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mozart

Merging Wilco A380 with Overland model

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I try to merge the Overland visual model with the panel of the Wilco A380.I have used the search funciton but not found what I needed.I have also tried to use a method which has worked for all my other planes: keep the Wilco folder, only replace the Wilco model folder by the Overland model folder and the Wilco texture folder(s) with the Overland texture folder(s). Keep the Wilco aircraft.cfg, only change contact points, lights, effects, tailhook, folding wings. I have had no problem whatsoever with that method on merging any imaginable combination (the theory is that the panel and .air file don't care what the model looks like. What the panel needs is a proper aircraft.cfg, all the more so when a functionable FMS/MCDU is involved).Any hints?ThanksChris

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Hi,I just copied the panel folder from the wilco model into the SMS 380 folder,and added the SMS VC entries into the Panel.cfg file like this, below the [Windows07]Just make sure that you have installed all the gauges for the SMS A380._________________________________________________//--------------------------------------------------------[Vcockpit01]Background_color=0,0,0 size_mm=512visible=1pixel_size=512texture=$ng380gauge00=Z_PAPA380!ABS Aps Window, 1,2,460,38gauge01=PAPA340!Nav Display Switch, 79,46,96,69gauge02=PAPA340!Baro Reference, 1,46,70,99gauge03=PAPA340!Master Warning Light, 180,48,40,39gauge04=PAPA340!Autobrakes Switch, 159,166,154,180gauge05=PAPA340!Flight Director Switch, 228,48,34,32gauge06=PAPA340!Autopilot ILS Switch, 270,48,34,32gauge07=PAPA340!Autopilot IAS-Mach Switch, 309,49,34,28gauge08=PAPA340!Autopilot Localizer Switch, 347,49,34,30gauge09=PAPA340!Autopilot Master Switch, 385,49,33,31gauge10=PAPA340!Autopilot Nav Switch, 424,49,34,32gauge11=PAPA340!Autopilot Speed Switch, 309,83,34,29gauge12=PAPA340!Autopilot Altitude Hold Switch, 347,84,35,29gauge13=PAPA340!Autopilot Approach Switch, 386,84,35,31gauge14=PAPA340!Autothrottle Switch, 425, 86 ,33,29gauge15=Boeing777-300!Backup_Attitude, 0,167,135,135gauge16=Z_PAPA380!A380_RMI, -2,301,157,203gauge17=simicons!Kneeboard Icon, 128,119,39,45gauge18=simicons!ATC Icon, 170,120,41,43gauge19=simicons!Map Icon, 216,120,39,43gauge20=Z_PAPA380!Avionics Icon, 258,119,39,43gauge21=Z_PAPA380!GPS Icon, 345,119,41,44gauge22=Z_PAPA380!Clock, 160,351,130,129gauge23=Z_PAPA380!A380 Brake_Press, 297,351,120,121gauge24=PAPA340!Engine Start Knob 1, 317,237,54,54gauge25=PAPA340!Engine Start Knob 2, 374,237,54,54gauge26=PAPA340!Engine Start Knob 3, 317,293,54,54gauge27=PAPA340!Engine Start Knob 4, 374,293,54,54gauge28=Z_PAPA380!Pitot Heat Switch, 371,167,46,43gauge29=Z_PAPA380!A380_Panel_Control2, 296,474,106,37gauge30=PAPA340!VC_Anti Ice Eng1 Switch, 161,482,31,27gauge31=PAPA340!VC_Anti Ice Eng2 Switch, 194,482,31,27gauge32=PAPA340!VC_Anti Ice Eng3 Switch, 227,482,31,27gauge33=PAPA340!VC_Anti Ice Eng4 Switch, 260,482,31,27//--------------------------------------------------------[Vcockpit02]Background_color=0,0,0 size_mm=512visible=1pixel_size=1024texture=$dg380gauge00=Z_PAPA380!Primary Flight Display, 5,5,245,250gauge01=PAPA340!ABS EICAS Display, 2,252,251,256gauge02=PAPA340!Multi-Function Display, 272,3,229,283gauge03=PAPA340!Door Display, 264,270,240,238//--------------------------------------------------------[Vcockpit03]size_mm=512visible=0pixel_size=512texture=$gpsgauge00=fs9gps!gps_500, 0,0,512,408[Default View]X=0Y=0SIZE_X=8192SIZE_Y=3350Day=255,255,255Night=120,120,120Luminous=180,180,180______________________________________________And here is the Aircraft.cfg that I made for the merge.Ofcourse you have to replace the livery entries with your own.[fltsim.0]title=FSPAP Airbus A380-800 Singapore Airlines (VC)sim=a380-800model=vcpanel=sound=texture=siaatc_id=9V-SKAatc_airline=Singaporeatc_flight_number=380atc_heavy=1ui_manufacturer=Simmer's Skyui_type=Airbus A380-800ui_variation=Singapore Airlines (VC)description=Overland Co.,Ltd. Products --- Airbus A380-800\n\nPaint by Tom Collins\n\nL1 Lower Cabin Door [shift+E] then [1]\nCargo Door Operate with Door Display Gauge\nL2 Lower Cabin Door Operate with Door Display Gauge [General]visual_damage=0 // 0=off, 1=onatc_type=Airbusatc_model=A380editable=0performance=Cruise Speed\tMach .85\nMaximum Range\t8,000 nm\nService Ceiling\t43,000 ft\nMax Takeoff Weight\t1,234,600 lb\nSeating\t\t523 to 555\nCargo Capacity\t38 standard LD3s containers \n\nPowerplants\tRolls-Royce Trent 900 turbofans\n[pitot_static]vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI[WEIGHT_AND_BALANCE]max_gross_weight = 1238998 // (pounds)empty_weight = 609974 // (pounds)reference_datum_position = 10, 0, -3.5 // 83.5(feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)empty_weight_CG_position = 0, 0, 0 // 90.5(feet) longitudinal, lateral, vertical distance from specified datummax_number_of_stations = 50//Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.0 = "170.0, 109.0, -2.0, 8.0, Pilot" station_load.1 = "170.0, 109.0, 2.0, 8.0, Co-Pilot" station_load.2 = "1700.0, 17.5, 0.0, 0.0, Crew" station_load.3 = "3520.0, 63.0, 0.0, 0.0, 1F First Class" station_load.4 = "22720.0, 19.0, 0.0, 0.0, 1F Tourist Class 1-15" station_load.5 = "17280.0, -29.0, 0.0, 0.0, 1F Tourist Class 16-26" station_load.6 = "13440.0, -80.0, 0.0, 0.0, 1F Tourist Class 27-35" station_load.7 = "4950.0, 63.0, 0.0, 0.0, 2F Business Class 1-5" station_load.8 = "10890.0, 43.0, 0.0, 0.0, 2F Business Class 6-16" station_load.9 = "8020.0, -49.0, 0.0, 0.0, 2F Tourist Class 8-18" station_load.10 = "16640.0, -70.0, 0.0, 0.0, 2F Tourist Class 19-34" station_load.11 = "1000.0, 28.0, 0.0, -6.0, Forward Baggage" station_load.12 = "1100.0, -33.0, 0.0, -6.0, Aft Baggage" ;Moments of Inertiaempty_weight_pitch_MOI = 24223159empty_weight_roll_MOI = 15352310empty_weight_yaw_MOI = 19531785empty_weight_coupled_MOI = 0[fuel]//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)Center1 = -13.5, 0.0, -2.0, 22545.0, 3.0Center2 = 13.5, 0.0, -2.0, 21300.0, 0.0LeftMain = 0.0, -15.0, 2.0, 11720.0, 3.0LeftAux = -0.5, -22.0, 4.0, 4850.0, 0.0RightMain = 0.0, 15.0, 2.0, 11720.0, 3.0RightAux = -0.5, 22.0, 4.0, 4850.0, 0.0 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetAnumber_of_tank_selectors = 1 electric_pump=0[airplane_geometry]wing_area = 8074.98 //Square feetwing_span = 261.6 //Feetwing_root_chord = 57.96 //Feetwing_dihedral = 2.0 //7 Degreeswing_incidence = 1.6 //Degreeswing_twist = 0.8 //Degreesoswald_efficiency_factor= 0.81 //Measure of lift effeciency of wingwing_winglets_flag = 1 //Are winglets available?wing_sweep = 39.5 //Degrees, wing leading edgewing_pos_apex_lon = 50.64 //Feet, longitudinal distance from reference point, negative going aftwing_pos_apex_vert = 0.5 //Feet, vertical distance from reference point, positive going uphtail_area = 1910 //Square feethtail_span = 99.65 //Feethtail_pos_lon = -82.3 //Feet, longitudinal distance from reference point, negative going afthtail_pos_vert = 11.0 //Feet, vertical distance from reference point, positive going uphtail_incidence = -1.0 //Degreeshtail_sweep = 37.5 //Degrees, horizontal tail leading edgevtail_area = 1171.9 //Square feetvtail_span = 47.9 //Feet, tip to bodyvtail_sweep = 45.0 //Degrees, vertical tail leading edgevtail_pos_lon = -70.5 //Feet, longitudinal distance from reference point, negative going aftvtail_pos_vert = 20.6 //Feet, vertical distance from reference point, positive going upelevator_area = 636 //Square feetaileron_area = 425 //Square feetrudder_area = 390 //Square feetelevator_up_limit = 27 //Degreeselevator_down_limit = 22 //Degreesaileron_up_limit = 25 //Degreesaileron_down_limit = 18 //Degreesrudder_limit = 31.5 //Degreeselevator_trim_limit = 20 //Degreesspoiler_limit = 45 //Degreesspoilerons_available = 1 //Spoilerons Available?aileron_to_spoileron_gain = 3 //Aileron to spoileron gainmin_ailerons_for_spoilerons = 13.5 //Degreesmin_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate[Reference Speeds]flaps_up_stall_speed = 140.0 //Knots True (KTAS)full_flaps_stall_speed = 112.0 //Knots True (KTAS)cruise_speed = 505.0 //Knots True (KTAS)max_indicated_speed = 497.6max_mach=0.90[flaps.0]type=1 // 1 - tail, 2 - leadspan-outboard=0.2 // 0.0 .. 1.0extending-time=25 // secondsflaps-position.0=0 flaps-position.1=8flaps-position.2=17flaps-position.3=26flaps-position.4=32damaging-speed=260 // KIASblowout-speed=280 // KIASlift_scalar=0.45drag_scalar=0.55pitch_scalar=0.55system_type=1 //Hydraulic[flaps.1]type=1 // 1 - tail, 2 - leadspan-outboard=0.8 // 0.0 .. 1.0extending-time=23 // secondsflaps-position.0=0 flaps-position.1=8flaps-position.2=17flaps-position.3=26flaps-position.4=32damaging-speed=260 // KIASblowout-speed=280 // KIASlift_scalar=0.25drag_scalar=0.35pitch_scalar=0.35system_type=1 //Hydraulic[flaps.2]type=2 // 1 - tail, 2 - leadspan-outboard=0.8 // 0.0 .. 1.0extending-time=14 // secondsflaps-position.0=0 // degreesflaps-position.1=0.7 // degreesflaps-position.3=1.0 // degreesdamaging-speed=260 // KIASblowout-speed=300 // KIASlift_scalar=0.04drag_scalar=0.05pitch_scalar=0.05system_type=1 //Hydraulic[flaps.3] //Outboard Leading Edge Slattype=2 // 1 - tail, 2 - leadspan-outboard=0.8 // 0.0 .. 1.0extending-time=13 // secondsflaps-position.0=0 //flaps-position.1=20 //flaps-position.3=23 //damaging-speed=250 // KIASblowout-speed=300 // KIASlift_scalar=0.04drag_scalar=1.0pitch_scalar=1.0system_type=1 //Hydraulic[flight_tuning]cruise_lift_scalar = 1.100parasite_drag_scalar = 1.300induced_drag_scalar = 1.300elevator_effectiveness = 1.0aileron_effectiveness = 1.0rudder_effectiveness = 1.0pitch_stability = 1.0roll_stability = 1.0yaw_stability = 1.0elevator_trim_effectiveness = 1.0aileron_trim_effectiveness = 1.0rudder_trim_effectiveness = 1.0[GeneralEngineData]engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=TurbopropEngine.0 = -15.5, -82.6, -0.4 //(feet) longitudinal, lateral, vertical distance from reference datumEngine.1 = 12.0, -47.6, -3.9 //(feet) longitudinal, lateral, vertical distance from reference datumEngine.2 = 12.0, 47.6, -3.9 //(feet) longitudinal, lateral, vertical distance from reference datumEngine.3 = -15.5, 82.6, -0.4 //(feet) longitudinal, lateral, vertical distance from reference datumfuel_flow_scalar = 0.93 //Scalar for fuel flow efficiencymin_throttle_limit=-0.219934[TurbineEngineData]fuel_flow_gain = 0.002 //Gain on fuel flowinlet_area = 78.5 //Square Feet, engine nacelle inlet arearated_N2_rpm = 29920 //RPM, second stage compressor rated valuestatic_thrust = 70000 //Lbs, max rated static thrust at Sea Levelafterburner_available = 0 //Afterburner available?reverser_available = 1 //Thrust reverser available?[jet_engine]thrust_scalar = 0.9[autopilot]autopilot_available = 1flight_director_available = 1default_vertical_speed = 0.0autothrottle_available = 1autothrottle_arming_required = 1autothrottle_max_rpm = 90autothrottle_takeoff_ga = 1pitch_takeoff_ga = 8;max_pitch=10.000000max_pitch_acceleration=1.000000max_pitch_velocity_lo_alt=2.000000max_pitch_velocity_hi_alt=1.500000max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=1.800000max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[LIGHTS]//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -120.00, 0.18, 11.37, fx_navwhi , //-194.95light.1 = 3, -120.00, -0.18, 11.37, fx_navwhi , //-194.95light.2 = 2, -120.00, 0.00, 11.05, fx_strobe , //-194.95light.3 = 1, 46.05, -0.09, 21.75, fx_beaconh ,light.4 = 1, 2.30, 0.00, -7.98, fx_beaconb ,[contact_points] //0 Class <0=none,1=wheel, 2=scrape, 3=float> //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS)point.0 = 1, 94.5, 0.0, -13.2, 1000.0, 0, 1.8, 52.0, 0.4, 0.8, 0.510, 11.0, 11.2, 0, 220, 250point.1 = 1, -1.5, -20.4, -15.1, 2000.0, 1, 2.0, 0.0, 1.5, 1.5, 1.800, 11.0, 9.0, 2, 220, 250point.2 = 1, -1.5, 20.4, -15.1, 2000.0, 1, 2.0, 0.0, 1.5, 1.5, 1.800, 11.0, 9.0, 2, 220, 250point.3 = 1, -10.5, -8.6, -15.1, 2000.0, 1, 2.0, -3.0, 1.5, 1.5, 1.800, 11.0, 9.0, 2, 220, 250point.4 = 1, -10.5, 8.6, -15.1, 2000.0, 1, 2.0, -3.0, 1.5, 1.5, 1.800, 11.0, 9.0, 2, 220, 250point.5 = 2, -12.6, -103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0point.6 = 2, -12.6, 103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0point.7 = 2, 3.0, 0.0, 0.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0point.8 = 2, -112.7, 0.0, 4.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0static_pitch = 0.0static_cg_height = 17.4gear_system_type=1[Views]eyepoint = 100.74, -1.71, 10.24 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)[electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)autopilot = 0, 5 , 17.0avionics_bus = 0, 10, 17.0avionics = 1, 5 , 17.0gear_warning = 0, 2 , 17.0fuel_pump = 0, 5 , 17.0light_nav = 0, 5 , 17.0light_beacon = 0, 5 , 17.0light_landing = 0, 5 , 17.0light_taxi = 0, 5 , 17.0light_strobe = 0, 5 , 17.0light_panel = 0, 5 , 17.0[Radios]// Radio Type = availiable, standby frequency, has glide slopeAudio.1 = 1Com.1 = 1, 1Com.2 = 1, 1Nav.1 = 1, 1, 1Nav.2 = 1, 1, 0Adf.1 = 1Transponder.1 = 1Marker.1 = 1[direction_indicators]//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another//2 Indicator number of slaving indicator if Type = 4direction_indicator.0=3,0[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, 250aileron = 150, 250rudder = 150, 250[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[exits]number_of_exits = 2exit_rate.0 = 0.4 ;Percent per secondexit_rate.1 = 0.4 ;Percent per second[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[brakes]toe_brakes_scale=0.789926parking_brake=1[gear_warning_system]gear_warning_available=1pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=5.042029[hydraulic_system]electric_pumps=0engine_map=1,1,1,1normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=1[turn_indicators]turn_indicator.0=1,0[folding_wings]wing_fold_system_type=4 ;0=Nonefold_rates=0.1,1 ;Percent per second[TailHook]tailhook_length=4 ;(feet)tailhook_position=0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datumcable_force_adjust=0.0[exits]number_of_exits = 2exit_rate.0 = 100 ;Percent per secondexit_rate.1 = 100 ;Percent per second

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