.
wing_fold_system_type = 4 ;0=None
fold_rates = 0.070, 0.070 ;Percent per second
cable_force_adjust = 1.0
[exits]
number_of_exits = 2
exit_rate.0 = 0.4
exit_rate.1 = 0.4
[TailHook] // For opening cargo door.
tailhook_length=1 ;(feet)
tailhook_position = 0.0, 0.0, 0.0 fold_rates = .070, .07
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 1, -22.95, 0.600, 19.100, Opensky_beacon ,
light.1 = 1, -74.500, 0.000, -7.080, Opensky_beacon ,
light.2 = 2, -130.00, -95.000, 8.80, fx_strobeh ,
light.3 = 2, -130.00, 95.000, 8.80, fx_strobeh ,
light.4 = 3, -210.700, -0.250, 12.300, Opensky_nav_yellow ,
light.5 = 3, -210.700, 0.250, 12.300, Opensky_nav_yellow ,
light.6 = 2, -210.900, 0.000, 11.450, fx_strobeh ,
light.7 = 3, -4.850, 0.000, 14.850, fx_vclighth ,
light.8 = 3, -199.500, -4.500, 43.750, Opensky_wing_light ,
light.9 = 3, -199.500, 4.500, 43.750,
Opensky_wing_light ,
light.10= 5, -70.700, -29.200, 0.000, Opensky_nacelle_refl ,
light.11= 5, -70.700, 29.200, 0.000, Opensky_nacelle_refl ,
light.12= 5, -37.500, -11.700, 2.000, Opensky_nacelle_refl ,
light.13= 5, -37.500, 11.700, 2.000, Opensky_nacelle_refl ,
light.14= 5, -31.500, -13.700, 3.900, Opensky_nacelle_refl ,
light.15= 5, -31.500, 13.700, 3.900, Opensky_nacelle_refl ,
light.16= 5, -5.333, 0.000, -2.000, Opensky_nacelle_refl ,
light.17= 3, -9.300, -6.500, 6.000, Opensky_nacelle_refl ,
light.18= 3, -43.610, -4.500, 6.000, Opensky_nacelle_refl ,
light.19= 3, -135.510, 0.000, -3.000, Opensky_wing_light ,
[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 = available, 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
[brakes]
toe_brakes_scale=.90555
parking_brake=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
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
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