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Request Payload Models Now! - Printable Version

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+--- Thread: Request Payload Models Now! (/showthread.php?tid=10291)

Pages: 1 2 3 4 5

Request Payload Models Now! - Jambone - 13-02-2007

All you have to do is send me the aircraft.cfg and a jpeg image of the aircraft and i shall put it together Wink


James



Re: Request Payload Models Now! - DBE - 13-02-2007

Very generous offer, James! Top

Your help will be greatly appreciated..



Re: Request Payload Models Now! - Jambone - 13-02-2007

Heres one i put together just now Wink

[Image: 747-400.jpg]



Re: Request Payload Models Now! - Russ - 13-02-2007

Thank you, James Applause

I'll get my order in ASAP!



Re: Request Payload Models Now! - Russ - 13-02-2007

As promised, here is the aircraft config and pic for VC-10 payload model.

If anything is not right, just let me know.

Thanks in advance! Beer

I'll leave a message for you with my email address.

[Image: Parked.jpg]

Super VC-10

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[General]
performance=Max Payload: 58,172 lb\nMax Payload, with full fuel: 24,000 lb\nLength: 171 ft 8 in\nSpan: 146 ft 2in\nEngines: Rolls-Royce Conway 43
Mk 550\n\nFSDS2 model by David Maltby\nPanel by Dave Booker & David Maltby\nCheck for updates at the website\nwww.DMflightsim.co.uk
atc_type=BRITISHAEROSPACE
atc_model=VC10

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, -2.000
max_number_of_stations=50
station_load.0= 13000.000, 45.000, 0.000, -2.000
station_load.0=27500.000, -34.000, 0.000, -2.000
empty_weight= 157000.000
empty_weight_roll_MOI= 16000000.000
empty_weight_pitch_MOI= 12000000.000
empty_weight_yaw_MOI= 12000000.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 335000.000
CG_forward_limit= 0.000
CG_aft_limit= 0.000
station_load.1= 11000.000, -35.000, 0.000, -2.000

[fuel]
Center1= 0.000, 0.000, 0.000, 5260.000, 0.000
Center2= 0.000, 0.000, 0.000, 1620.000, 0.000
LeftAux= 0.000, 20.000, 0.000, 8180.000, 600.000
RightAux= 0.000, -20.000, 0.000, 8180.000, 600.000
fuel_type=2.000000
number_of_tank_selectors=4
electric_pump=1

[airplane_geometry]
wing_area= 2932.000
wing_span= 146.000
wing_root_chord= 34.000
wing_dihedral= 4.000
wing_incidence= 1.800
wing_twist= -0.100
oswald_efficiency_factor= 0.800
wing_winglets_flag= 0
wing_sweep= 35.000
wing_pos_apex_lon= 13.000
wing_pos_apex_vert= -2.000
htail_area= 640.000
htail_span= 44.000
htail_pos_lon= -65.000
htail_pos_vert= 25.000
htail_incidence= 0.000
htail_sweep= 40.000
vtail_area= 350.000
vtail_span= 16.000
vtail_sweep= 30.000
vtail_pos_lon= -48.000
vtail_pos_vert= 8.000
elevator_area= 175.000
aileron_area= 250.000
rudder_area= 80.000
elevator_up_limit= 22.000
elevator_down_limit= 22.000
aileron_up_limit= 22.000
aileron_down_limit= 22.000
rudder_limit= 22.000
elevator_trim_limit= 11.000
spoiler_limit= 20.000
spoilerons_available= 1
aileron_to_spoileron_gain= 2.000
min_ailerons_for_spoilerons= 10.000
min_flaps_for_spoilerons= 0.000

[contact_points]
point.0= 1.000, 59.307, 0.000, -9.350, 1574.803, 0.000, 1.548, 75.000, 1.000, 1.273, 0.600, 6.000, 6.000, 0.000, 0.000, 0.000
point.1= 1.000, -14.167, -12.750, -11.000, 1574.803, 1.000, 1.846, 0.000, 1.500, 1.233, 0.600, 8.000, 8.000, 2.000, 0.000, 0.000
point.2= 1.000, -14.167, 12.750, -11.000, 1574.803, 2.000, 1.846, 0.000, 1.500, 1.233, 0.600, 8.500, 8.500, 3.000, 0.000, 0.000
point.3= 2.000, -39.000, -73.000, 2.500, 501.849, 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, -39.000, 73.000, 2.500, 501.849, 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, -51.675, 0.000, 0.000, 501.849, 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, 52.450, 0.000, -4.625, 501.849, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= -0.600
static_cg_height= 10.098
gear_system_type=0

[GeneralEngineData]
engine_type= 1
Engine.0= -58.000, -15.000, 2.275
Engine.1= -58.000, -10.000, 2.275
Engine.2= -58.000, 10.000, 2.275
Engine.3= -58.000, 15.000, 2.275
fuel_flow_scalar= 0.780
min_throttle_limit=-0.15

[TurbineEngineData]
fuel_flow_gain= 0.003
inlet_area= 9.700
rated_N2_rpm= 30000.000
static_thrust= 22500.000
afterburner_available= 0
reverser_available= 1

[Reference Speeds]
flaps_up_stall_speed= 180.000
full_flaps_stall_speed= 110.000
cruise_speed= 490.000
max_indicated_speed=330.000000
max_mach=0.886

[keyboard_response]
elevator=100.000000,200.000000
aileron=100.000000,200.000000
rudder=100.000000,200.000000

[Views]
eyepoint=64.36, -1.74, 4.96 //(feet) longitudinal, lateral, vertical distance from reference datum

[pitot_static]
vertical_speed_time_constant=15 //Increasing this value will cause a more instantaneous reaction in the VSI

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1500.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=93.000000
pitch_takeoff_ga=8.000000
USE_NO_DEFAULT_PITCH=1
USE_NO_DEFAULT_BANK=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=2.000000
max_pitch_velocity_lo_alt=2.500000
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=20.000000
max_bank_acceleration=2.000000
max_bank_velocity=3.000000
max_throttle_rate=0.200000
nav_proportional_control=15.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=12.520000
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

[direction_indicators]
direction_indicator.0=3,0

[jet_engine]
thrust_scalar=1.000

[flight_tuning]
cruise_lift_scalar=0.868
pitch_stability=2.002
roll_stability=0.640
yaw_stability=2.002
parasite_drag_scalar=1.398
induced_drag_scalar=1.278
elevator_effectiveness=1.240
aileron_effectiveness=2.002
rudder_effectiveness=1.240
elevator_trim_effectiveness=0.512
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//fuse strobes
light.0=1, 30.91, 0, 9.7, fx_beaconh
light.1=1, 25.01, 0, -5.18, fx_beaconh
//nav
//light.2=3, -38.40, -73.50, 2.93, fx_navredh
//light.3=3, -38.40, 73.50, 2.93, fx_navgreh
//light.4=3, -38.40, -73.50, 2.53, fx_navred
//light.5=3, -38.40, 73.50, 2.53, fx_navgre
//Wing strobes
//light.6=2, -38.00, -73.30, 2.73, fx_strobeh
//light.7=2, -38.00, 73.30, 2.73, fx_strobeh
//wing landing
//front landing

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Adf.2=1
Transponder.1=1
Marker.1=1

[SMOKESYSTEM]
Smoke.0=2.50, -57.70, -9.60, DM_VC10_SMOKE_R
Smoke.1=2.50, -57.70, -15.10, DM_VC10_SMOKE_R
Smoke.2=2.50, -57.70, 9.60, DM_VC10_SMOKE_L
Smoke.3=2.50, -57.70, 15.10, DM_VC10_SMOKE_L
//smoke.4=0,-36,-73, fx_contrail_320
//smoke.5=0,-36, 73, fx_contrail_320

[TailHook]
tailhook_length=1 ;(feet)
tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0
[brakes]
toe_brakes_scale=0.457778
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=45.0
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

[Flaps.0]
type= 2
span-outboard= 0.900
extending-time= 12.000
system_type= 1
damaging-speed= 270.000
blowout-speed= 300.000
lift_scalar= 0.000
drag_scalar= 0.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 100.000, 0.000
flaps-position.2= 100.000, 0.000
flaps-position.3= 100.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.650
extending-time= 20.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 260.000
lift_scalar= 0.000
drag_scalar= 0.000
pitch_scalar= 0.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 44.444, 0.000
flaps-position.2= 77.778, 0.000
flaps-position.3= 100.000, 0.000
[Flaps.2]
type= 1
span-outboard= 0.650
extending-time= 20.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 260.000
lift_scalar= 0.210
drag_scalar= 0.350
pitch_scalar= 0.050
flaps-position.0= 0.000, 0.000
flaps-position.1= 44.444, 0.000
flaps-position.2= 44.444, 0.000
flaps-position.3= 44.444, 0.000
[Flaps.3]
type= 1
span-outboard= 0.650
extending-time= 20.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 260.000
lift_scalar= 0.120
drag_scalar= 0.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 77.778, 0.000
flaps-position.3= 100.000, 0.000



Re: Request Payload Models Now! - FsP Dennis - 13-02-2007

James I think you got work for the next week when people has posted their request Smile
I think your help would be appreciated a lot too! Top
This Forum simply got a good comunication!



Re: Request Payload Models Now! - FsP Dennis - 13-02-2007

I would like a payload model for United 747-400!
[Image: 1172678.jpg]

[General]
atc_type=BOEING
atc_model=B744
editable=0
performance="Cruise: 0.86 Mach/565 mph/910 km/h\nEngine: General Electric CF6-80C2B1F, Rolls Royce RB211 or Pratt & Whitney
PW4000\nMaximum Range : 7,325 nm [13,570 km]\nMaximum Certified Altitude : 45,100 ft [13,747 m]\nFuel Capacity : 57,285 gal
[216,840 L]\nBasic Operating Weight : 394,088 lb [178,755 kg]\nMax Gross Weight : 875,000 lb [396,893 kg]\nLength : 231 ft 10 in [70.6 m]
\nWingspan : 211 ft 5 in [64.4 m]\nHeight : 63 ft 8 in [19.4 m]\nSeating : Typical 3-class configuration - 416\nTypical 2-class configuration -
524"

[pitot_static]
vertical_speed_time_constant = 99


[WEIGHT_AND_BALANCE]
empty_weight = 394088.0 // 3-Class
max_gross_weight = 875000.0 // 800, 833, 850, 870, 875 x 10^3 lbs [+2000 for max ramp]
max_landing_weight = 630000.0 // 574, 630 x 10^3 lbs
max_zerofuel_weight = 542500.0 // 535, 542.5 x 10^3 lbs
CG_forward_limit=0.130 // 11% 572000-775000 lbs
CG_aft_limit=0.331
// WARNING : DO NOT EDIT !
reference_datum_position = 112.714, 0.0, 5.502 // (feet) Boeing Section2.0 reference position (RefPos)
empty_weight_CG_position = -97.85, 0, 0 // (feet) from RefPos 19.75% MAC

max_number_of_stations =50


;Moments of Inertia
empty_weight_pitch_MOI = 17018677.379279
empty_weight_roll_MOI = 15962454.863936
empty_weight_yaw_MOI = 16890566.121607
empty_weight_coupled_MOI = 2048.0
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.0=0, -95.55, 0.00, 0.00, First Deck
station_load.1=0, -97.85, 0.00, 8.00, Upper Deck
station_load.2=0, -97.85, 0.00, 0.00, Busn Deck
station_load.3=0, -98.00, 0.00, 0.00, Econ Deck
station_load.4=0, -97.11, 0.00, -8.00, Cargo Deck

[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -107.5, -53.3, -6.9 //(feet) from RefPos
Engine.1 = -76.0, -30.0, -10.4 //(feet) from RefPos
Engine.2 = -76.0, 30.0, -10.4 //(feet) from RefPos
Engine.3 = -107.5, 53.3, -6.9 //(feet) from RefPos
fuel_flow_scalar = 1.07 // sfc [...]
min_throttle_limit = -0.20 // reverse

[TurbineEngineData]
//
// Model : CF6-80C2B1F ~58K
//
fuel_flow_gain = 0.0036 //Gain on fuel flow
inlet_area = 61.283 //Square Feet, engine nacelle inlet area [d=106 in]
rated_N2_rpm = 13635.0 //max RPM HPC
static_thrust = 58000.0 //Lbs, nominal SLS adjusted thru EEC
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?

[jet_engine]
thrust_scalar = 1.0

[fuel] // Combi/ER + optional stab (Center2)
LeftAux = -112.0, -36.5, -3.0, 4482.0, 0.0 // Main 1
LeftMain = -96.0, -28.0, -4.0, 12546.0, 0.0 // Main 2
RightMain = -96.0, 28.0, -4.0, 12546.0, 0.0 // Main 3
RightAux = -112.0, 36.5, -3.0, 4482.0, 0.0 // Main 4
LeftTip = -130.0, -73.0, 0.0, 1322.0, 0.0 // R2
RightTip = -130.0, 73.0, 0.0, 1322.0, 0.0 // R3
Center1 = -83.5, 0.0, -7.0, 17164.0, 0.0 // CWT
Center2 = -193.5, 0.0, 6.0, 3300.0, 0.0 // STAB [Optional]
Center3 = -83.5, 0.0, -7.0, 50.0, 0.0 // Other
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 4
electric_pump=0

[airplane_geometry]
wing_area = 5825.0 //Square feet
wing_span = 211.4 //Feet [Jig Position (213.0 at full weight)]
wing_root_chord = 47.298 //Feet
wing_dihedral = 7.0 //Degrees
wing_incidence = 0.0 //Degrees [Inop in FS9]
wing_twist = 0.0 //Degrees [Inop in FS9]
oswald_efficiency_factor = 0.504 //[...]
wing_winglets_flag = 1 //Winglet flag [0:false/1:true]
wing_sweep = 37.5 //Degrees at 25% MAC
wing_pos_apex_lon = -60.606 //Feet from RefPos
wing_pos_apex_vert = 0.0 //Feet from RefPos
htail_area = 1470.0 //Square feet
htail_span = 75.75 //Feet
htail_pos_lon = -210.0 //Feet, from RefPos
htail_pos_vert = 7.32 //Feet, from RefPos
htail_incidence = 0.0 //Degrees [Inop in FS9]
htail_sweep = 37.5 //Degrees, horizontal tail leading edge
vtail_area = 1060.0 //Square feet
vtail_span = 37.1 //Feet, tip to body
vtail_sweep = 45.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -198.5 //Feet from RefPos
vtail_pos_vert = 26.1 //Feet from RefPos
elevator_area = 342.0 //Square feet
aileron_area = 225.0 //Square feet
rudder_area = 230.0 //Square feet
elevator_up_limit = 28.0 //Degrees
elevator_down_limit = 20.0 //Degrees
aileron_up_limit = 29.5 //Degrees
aileron_down_limit = 27.5 //Degrees
rudder_limit = 31.5 //Degrees
elevator_trim_limit = 20.0 //Degrees
spoiler_limit = 70.0 //Degrees
spoilerons_available = 0 //Spoilerons Available?
aileron_to_spoileron_gain = 3.2 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 4.0 //Degrees
min_flaps_for_spoilerons = 0.0 //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed = 174.55 //Stall clean KTAS @450,000 lbs
full_flaps_stall_speed = 122.0 //Stall flaps KTAS
cruise_speed = 485.0 //Cruise KTAS
max_mach = 0.920 //Barber pole MACH
max_indicated_speed = 372.0 // KIAS / modified provision for CAS->KIAS

[flaps.0]
type = 1 // Trailing edge
span-outboard = 0.7 // 0.0 .. 1.0
extending-time = 60 // seconds
flaps-position.0 = 0 // pseudo-degrees
flaps-position.1 = 0.00,280 // 1 - no TE
flaps-position.2 = 25.0,260 // 5
flaps-position.3 = 27.5,240 // 10
flaps-position.4 = 30.0,230 // 20
flaps-position.5 = 31.5,205 // 25
flaps-position.6 = 33.0,180 // 30
lift_scalar = 1.0
drag_scalar = 0.1
pitch_scalar= 1.0
system_type = 1 //Hydraulic

[flaps.1]
type = 2 // Inboard/midboard leading edge
span-outboard = 0.53333 // 0.0 .. 1.0
extending-time = 12 // seconds
flaps-position.0 = 0 // pseudo-degrees
flaps-position.1 = 1.0 // 1
damaging-speed = 275 // KIAS
blowout-speed = 280 // KIAS
lift_scalar = 0.88
drag_scalar = 1.54
pitch_scalar= 1.0
system_type = 1 //Hydraulic

[flaps.2]
type = 2 // Outboard leading edge
span-outboard = 0.2666 // 0.0 .. 1.0
extending-time = 10 // seconds
flaps-position.0 = 0 // pseudo-degrees
flaps-position.1 = 0.0 // 1 - no effect
flaps-position.2 = 5.0 // 5
damaging-speed = 255 // KIAS
blowout-speed = 260 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic

[flaps.3]
type = 2 // Correct 5-30 / TE LIFT
span-outboard = 0.7 // 0.0 .. 1.0
extending-time = 50 // seconds
flaps-position.0 = 0 // pseudo-degrees
flaps-position.1 = 0.00
flaps-position.2 = 25.0
flaps-position.3 = 21.0
flaps-position.4 = 16.1
flaps-position.5 = 8.7
flaps-position.6 = 4.7
lift_scalar = -1.22
drag_scalar = 0.00
pitch_scalar = -0.12
system_type = 1 //Hydraulic

[flaps.4]
type = 2 // Correct 10 / TE DRAG
span-outboard = 0.7 // 0.0 .. 1.0
extending-time = 60 // seconds
flaps-position.0 = 0 // pseudo-degrees
flaps-position.1 = 0.0
flaps-position.2 = 0.0
flaps-position.3 = 1.0
flaps-position.4 = 0.1
flaps-position.5 = 3.0
lift_scalar = 0.00
drag_scalar = -1.00
pitch_scalar = 0.00
system_type = 1 //Hydraulic

[flaps.5]
type = 2 // Correct 30 / TE DRAG
span-outboard = 0.7 // 0.0 .. 1.0
extending-time = 60 // seconds
flaps-position.0 = 0 // pseudo-degrees
flaps-position.1 = 0.0
flaps-position.2 = 0.0
flaps-position.3 = 0.0
flaps-position.4 = 0.0
flaps-position.5 = 0.0
flaps-position.6 = 6.5
lift_scalar = 0.00
drag_scalar = 1.00
pitch_scalar = 0.00
system_type = 1 //Hydraulic

[flaps.6]
type = 1 // Model
span-outboard = 0.7
extending-time = 60
flaps-position.0 = 0.0
flaps-position.1 = 1.0
flaps-position.2 = 5.0
flaps-position.3 = 10.0
flaps-position.4 = 20.0
flaps-position.5 = 25.0
flaps-position.6 = 30.0
lift_scalar = 0.0
drag_scalar = 0.0
pitch_scalar= 0.0
system_type = 1

[autopilot]
autopilot_available = 0
autothrottle_available = 0
default_pitch_mode=0
default_bank_mode=0

//Do Not Alter the following line or your 747-400 may cease operating.
[AFDSAuth]
---BEGIN SHA1---
A4160C6C90B3E606CD280AC89815C9BCE9F05729
---END SHA1---
// Do Not Alter the above lines.

[contact_points]
//
point.0 = 1, -24.194, 0.000, -17.546, 1500.0, 0, 1.932, 56.0, 1.45, 0.128, 0.780, 9.0, 12.0, 0, 270, 320
point.1 = 1, -102.496, -16.009, -18.941, 1500.0, 1, 1.932, 0.0, 1.54, 1.171, 0.880, 16.0, 21.0, 2, 270, 320
point.2 = 1, -102.496, 16.009, -18.941, 1500.0, 2, 1.932, 0.0, 1.54, 1.171, 0.880, 15.0, 20.0, 3, 270, 320
point.3 = 1, -115.277, -4.253, -18.598, 1700.0, 1, 1.932, 0.0, 1.50, 1.203, 0.820, 15.0, 18.0, 2, 270, 320
point.4 = 1, -115.277, 4.253, -18.598, 1700.0, 1, 1.932, 0.0, 1.50, 1.203, 0.820, 15.0, 18.0, 2, 270, 320
//
point.5 = 2, -153.600, -103.500, 3.000, 1250.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0
point.6 = 2, -153.600, 103.500, 3.000, 1250.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0
point.7 = 2, -2.945, 0.000, -3.312, 1500.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0
point.8 = 2, -156.766, 0.000, -9.961, 1500.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0

static_pitch = -0.29
static_cg_height = 12.09
gear_system_type=0

[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 5.0 //Flap angle that activates warning at idle
flap_limit_power = 31.5 //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.78 //Brake scalar

[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,1,1 //pumps on Eng1,2,3,4

[Views]
eyepoint = -19.100, -1.312, 11.122 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)
//eyepoint= -18.848, -1.312, 11.122

[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, 5 , 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

[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
Adf.2 = 1
Transponder.1 = 1
Marker.1 = 1

[LIGHTS]
light.0 = 3, -225.500, -0.50, 4.745, fx_navwhih, //Position Aft
light.1 = 2, -225.500, 0.50, 4.745, fx_strobeh, //Strobe Aft
light.2 = 1, -33.596, 0.00, 14.868, fx_pmdg744_beacon, //Beacon Top
light.3 = 1, -86.149, 0.00, -11.735, fx_pmdg744_beacon, //Beacon Bottom
light.4 = 9, -210.149, 8.00, 35.117, fx_pmdg744_logo, //Logo Right
light.5 = 9, -210.149, -8.00, 35.117, fx_pmdg744_logo, //Logo Left
light.6 = 8, -77.000, 26.00, -4.000, fx_pmdgwinglight, //Wing Right
light.7 = 8, -77.000, -26.00, -4.000, fx_pmdgwinglight, //Wing Left

[SMOKESYSTEM]
smoke.0 = 0.00, -20.5, 0.00, fx_pmdg744_cockpit,

[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

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 1

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0

[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 = 150, 250
aileron = 150, 250
rudder = 150, 250

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second

[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

[stall_warning]
type=2


PS. I would like the weights in LBS if possible.



Re: Request Payload Models Now! - Drew - 13-02-2007

I can see this being a longggggggg post in 2 ways.

Long in replies with people requesting
Long in post, with all of these cfg's getting posted lol



Post Edited ( 02-13-07 20:50 )

Re: Request Payload Models Now! - Jambone - 13-02-2007

United 747 Status: COMPLETE Keep an eye out, direct link will be posted shortly Wink
VC-10 Status: COMPLETE Keep an eye out, direct link will be posted shortly Wink



Post Edited ( 02-13-07 23:24 )

Re: Request Payload Models Now! - Jambone - 13-02-2007

Shop shut until tomorrow (GMT) Wink I cant stay up all night Smile

I expect to see a whole list of requests by tommorow Wink

James



Re: Request Payload Models Now! - Russ - 14-02-2007

Quote:Jambone wrote:
VC-10 Status: COMPLETE Keep an eye out, direct link will be posted shortly Wink

Thanks James, eyes peeled for link.

If you weren't so young, I'd buy you a beer! lol



Re: Request Payload Models Now! - Dixe - 14-02-2007

Hi
i want to douwnload the F1 C 441 Conquest ,i don't find it. Can You make me an Payload Modell?
I found one but the Fspassenger say that this is an Default .So i can't fly this one.Can You help me ?
Thanks a'lot
Dirk






[fltsim.0]
title=Flight One Conquest 441
sim=F1_C441
model=
panel=
sound=
texture=
panel_alias =
sound_alias =
kb_checklists=C441_check
kb_reference=C441_ref
atc_id=N441HC
atc_id_color=0xffffffff
atc_parking_types=RAMP
atc_parking_code=1
ui_manufacturer=Flight One Software
ui_type=441 Conquest
ui_variation=Burgundy and White
description=Flight Model for Cessna 441 Conquest © Flight1 Software, Roger L. Dial. Flight Dynamics © Jerry Beckwith
visual_damage=0

[General]
atc_type=Cessna
atc_model=C441
editable=1
performance=Power: Garrett AirResearch TPE 331 flat rated @ 635.5 Hp. Max speed: 297 kts @ 28000 ft. Max speed @ SL: 243 kts
(Vmo limited). Initial climb rate: 2435 ft/min @ 115 kts. For detailed performance and specifications see documentation provided. Flight
Dynamics By: Jerry Beckwith Mudpond Virtual Aircraft

[pitot_static]
vertical_speed_time_constant = 2

[weight_and_balance]

max_gross_weight = 9925
empty_weight = 5716
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 11990
empty_weight_roll_MOI = 7882
empty_weight_yaw_MOI = 18144
empty_weight_coupled_MOI = 0
max_number_of_stations = 13


station_load.0 =0, 8.73, 0, 0 // Nose Cargo
station_load.1 =170, 3.23, -1.4, 0 // Pilot
station_load.2 =170, 3.23, 1.4, 0 // Co-Pilot
station_load.3 =0, -0.18, -1.43, 0 // Passenger 3
station_load.4 =0, -0.085, 1.43, 0 // Passenger 4
station_load.5 =170, -2.77, -1.44, 0 // Passenger 5
station_load.6 =170, -2.77, 1.44, 0 // Passenger 6
station_load.7 =0, -6.1, -1.44, 0 // Passenger 7
station_load.8 =0, -6.1, 1.44, 0 // Passenger 8
station_load.9 =0, -10.4, -1.44, 0 // Passenger 9
station_load.10 =0, -10.4, 1.44, 0 // Passenger 10
station_load.11 =0, -11.76, 0, 0 // Bay B
station_load.12 = 0, 0, 0, 0 //


[lights]

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

light.0 = 3, 0.17, -24.82, 0.31, fx_navredh
light.1 = 3, 0.17, 24.82, 0.31, fx_navgreh
light.2 = 3, -20.9, 0, 1.325, fx_navwhih
light.3 = 2, -0.12, -24.82, 0.31, fx_strobeh
light.4 = 2, -0.12, 24.82, 0.31, fx_strobeh
light.5 = 1, -20.6, 0, 10.1, fx_beaconh
light.6 = 2, -1.04, 0, -2.25, fx_strobeh
light.7 = 4, 3.44, 0, 2.3, fx_441_vc
light.8 = 4, -2.04, 0, 2.3, fx_441_cabin
light.9 = 4, -7.04, 0, 2.3, fx_441_cabin
light.10 = 4, -11.04, 0, 2.3, fx_441_cabin
light.11 = 8, 2.50, -17.45, 2.0, fx_441ice
light.12 = 8, 2.50, 17.45, 2.0, fx_441ice
light.13 = 8, 2.35, -9.25, -0.15, fx_landing
light.14 = 8, 2.35, 9.25, -0.15, fx_landing
light.15 = 3, -0.39, 24.82, 0.31, fx_navwhi
light.16 = 3, -0.39, -24.82, 0.31, fx_navwhi

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 0.95
engine.0 = 8, -8.2, 0
engine.1 = 8, 8.2, 0
min_throttle_limit=-0.250000

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s
windshield_rain_effect_available=1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2

LeftMain = 0, -4, -1.3, 240.75, 0
RightMain = 0, 4, -1.3, 240.75, 0
electric_pump=1


[contact_points]
static_pitch = 0
static_cg_height = 5.1
max_number_of_points = 7

point.0 = 1, 11.8354, 0, -5.3, 9000, 0, 0.8, 36.6, 0.25, 2.5, 0.99, 7.5, 6.5, 0, 182.16, 201.52
point.1 = 1, -1.3, -7.2, -5.35, 2500, 1, 0.9, 0, 0.35, 2.5, 0.99, 7.5, 7.5, 2, 182.16, 201.52
point.2 = 1, -1.3, 7.2, -5.35, 2500, 2, 0.9, 0, 0.35, 2.5, 0.99, 7.5, 7.7, 3, 182.16, 201.52
point.3 = 2, 0.06, -24.5, 0.4, 785, 0, 0, 0, 0, 0, 0, 0, 0, 5
point.4 = 2, 0.06, 24.5, 0.4, 785, 0, 0, 0, 0, 0, 0, 0, 0, 6
point.5 = 2, -21, 0, 1.3, 785, 0, 0, 0, 0, 0, 0, 0, 0, 9
point.6 = 2, 15.8, 0, -0.5, 785, 0, 0, 0, 0, 0, 0, 0, 0, 4
gear_system_type=1


[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 = 350, 500
aileron = 450, 1000
rudder = 200, 1000


[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
wing_area = 253.6
wing_span = 49.33
wing_root_chord = 5.14088789783093
wing_dihedral = 4
wing_incidence = 0
wing_twist = 0
oswald_efficiency_factor = 0.877424313387267
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 1.28522197445773
wing_pos_apex_vert = 0
htail_area = 63.38
htail_span = 19.07
htail_pos_lon = -19
htail_pos_vert = 0
htail_incidence = 0
htail_sweep = 0
vtail_area = 43.6
vtail_span = 7.6
vtail_sweep = 0
vtail_pos_lon = -20
vtail_pos_vert = 0
elevator_area = 21.57
aileron_area = 14.74
rudder_area = 16.15
elevator_up_limit = 25
elevator_down_limit = 15
aileron_up_limit = 25
aileron_down_limit = 15
rudder_limit = 20
elevator_trim_limit = 20
spoiler_limit = 90
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 160
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
starter3 = 0, 20, 17
starter4 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
prop_sync = 0, 15, 17
auto_feather = 0, 15, 17
auto_brakes = 0, 15, 17
standby_vacuum = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17

[flight_tuning]
cruise_lift_scalar=1
parasite_drag_scalar=1
induced_drag_scalar=1
elevator_effectiveness=1
aileron_effectiveness=1
rudder_effectiveness=1
pitch_stability=1
roll_stability=1
yaw_stability=1
elevator_trim_effectiveness=1
aileron_trim_effectiveness=1
rudder_trim_effectiveness=1
hi_alpha_on_roll = 1
hi_alpha_on_yaw = 1
p_factor_on_yaw = 1
torque_on_roll = 1
gyro_precession_on_roll = 1
gyro_precession_on_yaw = 1

[TurbineEngineData]
fuel_flow_gain=0.08 //Gain on fuel flow
inlet_area=0.1 //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920 //RPM, second stage compressor rated value
static_thrust=100 //Lbs, max rated static thrust at Sea Level
afterburner_available=0
reverser_available=0

[turboprop_engine]
power_scalar=1 //Scalar on Turboprop power
maximum_torque=1711 //Maximum torque available (ft-lbs)

[propeller]
thrust_scalar=1 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=7.5 //Propeller Diameter, (feet)
propeller_blades=4 //Number of propeller blades
propeller_moi=14.7 //Propeller moment of inertia
beta_max=65 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=10 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=22440 //Miminum governed RPM
prop_tc=0.01 //Prop time-constant
gear_reduction_ratio=14.96 //Propeller gear reduction ratio
fixed_pitch_beta=30 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700 //Minimum RPM for prop feathering
beta_feather=87.4 //Feathering pitch angle (degrees)
power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=1 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=2 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14 //Minimum pitch angle in reverse, (degrees)
rotation = 1, 1

[Views]
eyepoint=3.0, -1.3, 2.1

[flaps.0] //Trailing Edge Flaps
type = 1
span-outboard = 0.5
extending-time = 12
flaps-position.0 = 0
flaps-position.1 = 10, 200
flaps-position.2 = 20, 200
flaps-position.3 = 30, 180
damaging-speed = 220
blowout-speed = 240
system_type = 1
lift_scalar = 1
drag_scalar = 1
pitch_scalar = 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=2,0

[exits]
number_of_exits = 3
exit_rate.0 = 0.4
exit_rate.1 = 0.4

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1500
autothrottle_available=0
autothrottle_arming_required = 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga = 1
pitch_takeoff_ga=8
max_pitch_velocity_hi_alt = 1.5
max_pitch_velocity_lo_alt_breakpoint = 20000
max_pitch_velocity_hi_alt_breakpoint = 28000
max_pitch = 10
max_pitch_acceleration = 1
max_pitch_velocity_lo_alt = 2
max_bank= 25
max_bank_acceleration = 1.8
max_bank_velocity = 3
max_throttle_rate = 0.1
nav_proportional_control = 9
nav_integrator_control = 0.25
nav_derivative_control = 0
nav_integrator_boundary = 2.5
nav_derivative_boundary = 0
gs_proportional_control = 9.52
gs_integrator_control = 0.26
gs_derivative_control = 0
gs_integrator_boundary = 0.7
gs_derivative_boundary = 0
yaw_damper_gain = 1

[Reference Speeds]
flaps_up_stall_speed=67.8 //Knots True (KTAS)
full_flaps_stall_speed=57.4 //Knots True (KTAS)
cruise_speed=235 //Knots True (KTAS)
max_indicated_speed = 245 //Knots True (KTAS)
max_mach = 0.55 //Knots True (KTAS)

[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 22.5 //Flap angle that activates warning at idle
flap_limit_power = 11.25 //Flap angle that activates warning at above idle

[brakes]
//toe_brakes_scale = 0.999969481490524 //Brake scalar
toe_brakes_scale = 0.75 //Brake scalar
parking_brake = 1 //Parking brake available

[stall_warning]
type = 1

[hydraulic_system]
electric_pumps = 0 //no electric pumps
engine_map = 1, 1, 0, 0 //pumps on Eng1,2
normal_pressure = 1250 //PSI

[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

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=2

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0


[SMOKESYSTEM]
smoke.0=0.0, 0.0, 8.139, fx_441_Exhaust
smoke.1=0.0, 0.0, -8.139, fx_441_Exhaust



Re: Request Payload Models Now! - Dixe - 14-02-2007

Hi James ,i have too the Eagle-Sotware Cessna Citation CJ I and i ask You for creating an Payloadmodel.Can You make it for me
Thousend Thanks for Creating.
Dirk


//Release Flight Model June 10th 2004 - RY

[fltsim.0]
title=Eaglesoft Citation II
sim=CitationII
model=
panel=
sound=
texture=
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N700ES
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Corporate Full"
description="Eaglesoft Cessna Citation II"

[fltsim.1]
title=Eaglesoft Citation II Lite
sim=CitationII
model=lite
panel=lite
sound=
texture=lite
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N500ES
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Corporate Lite"
description="No VC Citation II"


[fltsim.2]
title=Eaglesoft Citation II Amb
sim=CitationII
model=amb
panel=
sound=
texture=amb
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N147DR
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Air Ambulance"
description="Lifeflight"

[General]
atc_type=Cessna
atc_model=C551
editable=1
performance=Pratt & Whitney JT15D-4 @ 2,500 lbs thrust


[WEIGHT_AND_BALANCE]
max_gross_weight=12500
empty_weight=7100 //equipped - no fuel or PAX

reference_datum_position=0, 0, -0.8
empty_weight_CG_position=-1.0, 0, 0 //-0.29

max_number_of_stations=12

station_load.0="170, 7.5, 0.0, 0.0, Pilot" // placed in the middle to overcome FS's pilot assymetry instability
station_load.1="0.00, 7.5, 1.2, 0.0, Co-Pilot" //This aircraft is cleared for single pilot operation
station_load.2="0, 0.5, -1.2, 0.0, Passenger Row 1"
station_load.3="0, 0.5, 1.2, 0.0, Passenger Row 1"
station_load.4="170, -3.5, -1.2, 0.0, Passenger Row 2"
station_load.5="0, -3.5, 1.2, 0.0, Passenger Row 2"
station_load.6="0.00, -6.0, -1.2, 0.0, Passenger Row 3"
station_load.7="0.00, -6.0, 1.2, 0.0, Passenger Row 3"
station_load.8="25, 4.0, 0.0, 0.0, Forward Baggage"
station_load.9= "25,-15.6, 0.0, 0.0, Rear Baggage"


;Moments of Inertia
empty_weight_pitch_MOI=42000
empty_weight_roll_MOI=38000
empty_weight_yaw_MOI=21000
empty_weight_coupled_MOI=0.0

[electrical]
max_battery_voltage=25.2
generator_alternator_voltage=28.5
max_generator_alternator_amps=400.0

;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-
7=Generator/AlternatorBus(1-4)
avionics_bus=0, 100, 20
avionics=1, 50 , 20
additional_system=0, 50, 20
marker_beacon=1, 10 , 20
fuel_pump=0, 15 , 20
fuel_transfer_pump=0, 15, 20
flap_motor=0, 40, 20
gear_motor=0, 60, 20
autopilot=1, 10, 20
pitot_heat=0, 30, 20
gear_warning=0, 4, 20
starter1=0, 100, 20
starter2=0, 100, 20
light_nav=0, 10, 20
light_beacon=0, 10, 20
light_strobe=0, 10, 20
light_landing=0, 10, 20
light_taxi=0, 30, 20
light_panel=0, 10, 20
hydraulic_pump=0, 20, 20
light_recognition=0, 10, 20
light_logo=0, 10, 20
light_wing=o, 10, 20


[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.13
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=0.66
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[GeneralEngineData]
engine_type=1
Engine.0=-13.0, -4.0, 1.6
Engine.1=-13.0, 4.0, 1.6
fuel_flow_scalar=1.6
min_throttle_limit=-0.24


[TurbineEngineData]
fuel_flow_gain=0.0040 // was 0.0020
inlet_area=1.7 //2.1
rated_N2_rpm=29920
static_thrust=2200 // nominal value is 2500 per engine. This param is superceded elsewhere
afterburner_available=0
reverser_available=1
//bypass ratio = 3.3

[jet_engine]
thrust_scalar=1.0


;point.0=1, 16.00, 0.00, -2.80, 1181.1, 0, 0.7549, 30.0, 0.4197, 2.5, 0.4, 10.0, 10.0, 0, 0.0, 0.0
;point.1=1, -3.45, -4.85, -2.80, 1574.8, 1, 0.8549, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 2, 0.0, 0.0
;point.2=1, -3.45, 4.85, -2.80, 1574.8, 2, 0.8549, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 3, 0.0, 0.0

[contact_points]
point.0=1, 16.00, 0.00, -2.45, 1181.1, 0, 0.7549, 34.0, 0.2350, 2.2, 0.4500, 10.0, 10.0, 0, 0.0, 0.0
point.1=1, -3.20, -4.85, -2.37, 1574.8, 1, 0.8549, 0.0, 0.2700, 2.2, 0.4800, 9.0, 9.0, 2, 0.0, 0.0
point.2=1, -3.20, 4.85, -2.37, 1574.8, 2, 0.8549, 0.0, 0.2700, 2.2, 0.4800, 9.0, 9.0, 3, 0.0, 0.0
point.3=2, -8.55, -22.00, -0.60, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -8.55, 22.00, -0.60, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -22.00, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 0.00, 0.00, - 1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0


static_pitch=0.55
static_cg_height=3.1
gear_system_type=0

[Views]
eyepoint=10.80, -1.33, 3.56

[flaps.0]
type=1
span-outboard=0.8
extending-time=5
flaps-position.0=0
flaps-position.1=15
flaps-position.2=35
flaps-position.3=40
damaging-speed=250
blowout-speed=300

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 1
Adf.1=1
Transponder.1=1
Marker.1=1

[keyboard_response]

elevator=150, 250
aileron=150, 250
rudder=150, 250

[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

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[brakes]
toe_brakes_scale=0.5
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=8.594367

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[fuel]
LeftMain= -3.5, -7.0, 0.0, 371.0, 0.0
RightMain= -3.5, 7.0, 0.0, 371.0, 0.0
fuel_type=2
number_of_tank_selectors=1
electric_pump=1
//total fuel load 5,008 lbs


[airplane_geometry]
wing_area=312.0
wing_span=51.66
wing_root_chord=6.8
wing_dihedral=2.5
wing_incidence=0.5
wing_twist=-1.5
oswald_efficiency_factor=0.6
wing_winglets_flag=1
wing_sweep=35.0
wing_pos_apex_lon=8.7
wing_pos_apex_vert=0.0
htail_area=67.0
htail_span=17.2
htail_pos_lon=-24.6
htail_pos_vert=0.0
htail_incidence=1.3
htail_sweep=25.0
vtail_area=42.0
vtail_span=7.4
vtail_sweep=30.0
vtail_pos_lon=-20.5
vtail_pos_vert=4.1
elevator_area=17.0
aileron_area=13.5
rudder_area=7.3
elevator_up_limit=17.0
elevator_down_limit=15.5
aileron_up_limit=18.0
aileron_down_limit=18.0
rudder_limit=30.0
elevator_trim_limit=15.0
spoiler_limit=60.0
spoilerons_available=0
aileron_to_spoileron_gain=4.600000
min_ailerons_for_spoilerons=4.984733
min_flaps_for_spoilerons=0.000000


[Reference Speeds]
flaps_up_stall_speed=76
full_flaps_stall_speed=90
cruise_speed=330.0
max_indicated_speed=277.000000
max_mach=0.705

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm=95
autothrottle_takeoff_ga=0
pitch_takeoff_ga=8
default_bank_mode=0
default_pitch_mode=0
use_no_default_bank=1
use_no_default_pitch=1
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=0.01
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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo
light.0=3, -1.7, -25.8, 2.1, fx_navred
light.1=3, -1.7, 25.8, 2.1, fx_navgre
light.2=7, -24.0, 0.00, 3.11, fx_navwhi.fx
light.3=7, -24.0, 0.00, 12.5, fx_beacon
light.4=10, 11.50, 0.30, 2.00, esbj400_panelflood.fx
light.5=10, 11.50, -0.30, 2.00, esbj400_panelflood.fx
light.6=2, -1.85, -25.8, 2.1, fx_strobe
light.7=2, -1.85, 25.8, 2.1, fx_strobe
light.10=8, 2.45, -2.7, 1.6, fx_navwhi.fx
light.11=8, 2.45, 2.7, 1.6, fx_navwhi.fx
light.12=8, 12.0, -17.8, 8.60, esbj400_icelight //rightwing icelight
light.13=8, 12.0, 17.8, 8.60, esbj400_icelight //leftwing icelight


[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second

[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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

//Copyright© Eaglesoft Development Group 6/2002 ALL RIGHTS RESERVED

[General]
performance=JT15D-5 2 2965 (3045) lb, 2414 lb @FL400, M 0.8\nSFC\tstatic 0.56, cruise 0.541?\nFlow\t75 lb\/sec\ndia \t2.28 ft, 4.07 ft^2
\nMax cruise 468 kt tas\nMax range 1770 nm\nCeiling\t45,000 ft\nMTOW\t16,000 lb\nClimb\t 4020 fpm\nFuel \t 744 gal 4912
lb\nalpha_o=-2.55\n



Re: Request Payload Models Now! - Joeflyer - 14-02-2007

Dirk, there is a C441 payload model already. I use it frequently. You only have to rename the .ini file to match with the aircraft name or vice
versa. It works just fine.



Re: Request Payload Models Now! - Jambone - 14-02-2007

Where are the pics people! I'll try my best without pics, but please try to include them Wink