timcool

Yes one more thing about the FMC, How do I make the Level-D fmc show up in the Captain sim VC fmc screen? Mine is all black in the VC but not in the 2d panel.Cheers Tim

Ah I've sucessfully managed to merge the LVL-D panel with the CS 757 model now or atleast the Exterior and "looking" parts with it, But I haven't discovered any problems with the system or at least not yet. Yes I remember you from youtube really liked your merge got the idea to merge these two great addons because of your vids :( but now there is allso this thing with the VC view position. Every time I click on "virtual cockpit" inside the sim I allways end up infront of the VC's position so I have to make some changes in either panel.cfg or Aircraft.cfg (change the view position for the VC view) but I'm not shure where I change this. Maybe you know? Well I've allso merged the Qualitywings panel with the CS 757 model and it worked very well. I merged the LVL-D and CS because I wanted a Speedtape EADI instead of the captain sim Round ball EADI Cheers Tim

Okey but you don't know what to change in the Panel.cfg? yes I tried to merge the QW panel aswell but same exterior problem occured. But may it be the CS control panel that needs to be put into the panel.cfg?/ Tim

Hi guys I have recently tried to merge the captain sim 757 model with the Level-D 767 panel, But i have a problem with the exterior of the CS757. Here is my Captain sim 757 Aircraft.cfg nothing added to it maybe you can help me of what to add to it?:[General]atc_type=BOEINGatc_model=B757editable=1performance=Weight: MTOW 408,000 lbs MLW: 320,000\nPower: GE CF6-80C2B7 @ 61,500\n\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 = 150000 // (pounds)empty_weight = 74170 // (pounds)reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)empty_weight_CG_position = -5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datummax_number_of_stations = 50station_load.0 = "170.0, 41.0, -1.5, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "170.0, 41.0, 1.5, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = "1360.0, 25.5, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = "8160.0, 11.0, 0.0, 0.0, Coach 3-10" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = "8160.0, -10.0, 0.0, 0.0, Coach 11-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = "7140.0, -30.5, 0.0, 0.0, Coach 19-25" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7 = "10000.0, 20.5, 0.0, 0.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8 = "4000.0, -27.5, 0.0, 0.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertiaempty_weight_pitch_MOI = 3172439empty_weight_roll_MOI = 2262183empty_weight_yaw_MOI = 3337024empty_weight_coupled_MOI = 0[flight_tuning]cruise_lift_scalar = 1.0parasite_drag_scalar = 1.0induced_drag_scalar = 1.0elevator_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 = 4.75, -16.1, -4.5 //(feet) longitudinal, lateral, vertical distance from reference datumEngine.1 = 4.75, 16.1, -4.5 //(feet) longitudinal, lateral, vertical distance from reference datumfuel_flow_scalar = 0.5 //Scalar for fuel flow efficiencymin_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reversermax_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear[TurbineEngineData]fuel_flow_gain = 0.002 //Gain on fuel flowinlet_area = 19.6 //Square Feet, engine nacelle inlet arearated_N2_rpm = 29920 //RPM, second stage compressor rated valuestatic_thrust = 23500 //Lbs, max rated static thrust at Sea Levelafterburner_available = 0 //Afterburner available?reverser_available = 1 //Thrust reverser available?[jet_engine]thrust_scalar = 1.0[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, 5, 17.0avionics = 1, 5 , 17.0pitot_heat = 0, 2 , 17.0additional_system = 0, 2, 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[contact_points]point.0=1, 58.50, 0.00, -10.80, 1181.1, 0, 1.5, 68.00, 0.15, 3.0, 0.9, 12.1, 12.1, 0, 240.0, 280.0point.1=1, -7.50, -11.00, -11.70, 1574.8, 1, 2.0, 0.00, 1.0, 1.0, 0.9, 10.9, 10.9, 2, 240.0, 280.0point.2=1, -7.50, 11.00, -11.70, 1574.8, 2, 2.0, 0.00, 1.0, 1.0, 0.9, 11.1, 11.1, 3, 240.0, 280.0point.3 = 2, -15, -62, 5.4, 787, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0point.4 = 2, 20, -22, -7.7, 787, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0point.5 = 2, 20, 22, -7.8, 787, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0point.6 = 2, -15, 62, 5.4, 787, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0point.7 = 2, 75, 0, -0.4, 787, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0point.8 = 2, 63, 0, -3.7, 787, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0point.9 = 2, -38, 0, -3.9, 787, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0point.10 = 2, -77, 0, 6.1, 787, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0max_number_of_points = 21static_pitch=0.00 //degrees, pitch when at rest on the ground (+=Up, -=Dn)static_cg_height=11 //feet, altitude of CG when at rest on the groundgear_system_type=1 //Hydraulic[gear_warning_system]gear_warning_available = 1 //Normalpct_throttle_limit = 0.1 //Percent throttle that activates warningflap_limit_idle = 5.0 //Flap angle that activates warning at idleflap_limit_power = 25.5 //Flap angle that activates warning at above idle[brakes]parking_brake = 1 //Parking brake availabletoe_brakes_scale = 0.885 //Brake scalar[hydraulic_system]normal_pressure = 3000.0 //PSIelectric_pumps = 0 //no electric pumpsengine_map = 1,1,0,0 //pumps on Eng1,2[Views]eyepoint=69.30, -2.10, -1.10ep1=69.30, -2.10, -1.10ep2=69.30, 2.10, -1.10ep3=59, -2.0, -0.5ep4=46, -4.3, -1.4ep5=33, -2.0, -0.5[flaps.0] //Trailing Edge Flapstype = 1 // 1 - tail, 2 - leadspan-outboard = 0.8 // 0.0 .. 1.0extending-time = 20 // secondsflaps-position.0 = 0 // degreesflaps-position.1 = 0 // degreesflaps-position.2 = 5 // degreesflaps-position.3 = 15 // degreesflaps-position.4 = 20 // degreesflaps-position.5 = 25 // degreesflaps-position.6 = 30 // degreesdamaging-speed = 250 // KIASblowout-speed = 300 // KIASlift_scalar = 1.0drag_scalar = 1.0pitch_scalar= 1.0system_type = 1 //Hydraulic[flaps.1] //Inboard Leading Edge Flapstype = 2 // 1 - tail, 2 - leadspan-outboard = 0.8 // 0.0 .. 1.0extending-time = 2 // secondsflaps-position.0 = 0 //flaps-position.1 = 1.0 //damaging-speed = 250 // KIASblowout-speed = 300 // KIASlift_scalar = 1.0drag_scalar = 1.0pitch_scalar= 1.0system_type = 1 //Hydraulic[flaps.2] //Outboard Leading Edge Slattype = 2 // 1 - tail, 2 - leadspan-outboard = 0.8 // 0.0 .. 1.0extending-time = 3 // secondsflaps-position.0 = 0 //flaps-position.1 = 0.5 //flaps-position.4 = 1.0 //damaging-speed = 250 // KIASblowout-speed = 300 // KIASlift_scalar = 1.0drag_scalar = 1.0pitch_scalar= 1.0system_type = 1 //Hydraulic[Radios]// Radio Type = availiable, standby frequency, has glide slopeAudio.1 = 1Com.1 = 1, 1Com.2 = 1, 1Nav.1 = 1, 0, 1Nav.2 = 1, 0, 1Adf.1 = 1Transponder.1 = 1Marker.1 = 1[LIGHTS] ;light.0 = 3, -14.59, 61.61, 5.47, cs757_navgre;light.1 = 3, -14.59, -61.61, 5.47, cs757_navred;light.2 = 2, -16.81, 61.97, 5.50, fx_strobe;light.3 = 2, -16.81, -61.97, 5.50, fx_strobe;light.4 = 3, -20.08, 61.71, 5.32, cs757_navwhi;light.5 = 3, -20.08, -61.71, 5.32, cs757_navwhilight.0 = 1, 3.00, 0.00, -3.90, fx_beaconhlight.1 = 1, 42.34, 0.30, 10.57, fx_beaconhlight.2 = 4, 70.78, 0.00, 5.19, fx_vclightwhilight.3 = 5, 17.55, 7.35, 0.10, cs757_landlight.4 = 5, 17.55, -7.35, 0.10, cs757_landlight.5 = 7, -17.00, -47.00, 1.00, cs757_sflight.6 = 7, -17.00, 47.00, 1.00, cs757_sf[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, 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[attitude_indicators]//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyroattitude_indicator.0 = 1 [turn_indicators]//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyroturn_indicator.0=0,0[exits]number_of_exits=4exit_rate.0 = 0.4exit_rate.1 = 0.4exit_rate.2 = 0.4exit_rate.3 = 0.4[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800autothrottle_available=1autothrottle_arming_required=1autothrottle_max_rpm = 90autothrottle_takeoff_ga=1pitch_takeoff_ga = 8;max_pitch=10.0max_pitch_acceleration=1.0max_pitch_velocity_lo_alt=2.0max_pitch_velocity_hi_alt=1.5max_pitch_velocity_lo_alt_breakpoint=20000.0max_pitch_velocity_hi_alt_breakpoint=28000.0max_bank=25.0max_bank_acceleration=1.8max_bank_velocity=3.00max_throttle_rate=0.10nav_proportional_control=12.00nav_integrator_control=0.25nav_derivative_control=0.00nav_integrator_boundary=2.50nav_derivative_boundary=0.00gs_proportional_control=25.0gs_integrator_control=0.53gs_derivative_control=0.00gs_integrator_boundary=0.70gs_derivative_boundary=0.00yaw_damper_gain = 1.0[fuel];Center1 = 0, 0, 0, 2313, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)LeftMain = -3, -19, 0, 1500, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)RightMain = -3, 19, 0, 1500, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetAnumber_of_tank_selectors = 1 electric_pump=0[airplane_geometry]wing_area = 1137.0 //Square feetwing_span = 94.75 //Feetwing_root_chord = 18.0 //Feetwing_dihedral = 6.2 //Degreeswing_incidence = 1.0 //Degreeswing_twist = -0.5 //Degreesoswald_efficiency_factor= 0.75 //Measure of lift effeciency of wingwing_winglets_flag = 0 //Are winglets available?wing_sweep = 25.0 //Degrees, wing leading edgewing_pos_apex_lon = 8.0 //Feet, longitudinal distance from reference point, negative going aftwing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going uphtail_area = 338.0 //Square feethtail_span = 41.7 //Feethtail_pos_lon = -35.0 //Feet, longitudinal distance from reference point, negative going afthtail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going uphtail_incidence = 0.0 //Degreeshtail_sweep = 30.0 //Degrees, horizontal tail leading edgevtail_area = 224.0 //Square feetvtail_span = 20.0 //Feet, tip to bodyvtail_sweep = 35.0 //Degrees, vertical tail leading edgevtail_pos_lon = -35.8 //Feet, longitudinal distance from reference point, negative going aftvtail_pos_vert = 5.8 //Feet, vertical distance from reference point, positive going upelevator_area = 70.5 //Square feetaileron_area = 26.9 //Square feetrudder_area = 56.2 //Square feetelevator_up_limit = 22.5 //Degreeselevator_down_limit = 19.5 //Degreesaileron_up_limit = 20.0 //Degreesaileron_down_limit = 20.0 //Degreesrudder_limit = 26.0 //Degreeselevator_trim_limit = 20.0 //Degreesspoiler_limit = 60.0 //Degreesspoilerons_available = 1 //Spoilerons Available?aileron_to_spoileron_gain = 2.5 //Aileron to spoileron gainmin_ailerons_for_spoilerons = 10 //Degreesmin_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate[Reference Speeds]flaps_up_stall_speed = 142.0 //Knots True (KTAS)full_flaps_stall_speed = 113.0 //Knots True (KTAS)cruise_speed = 477.0 //Knots True (KTAS)max_mach = 0.82max_indicated_speed = 340 //Red line (KIAS)[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[stall_warning]type=2[TailHook]tailhook_length=1tailhook_position=0,0,0,cable_force_adjust=0.00001[folding_wings]wing_fold_system_type=4fold_rates=10Here is a picture of the exterior problem:

Okay but I actually have the paint kit for ariane 737-800 but the problem is I dont know how to make the actuall repaint but I have all the softwares needed but not the knowledge of using them:P

I have a little request for a repaint If someone would have the time and want to.I would really like a "Norwegian ar shuttle" repaint for the Ariane 2x for FSXNorwegian air shuttle LN-NON tell me if you are intrested