OSS/Erick Cantu Embraer EMB-120

[Guest snake1]

Does anyone know where to get a full original copy of the OSS/Erick Cantu Embraer EMB-120? because OSS site doesn't work. thanks for your help.

[Opa 6]

Does anyone know where to get a full original copy of the OSS/Erick Cantu Embraer EMB-120? because OSS site doesn't work. thanks for your help.

Not sure what the "OSS" refers to but the following link to Eric's Embraer EMB-120 here in the library might be worth a look:http://library.avsim.net/esearch.php?CatID...&DLID=95277

[Guest snake1]

Not sure what the "OSS" refers to but the following link to Eric's Embraer EMB-120 here in the library might be worth a look:http://library.avsim.net/esearch.php?CatID...&DLID=95277

Hello, Thank you so much for the info. I did come across that one. But I believe that this is a different one he did or was involved in.the OSS stands for: Online Simulation Solutions, LLC. Copyright 2006, All Rights Reserved. There are about thirty textures for it here on avsim, but no original complete aircraft. This is one of the textures I'm referring to.Category: Flight Simulator 2004 - Aircraft Repaints, Textures and Modifications Trip Linhas A

[graemeb 14]

The file that David refers to is correct - that is the freeware Emb-120 that I have and it was at one time the OSS model.

[Guest belga1]

Hello,

description=Embraer EMB120 for FS2004\nAircraft by Online Simulation Solutions, LLC.\nCopyright 2006, All Rights Reserved.\n

snake1 send me a PM if you want the OSS original Embraer 120 file !(ASA airline texture included)Regards.

[Guest snake1]

Hello,snake1 send me a PM if you want the OSS original Embraer 120 file !(ASA airline texture included)Regards.

Thanks for your help guys.

[Carob 2]

The documentation for the model that Opa mentions says the modeling is directly from the default King Air. Is the original OSS model the same way?

[Opa 6]

The documentation for the model that Opa mentions says the modeling is directly from the default King Air. Is the original OSS model the same way?

I sure do not see that anywhere in the documentation. The only references which I see is that the panel and sounds have been aliased to the King Air and the .air file and performance data are from the same source. Those would have nothing to do with the actual "model" - the model is Eric's work as I read it.

[Carob 2]

I guess I used the wrong wording. The documentation says...I used the airfile data and performance data from the Kingair so this plane handles and flies just as the default Kingair. This was done to ensure that only the work of the model and texture authors are included in this package.

[Carob 2]

I just did a quick test flight with this thing and I can only imaging the handling is WAY off. I don't know if something is different in the one I grabbed (which is emb120_261796.zip) or not but holy cow.Here is the aircraft.cfg file. Maybe someone can compare.[General]atc_type=EMBRAERatc_model=E120editable=0performance="Cruise Speed\t\n315 kts 363 mph 583 km\/h\n\nEngines\t\nPratt & Whitney PT6A-60A 1,050 shp\n\nMaximum Range\t\n1,765 nm 2,031 m\t 3,269 km\n\nService Ceiling\t\n35,000 ft 10,668 m\n\nFuel Capacity\t\n539 U.S. gal 2,040 L\n\nMaximum Takeoff Weight \n15,000 lb\t 6,818 kg\n\nLength\t\n46.7 ft\t 14.23 m\n\nWingspan\t\n57.9 ft\t 17.65 m\n\nHeight\t\n14.3 ft\t 4.36 m\n\nSeating\t\nUp to 11\n\nUseful Load\t\n5,910 lb\t 2,681 kg"[WEIGHT_AND_BALANCE]max_gross_weight = 15000 // (pounds)empty_weight = 9090 // (pounds)reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)empty_weight_CG_position = 0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datummax_number_of_stations = 50station_load.0 = "170, 5.0, -2.0, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.1 = "170, 5.0, 2.0, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.2 = "170, -2.1, -2.0, 0.0, Passenger" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.3 = "170, -2.1, 2.0, 0.0, Passenger" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.4 = "170, -5.3, -2.0, 0.0, Passenger" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)station_load.5 = "170, -5.3, 2.0, 0.0, Passenger" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet);Moments of Inertiaempty_weight_pitch_MOI = 30000empty_weight_roll_MOI = 18200empty_weight_yaw_MOI = 36500empty_weight_coupled_MOI= 0.0[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 = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=TurbopropEngine.0 = -8.3, -4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datumEngine.1 = -8.3, 4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datumfuel_flow_scalar = 1.0 //Scalar for fuel flow efficiencymin_throttle_limit = -0.25; //Minimum percent throttle. Generally negative for turbine reverser[propeller]thrust_scalar = 1.0 //Propeller thrust scalarpropeller_type = 0 //0=Constant Speed, 1=Fixed Pitchpropeller_diameter = 8.8 //Propeller Diameter, (feet)propeller_blades = 4 //Number of propeller bladespropeller_moi = 24 //Propeller moment of inertiabeta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees)beta_min = 15.2 //Minimum blade pitch angle for constant speed prop, (degrees)min_gov_rpm = 25520 //Miminum governed RPMprop_tc = 0.004 //Prop time-constantgear_reduction_ratio = 17.6 //Propeller gear reduction ratiofixed_pitch_beta = 0 //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=TRUEprop_deice_available = 1 //Prop de-icing available? 0=FALSE, 1=TRUEprop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUEprop_auto_feathering_available= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUEmin_rpm_for_feather = 700 //Minimum RPM for prop featheringbeta_feather = 79.3 //Feathering pitch angle (degrees)power_absorbed_cf = 0.9 //Coefficient of friction for power absorbed by propellerdefeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available = 1 //Prop reverse available? 0=FALSE, 1=TRUEminimum_on_ground_beta = 1.0 //Miminum pitch angle on ground, (degrees)minimum_reverse_beta = -14.0 //Minimum pitch angle in reverse, (degrees)[TurbineEngineData]fuel_flow_gain = 0.011 //Gain on fuel flowinlet_area = 1.0 //Square Feet, engine nacelle inlet arearated_N2_rpm = 29920 //RPM, second stage compressor rated valuestatic_thrust = 158 //Lbs, max rated static thrust at Sea Level[turboprop_engine]power_scalar = 1.0 //Scalar on Turboprop powermaximum_torque = 3270 //Maximum torque available (ft-lbs)[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 //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, 13.00, 0.00, -5.30, 1181, 0, 0.596, 39.9, 0.296, 1.581, 0.9516, 4.8, 4.8, 0, 184.0, 184.0point.1=1, -1.67, -8.58, -5.9, 1574, 1, 0.596, 0.0, 0.642, 1.581, 0.8152, 4.5, 5.2, 2, 184.0, 184.0point.2=1, -1.67, 8.58, -5.9, 1574, 2, 0.596, 0.0, 0.642, 1.581, 0.8152, 4.8, 4.9, 3, 184.0, 184.0point.3=2, -3.33, -23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0point.4=2, -3.33, 23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0point.5=2, -22.67, 0.00, 0.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0point.6=2, 23.08, 0.00, -1.50, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0static_pitch = -1.0static_cg_height = 4.3gear_system_type=1 //Hydraulic[gear_warning_system]gear_warning_available = 1 //Normalpct_throttle_limit = 0.1 //Percent throttle that activates warningflap_limit_idle = 15.0 //Flap angle that activates warning at idleflap_limit_power = 30.0 //Flap angle that activates warning at above idle[brakes]parking_brake = 1 //Parking brake availabletoe_brakes_scale = 1.0 //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 = 4.54, -1.20, 3.25[flaps.0]type = 1 // 1 - tail, 2 - leadspan-outboard = 0.5 // 0.0 .. 1.0extending-time = 5 // secondsflaps-position.0 = 0 // degreesflaps-position.1 = 20 // degreesflaps-position.2 = 40 // degreesdamaging-speed = 250 // KIASblowout-speed = 300 // KIAS[Radios]// Radio Type = availiable, standby frequency, has glide slopeAudio.1 = 1Com.1 = 1, 0Com.2 = 1, 0Nav.1 = 1, 0, 1Nav.2 = 1, 0, 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[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=1,0[LIGHTS]//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpitlight.0 = 3, 0.90, -32.00, 2.90, fx_navred ,light.1 = 3, 0.90, 32.00, 2.90, fx_navgre ,light.2 = 3, -39.80, 0.00, 16.00, fx_navwhi ,light.3 = 2, 0.70, -32.00, 2.90, fx_strobe ,light.4 = 2, 0.70, 32.00, 2.90, fx_strobe ,light.5 = 1, 0.00, 0.00, 7.0, fx_beacon ,light.6 = 2, -4.55, 0.00, -1.85, fx_strobe ,light.7 = 4, 4.91, 0.00, 1.64, fx_vclight,[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn_s, 1[fuel]LeftMain = 0.0, -14.5, -1.0, 190.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)LeftAux = 0.0, -6.0, -1.5, 79.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)RightMain = 0.0, 14.5, -1.0, 190.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)RightAux = 0.0, 6.0, -1.5, 79.5, 0.0 //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=1[airplane_geometry]wing_area = 310.0 //Square feetwing_span = 57.2 //Feetwing_root_chord = 5.4 //Feetwing_dihedral = 6.0 //Degreeswing_incidence = 1.0 //Degreeswing_twist = -1.5 //Degreesoswald_efficiency_factor= 0.7 //Measure of lift effeciency of wingwing_winglets_flag = 1 //Are winglets available?wing_sweep = 1.0 //Degrees, wing leading edgewing_pos_apex_lon = 2.1 //Feet, longitudinal distance from reference point, negative going aftwing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going uphtail_area = 67.0 //Square feethtail_span = 17.2 //Feethtail_pos_lon = -22.6 //Feet, longitudinal distance from reference point, negative going afthtail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going uphtail_incidence = 0.5 //Degreeshtail_sweep = 20.0 //Degrees, horizontal tail leading edgevtail_area = 42.0 //Square feetvtail_span = 7.4 //Feet, tip to bodyvtail_sweep = 40.0 //Degrees, vertical tail leading edgevtail_pos_lon = -20.5 //Feet, longitudinal distance from reference point, negative going aftvtail_pos_vert = 4.1 //Feet, vertical distance from reference point, positive going upelevator_area = 17.0 //Square feetaileron_area = 13.5 //Square feetrudder_area = 7.3 //Square feetelevator_up_limit = 17.0 //Degreeselevator_down_limit = 15.5 //Degreesaileron_up_limit = 18.0 //Degreesaileron_down_limit = 18.0 //Degreesrudder_limit = 30.0 //Degreeselevator_trim_limit = 15.0 //Degreesspoiler_limit = 60.0 //Degreesspoilerons_available = 0 //Spoilerons Available?aileron_to_spoileron_gain = 0 //Aileron to spoileron gainmin_ailerons_for_spoilerons = 0 //Degreesmin_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate[Reference Speeds]flaps_up_stall_speed = 96.0 //Knots True (KTAS)full_flaps_stall_speed = 76.8 //Knots True (KTAS)cruise_speed = 300.0 //Knots True (KTAS)max_mach = 0.58max_indicated_speed = 263 //Red line (KIAS)[autopilot]autopilot_available= 1flight_director_available= 1default_vertical_speed= 1800.0autothrottle_available= 0pitch_takeoff_ga=8.0max_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=9.00nav_integrator_control=0.25nav_derivative_control=0.00nav_integrator_boundary=2.50nav_derivative_boundary=0.00gs_proportional_control=9.52gs_integrator_control=0.26gs_derivative_control=0.00gs_integrator_boundary=0.70gs_derivative_boundary=0.00yaw_damper_gain = 1.0[forcefeedback]stick_shaker_magnitude=5000 ; 0 - 10000stick_shaker_direction=0 ; 0 - 35999 degreesstick_shaker_period=111111 ; in microsecondsgear_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=9000 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=27000 ; 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[exits]number_of_exits=2exit_rate.0=0.4 ;Percent per secondexit_rate.1=0.4 ;Percent per second[TailHook] //landing lights (normally shift+T)tailhook_length= 4tailhook_position= 0.0, 0.0, 0.0cable_force_adjust= 0.5[folding_wings] //Airstairs (normally shift+F)wing_fold_system_type= 4fold_rates= 0.110,0.110

[Opa 6]

The file I got was emb120.zip. http://library.avsim.net/esearch.php?DLID=95277I am no expert on how it "should" handle, but a brief test flight of this one seemed to perform just fine for me - even made a nice landing on first attempt. :(

[Carob 2]

The file I got was emb120.zip. http://library.avsim.net/esearch.php?DLID=95277I am no expert on how it "should" handle, but a brief test flight of this one seemed to perform just fine for me - even made a nice landing on first attempt. :(

How does my aircraft.cfg file compare to yours?

[Guest belga1]

Hello,This is the original OSS Embraer 120 aircraft.cfg[fltsim.0]title=EMB120 Atlantic Southeastsim=EMB120model=panel=sound=texture=asakb_checklists=description=Embraer EMB120 for FS2004\nAircraft by Online Simulation Solutions, LLC.\nCopyright 2006, All Rights Reserved.\nui_manufacturer=Embraerui_type=EMB120ui_variation=Atlantic Southeastatc_airline=Atlantic Southeastatc_id=Skywestatc_flight_number=atc_heavy=0atc_id_color=0x00000000atc_id_font=Verdana,-11,1,600,0visual_damage=1atc_parking_types=RAMPprop_anim_ratio=1.72[General]performance=MTOW 26,433 lbs\nMLW 25,794 lbs\nZFW 20,610 lbs\nPower: 1800 shp PW118A\nTakeoff Power: 1980 shp\nStall Speeds: 120\/89 kts\nMmo\/Mo: 0.52M\/250kts\nRange: 1570nm + reserve\nEconomic cruise 270kts FL250\nMax cruise 310kts atc_type=EMBRAER atc_model= editable=0 [weight_and_balance]max_gross_weight = 31285.5empty_weight = 16507reference_datum_position = 1.5, 0, 0empty_weight_CG_position = 3, 0, 0empty_weight_pitch_MOI = 168681empty_weight_roll_MOI = 213440empty_weight_yaw_MOI = 244114empty_weight_coupled_MOI = 1300max_number_of_stations = 13station_load.0 = 400, 19.000, 0.000, 3.000station_load.1 = 200, 16.000, -1.650, 3.000station_load.2 = 170, 11.500, 0.000, 3.000station_load.3 = 340, 9.000, 0.000, 3.000station_load.4 = 340, 6.500, 0.000, 3.000station_load.5 = 340, 4.000, 0.000, 3.000station_load.6 = 340, 1.200, 0.000, 3.000station_load.7 = 340, -1.500, 0.000, 3.000station_load.8 = 340, -4.000, 0.000, 3.000station_load.9 = 340, -8.300, 0.000, 3.000station_load.10 = 340, -10.800, 0.000, 3.000station_load.11 = 340, -13.500, 0.000, 3.000station_load.12 = 520, -19.000, 0.000, 3.000[lights]//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landinglight.0 = 3, -0.6, -31.8, 2.9, fx_navredlight.1 = 3, -0.6, 31.8, 2.9, fx_navgrelight.2 = 3, -41.14, 0, 15.7, fx_navwhilight.3 = 2, -0.6, -31.78, 2.9, fx_strobelight.4 = 2, -0.68, 31.78, 2.9, fx_strobelight.5 = 2, -41.14, 0, 15.8, fx_strobelight.6 = 1, -1.65, 0, 7, fx_beaconlight.7 = 1, 0.85, 0, -1.67, fx_beaconlight.8 = 4, 17.92, 0.00, 5.26, fx_vclight,[GeneralEngineData]//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turbopropengine_type = 5fuel_flow_scalar = 0.75min_throttle_limit = -0.249939engine.0 = 5.761, -10.7, 0,engine.1 = 5.761, 10.7, 0,[effects]dirt = fx_tchdrtconcrete = fx_sparkstouchdown = fx_tchdwn_s, 1windshield_rain_effect_available = 1[fuel]//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)fuel_type = 2number_of_tank_selectors = 1electric_pump = 0LeftMain = 0, -14.5, -1, 440.7, 3RightMain = 0, 14.5, -1, 440.7, 3[contact_points]static_pitch = -1static_cg_height = 5.96tailwheel_lock = 0gear_system_type = 0max_number_of_points = 7point.0 = 1, 22.9, 0, -5.2, 2500, 0, 0.696, 45, 0.575, 1.8, 0.952, 6, 7.5, 0, 250, 275point.1 = 1, -1.9, -10.5, -5.9, 2500, 1, 1, 0, 0.725, 1.8, 0.952, 8, 8, 2, 250, 275point.2 = 1, -1.9, 10.5, -5.9, 2500, 2, 1, 0, 0.725, 1.5, 0.952, 7, 7, 3, 250, 275point.3 = 2, 1.152, -32.500, 3.845, 1800.0, 0, 0.000, 0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 5.000, 000, 000point.4 = 2, 1.152, 32.500, 3.845, 1800.0, 0, 0.000, 0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 6.000, 000, 000point.5 = 2, -30.340, 0.000, 4.700, 1800.0, 0, 0.000, 0.0, 0.00, 0.000, 0.000, 0.0, 0.0, 9.000, 000, 000point.6 = 2, 30.1, 0, -0.5, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0[keyboard_response]elevator = 150, 250aileron = 150, 250rudder = 150, 250[forcefeedback]gear_bump_nose_magnitude = 3000gear_bump_nose_direction = 18000gear_bump_nose_duration = 250000gear_bump_left_magnitude = 2700gear_bump_left_direction = 9000gear_bump_left_duration = 250000gear_bump_right_magnitude = 2700gear_bump_right_direction = 27000gear_bump_right_duration = 250000ground_bumps_magnitude1 = 1300ground_bumps_angle1 = 08900ground_bumps_intercept1 = 3.0ground_bumps_slope1 = 0.20ground_bumps_magnitude2 = 200ground_bumps_angle2 = 09100ground_bumps_intercept2 = 1.075ground_bumps_slope2 = 0.035crash_magnitude1 = 10000crash_direction1 = 01000crash_magnitude2 = 10000crash_direction2 = 9000crash_period2 = 75000crash_duration2 = 2500000stick_shaker_magnitude = 5000stick_shaker_direction = 0stick_shaker_period = 111111[airplane_geometry]wing_area = 425.000000wing_span = 64.833333wing_root_chord = 6.583333wing_dihedral = 6.300659wing_incidence = 1.299756wing_twist = 1.499634oswald_efficiency_factor = 0.909222wing_winglets_flag = 0wing_sweep = 0.000000wing_pos_apex_lon = 0.000000wing_pos_apex_vert = 0.000000htail_area = 105.000000htail_span = 22.000000htail_pos_lon = -32.000000htail_pos_vert = 0.000000htail_incidence = 0.000000htail_sweep = 0.000000vtail_area = 89.000000vtail_span = 10.756393vtail_sweep = 0.000000vtail_pos_lon = -30.833333vtail_pos_vert = 5.833333elevator_area = 26.250000aileron_area = 17.000000rudder_area = 15.130000elevator_up_limit = 27.501974elevator_down_limit = 20.626481aileron_up_limit = 19.480565aileron_down_limit = 14.896903rudder_limit = 23.491270elevator_trim_limit = 19.480565spoiler_limit = 0.000000aileron_to_spoileron_gain = 0.000000spoiler_handle_available = 1min_ailerons_for_spoilerons = 0.000000min_flaps_for_spoilerons = 0.000000spoilerons_available = 0[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 60engine_generator_map = 1,1electric_always_available = 0[exits]number_of_exits = 2exit_rate.0 = 0.4 ;Percent per second[flight_tuning]cruise_lift_scalar=1.000 pitch_stability=1.500 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=0.850 induced_drag_scalar=0.850 elevator_effectiveness=0.750 aileron_effectiveness=0.925 rudder_effectiveness=0.850 elevator_trim_effectiveness=1.200 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [TurbineEngineData]fuel_flow_gain=0.009 inlet_area=1.0 rated_N2_rpm=33300 static_thrust=230 afterburner_available=0 [propeller]thrust_scalar=1.0 propeller_type=0 propeller_diameter=10.6 propeller_blades=4 propeller_moi=30 beta_max=45.0 beta_min=15.0 min_gov_rpm=16653 prop_tc=0.004 gear_reduction_ratio=25.62 fixed_pitch_beta=0 low_speed_theory_limit=80 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=600 beta_feather=79.2 power_absorbed_cf=0.9 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=1.0 minimum_reverse_beta=-15.0 [turboprop_engine]power_scalar=1.0 maximum_torque=7272 max_rpm_mechanical_efficiency_scalar=1.000idle_rpm_mechanical_efficiency_scalar=1.000max_rpm_friction_scalar=1.000idle_rpm_friction_scalar=1.000[Reference Speeds]flaps_up_stall_speed=120.000000 full_flaps_stall_speed=96.000000 cruise_speed=359.547707 max_indicated_speed=250.906250max_mach=0.518994[Views]eyepoint=0.00, -1.70, 5.77 [autopilot]autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.000000 autothrottle_available=1 autothrottle_arming_required = 0autothrottle_takeoff_ga = 0autothrottle_max_rpm = 90.000000pitch_takeoff_ga=8.000000 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[direction_indicators]direction_indicator.0=3,0 [pitot_static]vertical_speed_time_constant = 150[brakes]toe_brakes_scale=0.885037parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=30.022988flap_limit_idle=15.011494[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[Flaps.0]type= 1span-outboard= 0.500extending-time= 13.000system_type= 0damaging-speed= 250.000blowout-speed= 300.000lift_scalar= 1.000drag_scalar= 1.000pitch_scalar= 1.000flaps-position.0= 0.000, 0.000flaps-position.1= 15.000, 0.000flaps-position.2= 25.000, 0.000flaps-position.3= 45.000, 0.000Some differences Regards.

[Opa 6]

How does my aircraft.cfg file compare to yours?

Wouldn't it be simpler to DL the one I have and compare them yourself?I did provide a link.

[Carob 2]

Does anyone know how to fix this problem? (Pic attached.) For whatever reason the outside window doesn't come down far enough. And if I stretch it down, the view changes to the point where looking forward is really looking up.