You want a specific paylaod model? - Printable Version +- FsPassengers Forums (http://www.fspassengers.com/forum) +-- Forum: FsPassengers (http://www.fspassengers.com/forum/forumdisplay.php?fid=3) +--- Forum: FsPassengers Customizing (http://www.fspassengers.com/forum/forumdisplay.php?fid=6) +--- Thread: You want a specific paylaod model? (/showthread.php?tid=9576) |
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: 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 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 |