13-02-2007, 11:00 AM
All you have to do is send me the aircraft.cfg and a jpeg image of the aircraft and i shall put it together
James
James
Request Payload Models Now!
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13-02-2007, 11:00 AM
All you have to do is send me the aircraft.cfg and a jpeg image of the aircraft and i shall put it together
James
13-02-2007, 11:30 AM
Heres one i put together just now
13-02-2007, 12:49 PM
Thank you, James
I'll get my order in ASAP! "Boys will be boys, and so will a lot of middle-aged men." - Kin Hubbard
13-02-2007, 08:16 PM
As promised, here is the aircraft config and pic for VC-10 payload model.
If anything is not right, just let me know. Thanks in advance! I'll leave a message for you with my email address. Super VC-10 [forcefeedback] gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [General] performance=Max Payload: 58,172 lb\nMax Payload, with full fuel: 24,000 lb\nLength: 171 ft 8 in\nSpan: 146 ft 2in\nEngines: Rolls-Royce Conway 43 Mk 550\n\nFSDS2 model by David Maltby\nPanel by Dave Booker & David Maltby\nCheck for updates at the website\nwww.DMflightsim.co.uk atc_type=BRITISHAEROSPACE atc_model=VC10 [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, -2.000 max_number_of_stations=50 station_load.0= 13000.000, 45.000, 0.000, -2.000 station_load.0=27500.000, -34.000, 0.000, -2.000 empty_weight= 157000.000 empty_weight_roll_MOI= 16000000.000 empty_weight_pitch_MOI= 12000000.000 empty_weight_yaw_MOI= 12000000.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 335000.000 CG_forward_limit= 0.000 CG_aft_limit= 0.000 station_load.1= 11000.000, -35.000, 0.000, -2.000 [fuel] Center1= 0.000, 0.000, 0.000, 5260.000, 0.000 Center2= 0.000, 0.000, 0.000, 1620.000, 0.000 LeftAux= 0.000, 20.000, 0.000, 8180.000, 600.000 RightAux= 0.000, -20.000, 0.000, 8180.000, 600.000 fuel_type=2.000000 number_of_tank_selectors=4 electric_pump=1 [airplane_geometry] wing_area= 2932.000 wing_span= 146.000 wing_root_chord= 34.000 wing_dihedral= 4.000 wing_incidence= 1.800 wing_twist= -0.100 oswald_efficiency_factor= 0.800 wing_winglets_flag= 0 wing_sweep= 35.000 wing_pos_apex_lon= 13.000 wing_pos_apex_vert= -2.000 htail_area= 640.000 htail_span= 44.000 htail_pos_lon= -65.000 htail_pos_vert= 25.000 htail_incidence= 0.000 htail_sweep= 40.000 vtail_area= 350.000 vtail_span= 16.000 vtail_sweep= 30.000 vtail_pos_lon= -48.000 vtail_pos_vert= 8.000 elevator_area= 175.000 aileron_area= 250.000 rudder_area= 80.000 elevator_up_limit= 22.000 elevator_down_limit= 22.000 aileron_up_limit= 22.000 aileron_down_limit= 22.000 rudder_limit= 22.000 elevator_trim_limit= 11.000 spoiler_limit= 20.000 spoilerons_available= 1 aileron_to_spoileron_gain= 2.000 min_ailerons_for_spoilerons= 10.000 min_flaps_for_spoilerons= 0.000 [contact_points] point.0= 1.000, 59.307, 0.000, -9.350, 1574.803, 0.000, 1.548, 75.000, 1.000, 1.273, 0.600, 6.000, 6.000, 0.000, 0.000, 0.000 point.1= 1.000, -14.167, -12.750, -11.000, 1574.803, 1.000, 1.846, 0.000, 1.500, 1.233, 0.600, 8.000, 8.000, 2.000, 0.000, 0.000 point.2= 1.000, -14.167, 12.750, -11.000, 1574.803, 2.000, 1.846, 0.000, 1.500, 1.233, 0.600, 8.500, 8.500, 3.000, 0.000, 0.000 point.3= 2.000, -39.000, -73.000, 2.500, 501.849, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -39.000, 73.000, 2.500, 501.849, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -51.675, 0.000, 0.000, 501.849, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 52.450, 0.000, -4.625, 501.849, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= -0.600 static_cg_height= 10.098 gear_system_type=0 [GeneralEngineData] engine_type= 1 Engine.0= -58.000, -15.000, 2.275 Engine.1= -58.000, -10.000, 2.275 Engine.2= -58.000, 10.000, 2.275 Engine.3= -58.000, 15.000, 2.275 fuel_flow_scalar= 0.780 min_throttle_limit=-0.15 [TurbineEngineData] fuel_flow_gain= 0.003 inlet_area= 9.700 rated_N2_rpm= 30000.000 static_thrust= 22500.000 afterburner_available= 0 reverser_available= 1 [Reference Speeds] flaps_up_stall_speed= 180.000 full_flaps_stall_speed= 110.000 cruise_speed= 490.000 max_indicated_speed=330.000000 max_mach=0.886 [keyboard_response] elevator=100.000000,200.000000 aileron=100.000000,200.000000 rudder=100.000000,200.000000 [Views] eyepoint=64.36, -1.74, 4.96 //(feet) longitudinal, lateral, vertical distance from reference datum [pitot_static] vertical_speed_time_constant=15 //Increasing this value will cause a more instantaneous reaction in the VSI [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1500.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=93.000000 pitch_takeoff_ga=8.000000 USE_NO_DEFAULT_PITCH=1 USE_NO_DEFAULT_BANK=1 default_pitch_mode=0 default_bank_mode=0 max_pitch=10.000000 max_pitch_acceleration=2.000000 max_pitch_velocity_lo_alt=2.500000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=20.000000 max_bank_acceleration=2.000000 max_bank_velocity=3.000000 max_throttle_rate=0.200000 nav_proportional_control=15.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=12.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=1.000000 [direction_indicators] direction_indicator.0=3,0 [jet_engine] thrust_scalar=1.000 [flight_tuning] cruise_lift_scalar=0.868 pitch_stability=2.002 roll_stability=0.640 yaw_stability=2.002 parasite_drag_scalar=1.398 induced_drag_scalar=1.278 elevator_effectiveness=1.240 aileron_effectiveness=2.002 rudder_effectiveness=1.240 elevator_trim_effectiveness=0.512 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //fuse strobes light.0=1, 30.91, 0, 9.7, fx_beaconh light.1=1, 25.01, 0, -5.18, fx_beaconh //nav //light.2=3, -38.40, -73.50, 2.93, fx_navredh //light.3=3, -38.40, 73.50, 2.93, fx_navgreh //light.4=3, -38.40, -73.50, 2.53, fx_navred //light.5=3, -38.40, 73.50, 2.53, fx_navgre //Wing strobes //light.6=2, -38.00, -73.30, 2.73, fx_strobeh //light.7=2, -38.00, 73.30, 2.73, fx_strobeh //wing landing //front landing [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Adf.2=1 Transponder.1=1 Marker.1=1 [SMOKESYSTEM] Smoke.0=2.50, -57.70, -9.60, DM_VC10_SMOKE_R Smoke.1=2.50, -57.70, -15.10, DM_VC10_SMOKE_R Smoke.2=2.50, -57.70, 9.60, DM_VC10_SMOKE_L Smoke.3=2.50, -57.70, 15.10, DM_VC10_SMOKE_L //smoke.4=0,-36,-73, fx_contrail_320 //smoke.5=0,-36, 73, fx_contrail_320 [TailHook] tailhook_length=1 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0 [brakes] toe_brakes_scale=0.457778 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=45.0 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [Flaps.0] type= 2 span-outboard= 0.900 extending-time= 12.000 system_type= 1 damaging-speed= 270.000 blowout-speed= 300.000 lift_scalar= 0.000 drag_scalar= 0.000 pitch_scalar= 0.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 100.000, 0.000 flaps-position.2= 100.000, 0.000 flaps-position.3= 100.000, 0.000 [Flaps.1] type= 1 span-outboard= 0.650 extending-time= 20.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 260.000 lift_scalar= 0.000 drag_scalar= 0.000 pitch_scalar= 0.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 44.444, 0.000 flaps-position.2= 77.778, 0.000 flaps-position.3= 100.000, 0.000 [Flaps.2] type= 1 span-outboard= 0.650 extending-time= 20.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 260.000 lift_scalar= 0.210 drag_scalar= 0.350 pitch_scalar= 0.050 flaps-position.0= 0.000, 0.000 flaps-position.1= 44.444, 0.000 flaps-position.2= 44.444, 0.000 flaps-position.3= 44.444, 0.000 [Flaps.3] type= 1 span-outboard= 0.650 extending-time= 20.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 260.000 lift_scalar= 0.120 drag_scalar= 0.500 pitch_scalar= 0.100 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.000, 0.000 flaps-position.2= 77.778, 0.000 flaps-position.3= 100.000, 0.000 "Boys will be boys, and so will a lot of middle-aged men." - Kin Hubbard
13-02-2007, 08:43 PM
James I think you got work for the next week when people has posted their request
I think your help would be appreciated a lot too! This Forum simply got a good comunication!
13-02-2007, 08:49 PM
I would like a payload model for United 747-400!
[General] atc_type=BOEING atc_model=B744 editable=0 performance="Cruise: 0.86 Mach/565 mph/910 km/h\nEngine: General Electric CF6-80C2B1F, Rolls Royce RB211 or Pratt & Whitney PW4000\nMaximum Range : 7,325 nm [13,570 km]\nMaximum Certified Altitude : 45,100 ft [13,747 m]\nFuel Capacity : 57,285 gal [216,840 L]\nBasic Operating Weight : 394,088 lb [178,755 kg]\nMax Gross Weight : 875,000 lb [396,893 kg]\nLength : 231 ft 10 in [70.6 m] \nWingspan : 211 ft 5 in [64.4 m]\nHeight : 63 ft 8 in [19.4 m]\nSeating : Typical 3-class configuration - 416\nTypical 2-class configuration - 524" [pitot_static] vertical_speed_time_constant = 99 [WEIGHT_AND_BALANCE] empty_weight = 394088.0 // 3-Class max_gross_weight = 875000.0 // 800, 833, 850, 870, 875 x 10^3 lbs [+2000 for max ramp] max_landing_weight = 630000.0 // 574, 630 x 10^3 lbs max_zerofuel_weight = 542500.0 // 535, 542.5 x 10^3 lbs CG_forward_limit=0.130 // 11% 572000-775000 lbs CG_aft_limit=0.331 // WARNING : DO NOT EDIT ! reference_datum_position = 112.714, 0.0, 5.502 // (feet) Boeing Section2.0 reference position (RefPos) empty_weight_CG_position = -97.85, 0, 0 // (feet) from RefPos 19.75% MAC max_number_of_stations =50 ;Moments of Inertia empty_weight_pitch_MOI = 17018677.379279 empty_weight_roll_MOI = 15962454.863936 empty_weight_yaw_MOI = 16890566.121607 empty_weight_coupled_MOI = 2048.0 station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation" station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation" station_load.0=0, -95.55, 0.00, 0.00, First Deck station_load.1=0, -97.85, 0.00, 8.00, Upper Deck station_load.2=0, -97.85, 0.00, 0.00, Busn Deck station_load.3=0, -98.00, 0.00, 0.00, Econ Deck station_load.4=0, -97.11, 0.00, -8.00, Cargo Deck [GeneralEngineData] engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -107.5, -53.3, -6.9 //(feet) from RefPos Engine.1 = -76.0, -30.0, -10.4 //(feet) from RefPos Engine.2 = -76.0, 30.0, -10.4 //(feet) from RefPos Engine.3 = -107.5, 53.3, -6.9 //(feet) from RefPos fuel_flow_scalar = 1.07 // sfc [...] min_throttle_limit = -0.20 // reverse [TurbineEngineData] // // Model : CF6-80C2B1F ~58K // fuel_flow_gain = 0.0036 //Gain on fuel flow inlet_area = 61.283 //Square Feet, engine nacelle inlet area [d=106 in] rated_N2_rpm = 13635.0 //max RPM HPC static_thrust = 58000.0 //Lbs, nominal SLS adjusted thru EEC afterburner_available = 0 //Afterburner available? reverser_available = 1 //Thrust reverser available? [jet_engine] thrust_scalar = 1.0 [fuel] // Combi/ER + optional stab (Center2) LeftAux = -112.0, -36.5, -3.0, 4482.0, 0.0 // Main 1 LeftMain = -96.0, -28.0, -4.0, 12546.0, 0.0 // Main 2 RightMain = -96.0, 28.0, -4.0, 12546.0, 0.0 // Main 3 RightAux = -112.0, 36.5, -3.0, 4482.0, 0.0 // Main 4 LeftTip = -130.0, -73.0, 0.0, 1322.0, 0.0 // R2 RightTip = -130.0, 73.0, 0.0, 1322.0, 0.0 // R3 Center1 = -83.5, 0.0, -7.0, 17164.0, 0.0 // CWT Center2 = -193.5, 0.0, 6.0, 3300.0, 0.0 // STAB [Optional] Center3 = -83.5, 0.0, -7.0, 50.0, 0.0 // Other fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 4 electric_pump=0 [airplane_geometry] wing_area = 5825.0 //Square feet wing_span = 211.4 //Feet [Jig Position (213.0 at full weight)] wing_root_chord = 47.298 //Feet wing_dihedral = 7.0 //Degrees wing_incidence = 0.0 //Degrees [Inop in FS9] wing_twist = 0.0 //Degrees [Inop in FS9] oswald_efficiency_factor = 0.504 //[...] wing_winglets_flag = 1 //Winglet flag [0:false/1:true] wing_sweep = 37.5 //Degrees at 25% MAC wing_pos_apex_lon = -60.606 //Feet from RefPos wing_pos_apex_vert = 0.0 //Feet from RefPos htail_area = 1470.0 //Square feet htail_span = 75.75 //Feet htail_pos_lon = -210.0 //Feet, from RefPos htail_pos_vert = 7.32 //Feet, from RefPos htail_incidence = 0.0 //Degrees [Inop in FS9] htail_sweep = 37.5 //Degrees, horizontal tail leading edge vtail_area = 1060.0 //Square feet vtail_span = 37.1 //Feet, tip to body vtail_sweep = 45.0 //Degrees, vertical tail leading edge vtail_pos_lon = -198.5 //Feet from RefPos vtail_pos_vert = 26.1 //Feet from RefPos elevator_area = 342.0 //Square feet aileron_area = 225.0 //Square feet rudder_area = 230.0 //Square feet elevator_up_limit = 28.0 //Degrees elevator_down_limit = 20.0 //Degrees aileron_up_limit = 29.5 //Degrees aileron_down_limit = 27.5 //Degrees rudder_limit = 31.5 //Degrees elevator_trim_limit = 20.0 //Degrees spoiler_limit = 70.0 //Degrees spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 3.2 //Aileron to spoileron gain min_ailerons_for_spoilerons = 4.0 //Degrees min_flaps_for_spoilerons = 0.0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed = 174.55 //Stall clean KTAS @450,000 lbs full_flaps_stall_speed = 122.0 //Stall flaps KTAS cruise_speed = 485.0 //Cruise KTAS max_mach = 0.920 //Barber pole MACH max_indicated_speed = 372.0 // KIAS / modified provision for CAS->KIAS [flaps.0] type = 1 // Trailing edge span-outboard = 0.7 // 0.0 .. 1.0 extending-time = 60 // seconds flaps-position.0 = 0 // pseudo-degrees flaps-position.1 = 0.00,280 // 1 - no TE flaps-position.2 = 25.0,260 // 5 flaps-position.3 = 27.5,240 // 10 flaps-position.4 = 30.0,230 // 20 flaps-position.5 = 31.5,205 // 25 flaps-position.6 = 33.0,180 // 30 lift_scalar = 1.0 drag_scalar = 0.1 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.1] type = 2 // Inboard/midboard leading edge span-outboard = 0.53333 // 0.0 .. 1.0 extending-time = 12 // seconds flaps-position.0 = 0 // pseudo-degrees flaps-position.1 = 1.0 // 1 damaging-speed = 275 // KIAS blowout-speed = 280 // KIAS lift_scalar = 0.88 drag_scalar = 1.54 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.2] type = 2 // Outboard leading edge span-outboard = 0.2666 // 0.0 .. 1.0 extending-time = 10 // seconds flaps-position.0 = 0 // pseudo-degrees flaps-position.1 = 0.0 // 1 - no effect flaps-position.2 = 5.0 // 5 damaging-speed = 255 // KIAS blowout-speed = 260 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.3] type = 2 // Correct 5-30 / TE LIFT span-outboard = 0.7 // 0.0 .. 1.0 extending-time = 50 // seconds flaps-position.0 = 0 // pseudo-degrees flaps-position.1 = 0.00 flaps-position.2 = 25.0 flaps-position.3 = 21.0 flaps-position.4 = 16.1 flaps-position.5 = 8.7 flaps-position.6 = 4.7 lift_scalar = -1.22 drag_scalar = 0.00 pitch_scalar = -0.12 system_type = 1 //Hydraulic [flaps.4] type = 2 // Correct 10 / TE DRAG span-outboard = 0.7 // 0.0 .. 1.0 extending-time = 60 // seconds flaps-position.0 = 0 // pseudo-degrees flaps-position.1 = 0.0 flaps-position.2 = 0.0 flaps-position.3 = 1.0 flaps-position.4 = 0.1 flaps-position.5 = 3.0 lift_scalar = 0.00 drag_scalar = -1.00 pitch_scalar = 0.00 system_type = 1 //Hydraulic [flaps.5] type = 2 // Correct 30 / TE DRAG span-outboard = 0.7 // 0.0 .. 1.0 extending-time = 60 // seconds flaps-position.0 = 0 // pseudo-degrees flaps-position.1 = 0.0 flaps-position.2 = 0.0 flaps-position.3 = 0.0 flaps-position.4 = 0.0 flaps-position.5 = 0.0 flaps-position.6 = 6.5 lift_scalar = 0.00 drag_scalar = 1.00 pitch_scalar = 0.00 system_type = 1 //Hydraulic [flaps.6] type = 1 // Model span-outboard = 0.7 extending-time = 60 flaps-position.0 = 0.0 flaps-position.1 = 1.0 flaps-position.2 = 5.0 flaps-position.3 = 10.0 flaps-position.4 = 20.0 flaps-position.5 = 25.0 flaps-position.6 = 30.0 lift_scalar = 0.0 drag_scalar = 0.0 pitch_scalar= 0.0 system_type = 1 [autopilot] autopilot_available = 0 autothrottle_available = 0 default_pitch_mode=0 default_bank_mode=0 //Do Not Alter the following line or your 747-400 may cease operating. [AFDSAuth] ---BEGIN SHA1--- A4160C6C90B3E606CD280AC89815C9BCE9F05729 ---END SHA1--- // Do Not Alter the above lines. [contact_points] // point.0 = 1, -24.194, 0.000, -17.546, 1500.0, 0, 1.932, 56.0, 1.45, 0.128, 0.780, 9.0, 12.0, 0, 270, 320 point.1 = 1, -102.496, -16.009, -18.941, 1500.0, 1, 1.932, 0.0, 1.54, 1.171, 0.880, 16.0, 21.0, 2, 270, 320 point.2 = 1, -102.496, 16.009, -18.941, 1500.0, 2, 1.932, 0.0, 1.54, 1.171, 0.880, 15.0, 20.0, 3, 270, 320 point.3 = 1, -115.277, -4.253, -18.598, 1700.0, 1, 1.932, 0.0, 1.50, 1.203, 0.820, 15.0, 18.0, 2, 270, 320 point.4 = 1, -115.277, 4.253, -18.598, 1700.0, 1, 1.932, 0.0, 1.50, 1.203, 0.820, 15.0, 18.0, 2, 270, 320 // point.5 = 2, -153.600, -103.500, 3.000, 1250.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0 point.6 = 2, -153.600, 103.500, 3.000, 1250.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0 point.7 = 2, -2.945, 0.000, -3.312, 1500.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0 point.8 = 2, -156.766, 0.000, -9.961, 1500.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 static_pitch = -0.29 static_cg_height = 12.09 gear_system_type=0 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 5.0 //Flap angle that activates warning at idle flap_limit_power = 31.5 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.78 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,1,1 //pumps on Eng1,2,3,4 [Views] eyepoint = -19.100, -1.312, 11.122 ; Longitude, Latitude and Vertical position from Reference Point, (FEET) //eyepoint= -18.848, -1.312, 11.122 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4- 7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 avionics_bus = 0, 5 , 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 17.0 light_nav = 0, 5 , 17.0 light_beacon = 0, 5 , 17.0 light_landing = 0, 5 , 17.0 light_taxi = 0, 5 , 17.0 light_strobe = 0, 5 , 17.0 light_panel = 0, 5 , 17.0 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 1, 1 Nav.2 = 1, 1, 0 Adf.1 = 1 Adf.2 = 1 Transponder.1 = 1 Marker.1 = 1 [LIGHTS] light.0 = 3, -225.500, -0.50, 4.745, fx_navwhih, //Position Aft light.1 = 2, -225.500, 0.50, 4.745, fx_strobeh, //Strobe Aft light.2 = 1, -33.596, 0.00, 14.868, fx_pmdg744_beacon, //Beacon Top light.3 = 1, -86.149, 0.00, -11.735, fx_pmdg744_beacon, //Beacon Bottom light.4 = 9, -210.149, 8.00, 35.117, fx_pmdg744_logo, //Logo Right light.5 = 9, -210.149, -8.00, 35.117, fx_pmdg744_logo, //Logo Left light.6 = 8, -77.000, 26.00, -4.000, fx_pmdgwinglight, //Wing Right light.7 = 8, -77.000, -26.00, -4.000, fx_pmdgwinglight, //Wing Left [SMOKESYSTEM] smoke.0 = 0.00, -20.5, 0.00, fx_pmdg744_cockpit, [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=3,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 attitude_indicator.1 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [stall_warning] type=2 PS. I would like the weights in LBS if possible.
13-02-2007, 08:50 PM
I can see this being a longggggggg post in 2 ways.
Long in replies with people requesting Long in post, with all of these cfg's getting posted Post Edited ( 02-13-07 20:50 )
13-02-2007, 10:51 PM
United 747 Status: COMPLETE Keep an eye out, direct link will be posted shortly
VC-10 Status: COMPLETE Keep an eye out, direct link will be posted shortly Post Edited ( 02-13-07 23:24 )
13-02-2007, 11:54 PM
Shop shut until tomorrow (GMT) I cant stay up all night
I expect to see a whole list of requests by tommorow James
14-02-2007, 05:14 PM
Quote:Jambone wrote: Thanks James, eyes peeled for link. If you weren't so young, I'd buy you a beer! "Boys will be boys, and so will a lot of middle-aged men." - Kin Hubbard
14-02-2007, 05:27 PM
Hi
i want to douwnload the F1 C 441 Conquest ,i don't find it. Can You make me an Payload Modell? I found one but the Fspassenger say that this is an Default .So i can't fly this one.Can You help me ? Thanks a'lot Dirk [fltsim.0] title=Flight One Conquest 441 sim=F1_C441 model= panel= sound= texture= panel_alias = sound_alias = kb_checklists=C441_check kb_reference=C441_ref atc_id=N441HC atc_id_color=0xffffffff atc_parking_types=RAMP atc_parking_code=1 ui_manufacturer=Flight One Software ui_type=441 Conquest ui_variation=Burgundy and White description=Flight Model for Cessna 441 Conquest © Flight1 Software, Roger L. Dial. Flight Dynamics © Jerry Beckwith visual_damage=0 [General] atc_type=Cessna atc_model=C441 editable=1 performance=Power: Garrett AirResearch TPE 331 flat rated @ 635.5 Hp. Max speed: 297 kts @ 28000 ft. Max speed @ SL: 243 kts (Vmo limited). Initial climb rate: 2435 ft/min @ 115 kts. For detailed performance and specifications see documentation provided. Flight Dynamics By: Jerry Beckwith Mudpond Virtual Aircraft [pitot_static] vertical_speed_time_constant = 2 [weight_and_balance] max_gross_weight = 9925 empty_weight = 5716 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 11990 empty_weight_roll_MOI = 7882 empty_weight_yaw_MOI = 18144 empty_weight_coupled_MOI = 0 max_number_of_stations = 13 station_load.0 =0, 8.73, 0, 0 // Nose Cargo station_load.1 =170, 3.23, -1.4, 0 // Pilot station_load.2 =170, 3.23, 1.4, 0 // Co-Pilot station_load.3 =0, -0.18, -1.43, 0 // Passenger 3 station_load.4 =0, -0.085, 1.43, 0 // Passenger 4 station_load.5 =170, -2.77, -1.44, 0 // Passenger 5 station_load.6 =170, -2.77, 1.44, 0 // Passenger 6 station_load.7 =0, -6.1, -1.44, 0 // Passenger 7 station_load.8 =0, -6.1, 1.44, 0 // Passenger 8 station_load.9 =0, -10.4, -1.44, 0 // Passenger 9 station_load.10 =0, -10.4, 1.44, 0 // Passenger 10 station_load.11 =0, -11.76, 0, 0 // Bay B station_load.12 = 0, 0, 0, 0 // [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 0.17, -24.82, 0.31, fx_navredh light.1 = 3, 0.17, 24.82, 0.31, fx_navgreh light.2 = 3, -20.9, 0, 1.325, fx_navwhih light.3 = 2, -0.12, -24.82, 0.31, fx_strobeh light.4 = 2, -0.12, 24.82, 0.31, fx_strobeh light.5 = 1, -20.6, 0, 10.1, fx_beaconh light.6 = 2, -1.04, 0, -2.25, fx_strobeh light.7 = 4, 3.44, 0, 2.3, fx_441_vc light.8 = 4, -2.04, 0, 2.3, fx_441_cabin light.9 = 4, -7.04, 0, 2.3, fx_441_cabin light.10 = 4, -11.04, 0, 2.3, fx_441_cabin light.11 = 8, 2.50, -17.45, 2.0, fx_441ice light.12 = 8, 2.50, 17.45, 2.0, fx_441ice light.13 = 8, 2.35, -9.25, -0.15, fx_landing light.14 = 8, 2.35, 9.25, -0.15, fx_landing light.15 = 3, -0.39, 24.82, 0.31, fx_navwhi light.16 = 3, -0.39, -24.82, 0.31, fx_navwhi [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 5 fuel_flow_scalar = 0.95 engine.0 = 8, -8.2, 0 engine.1 = 8, 8.2, 0 min_throttle_limit=-0.250000 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s windshield_rain_effect_available=1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 2 LeftMain = 0, -4, -1.3, 240.75, 0 RightMain = 0, 4, -1.3, 240.75, 0 electric_pump=1 [contact_points] static_pitch = 0 static_cg_height = 5.1 max_number_of_points = 7 point.0 = 1, 11.8354, 0, -5.3, 9000, 0, 0.8, 36.6, 0.25, 2.5, 0.99, 7.5, 6.5, 0, 182.16, 201.52 point.1 = 1, -1.3, -7.2, -5.35, 2500, 1, 0.9, 0, 0.35, 2.5, 0.99, 7.5, 7.5, 2, 182.16, 201.52 point.2 = 1, -1.3, 7.2, -5.35, 2500, 2, 0.9, 0, 0.35, 2.5, 0.99, 7.5, 7.7, 3, 182.16, 201.52 point.3 = 2, 0.06, -24.5, 0.4, 785, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.4 = 2, 0.06, 24.5, 0.4, 785, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.5 = 2, -21, 0, 1.3, 785, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.6 = 2, 15.8, 0, -0.5, 785, 0, 0, 0, 0, 0, 0, 0, 0, 4 gear_system_type=1 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [forcefeedback] gear_bump_nose_magnitude = 6000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 6000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 6000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 10000 crash_direction1 = 1000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 stick_shaker_magnitude = 5000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] wing_area = 253.6 wing_span = 49.33 wing_root_chord = 5.14088789783093 wing_dihedral = 4 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.877424313387267 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 1.28522197445773 wing_pos_apex_vert = 0 htail_area = 63.38 htail_span = 19.07 htail_pos_lon = -19 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 43.6 vtail_span = 7.6 vtail_sweep = 0 vtail_pos_lon = -20 vtail_pos_vert = 0 elevator_area = 21.57 aileron_area = 14.74 rudder_area = 16.15 elevator_up_limit = 25 elevator_down_limit = 15 aileron_up_limit = 25 aileron_down_limit = 15 rudder_limit = 20 elevator_trim_limit = 20 spoiler_limit = 90 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [flight_tuning] cruise_lift_scalar=1 parasite_drag_scalar=1 induced_drag_scalar=1 elevator_effectiveness=1 aileron_effectiveness=1 rudder_effectiveness=1 pitch_stability=1 roll_stability=1 yaw_stability=1 elevator_trim_effectiveness=1 aileron_trim_effectiveness=1 rudder_trim_effectiveness=1 hi_alpha_on_roll = 1 hi_alpha_on_yaw = 1 p_factor_on_yaw = 1 torque_on_roll = 1 gyro_precession_on_roll = 1 gyro_precession_on_yaw = 1 [TurbineEngineData] fuel_flow_gain=0.08 //Gain on fuel flow inlet_area=0.1 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=100 //Lbs, max rated static thrust at Sea Level afterburner_available=0 reverser_available=0 [turboprop_engine] power_scalar=1 //Scalar on Turboprop power maximum_torque=1711 //Maximum torque available (ft-lbs) [propeller] thrust_scalar=1 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=7.5 //Propeller Diameter, (feet) propeller_blades=4 //Number of propeller blades propeller_moi=14.7 //Propeller moment of inertia beta_max=65 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=10 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=22440 //Miminum governed RPM prop_tc=0.01 //Prop time-constant gear_reduction_ratio=14.96 //Propeller gear reduction ratio fixed_pitch_beta=30 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=700 //Minimum RPM for prop feathering beta_feather=87.4 //Feathering pitch angle (degrees) power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=1 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=2 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=-14 //Minimum pitch angle in reverse, (degrees) rotation = 1, 1 [Views] eyepoint=3.0, -1.3, 2.1 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 12 flaps-position.0 = 0 flaps-position.1 = 10, 200 flaps-position.2 = 20, 200 flaps-position.3 = 30, 180 damaging-speed = 220 blowout-speed = 240 system_type = 1 lift_scalar = 1 drag_scalar = 1 pitch_scalar = 1 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=2,0 [exits] number_of_exits = 3 exit_rate.0 = 0.4 exit_rate.1 = 0.4 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1500 autothrottle_available=0 autothrottle_arming_required = 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga=8 max_pitch_velocity_hi_alt = 1.5 max_pitch_velocity_lo_alt_breakpoint = 20000 max_pitch_velocity_hi_alt_breakpoint = 28000 max_pitch = 10 max_pitch_acceleration = 1 max_pitch_velocity_lo_alt = 2 max_bank= 25 max_bank_acceleration = 1.8 max_bank_velocity = 3 max_throttle_rate = 0.1 nav_proportional_control = 9 nav_integrator_control = 0.25 nav_derivative_control = 0 nav_integrator_boundary = 2.5 nav_derivative_boundary = 0 gs_proportional_control = 9.52 gs_integrator_control = 0.26 gs_derivative_control = 0 gs_integrator_boundary = 0.7 gs_derivative_boundary = 0 yaw_damper_gain = 1 [Reference Speeds] flaps_up_stall_speed=67.8 //Knots True (KTAS) full_flaps_stall_speed=57.4 //Knots True (KTAS) cruise_speed=235 //Knots True (KTAS) max_indicated_speed = 245 //Knots True (KTAS) max_mach = 0.55 //Knots True (KTAS) [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 22.5 //Flap angle that activates warning at idle flap_limit_power = 11.25 //Flap angle that activates warning at above idle [brakes] //toe_brakes_scale = 0.999969481490524 //Brake scalar toe_brakes_scale = 0.75 //Brake scalar parking_brake = 1 //Parking brake available [stall_warning] type = 1 [hydraulic_system] electric_pumps = 0 //no electric pumps engine_map = 1, 1, 0, 0 //pumps on Eng1,2 normal_pressure = 1250 //PSI [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0=2 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,0 [SMOKESYSTEM] smoke.0=0.0, 0.0, 8.139, fx_441_Exhaust smoke.1=0.0, 0.0, -8.139, fx_441_Exhaust
Dirk
14-02-2007, 05:50 PM
Hi James ,i have too the Eagle-Sotware Cessna Citation CJ I and i ask You for creating an Payloadmodel.Can You make it for me
Thousend Thanks for Creating. Dirk //Release Flight Model June 10th 2004 - RY [fltsim.0] title=Eaglesoft Citation II sim=CitationII model= panel= sound= texture= kb_checklists=Citation II_check kb_reference=Citation II_ref atc_id=N700ES ui_manufacturer=Cessna ui_type="Cessna Citation II" ui_variation="Corporate Full" description="Eaglesoft Cessna Citation II" [fltsim.1] title=Eaglesoft Citation II Lite sim=CitationII model=lite panel=lite sound= texture=lite kb_checklists=Citation II_check kb_reference=Citation II_ref atc_id=N500ES ui_manufacturer=Cessna ui_type="Cessna Citation II" ui_variation="Corporate Lite" description="No VC Citation II" [fltsim.2] title=Eaglesoft Citation II Amb sim=CitationII model=amb panel= sound= texture=amb kb_checklists=Citation II_check kb_reference=Citation II_ref atc_id=N147DR ui_manufacturer=Cessna ui_type="Cessna Citation II" ui_variation="Air Ambulance" description="Lifeflight" [General] atc_type=Cessna atc_model=C551 editable=1 performance=Pratt & Whitney JT15D-4 @ 2,500 lbs thrust [WEIGHT_AND_BALANCE] max_gross_weight=12500 empty_weight=7100 //equipped - no fuel or PAX reference_datum_position=0, 0, -0.8 empty_weight_CG_position=-1.0, 0, 0 //-0.29 max_number_of_stations=12 station_load.0="170, 7.5, 0.0, 0.0, Pilot" // placed in the middle to overcome FS's pilot assymetry instability station_load.1="0.00, 7.5, 1.2, 0.0, Co-Pilot" //This aircraft is cleared for single pilot operation station_load.2="0, 0.5, -1.2, 0.0, Passenger Row 1" station_load.3="0, 0.5, 1.2, 0.0, Passenger Row 1" station_load.4="170, -3.5, -1.2, 0.0, Passenger Row 2" station_load.5="0, -3.5, 1.2, 0.0, Passenger Row 2" station_load.6="0.00, -6.0, -1.2, 0.0, Passenger Row 3" station_load.7="0.00, -6.0, 1.2, 0.0, Passenger Row 3" station_load.8="25, 4.0, 0.0, 0.0, Forward Baggage" station_load.9= "25,-15.6, 0.0, 0.0, Rear Baggage" ;Moments of Inertia empty_weight_pitch_MOI=42000 empty_weight_roll_MOI=38000 empty_weight_yaw_MOI=21000 empty_weight_coupled_MOI=0.0 [electrical] max_battery_voltage=25.2 generator_alternator_voltage=28.5 max_generator_alternator_amps=400.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4- 7=Generator/AlternatorBus(1-4) avionics_bus=0, 100, 20 avionics=1, 50 , 20 additional_system=0, 50, 20 marker_beacon=1, 10 , 20 fuel_pump=0, 15 , 20 fuel_transfer_pump=0, 15, 20 flap_motor=0, 40, 20 gear_motor=0, 60, 20 autopilot=1, 10, 20 pitot_heat=0, 30, 20 gear_warning=0, 4, 20 starter1=0, 100, 20 starter2=0, 100, 20 light_nav=0, 10, 20 light_beacon=0, 10, 20 light_strobe=0, 10, 20 light_landing=0, 10, 20 light_taxi=0, 30, 20 light_panel=0, 10, 20 hydraulic_pump=0, 20, 20 light_recognition=0, 10, 20 light_logo=0, 10, 20 light_wing=o, 10, 20 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.13 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=0.66 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [GeneralEngineData] engine_type=1 Engine.0=-13.0, -4.0, 1.6 Engine.1=-13.0, 4.0, 1.6 fuel_flow_scalar=1.6 min_throttle_limit=-0.24 [TurbineEngineData] fuel_flow_gain=0.0040 // was 0.0020 inlet_area=1.7 //2.1 rated_N2_rpm=29920 static_thrust=2200 // nominal value is 2500 per engine. This param is superceded elsewhere afterburner_available=0 reverser_available=1 //bypass ratio = 3.3 [jet_engine] thrust_scalar=1.0 ;point.0=1, 16.00, 0.00, -2.80, 1181.1, 0, 0.7549, 30.0, 0.4197, 2.5, 0.4, 10.0, 10.0, 0, 0.0, 0.0 ;point.1=1, -3.45, -4.85, -2.80, 1574.8, 1, 0.8549, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 2, 0.0, 0.0 ;point.2=1, -3.45, 4.85, -2.80, 1574.8, 2, 0.8549, 0.0, 0.4798, 2.5, 0.5456, 9.0, 9.0, 3, 0.0, 0.0 [contact_points] point.0=1, 16.00, 0.00, -2.45, 1181.1, 0, 0.7549, 34.0, 0.2350, 2.2, 0.4500, 10.0, 10.0, 0, 0.0, 0.0 point.1=1, -3.20, -4.85, -2.37, 1574.8, 1, 0.8549, 0.0, 0.2700, 2.2, 0.4800, 9.0, 9.0, 2, 0.0, 0.0 point.2=1, -3.20, 4.85, -2.37, 1574.8, 2, 0.8549, 0.0, 0.2700, 2.2, 0.4800, 9.0, 9.0, 3, 0.0, 0.0 point.3=2, -8.55, -22.00, -0.60, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -8.55, 22.00, -0.60, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -22.00, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 0.00, 0.00, - 1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch=0.55 static_cg_height=3.1 gear_system_type=0 [Views] eyepoint=10.80, -1.33, 3.56 [flaps.0] type=1 span-outboard=0.8 extending-time=5 flaps-position.0=0 flaps-position.1=15 flaps-position.2=35 flaps-position.3=40 damaging-speed=250 blowout-speed=300 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 1 Adf.1=1 Transponder.1=1 Marker.1=1 [keyboard_response] elevator=150, 250 aileron=150, 250 rudder=150, 250 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=3,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [brakes] toe_brakes_scale=0.5 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=8.594367 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [fuel] LeftMain= -3.5, -7.0, 0.0, 371.0, 0.0 RightMain= -3.5, 7.0, 0.0, 371.0, 0.0 fuel_type=2 number_of_tank_selectors=1 electric_pump=1 //total fuel load 5,008 lbs [airplane_geometry] wing_area=312.0 wing_span=51.66 wing_root_chord=6.8 wing_dihedral=2.5 wing_incidence=0.5 wing_twist=-1.5 oswald_efficiency_factor=0.6 wing_winglets_flag=1 wing_sweep=35.0 wing_pos_apex_lon=8.7 wing_pos_apex_vert=0.0 htail_area=67.0 htail_span=17.2 htail_pos_lon=-24.6 htail_pos_vert=0.0 htail_incidence=1.3 htail_sweep=25.0 vtail_area=42.0 vtail_span=7.4 vtail_sweep=30.0 vtail_pos_lon=-20.5 vtail_pos_vert=4.1 elevator_area=17.0 aileron_area=13.5 rudder_area=7.3 elevator_up_limit=17.0 elevator_down_limit=15.5 aileron_up_limit=18.0 aileron_down_limit=18.0 rudder_limit=30.0 elevator_trim_limit=15.0 spoiler_limit=60.0 spoilerons_available=0 aileron_to_spoileron_gain=4.600000 min_ailerons_for_spoilerons=4.984733 min_flaps_for_spoilerons=0.000000 [Reference Speeds] flaps_up_stall_speed=76 full_flaps_stall_speed=90 cruise_speed=330.0 max_indicated_speed=277.000000 max_mach=0.705 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_max_rpm=95 autothrottle_takeoff_ga=0 pitch_takeoff_ga=8 default_bank_mode=0 default_pitch_mode=0 use_no_default_bank=1 use_no_default_pitch=1 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.01 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=1.000000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo light.0=3, -1.7, -25.8, 2.1, fx_navred light.1=3, -1.7, 25.8, 2.1, fx_navgre light.2=7, -24.0, 0.00, 3.11, fx_navwhi.fx light.3=7, -24.0, 0.00, 12.5, fx_beacon light.4=10, 11.50, 0.30, 2.00, esbj400_panelflood.fx light.5=10, 11.50, -0.30, 2.00, esbj400_panelflood.fx light.6=2, -1.85, -25.8, 2.1, fx_strobe light.7=2, -1.85, 25.8, 2.1, fx_strobe light.10=8, 2.45, -2.7, 1.6, fx_navwhi.fx light.11=8, 2.45, 2.7, 1.6, fx_navwhi.fx light.12=8, 12.0, -17.8, 8.60, esbj400_icelight //rightwing icelight light.13=8, 12.0, 17.8, 8.60, esbj400_icelight //leftwing icelight [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds //Copyright© Eaglesoft Development Group 6/2002 ALL RIGHTS RESERVED [General] performance=JT15D-5 2 2965 (3045) lb, 2414 lb @FL400, M 0.8\nSFC\tstatic 0.56, cruise 0.541?\nFlow\t75 lb\/sec\ndia \t2.28 ft, 4.07 ft^2 \nMax cruise 468 kt tas\nMax range 1770 nm\nCeiling\t45,000 ft\nMTOW\t16,000 lb\nClimb\t 4020 fpm\nFuel \t 744 gal 4912 lb\nalpha_o=-2.55\n
Dirk
14-02-2007, 08:05 PM
Dirk, there is a C441 payload model already. I use it frequently. You only have to rename the .ini file to match with the aircraft name or vice
versa. It works just fine.
See FsPassengers Frequently Asked Questions: FAQ
14-02-2007, 08:15 PM
Where are the pics people! I'll try my best without pics, but please try to include them
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