Hello all,About 1 year ago somebody made a beautiful merge for the Overland A340 + PSS panel. http://forum.ivao.aero/index.php/topic,138787.0.htmlSomebody else changed some settings in the aircraft.cfg to let the panel work with Overland A330-300 + PSS panel. I spent a few hours figuring out how he did it, but it worked.Here are some shots:Well that looks nice, doesn't it?Then I looked at the Airbus A330-200 + PSS panel. I did exacly the same as I did with the A330-300There is only a small problem; the virtual cockpit is behind me (I think because the A332 is a bit shorter than the A333)Oke, still not a big problem, I just push Cntrl+Enter and I go back, But I can't go further than this;I think I need to change some values in the aircraft.cfg but I have no idea what numbers I need to change.The Aircraft.cfg is included in this topic. I anybody know what I need to change, please commend :( An other thing,It seems that the fuel is still set upped for the A340. Because I do not think the A330 can carry 120.000kg.Does somebody know how much it can carry?Thank you very much in advance,Robin Cornelissen
[General]visual_damage=0 // 0=off, 1=onatc_type=AIRBUSatc_model=A330editable=0performance=Cruise Speed\tMach .83\nMaximum Range\t5,500 nm\nService Ceiling\t33,000 ft\nMax Takeoff Weight\t467,380 lb\nSeating\t\t295 to 335\nCargo Capacity\t32 standard LD3 containers \n[WEIGHT_AND_BALANCE]reference_datum_position = 0.0, 0.0,-6.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)empty_weight_CG_position = 0.0, 0.0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datummax_number_of_stations=50station_load.0 = "170.0, 80.4, -2.0, 0.0, Pilot" //Weight (lbs),station_load.1 = "170.0, 80.4, 2.0, 0.0, Co-Pilot" //Weight (lbs),station_load.2 = "850.0, 3.0, 0.0, 0.0, Crew" //Weight (lbs),station_load.3 = "1200.0, 65.0, 0.0, 0.0, First Class" //Weight (lbs),station_load.4 = "2720.0, 34.0, 0.0, 0.0, Business" //Weight (lbs),station_load.5 = "6960.0, -7.0, 0.0, 0.0, Coach 1-8" //Weight (lbs),station_load.6 = "8800.0, -49.5, 0.0, 0.0, Coach 9-18" //Weight (lbs),station_load.6 = "2600.0, -75.5, 0.0, 0.0, Coach 19-23" //Weight (lbs),station_load.7 = "2000.0, 44.0, 0.0, -6.0, Forward Cargo" //Weight (lbs),station_load.8 = "500.0, -39.0, 0.0, -6.0, Aft Cargo" //Weight (lbs),;Moments of Inertiaempty_weight= 354700.000empty_weight_roll_MOI= 8955743.000empty_weight_pitch_MOI= 22600873.000empty_weight_yaw_MOI= 22751035.000empty_weight_coupled_MOI= 1000.000max_gross_weight= 515700.000CG_forward_limit= 0.000CG_aft_limit= 1.000[flight_tuning]cruise_lift_scalar =1.000parasite_drag_scalar =1.500induced_drag_scalar =1.300elevator_effectiveness =1.200aileron_effectiveness =1.500rudder_effectiveness =2.500pitch_stability =1.500roll_stability =1.000yaw_stability =1.000elevator_trim_effectiveness =1.000aileron_trim_effectiveness =1.000rudder_trim_effectiveness =1.000[GeneralEngineData]engine_type= 1Engine.0= 15.166, -30.386, -7.583Engine.1= 15.166, 30.386, -7.583fuel_flow_scalar= 0.4370min_throttle_limit=-0.409912[TurbineEngineData]bypass_ratio=4.66fuel_flow_gain= 0.001inlet_area= 48.150rated_N2_rpm= 29922.000static_thrust= 71100.000afterburner_available= 0reverser_available= 1[jet_engine]thrust_scalar =0.900[electrical];BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)flap_motor=0, 5 , 17.0gear_motor=0, 5 , 17.0autopilot=0, 5 , 17.0avionics_bus=0, 10, 17.0avionics=1, 5 , 17.0pitot_heat=0, 2 , 17.0additional_system=0, 20, 17.0marker_beacon=1, 2 , 17.0gear_warning=0, 2 , 17.0fuel_pump=0, 5 , 17.0starter1=0, 20, 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//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)[contact_points]point.0=1, 83.42, 0.00, -14.42, 1181.1, 0, 4.521, 72.0, 0.50, 2.1, 0.8135,11.0, 13.2, 0, 0.0, 0.0 //nosepoint.1=1, -7.20, -15.80, -16.04, 1574.8, 1, 4.737, 0.0, 1.51, 2.0, 0.7470, 9.7, 14.1, 2, 0.0, 0.0 //left mainpoint.2=1, -7.20, 15.80, -16.04, 1574.8, 2, 4.737, 0.0, 1.51, 2.0, 0.7470, 9.7, 14.1, 3, 0.0, 0.0 //right mainpoint.3=2, -10.17, -47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0point.4=2, -10.17, 47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0point.5=2, -83.33, 0.00, 2.50, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0point.7=5, -0, -0, -0, 0, 0, 0.00, 0.0, 0.0, 0.0, 0.00, 6, 6, 0, 0.0, 0.0//AES Orgvalue:static_pitch=-0.83 static_pitch=-.42//AES Orgvalue:static_cg_height=20.670static_cg_height=20.48gear_system_type=0[Views]eyepoint=98.07, -1.80, 5.85[LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landinglight.1 = 1, 30.25, 0.00, -7.90, fx_beaconb ,light.2 = 1, 17.60, 0.00, 12.00, fx_beaconh ,light.3 = 2, -97.42, 0.00, 9.00, fx_strobe ,light.4 = 3, -97.42, 0.00, 9.00, fx_navwhi ,light.5 = 4, 88.9, 0, 7.3, fx_vclighth[Flaps.0]type=1span-outboard=1.0extending-time=20system_type=1flaps-position.0= 0 flaps-position.1= 8flaps-position.2= 14flaps-position.3=18flaps-position.4=22flaps-position.5=32damaging-speed = 240 blowout-speed = 260 lift_scalar = 1.0drag_scalar = 1.0pitch_scalar= 1.0 //Hydraulic[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[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[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[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[fuel]Center1 = 5.0, 0.0, -4.0, 12500, 1043LeftMain = -5.0, -20.0, 0.0, 12150, 949RightMain = -5.0, 20.0, 0.0, 12150, 949fuel_type=2number_of_tank_selectors=1electric_pump=1[airplane_geometry]wing_area= 3892.000wing_span= 197.833wing_root_chord= 20.000wing_dihedral= 6.218wing_incidence= 0.000wing_twist= -0.500oswald_efficiency_factor= 0.600wing_winglets_flag= 1wing_sweep= 30.000wing_pos_apex_lon= 25.000wing_pos_apex_vert= 0.000htail_area= 1050.000htail_span= 69.700htail_pos_lon= -89.200htail_pos_vert= 0.000htail_incidence= 0.000htail_sweep= 40.000vtail_area= 690.000vtail_span= 27.300vtail_sweep= 35.000vtail_pos_lon= -83.676vtail_pos_vert= 5.800elevator_area= 137.000aileron_area= 68.000rudder_area= 232.000elevator_up_limit= 24.000elevator_down_limit= 18.000aileron_up_limit= 25.000aileron_down_limit= 25.000rudder_limit= 45.000elevator_trim_limit= 15.000spoiler_limit= 35.000spoilerons_available= 0aileron_to_spoileron_gain= 3.000min_ailerons_for_spoilerons= 9.969min_flaps_for_spoilerons= 0.000[Reference Speeds]flaps_up_stall_speed=150.0 //Knots True (KTAS)full_flaps_stall_speed=130.0 //Knots True (KTAS)cruise_speed=520.0 //Knots True (KTAS)max_indicated_speed=375.000000max_mach=0.860000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=800autothrottle_available=1autothrottle_arming_required=0autothrottle_takeoff_ga=8autothrottle_max_rpm=97pitch_takeoff_ga=4max_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[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=0.86000000parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=5.042029[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_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=100,100 ;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 = 3exit_rate.0 = 100 ;Percent per secondexit_rate.1 = 100 ;Percent per secondexit_rate.2 = 100 ;Percent per second