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You want a specific paylaod model? - Printable Version

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+--- Thread: You want a specific paylaod model? (/showthread.php?tid=9576)

Pages: 1 2 3 4 5


Re: You want a specific paylaod model? - rennman - 11-07-2005

ok , if it's first come first serve...here is my wish list!

//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"

[fltsim.3]
title=Eaglesoft Citation II 2002
sim=CitationII
model=2002
panel=2002
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 2002"
description="Eaglesoft Cessna Citation II"

[fltsim.4]
title=Eaglesoft Citation II Amb 2002
sim=CitationII
model=amb2002
panel=2002
sound=
texture=amb
kb_checklists=Citation II_check
kb_reference=Citation II_ref
atc_id=N700ES
ui_manufacturer=Cessna
ui_type="Cessna Citation II"
ui_variation="Air Ambulance 2002"
description="Eaglesoft Cessna Citation II"

[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=0.5
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







//Eaglesoft Raytheon Premier 1
//BL 08/06/03 @ 1:30pm

[fltsim.0]
title=Premier1
sim=ESPremier1
model=
panel=
sound=
texture=
kb_checklists=Premier 1_check
kb_reference=Premier 1_ref
atc_id=N3216P
atc_id_color=0xffffffff
atc_airline=
ui_manufacturer=Raytheon
ui_type=Eaglesoft Premier I
ui_variation=Eaglesoft Premier 1
description=The Raytheon Premier I is a small, high performance business jet utilizing unibody carbon composite construction where
possible, making it 25% lighter than if constructed of metals. It offers a max cruise of 451 kt @ 33,ooo ft, and max altitude of 41,000 with a
service range of about 1,500 nm. The aircraft is certified for single pilot operation and accomodates 6 passengers and an additional pilot
with luxury appointments such as leather seats with chrome accessories and bathroom.
visual_damage=0
atc_heavy=0

[General]
performance=Cruise Speed\tMach .77\nMaximum Range\t1,600 nm\nService Ceiling\t41,000 ft\nMax Gross Weight\t12,591
lb\nSeating\t\tUp to 8\nUseful Load\t4,350 lb\n
atc_type=BEECH
atc_model=PRM1
editable=1

// --------------------
//1000 nm, 2:25 hr, 2343 lb, FL390, NAM=0.427 avg
//Climb: 15 min to 37,000 ft. 220 kts / M 0.62
//[11:20-11:34 34 min 454 kts, M0.77, 648 lbs. 11,650 lbs; 1134 PPH @ 460 kts]
//Range: Max fuel, 946 lb payload: 1437 nm + reserve. 368 kt ave, 2901 lb
//High Speed Cruise: 460 kts / 1222 PPH 33,000 ft, 11,000 lb avg weight
//Long Range Cruise: 380 kts / 676 PPH, 41,000 ft, 11,000 lb avg weight

[pitot_static]
vertical_speed_time_constant=8

[WEIGHT_AND_BALANCE]
reference_datum_position=0.00, 0.00, 0.00
empty_weight_CG_position=-0.75, 0.00, -1.00

max_number_of_stations=20
station_load.0="170, 11.45, -1.2, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="0, 11.45, 1.2, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="0, 5.5, -1.2, 0.0, Port Front" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3="0, 5.5, 1.2, 0.0, Strbrd Front" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4="0, 2.8, -1.2, 0.0, Strbrd Middle" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5="170, 2.8, 1.2, 0.0, Port Middle" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6="170, -1.6, -1.2, 0.0, Strbrd Rear" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7="170, -1.6, 1.2, 0.0, Port Rear" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8="230, -8.0, 0.0, 0.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

empty_weight=7996
max_gross_weight=12590 //Ramp

//empty 7979 lb
//max fuel payload 946 2004 lb max
//fuel 3,648
//max 12,573

empty_weight_roll_MOI=20531 //15531 //8467 //10531
empty_weight_pitch_MOI=20888 //12760
empty_weight_yaw_MOI=21262 //22375
empty_weight_coupled_MOI=0 //300

[Views]
eyepoint=11.45,-1.15,3.5

[contact_points]
// Typ Y X Z Dmg Dia Steer Comp Rat DF Tex Tre
point.0=1, 17.00, 0.00, -5.05, 1200, 0, 0.90, 28.0, 0.15, 1.5, 0.63, 8.0, 8.0, 0.0, 0.0, 0.0
point.1=1, -1.33, -4.50, -5.45, 1600, 1, 0.90, 0.0, 0.45 2.5, 0.91, 9.0, 9.0, 2.0, 0.0, 0.0
point.2=1, -1.33, 4.50, -5.45, 1600, 2, 0.90, 0.0, 0.45, 2.5, 0.91, 9.0, 9.0, 3.0, 0.0, 0.0
point.3=2,-13.92,-19.17, -0.50, 300, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2,-13.92, 19.17, -0.50, 300, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2,-28.17, 0.00, -1.00, 300, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2, 18.50, 0.00, -0.42, 300, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch=0.00
static_cg_height=4.90
gear_system_type=0

[fuel]
Center1=0.00, 0.00, -1.50, 0.0, 0.00
LeftMain=-0.00,-6.0, -1.5, 275.0, 2.0
RightMain=-0.00, 6.0, -1.5, 275.0, 2.0
fuel_type=2
number_of_tank_selectors=1
electric_pump=0

[GeneralEngineData]
engine_type=1
Engine.0=-16.67, -3.75, 0.60
Engine.1=-16.67, 3.75, 0.60
fuel_flow_scalar=1.33
min_throttle_limit=0.000000

[TurbineEngineData]
fuel_flow_gain=0.005
inlet_area=1.8 //2.5
rated_N2_rpm=33000
static_thrust=2300
afterburner_available=0
reverser_available=0

[airplane_geometry]
// length: 46.0 ft
wing_area=247.0
wing_span=44.5
wing_root_chord=5.56
wing_dihedral=2.499390
wing_incidence=0.50
wing_twist=-1.5
oswald_efficiency_factor=0.70
wing_winglets_flag=0
wing_sweep=0.0
wing_pos_apex_lon=1.39
wing_pos_apex_vert=-1.0
htail_area=80.0
htail_span=16.08
htail_pos_lon=-23.33
htail_pos_vert=8.0
htail_incidence=-1.00
htail_sweep=0.0
vtail_area=120.0
vtail_span=12.49
vtail_sweep=0.00
vtail_pos_lon=-20.00
vtail_pos_vert=5.83
elevator_area=20.00
aileron_area=21.00
rudder_area=20.40
elevator_up_limit=20.0
elevator_down_limit=10.0
aileron_up_limit=15.5
aileron_down_limit=12.0
rudder_limit=25.0
elevator_trim_limit=18.50
spoiler_limit=60.0
spoilerons_available=1
aileron_to_spoileron_gain=1.75
min_ailerons_for_spoilerons=8.0
min_flaps_for_spoilerons=0.0

[Reference Speeds]
flaps_up_stall_speed=108.0
full_flaps_stall_speed=95.0
cruise_speed=408
max_indicated_speed=330.000000
max_mach=0.809961

[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=1.6
roll_stability=0.7
yaw_stability=2.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo
light.1=1, -23.5, 0.00, 9.543, fx_beacon
light.2=2, -4.067638, -21.542856, -1.343440, fx_strobeh
light.3=2, -4.007101, 21.766573, -1.346386, fx_strobeh
light.4=2, -21.875, 0.0, 3.232653, fx_strobeh
light.5=3, -3.470554, -21.257143, -1.355545, fx_navredm
light.6=3, -3.558306, 21.486074, -1.392181, fx_navgrem
light.7=7, 8.857142, 0.0, 4.514647, esdg_prem_cabinlight_fwd //recognition switch
light.8=7, 1.8, 0.0, 4.510, esdg_prem_cabinlight //recognition switch
light.9=6, 22.228572, 0.00, -10.0, esdg_prem_LL, //landing light switch
light.10=9, 12.5, 0.30, 0.50, esdg_prem_cabinlight_fwd //autoswitch controlled
light.11=9, 12.5, -0.30, 0.50, esdg_prem_cabinlight_fwd //autoswitch controlled
light.12=8, 10.3, -18.6, 8.60, esbj400_icelight //rightwing icelight
light.13=8, 10.3, 18.6, 8.60, esbj400_icelight //leftwing icelight
light.14=8, 5.4, -2.60, -1.2, fx_navwhi.fx //rightwing icelight point source
light.15=8, 5.4, 2.60, -1.2, fx_navwhi.fx //leftwing icelight point source

[SMOKESYSTEM]
smoke.2=-12.0, -15.0, -21.6, fx_contrail_s.fx
smoke.3=-12.0, -15.0, 21.6, fx_contrail_s.fx

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


[Flaps.0]
type=1
span-outboard=0.5
extending-time=10
system_type=0
flaps-position.0=0.0,
flaps-position.1=10.0, 200
flaps-position.2=20.0, 200
flaps-position.3=30.0, 165

[keyboard_response]
elevator=150, 250
aileron=150, 250
rudder=150, 250

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2200
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=95.0
pitch_takeoff_ga=14.0
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

[direction_indicators]
direction_indicator.0=3,0

[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


[electrical]
max_battery_voltage=25.2
generator_alternator_voltage=28.5
max_generator_alternator_amps=100.0

additional_system=0, 1, 16
autopilot=0, 5, 21
avionics_bus=0, 20, 17
avionics=1, 10, 21
flap_motor=0, 20, 20
gear_motor=0, 50, 20
gear_warning=0, 1, 15
light_beacon=0, 5, 19
light_landing=0, 20, 16
light_logo=0, 5, 19
light_nav=0, 5, 17
light_panel=0, 2, 16
light_recognition=0, 10, 18
light_strobe=0, 5, 19
light_taxi=0, 20, 16
light_wing=0, 20, 18
marker_beacon=1, 1, 21
pitot_heat=0, 5, 17
starter1=0,400, 21
starter2=0,400, 21


[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

[brakes]
toe_brakes_scale=1.000000
parking_brake=1

[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


Re: You want a specific paylaod model? - AST416 - 12-07-2005

I would love to have a Payload model for the Citation X Deluxe
Sorry don't have a picture for the plane. Can't seem to get it to work.



//*For Flight Simulator 2002/2004*
//*Copyright© 2002 By Eaglesoft Development Group*
//*All Rights Reserved*
//*Flight Model by Rob Young
//*March3rd 2004 RY Service Release 1

[fltsim.0]
title=Eaglesoft Citation X Deluxe
sim=CitationX
model=
panel=
sound=
texture=
kb_checklists=cessnaCitationX_check
atc_id=N500ES
ui_manufacturer=Cessna
ui_type=Eaglesoft Citation X Deluxe
ui_variation=Blue and Maroon Sweep
description=The Citation X will climb to 43,000 feet in just 30 minutes at its maximum takeoff weight, lifting you swiftly to transcontinental
and transatlantic crossing altitudes. And the Citation X is certified to fly as high as 51,000 feet - where fuel efficiency is optimized and
airline traffic is nonexistent. At 600 mph, the Citation X will run the mile in a sizzling six seconds. It covers 3,300 nautical miles in less
time than any other business jet. It streaks from LA to New York in under four hours. And it shrinks the New York-to-London flight to under
six hours. The Citation X can cross half a dozen time zones without a refueling stop. It combines cruising speeds of Mach .92 with true
intercontinental and transatlantic range. The Citation X is no conventional aircraft. No other business aircraft in the world flies so far, so
fast, on so little.

[fltsim.1]
title=EagleSoft Citation X Standard
sim=CitationX
model=1
panel=
sound=
texture=
kb_checklists=cessnaCitationX_check
atc_id=N500CX
ui_manufacturer=Cessna
ui_type=Eaglesoft Citation X Standard
ui_variation=Maroon Grey Ribbon
description=The Citation X will climb to 43,000 feet in just 30 minutes at its maximum takeoff weight, lifting you swiftly to transcontinental
and transatlantic crossing altitudes. And the Citation X is certified to fly as high as 51,000 feet - where fuel efficiency is optimized and
airline traffic is nonexistent. At 600 mph, the Citation X will run the mile in a sizzling six seconds. It covers 3,300 nautical miles in less
time than any other business jet. It streaks from LA to New York in under four hours. And it shrinks the New York-to-London flight to under
six hours. The Citation X can cross half a dozen time zones without a refueling stop. It combines cruising speeds of Mach .92 with true
intercontinental and transatlantic range. The Citation X is no conventional aircraft. No other business aircraft in the world flies so far, so
fast, on so little.

[fltsim.2]
title=EagleSoft Citation X Light
sim=CitationX
model=2
panel=
sound=
texture=
kb_checklists=cessnaCitationX_check
atc_id=N8JC
ui_manufacturer=Cessna
ui_type=Eaglesoft Citation X Light
ui_variation=Brown Gold Silk
description=The Citation X will climb to 43,000 feet in just 30 minutes at its maximum takeoff weight, lifting you swiftly to transcontinental
and transatlantic crossing altitudes. And the Citation X is certified to fly as high as 51,000 feet - where fuel efficiency is optimized and
airline traffic is nonexistent. At 600 mph, the Citation X will run the mile in a sizzling six seconds. It covers 3,300 nautical miles in less
time than any other business jet. It streaks from LA to New York in under four hours. And it shrinks the New York-to-London flight to under
six hours. The Citation X can cross half a dozen time zones without a refueling stop. It combines cruising speeds of Mach .92 with true
intercontinental and transatlantic range. The Citation X is no conventional aircraft. No other business aircraft in the world flies so far, so
fast, on so little.

[fltsim.3]
title=EagleSoft Citation X Ultra Light
sim=CitationX
model=3
panel=1
sound=
texture=
kb_checklists=cessnaCitationX_check
atc_id=N700CX
ui_manufacturer=Cessna
ui_type=Eaglesoft Citation X Ultra Light
ui_variation=Blue Grey Ribbon
description=The Citation X will climb to 43,000 feet in just 30 minutes at its maximum takeoff weight, lifting you swiftly to transcontinental
and transatlantic crossing altitudes. And the Citation X is certified to fly as high as 51,000 feet - where fuel efficiency is optimized and
airline traffic is nonexistent. At 600 mph, the Citation X will run the mile in a sizzling six seconds. It covers 3,300 nautical miles in less
time than any other business jet. It streaks from LA to New York in under four hours. And it shrinks the New York-to-London flight to under
six hours. The Citation X can cross half a dozen time zones without a refueling stop. It combines cruising speeds of Mach .92 with true
intercontinental and transatlantic range. The Citation X is no conventional aircraft. No other business aircraft in the world flies so far, so
fast, on so little.

[fltsim.4]
title=EagleSoft Citation X Standard House Colors
sim=CitationX
model=1
panel=
sound=
texture=1
kb_checklists=cessnaCitationX_check
atc_id=N750ES
ui_manufacturer=Cessna
ui_type=Eaglesoft Citation X Standard
ui_variation=Eaglesoft House Colors
description=The Citation X will climb to 43,000 feet in just 30 minutes at its maximum takeoff weight, lifting you swiftly to transcontinental
and transatlantic crossing altitudes. And the Citation X is certified to fly as high as 51,000 feet - where fuel efficiency is optimized and
airline traffic is nonexistent. At 600 mph, the Citation X will run the mile in a sizzling six seconds. It covers 3,300 nautical miles in less
time than any other business jet. It streaks from LA to New York in under four hours. And it shrinks the New York-to-London flight to under
six hours. The Citation X can cross half a dozen time zones without a refueling stop. It combines cruising speeds of Mach .92 with true
intercontinental and transatlantic range. The Citation X is no conventional aircraft. No other business aircraft in the world flies so far, so
fast, on so


[General]
atc_type=Cessna
atc_model=C750
editable=1
performance="Please see your Eaglesoft Development Group Cessna Citation X documentation for performance information. Available
on our Downloads Page"


[WEIGHT_AND_BALANCE]
max_gross_weight=36400.0 // (pounds)
empty_weight=21600.0 // (pounds)

reference_datum_position=0.00, 0.00, 0.00 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline,
waterline)
empty_weight_CG_position=-1.0, 0.00, 0.0 // -3.9 (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0="170, 19.0, 0, 0.0, Pilot" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.1="170, 19.0, 0, 0.0, Co-Pilot" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.2="170, 11.5, 0, 0.0, Passenger 1" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.3="170, -22.5,0, 0.0, Passenger 2" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.4="170, -26.7,0, 0.0, Passenger 3" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.5="170, -26.7,0, 0.0, Passenger 4" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.6= "170, -30.9,0, 0.0, Passenger 5" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.7= "170, -30.9,0, 0.0, Passenger 6" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)

;Moments of Inertia
empty_weight_pitch_MOI=280000
empty_weight_roll_MOI=176000
empty_weight_yaw_MOI=110000
empty_weight_coupled_MOI=0.0

[electrical]
max_battery_voltage=24.0
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, 5 , 9.5
avionics=1, 5 , 9.5
additional_system=0, 2 , 9.5
marker_beacon=1, 2 , 9.0
fuel_pump=0, 5 , 9.0

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.12
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=2.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[GeneralEngineData]
engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-10.4, -5.2, 4.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-10.4, 5.2, 4.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.176 //Scalar for fuel flow efficiency
min_throttle_limit=-0.35 //Minimum percent throttle. Generally negative for turbine reverser

[TurbineEngineData]
fuel_flow_gain=0.0030
inlet_area=1.74 // 1.94
rated_N2_rpm=29920
static_thrust=3500 //Lbs, max rated static thrust at Sea Level
afterburner_available=0 //Afterburner available?
reverser_available=1 //Thrust reverser available?

[jet_engine]
thrust_scalar=1.09 //DO NOT CHANGE!!!


//0 Class
//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
[contact_points]
point.0=1, 22.4, 0.00, -4.42, 1181.1, 0, 0.6349, 49.0, 0.2400, 2.5, 0.5460, 8.0, 8.0, 0, 260.0, 260.0
point.1=1, -3.2, -5.30, -4.96, 1574.8, 1, 0.6349, 0.0, 0.5300, 2.5, 0.5456, 9.0, 9.0, 2, 260.0, 260.0
point.2=1, -3.2, 5.30, -4.96, 1574.8, 2, 0.6349, 0.0, 0.5300, 2.5, 0.5456, 9.0, 9.0, 3, 260.0, 260.0
point.3=2, -15.8, -31.4, 0.70, 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, -15.8, 31.4, 0.70, 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, -25.6, 0.00, 3.20, 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, 29.0, 0.00, -0.08, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0

static_pitch=-0.82
static_cg_height=4.6
gear_system_type=1 //Hydraulic

[gear_warning_system]
gear_warning_available=1 //Normal
pct_throttle_limit=0.1 //Percent throttle that activates warning
flap_limit_idle=15.0 //Flap angle that activates warning at idle
flap_limit_power=30.0 //Flap angle that activates warning at above idle

[brakes]
parking_brake=1 //Parking brake available
toe_brakes_scale=0.5 //Brake scalar

[hydraulic_system]
normal_pressure=3000.0 //PSI
electric_pumps=1 //electric pumps enabled
engine_map=1,1,0,0 //pumps on Eng1,2

[Views]
eyepoint=20.2, -.825, 3.15 //RH //Longitudinal, Lateral, Vertical (feet)
//;eyepoint= 20.310204, -1.1, 3.35 //BH //Longitudinal, Lateral, Vertical (feet)

//[RYViews]
;eyepoint=19.9, -1.1, 3.45 //RY
;eyepoint= 20.9, -1.1, 3.35


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo, 10=cockpit
light.0=3, -14.80, -31.2, 0.883441, fx_navredm ,
light.1=3, -14.80, 31.2, 0.883441, fx_navgrem ,
light.2=3, -34.971428, 0.00, 11.37128, fx_navwhi ,
light.3=1, -4.930720, 0.00, -2.383679, fx_beaconb , //belly beacon
light.4=2, -15.95, -31.400158, 0.895627, fx_strobe , //Leftwing strobe
light.5=2, -15.95, 31.400158, 0.895627, fx_strobe , //Rightwing strobe
light.6=1, -27.428572, 0.00, 13.495714, fx_beaconh ,//Horz StabBeacon
light.7=5, 7.09, -4.048980, -0.970262, fx_landing ,//Left
light.8=5, 7.09, 4.048980, -0.970262, fx_landing ,//right
light.9=10, 21.00, 0.00, 2.25, citx_panelflood.fx,
light.10=10, 21.00, 0.00, 0.25, citx_panelflood.fx,
light.11=8, 11.3, -18.6, 7.60, citx_icelight //rightwing icelight
light.12=8, 11.3, 18.6, 7.60, citx_icelight //leftwing icelight
light.13=8, 8.85, -3.1, -.1, fx_navwhi.fx //rightwing icelight point source
light.14=8, 8.85, 3.1, -.1, fx_navwhi.fx //leftwing icelight point source

[SMOKESYSTEM]
smoke.1=-13.3, -22.6, -22.6, fx_contrail_s.fx
smoke.2=-13.3, -22.60, 22.6, fx_contrail_s.fx

[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=1.0 // 0.0 .. 1.0
extending-time=10 // seconds
flaps-position.0=0 // degrees
flaps-position.1=0.01 // degrees
flaps-position.2=5 // degrees
flaps-position.3=15
flaps-position.4=35
damaging-speed=250 // KIAS
blowout-speed=300 // KIAS
system_type=0

[flaps.1]
type=2 // 1 - tail, 2 - lead
span-outboard=1.0 // 0.0 .. 1.0
extending-time=2 // seconds
flaps-position.0=0 // degrees
flaps-position.1=3 // degrees
damaging-speed=250 // KIAS
blowout-speed=300
system_type=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=1,0
Transponder.1=1
Marker.1=1

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

[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

[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

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

[fuel]
Center1= 0.0, 0.0, -1.5, 895.52, 0.0
LeftMain= 0.0, 6.5, -0.8, 522.0, 0.0
RightMain=0.0,-6.5, -0.8, 522.0, 0.0
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=2
electric_pump=1

[airplane_geometry]
wing_area=390.0 //Square feet
wing_span=63.9 //Feet
wing_root_chord=14.9 //Feet
wing_dihedral=3.0 //Degrees
wing_incidence=0.5 //Degrees
wing_twist=-1.5 //Degrees
oswald_efficiency_factor=0.86 //Measure of lift effeciency of wing 0.816
wing_winglets_flag=0 //Are winglets available?
wing_sweep=26.0 //Degrees, wing leading edge
wing_pos_apex_lon=7.9 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.5 //Feet, vertical distance from reference point, positive going up
htail_area=67.0 //Square feet
htail_span=25.6 //Feet
htail_pos_lon=-27.82 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=11.724 //Feet, vertical distance from reference point, positive going up
htail_incidence=1.0 //Degrees
htail_sweep=27.0 //Degrees, horizontal tail leading edge
vtail_area=42.0 //Square feet
vtail_span=7.4 //Feet, tip to body
vtail_sweep=30.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-55.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=4.1 //Feet, vertical distance from reference point, positive going up
elevator_area=17.0 //Square feet
aileron_area=13.5 //Square feet
rudder_area=18.3 //Square feet
elevator_up_limit=17.0 //Degrees
elevator_down_limit=16.5 //Degrees
aileron_up_limit=18.0 //Degrees
aileron_down_limit=16.0 //Degrees
rudder_limit=70.0 //Degrees
elevator_trim_limit=22.0 //Degrees
spoiler_limit=75.0 //Degrees
spoilerons_available=1 //Spoilerons Available?
aileron_to_spoileron_gain=5.6 //Aileron to spoileron gain
min_ailerons_for_spoilerons=10 //Degrees
min_flaps_for_spoilerons=0.0 //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed=112.0 //Knots True (KTAS)
full_flaps_stall_speed=102.0 //Knots True (KTAS)
cruise_speed=494.0 //MAX Knots True (KTAS)
max_mach=0.922
max_indicated_speed=350 //Red line (KIAS)

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2200.0
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm=97.5
autothrottle_takeoff_ga=0
pitch_takeoff_ga=8;
max_pitch=12.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.07
nav_proportional_control=11.00
nav_integrator_control=0.20
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=1.0
Use_no_default_bank=1
Use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0


[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

[stall_warning]
type=1


Re: You want a specific paylaod model? - altstiff - 12-07-2005

DH-2 Beaver?




Re: You want a specific paylaod model? - Tanz - 13-07-2005

AST 416...
There is already a payload model for the Citation X...Check "more download" section, you'll find it in payload updates made by Seb.

FOR ALL REQUESTS:
1/ PLEASE MP ME YOUR EMAIL ADRESS SO I CAN SEND YOU THE FILE FOR TESTIING PURPOSE BEFORE I RELEASE IT ON FSP
WEBSITE.
2/ JUST POST WEIGHT & BALANCE DATAS.
3/ TELL ME THE EXACT NAME OF THE AIRCRAFT THAT FS IS USING (TO AVOID FSP NOT TO RECOGNIZE THE MODEL)

thanks



Post Edited ( 07-14-05 16:14 )


Re: You want a specific paylaod model? - Tanz - 13-07-2005

Hi again guys,

I've finished the Tu-154 & C441...just waiting for those who request them to test it.
Here are the next projects i'm working on:

1/ MD83
2/ MD80
3/ RAYTHEON PREMIER I
4/ DHC2
5/ C421

Cheers



Post Edited ( 07-14-05 16:10 )


Re: You want a specific paylaod model? - taxader - 13-07-2005

Hey altstiff, what beaver are you flying? I'm using Banting's FS2002 MKI model with it's awesome panel. Is there a good FS9 one out
there? I don't like aerosoft's panel at all, although the textures are great. I was going to do my own payload model, but maybe I'll wait for
Tanz's.

And Tanz, you busy lad you!, Did you expect this much feedback, if so my flight helmet's off to you.

Nigel


Re: You want a specific paylaod model? - Tanz - 13-07-2005

hehe taxader...i'm ok with it! lol...but i won't be a payload model factory...with a 24h delivery...hehe..
Tx!




Re: You want a specific paylaod model? - rennman - 13-07-2005

I'm the one who first asked for the cessna citation ll....actually this was a mistake by me....i meant to ask for the citation X...if you could
substitute my previous request for this one that would be cool....no big deal if you can't...thanks


Re: You want a specific paylaod model? - Tanz - 13-07-2005

yop...rennman....check on previous post...Citation X has been already released on a 30 payload models package made by Seb...check
more download section please (must have)...
Cheers




Re: You want a specific paylaod model? - FSfreak - 14-07-2005

Sorry Tanz

i forgot about the Email address: sledge_hockey_master98@hotmail.com

PS: please put the name of the payload model on the Email so i do not make a mistake and delete it,

Thanks

fsfreak


Re: You want a specific paylaod model? - rennman - 14-07-2005

after i put the c441 files in the payload folder... i added the plane to my fleet
...i engaged fsp and the message said that there was no payload for this
aircraft....also the select payload box was greyed out


Re: You want a specific paylaod model? - altstiff - 14-07-2005

Quote:taxader wrote:
Hey altstiff, what beaver are you flying? I'm using Banting's FS2002 MKI model with it's awesome panel. Is there a good FS9 one out
there? I don't like aerosoft's panel at all, although the textures are great. I was going to do my own payload model, but maybe I'll wait for
Tanz's.

And Tanz, you busy lad you!, Did you expect this much feedback, if so my flight helmet's off to you.

Nigel

I have the aerosoft beaver, I fly from the VC so it was the only way to go for me.

Also, thanks Tanz for doing the payload model.



Post Edited ( 07-14-05 07:03 )


Re: You want a specific paylaod model? - altstiff - 14-07-2005

This is from the five seater modern wheels Aerosoft version DH-2

[weight_and_balance]
max_gross_weight = 4650 //MTOW for small wheels
empty_weight = 2850 //DOW for small wheels
reference_datum_position = 0.15, 0, 0 //17.45in in behind wing LE
empty_weight_CG_position = 0.20, 0, 0.5
empty_weight_pitch_MOI = 3210
empty_weight_roll_MOI = 2959
empty_weight_yaw_MOI = 5243
empty_weight_coupled_MOI = 0
max_number_of_stations = 7

station_load.0 = 170, 0.58, -1.25, 0.5, Pilot
station_load.1 = 170, 0.58, 1.25, 0.5, Co-pilot
station_load.2 = 0, -2.42, -1.10, 0.5, PAX 1
station_load.3 = 170, -2.42, 0.00, 0.5, PAX 2
station_load.4 = 0, -2.42, 1.10, 0.5, Pax 3
station_load.5 = 0, -5.17, 0.00, 0.0, baggage front
station_load.6 = 190, -7.83, 0.00, 0.0, baggage rear




Re: You want a specific paylaod model? - Tanz - 14-07-2005

Hi!

Quote:after i put the c441 files in the payload folder... i added the plane to my fleet
...i engaged fsp and the message said that there was no payload for this
aircraft....also the select payload box was greyed out

I think that's a filename problem of the c441.ini file....it should match closely your aircraft name....
Go into the payload editor...open c441, then change the file name and save....

Example form help file:

Example, Say you fly an aircraft:
PMDG 737-800 Swiss livery

Below is a list of existing payload ini name:
MATCH:
737-800. ini
737.ini
PMDG 737.ini

DON'T MATCH:
747-400.ini
PMDG 737-700.ini

tell me if it helps!




Re: You want a specific paylaod model? - rennman - 14-07-2005

i did what you said and it worked!...i guess we have to be sure to use the excact name that is in the title of cfg file....the last a/c i need to
add to my fleet is the "Flight One Golden Eagle 421C".....at your convenience of course...thanks...mike

//********************************************************************
//* CESSNA 421 GOLDEN EAGLE AIRCRAFT CONFIGURATION *
//* For Flight Simulator 2002 *
//* Copyright© 2001 By Flight1 Software, *
//* Roger L. Dial and Steve Small *
//* All Rights Reserved *
//********************************************************************


[fltsim.0]
title=Flight One Golden Eagle 421C
sim=F1_C421
model=
panel=
sound=
texture=
kb_checklists=C421_check
kb_reference=C421_ref
atc_id=N3968G
ui_manufacturer=Flight One Software
ui_type=421C Golden Eagle
ui_variation=White & Blue
editable=0
description=Flight Model for Cessna 421 Golden Eagle © Flight1 Software

[General]
atc_type=CESSNA
atc_model=C421
performance=Power : Continental GTSIO-520-L rated 375Hp @ 2235 Prop RPM. Max Cruise power 32.5 In MAP @ 1900 RPM produces
236 Kts @ 25,000 feet / 195 Kts @ 5,000 feet. For detailed performance and specifications see documentation provided ...

[WEIGHT_AND_BALANCE]
max_gross_weight=7610 // (pounds)
empty_weight=5387 // (pounds)

reference_datum_position=6.96, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-6.06, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

//-----Lightweight loadout : Pilot & Co-pilot only------------------------

station_load.0=0, -3.5, 0.0, 0.0 // Baggage 1 - Nose Locker
station_load.1=170, -6.5, -1.20, 0.0 // Pilot
station_load.2=170, -6.5, 1.20, 0.0 // Co-Pilot
station_load.3=0, -9.8, -1.20, 0.0 // Pax 1
station_load.4=0, -9.8, 1.20, 0.0 // Pax 2
station_load.5=0, -15.2, -1.1, 0.0 // Pax 3
station_load.6=0, -15.2, 1.1, 0.0 Pax 4
station_load.7=0, -17.0, 0.0, 0.0 Baggage 2 - Aft Cabin


;Moments of Inertia
empty_weight_pitch_MOI=22000.00
empty_weight_roll_MOI=11500.00
empty_weight_yaw_MOI=10700.00
empty_weight_coupled_MOI=0.0

[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

[pitot_static]
vertical_speed_time_constant=99

[GeneralEngineData]
engine_type=0
Engine.0=-2.000000,-18.000000,0.700000
Engine.1=-2.000000,18.000000,0.700000
fuel_flow_scalar= 0.915
min_throttle_limit=0.120000

[piston_engine]
power_scalar=1.0
cylinder_displacement= 86.700
compression_ratio= 8.000
number_of_cylinders= 6
max_rated_rpm= 2235.000
max_rated_hp= 375.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.700
turbocharged= -1
max_design_mp= 39.000
min_design_mp= 1.000
critical_altitude= 25000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
propeller_type=0
rotation=-1,1
thrust_scalar=1.0
propeller_diameter=8.3
propeller_blades=3
propeller_moi=5.000000
beta_max=47.000000
beta_min=16.600000
min_gov_rpm=1250.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=900.000000
beta_feather=84.500000
power_absorbed_cf=0.500000
defeathering_accumulators_available=1
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000

[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.55 // 0.0 .. 1.0
extending-time=12 // seconds
flaps-position.0=0 // degrees
flaps-position.1=15 // degrees
flaps-position.2=30 // degrees
flaps-position.3=45 // degrees
damaging-speed=200 // KIAS
blowout-speed=250 // KIAS

[electrical]

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

max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=240.0

flap_motor = 0, 20, 17.0
gear_motor = 0, 25, 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 20, 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 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_static]
vertical_speed_time_constant=100.0

[exits]
number_of_exits=1
exit_rate.0=0.4

[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

[Views]
eyepoint=-6.22, -1.1, 2.10 //Longitudinal, Lateral, Vertical (feet)

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//Longitudinal, Lateral, Vertical (feet)
light.0=3, -8.00, -20.00, 0.325, fx_navred ,
light.1=3, -8.00, 20.00, 0.325, fx_navgre ,
light.2=3, -26.50, 0.00, 1.325, fx_navwhi ,
light.3=2, -8.00, -20.00, 0.325, fx_strobe ,
light.4=2, -8.00, 20.00, 0.325, fx_strobe ,
light.5=1, -27.00, 0.00, 8.825, fx_beacon ,
light.6=2, -8.00, 0.00,-1.675, fx_strobe ,
light.7=4, -5.50, 0.00, 2.00, fx_421_vc,
light.8=4, -10.00, 0.00, 2.00, fx_421_cabin,
light.9=4, -14.00, 0.00, 2.00, fx_421_cabin,
light.10=4,-18.00, 0.00, 2.00, fx_421_cabin,

[keyboard_response]
elevator=150, 250
aileron=150, 250
rudder=150, 350

[direction_indicators]
direction_indicator.0=3,0

[fuel]
//--------Fwd/Aft--L/R----Vert--Cap--Unusable
LeftMain=-8.5, -15.0, 0.0, 121.0, 4.0
RightMain=-8.5, 15.0, 0.0, 121.0, 4.0
fuel_type=1 //Fuel type: 1 = Avgas
number_of_tank_selectors=2
electric_pump=1

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

[airplane_geometry]
wing_area=196.0 //Square feet
wing_span=38.2 //Feet
wing_root_chord=5.3 //Feet
wing_dihedral=3.5 //Degrees
wing_incidence=0.0 //Degrees
wing_twist=-1.2 //Degrees
oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=2.5 //Degrees, wing leading edge
wing_pos_apex_lon=-5.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_area=56.0 //Square feet
htail_span=16.0 //Feet
htail_pos_lon=-22.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence=0.5 //Degrees
htail_sweep=6.0 //Degrees, horizontal tail leading edge
vtail_area=38.0 //Square feet
vtail_span=10.7 //Feet, tip to body
vtail_sweep=45.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-22.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=3.0 //Feet, vertical distance from reference point, positive going up
elevator_area=20.0 //Square feet
aileron_area=11.3 //Square feet
rudder_area=10.5 //Square feet
elevator_up_limit=25.0 //Degrees
elevator_down_limit=16.0 //Degrees
aileron_up_limit=20.0 //Degrees
aileron_down_limit=20.0 //Degrees
rudder_limit=33.0 //Degrees
elevator_trim_limit=15.0 //Degrees
spoiler_limit=90.0 //Degrees
spoilerons_available=0 //Spoilerons Available?
aileron_to_spoileron_gain=0 //Aileron to spoileron gain
min_ailerons_for_spoilerons=0 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed=86.0
full_flaps_stall_speed=77.0
cruise_speed=241.0
max_indicated_speed=216.000000

[autopilot]
use_no_default_pitch=1
use_no_default_bank=1
autopilot_available=1
flight_director_available=1
default_vertical_speed=700.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
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=0.5

[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

[contact_points]
//0 Class
//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

// Gear 1 2 3 4 5 6 7 8 9 10 11 12 13

point.0=1.0, 2.2, 0.0, -5.42, 1600.0, 0.0, 0.5, 36.6, 0.225, 2.5, 1.5, 7.5, 6.5, 0.0, 0.0, 0.0
point.1=1.0, -8.0,-8.4, -5.20, 1850.0, 1.0, 0.5, 0.0, 0.300, 2.5, 0.9, 7.5, 7.5, 2.0, 0.0, 0.0
point.2=1.0, -8.0, 8.4, -5.20, 1850.0, 2.0, 0.5, 0.0, 0.300, 2.5, 0.9, 7.5, 7.7, 3.0, 0.0, 0.0

// Scrapes 1 2 3 4 5 6 7 8 9 10 11 12 13

point.3=2.0, -6.9,-19.9, 0.60, 785.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2.0, -6.9, 19.9, 0.60, 785.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2.0,-26.0, 0.0, 1.60, 785.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2.0, 6.5 ,0.0, -0.80, 785.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch=1.70000
static_cg_height=4.825000
gear_system_type=0
[brakes]
toe_brakes_scale=0.518815
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.1
flap_limit_power=0
flap_limit_idle=0
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=2
[turn_indicators]
turn_indicator.0=1,0