August 22, 2025Aug 22 Based on my brief experience with SU3, I would say significant changes have been made in the simulator's components with respect to performance. When I started SU3 and without any settings changes (but cleared shader cache, etc. prior to starting), FPS tanked. I have a midrange system with the Community folder currently having only the PMDG B777-300ER and Navigraph, and was getting about 60 FPS with no stutters prior to SU3. With SU3, on the ground and on the runway the FPS was maxing out at about 20 and the test takeoff roll was stutter city....unusable. I then played around with the graphics settings and the one that seems to have made a big difference is Frame Generation. It was OFF prior to SU3, it is ON now and the FPS fluctuates between 80-100. I have no stutters and even though performance-wise I have moved in the right direction, I am not declaring victory yet because my SU3 experience is very limited. My recommendation to people who are having performance problems is to treat SU3 as a new product and revisit every single graphics setting, i.e., a configuration that yielded good/acceptable performance prior to SU3 does not seem to have any bearing on the current MSFS2024 performance. zachlog
August 22, 2025Aug 22 3 hours ago, MarcG said: Indeed you are but it's the severity of those drops that's the main concern here, something Asobo clearly still need to work on. Asobo 737 Max 8 flight from Poland to Bulgaria yesterday, usually fps prior to SU3 would be 29 to 34 fps, but during the latter end of the flight the fps started to oscillate between 30 & 10. Haven't had that before. T45
August 22, 2025Aug 22 Commercial Member 4 hours ago, Fiorentoni said: MSFS2024 implemented aggressive out-of-view LODs which make the sim perform significantly better (up to 50%!) for everybody. Of course this comes with the side effect of loading when changing the view angle drastically (-> panning 360 degrees). Well you can‘t have it all, no stutters while panning around 360 degrees *and* high FPS. I prefer the latter, because the angle of panning when in the cockpit is max. 60 degrees to each side. So I rarely have stutters and yet 60 FPS on ultra at heavy payware airports with full BATC traffic. I think they did very well with the LODs in MSFS2024 overall. Hello @Fiorentoni, If you want, you can disable the out-of-view LODs by going to your graphics options and setting "Off-screen Terrain Pre-Caching" to "Ultra". This will give you full visual quality when panning the camera around (no more waiting a brief moment for the high def terrain to "pop in"), at the tradeoff of using more VRAM. If you have a PC with a high-end GPU, you should be able to set that option to Ultra without it impacting your performance too much. Thanks, SeedyL, MSFS Community Manager
August 22, 2025Aug 22 One of the biggest improvements (I've jumped from SU2 to SU3 today) is the clarity - both the outside world as my airplanes seem more real than ever before - quite outstanding!
August 22, 2025Aug 22 11 hours ago, btacon said: FWIW. I was in SU3 Beta from day one. I would read all about the stutters folks were experiencing, especially on landing or during departure. I never had those issues. 98% of the time, smooth as silk. Now it’s a big stuttering mess for me. Go figure! Something has changed and it’s not my PC Blue skies, -B EDIT. So I took a look at settings and saw that Multiplayer was turned on. I’ve always turned Multiplayer off since Release Day One MSFS 2020. Anyway, must have been enabled during yesterday’s release. I turned it back off and for me? Stutter free once again. Try it. You might like it. Even tho it’s been suggested that it’s just a placebo, in my case it has restored my system back to its SU3 BETA smoothness. Flying now KMIA/KDEN in PMDG 777-200 ER. Departure from KMIA was flawless with frames in high 30’s to mid 40’s. Once airborne frames remained in the 40’s until passing 10k or so where they transitioned to low to mid 50’s with nary a stutter in sight. Stock TAA, no FG on my RTX 4070ti. Very much my experience during most of the beta. I’m well pleased once again and suggest one more time to insure MultiPlayer s disabled if you don’t use it. I suspect the injected MP aircraft were causing most of my “stuttering mess”. Blue skies!, -B
August 22, 2025Aug 22 23 hours ago, SN737 said: Thanks very much, I'm only flying in 2024 now, I use the iFly and pmdg 737. These settings are for any 737? (pmdg and iFly) Try this and see if it is what you are looking for Ifly: [VERSION] major = 1 minor = 0 [WEIGHT_AND_BALANCE] max_gross_weight = 181700 ; Empty weight, (LBS) empty_weight = 99360 ; Empty weight, (LBS) reference_datum_position = 0,0,0 ; Position of reference datum relative to FS(0,0,0) (FEET), z, x, y empty_weight_CG_position = -6.171,0,0 ; Position of airplane empty weight CG relative to reference datum (FEET), z, x, y CG_forward_limit = 0.0 ; Gravity center forward limit (longitudinal offset) for longitudinal stability CG_aft_limit = 1.0 ; Gravity center after limit (longitudinal offset z) w.r.t reference datum for longitudinal stability (FEET) empty_weight_pitch_MOI = 3000000 ; 2148488 ; Empty pitch moment of inertia, Jxx (SLUG SQ FEET) empty_weight_roll_MOI = 1600000 ; 1470096 ; Empty roll moment of inertia, Jzz (SLUG SQ FEET) empty_weight_yaw_MOI = 1600000 ; Empty yaw moment of inertia, Jyy (SLUG SQ FEET) empty_weight_coupled_MOI = 0 ; Empty transverse moment of inertia, Jyz (SLUG SQ FEET) activate_mach_limit_based_on_cg = 0 ; Activate mach limitation depending on CG position (true if > 0 /false othewise). Mostly for Concorde). activate_cg_limit_based_on_mach = 0 ; Activate cg limitation depending on mach value (true if > 0 /false othewise). Mostly for Concorde). max_number_of_stations = 13 ; Number of payload stations station_load.0=220, 28.82, 0, 1, Pilot, 1 station_load.1=400, 25.10, 0, 1, FA fwd, 0 station_load.2=400, -29.38, 0, 1, FA aft, 0 station_load.3=2341, 18.91, 0, 1, PAX A, 3 station_load.4=5853, 6.10, 0, 1, PAX B, 3 station_load.5=1171, -6.28, 0, 1, PAX C, 3 station_load.6=3317, -10.00, 0, 1, PAX D, 3 station_load.7=3512, -13.00, 0, 1, PAX E, 3 station_load.8=3902, -18.00, 0, 1, PAX F, 3 station_load.9=2536, -22.30, 0, 1, PAX G, 3 station_load.10=5752, 12.10, 0, 1, Cargo fwd, 6 station_load.11=8018, -17.00, 0, 1, Cargo aft, 6 station_load.12=220, 28.82, 0, 1, Co-Pilot, 2 station_name.0=Pilot station_name.1=FA fwd station_name.2=FA aft station_name.3=PAX A station_name.4=PAX B station_name.5=PAX C station_name.6=PAX D station_name.7=PAX E station_name.8 =PAX F station_name.9 =PAX G station_name.10=Cargo fwd station_name.11=Cargo aft station_name.12=Co-Pilot [CONTACT_POINTS] static_pitch = -0 ; degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height = 11.7 ; feet, altitude of CG when at rest on the ground gear_system_type = 1 ; gear system type (betweeen 0 and 4) 0 = electrical, 1 = hydraulic, 2 = pneumatic, 3 = manual, 4 = none, 5 = undefined max_number_of_points = 14 ; Number of contact points point.0 = 1, 43.60, 0.000, -11.435, 1181, 0, 1.1333, 50.0, 0.388373, 1.5929, 0.99, 8.0, 8.0, 0, 265.0, 315.0, 2 point.1 = 1, -8.25, -9.35, -12.55, 1575, 1, 1.85, 0, 1.13648, 1.17318, 0.650, 9.0, 9.0, 2, 265.0, 315.0, 2 point.2 = 1, -8.25, 9.35, -12.55, 1575, 2, 1.85, 0, 1.13648, 1.17318, 0.650, 9.0, 9.0, 3, 265.0, 315.0, 2 point.3 = 2, -25.00,-58.5,-2.00,350,0,0.0001,0,0.0001,0.0001,0,0,0,5,0,0,1 point.4 = 2, -25.00,58.5,-2.00,350,0,0.0001,0,0.0001,0.0001,0,0,0,6,0,0,1 point.5 = 2, 44.35,-0,2.234,350,0,0.0001,0,0.0001,0.0001,0,0,0,4,0,0,1 point.6 = 2, 30.599,0,-2.126,500,0,0.0001,0,0.0001,0.0001,0,0,0,4,0,0,1 point.7 = 2, 22.65,0,11.483,1,0,0.0001,0,0.0001,0.0001,0,0,0,4,0,0,1 point.8 = 2, 9.43,-15.82,-8.526,500,0,0.0001,0,0.0001,0.0001,0,0,0,5,0,0,1 point.9= 2, 9.43,15.82,-8.526,500,0,0.0001,0,0.0001,0.0001,0,0,0,6,0,0,1 point.10= 2,-32.26,-0,-2.126,500,0,0.0001,0,0.0001,0.0001,0,0,0,4,0,0,1 point.11= 2,-71.5,0,4.1,750,0,0.0001,0,0.0001,0.0001,0,0,0,9,0,0,1 point.12= 2,-68.83,0,30.441999,350,0,0.0001,0,0.0001,0.0001,0,0,0,9,0,0,1 point.13= 2,-56.54,0.00,-2.61,350,0,0.0001,0,0.0001,0.0001,0,0,0,9,0,0,1 tailwheel_lock = 0 ; Is tailwheel lock available TRUE/FALSE gear_locked_on_ground = 0 ; Defines whether or not the landing gear handle is locked to down when the plane is on the ground. gear_locked_above_speed = -1 ; Defines the speed at which the landing gear handle becomes locked in the up position. (-1 = Disabled) ///////////////////////////////////////////////////////////////////////// max_speed_full_steering = 10 max_speed_decreasing_steering = 60 min_available_steering_angle_pct = 0.1 steering_time_constants= 8, 8 allow_stopped_steering=1 //////////////////////////////////////////////////////////////////////// emergency_extension_type = 0 hyd_need_power_to_function = 0 locked_tailwheel_max_range = 0 [fuel] Center1 = -1.00, 0.0, -1.5, 4274, 1.2 LeftMain = -5.75, -16.0, -0.4, 1273, 2.2 RightMain = -5.75, 16.0, -0.4, 1273, 2.2 leftaux = 0, 0, 0, 0, 0 rightaux = 0, 0, 0, 0, 0 center2 = 0, 0, 0, 0, 0 center3 = 0, 0, 0, 0, 0 lefttip = 0, 0, 0, 0, 0 righttip = 0, 0, 0, 0, 0 external1 = 0, 0, 0, 0, 0 external2 = 0, 0, 0, 0, 0 fuel_type = 2 number_of_tank_selectors = 2 electric_pump=1 fuel_dump_rate = 0.0167 engine_driven_pump=1 manual_transfer_pump=0 manual_pump=0 anemometer_pump=0 default_fuel_tank_selector.1=1 default_fuel_tank_selector.2=1 default_fuel_tank_selector.3=1 default_fuel_tank_selector.4=1 [AIRPLANE_GEOMETRY] wing_area = 1370//aircraft.cfg wing_span = 117.83//aircraft.cfg wing_root_chord = 18.9//aircraft.cfg wing_camber = 1 wing_thickness_ratio = 0.05 wing_dihedral = 6.2//aircraft.cfg wing_incidence = 1//aircraft.cfg wing_twist = -0.5//aircraft.cfg oswald_efficiency_factor = 0.74//aircraft.cfg wing_winglets_flag = 1//aircraft.cfg wing_sweep = 25.3//aircraft.cfg wing_pos_apex_lon = 9.28//aircraft.cfg wing_pos_apex_vert = -3//aircraft.cfg htail_area = 282.3//352.84//aircraft.cfg htail_span = 47.1//aircraft.cfg htail_pos_lon = -50.8//aircraft.cfg htail_pos_vert = 6.2//aircraft.cfg htail_incidence = 3.0//aircraft.cfg htail_sweep = 30.0//aircraft.cfg htail_thickness_ratio = 0.1 vtail_area = 284.0//aircraft.cfg vtail_span = 23.5//aircraft.cfg vtail_sweep = 35.0//aircraft.cfg vtail_pos_lon = -58.8//aircraft.cfg vtail_pos_vert = 12.6//aircraft.cfg vtail_thickness_ratio = 0.1 fuselage_length = 112 fuselage_diameter = 13 fuselage_center_pos = -7,0,5 elevator_area = 70.5//aircraft.cfg aileron_area = 26.9//aircraft.cfg rudder_area = 56.2//aircraft.cfg elevator_up_limit = 22.5//aircraft.cfg elevator_down_limit = 19.5//aircraft.cfg aileron_up_limit = 20.0//aircraft.cfg aileron_down_limit = 20.0//aircraft.cfg rudder_limit = 26.0//aircraft.cfg rudder_trim_limit = 10.0 elevator_trim_limit = 17.1//aircraft.cfg spoiler_limit = 60.0//aircraft.cfg spoiler_extension_time = 2.0//aircraft.cfg spoiler_handle_available = 1 auto_spoiler_available = 0//aircraft.cfg auto_spoiler_auto_retracts = 0 auto_spoiler_min_speed = 0 positive_g_limit_flaps_up = 4.0//aircraft.cfg positive_g_limit_flaps_down = 3.0//aircraft.cfg negative_g_limit_flaps_up = -3.0//aircraft.cfg negative_g_limit_flaps_down = -2.0//aircraft.cfg load_safety_factor = 1.5//aircraft.cfg spoilerons_available = 1//aircraft.cfg aileron_to_spoileron_gain = 1.5//aircraft.cfg min_ailerons_for_spoilerons = 10//aircraft.cfg min_flaps_for_spoilerons = 0//aircraft.cfg elevator_trim_neutral = 0 aileron_to_rudder_scale = 0 flap_to_aileron_scale = 0 fly_by_wire = 0 aileron_to_elevator_gain = 0 air_spoiler_limit = 60 spoiler_disabled_by_flaps = 0 fly_by_wire_from_flaps = 0 controls_reactivity_scalar = 0 ////////////////////////////////////////////////////////////////////////////////////////////////////////////// elevator_trim_elasticity_table = 0:0.7, 100:0.8, 250:0.7, 800:0.4, 1500:0.15 elevator_elasticity_table = 0:0.7, 80:0.9, 160:1.0, 250:0.9, 400:0.75 //0:0.6, 60:0.8, 120:0.9, 200:0.85, 400:0.7 aileron_elasticity_table = 0:0.7, 90:0.9, 180:1.0, 280:0.95, 400:0.85 //0:0.6, 70:0.8, 150:0.9, 250:0.95, 400:0.85 rudder_elasticity_table = 0:0.6, 100:0.8, 180:0.9, 280:0.8, 600:0.65, 1500:0.25 //0:0.5, 80:0.7, 150:0.9, 250:0.8, 600:0.6, 1500:0.2 //////////////////////////////////////////////////////////////////////////////////////////////////////////////// [AERODYNAMICS] //Table 341 elevator_scaling_table=-0.758:1.000000, -0.524000:0.900000, -0.175000:0.800000, 0.000000:0.700000, 0.175000:0.800000, 0.524000:0.900000, 0.785000:1.000000 //Table 342 aileron_scaling_table=-0.785000:1.000000, -0.524000:1.000000, -0.175000:0.975000, 0.000000:0.700000, 0.175000:0.975000, 0.524000:1.000000, 0.785000:1.000000 //Table 343 rudder_scaling_table=-0.785000:1.000000, -0.524000:1.000000, -0.175000:0.975000, 0.000000:0.900000, 0.175000:0.975000, 0.524000:1.000000, 0.785000:1.000000 //Table 400 lift_coef_ground_effect_mach_table=0.054000:1.060000, 0.100000:1.051500, 0.200000:1.039000, 0.300000:1.030000, 0.400000:1.024000, 0.500000:1.018000, 0.600000:1.013500, 0.700000:1.010000, 0.800000:1.006000, 0.900000:1.003000, 1.000000:1.00000 //Table 401 lift_coef_mach_table=0.000000:1.000000, 0.200000:1.020000, 0.400000:1.050000, 0.600000:1.115000, 0.800000:1.246000, 1.000000:1.180000, 1.200000:0.672100, 1.400000:0.434000, 1.600000:0.295200, 1.800000:0.235700, 2.000000:0.186400, 2.200000:0.156800, 2.400000:0.148100, 2.600000:0.137300, 2.800000:0.127400, 3.000000:0.127400, 3.200000:0.327400 //Table 404/1545 lift_coef_aoa_table=-3.141593:-0.000000, -2.792527:0.360000, -2.356194:0.500000, -1.919862:0.360000, -0349066:-0.400000, -0.087266:-0.250000, -0.034907:-0.020000, 0.034907:0.345000, 0.174533:1.060000, 0.226893:1.300000, 0.261799:1.450000, 0.296706:1.490000, 0.331613:1.490000, 0.383972:1.450000, 0.575959:0.200000, 1.570000:-0.080000, 1.960000:-0.140000, 2.360000:-0.200000, 3.140000:0.000000 //Table 430 drag_coef_zero_lift_mach_tab=0.000000:0.000000, 0.200000:0.000970, 0.400000:0.002440, 0.600000:0.004390, 0.800000:0.006830, 1.000000:0.039060, 1.200000:0.06250, 1.400000:0.047360, 1.600000:0.041010, 1.800000:0.036620, 2.000000:0.036620, 2.200000:0.036620, 2.400000:0.036620, 2.600000:0.036620, 2.800000:0.036620, 3.000000:0.036620, 3.200000:0.036620 //Table 410 lift_coef_delta_elevator_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:-0.010250, 0.600000:-0.040030, 0.800000:-0.120110, 1.000000:-0.120110, 1.200000:-0.100147, 1.400000:-0.080117, 1.600000:-0.060088, 1.800000:-0.040059, 2.000000:-0.020029, 2.200000:-0.020029, 2.400000:-0.020029, 2.600000:-0.020029, 2.800000:-0.020029, 3.000000:-0.020029, 3.200000:-0.020029 //Table 411 lift_coef_daoa_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.200190, 0.600000:0.500000, 0.800000:1.100090, 1.000000:1.700190, 1.200000:1.100090, 1.400000:0.500000, 1.600000:0.200190, 1.800000:0.200190, 2.000000:0.200190, 2.200000:0.200190, 2.400000:0.200190, 2.600000:0.200190, 2.800000:0.200190, 3.000000:0.200190, 3.200000:0.200190 //Table 412 lift_coef_pitch_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:-0.200190, 0.600000:-0.500000, 0.800000:-1.200190, 1.000000:-1.200190, 1.200000:-0.500000, 1.400000:-0.200190, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 413 lift_coef_horizontal_incidence_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.009760, 0.600000:0.040030, 0.800000:0.160150, 1.000000:0.160150, 1.200000:0.160150, 1.400000:0.160150, 1.600000:0.160150, 1.800000:0.160150, 2.000000:0.160150, 2.200000:0.160150, 2.400000:0.160150, 2.600000:0.160150, 2.800000:0.160150, 3.000000:0.160150, 3.200000:0.160150 //Table 420 pitch_moment_delta_elevator_mach_table=0.000000:0.000000, 0.200000:0.067870, 0.400000:0.135740, 0.600000:0.203610, 0.800000:0.303710, 1.000000:0.403800, 1.200000:0.403800, 1.400000:0.403800, 1.600000:0.403800, 1.800000:0.403800, 2.000000:0.403800, 2.200000:0.403800, 2.400000:0.403800, 2.600000:0.403800, 2.800000:0.403800, 3.000000:0.403800, 3.200000:0.403800 //Table 421 pitch_moment_daoa_mach_table=0.000000:0.000000, 0.200000:0.024900, 0.400000:0.100090, 0.600000:0.274900, 0.800000:0.750000, 1.000000:1.000000, 1.200000:0.000000, 1.400000:-3.000000, 1.600000:-4.000000, 1.800000:-4.500000, 2.000000:-5.000000, 2.200000:-5.000000, 2.400000:-5.000000, 2.600000:-5.000000, 2.800000:-5.000000, 3.000000:-5.000000, 3.200000:-5.000000 //Table 422 pitch_moment_pitch_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:-0.062500, 0.600000:-0.125000, 0.800000:-0.187500, 1.000000:-0.250000, 1.200000:-0.187500, 1.400000:-0.125000, 1.600000:-0.062500, 1.800000:0.000000, 2.000000:0.125000, 2.200000:0.250000, 2.400000:0.250000, 2.600000:0.250000, 2.800000:0.250000, 3.000000:0.250000, 3.200000:0.250000 //Table 423 pitch_moment_horizontal_incidence_mach_table=0.000000:0.000000, 0.200000:0.049800, 0.400000:0.100090, 0.600000:0.200190, 0.800000:0.500000, 1.000000:0.350090, 1.200000:0.350090, 1.400000:0.350090, 1.600000:0.350090, 1.800000:0.350090, 2.000000:0.350090, 2.200000:0.350090, 2.400000:0.350090, 2.600000:0.350090, 2.800000:0.350090, 3.000000:0.350090, 3.200000:0.350090 //Table 433 pitch_moment_aoa_0_mach_table=0.000000:0.000000, 0.200000:0.000480, 0.400000:0.000970, 0.600000:0.001950, 0.800000:0.003900, 1.000000:0.024410, 1.200000:0.012200, 1.400000:0.009760, 1.600000:0.009760, 1.800000:0.009760, 2.000000:0.009760, 2.200000:0.009760, 2.400000:0.009760, 2.600000:0.009760, 2.800000:0.009760, 3.000000:0.009760, 3.200000:0.009760 //Table 440 side_force_slip_angle_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 441 side_force_delta_rudder_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:-0.004880, 1.000000:-0.004880, 1.200000:-0.004880, 1.400000:-0.004880, 1.600000:-0.004880, 1.800000:-0.004880, 2.000000:-0.004880, 2.200000:-0.004880, 2.400000:-0.004880, 2.600000:-0.004880, 2.800000:-0.004880, 3.000000:-0.004880, 3.200000:-0.004880 //Table 442 side_force_yaw_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 443 side_force_roll_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 450 roll_moment_slip_angle_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 451 roll_moment_slip_angle_aoa_table=-180.000000:1.000000, -90.000000:0.200000, -18.000000:0.560000, -10.000000:0.940000, 0.000000:1.000000, 10.000000:0.950000, 18.000000:0.560000, 90.000000:0.200000, 180.000000:1.000000 //Table 452 roll_moment_delta_rudder_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 453 roll_moment_delta_aileron_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:-0.004880, 0.600000:-0.010250, 0.800000:-0.020010, 1.000000:-0.024900, 1.200000:-0.024900, 1.400000:-0.024900, 1.600000:-0.024900, 1.800000:-0.024900, 2.000000:-0.024900, 2.200000:-0.024900, 2.400000:-0.024900, 2.600000:-0.024900, 2.800000:-0.024900, 3.000000:-0.024900, 3.200000:-0.024900 //Table 454 roll_moment_yaw_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 455 roll_moment_roll_rate_mach_table=0.000000:0.000000, 0.200000:-0.004880, 0.400000:-0.020010, 0.600000:-0.049800, 0.800000:-0.100090, 1.000000:-0.109860, 1.200000:-0.109860, 1.400000:-0.109860, 1.600000:-0.109860, 1.800000:-0.109860, 2.000000:-0.109860, 2.200000:-0.109860, 2.400000:-0.109860, 2.600000:-0.109860, 2.800000:-0.109860, 3.000000:-0.109860, 3.200000:-0.109860 //Table 456 roll_moment_roll_rate_aoa_table=-180.000000:1.000000, -90.000000:0.300000, -18.000000:0.400000, -10.000000:0.650000, 0.000000:1.000000, 10.000000:0.650000, 18.000000:0.400000, 90.000000:0.300000, 180.000000:1.000000 //Table 459 yaw_moment_slip_angle_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 460 yaw_moment_slip_angle_aoa_table=-180.000000:1.000000, -90.000000:0.000000, -18.000000:0.200000, -10.000000:0.300000, 0.000000:1.000000, 10.000000:0.300000, 18.000000:0.200000, 90.000000:0.000000, 180.000000:1.000000 //Table 461 yaw_moment_delta_rudder_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 462 yaw_moment_delta_aileron_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:-0.000970, 0.600000:-0.001950, 0.800000:-0.002920, 1.000000:-0.002920, 1.200000:-0.002920, 1.400000:-0.002920, 1.600000:-0.002920, 1.800000:-0.002920, 2.000000:-0.002920, 2.200000:-0.002920, 2.400000:-0.002920, 2.600000:-0.002920, 2.800000:-0.002920, 3.000000:-0.002920, 3.200000:-0.002920 //Table 463 yaw_moment_yaw_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 464 yaw_moment_yaw_rate_aoa_table=-180.000000:1.000000, -90.000000:0.100000, -18.000000:0.700000, -10.000000:0.930000, 0.000000:1.000000, 10.000000:0.960000, 18.000000:0.700000, 90.000000:0.100000, 180.000000:1.000000 //Table 465 yaw_moment_roll_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 473/1546 pitch_moment_aoa_table=-3.141593:0.000000, -1.047198:-0.031416, -0.436332:-0.031416, -0.383972:-0.017453, -0.349066:-0.013090, -0.279253:-0.008727, 0.000000:0.000000, 0.279253:0.008727, 0.349066:0.013090, 0.383972:0.017453, 0.436332:0.031416, 1.047198:0.031416, 3.141593:0.000000 //Table 536 pitch_moment_delta_elevator_aoa_table=-25.000000:0.100000, -12.000000:1.000000, 12.000000:1.000000, 16.000000:0.560600, 25.000000:0.100000 //Table 537 pitch_moment_horizontal_incidence_aoa_table=0.000000:1.000000 //Table 538 pitch_moment_daoa_aoa_table=0.000000:1.000000 //Table 539 pitch_moment_pitch_alpha_table=0.000000:1.000000 //Table 546 aileron_load_factor_effectiveness_table=0.000000:1.000000 //Table 1101 lift_coef_pitch_rate=-10.25390625//Table 1101, CL_q lift_coef_daoa=2.197265625//Table 1101, CL_adot lift_coef_delta_elevator=-0.3564453125//Table 1101, CL_de lift_coef_horizontal_incidence=-1.46484375//Table 1101, CL_dh lift_coef_flaps=1.234000//Table 1101, CL_df lift_coef_spoilers=-0.045000//Table 1101, CL_ds lift_coef_air_spoilers=-0.045000//New lift_coef_at_drag_zero_flaps=0//New lift_coef_at_drag_zero=0//New drag_coef_zero_lift=0.02001953125//Table 1101, Cd0 drag_coef_flaps=0.0732421875//Table 1101, Cd_df drag_coef_gear=0.029296875//Table 1101, Cd_dg drag_coef_spoilers=0.01708984375//Table 1101, Cd_ds drag_coef_air_spoilers=0.01708984375//New side_force_slip_angle=-0.1220703125//Table 1101, CY_beta side_force_roll_rate=0.0146484375//Table 1101, CY_p side_force_yaw_rate=0//Table 1101, CY_r side_force_delta_rudder=-0.15869140625//Table 1101, CY_dr pitch_moment_horizontal_incidence=-6.591796875//Table 1101, Cm_dh pitch_moment_delta_elevator=-0.9765625//Table 1101, Cm_de pitch_moment_delta_trim=-2.0//Table 1101, Cm_dt //////////////////////////////////////////// pitch_moment_pitch_damping=-95.0 ; -120.0 /////////////////////////////////////////// pitch_moment_aoa_0=0.00//Table 1101, Cmo pitch_moment_daoa=9.27734375//Table 1101, Cm_adot pitch_moment_flaps=0.015//Table 1101, Cm_df pitch_moment_gear=0.0030//Table 1101, Cm_dg pitch_moment_spoilers=-0.005//Table 1101, Cm_ds pitch_moment_delta_elevator_propwash=0//Table 1101, Cm_de pitch_moment_pitch_propwash=-0.01//Table 1101, Cm_q roll_moment_slip_angle=0.0732421875//Table 1101, Cl_beta //////////////////////////////////////////////////////////////////// roll_moment_roll_damping=-1.2 ;-1.8 ///////////////////////////////////////////////////////////////////// roll_moment_yaw_rate=-0.01953125//Table 1101, Cl_r roll_moment_spoilers=0.050000//Table 1101, Cl_adot roll_moment_delta_aileron=-0.1953125//Table 1101, Cl_da roll_moment_delta_rudder=0.01953125//Table 1101, Cl_dr roll_moment_delta_aileron_trim_scalar=-0.2//Table 516 yaw_moment_slip_angle=0.1708984375//Table 1101, Cn_beta yaw_moment_roll=0.03662109375//Table 1101, Cn_p //////////////////////////////////////////////////////////////////////// yaw_moment_yaw_damping=-1.2 //-1.8 ///////////////////////////////////////////////////////////////////////// yaw_moment_yaw_propwash=0//Table 1101, damping yaw_moment_delta_aileron=-0.009765625//Table 1101, Cn_da yaw_moment_delta_rudder=0.1220703125//Table 1101, Cn_dr yaw_moment_delta_rudder_propwash=0//Table 1101, Cn_dp yaw_moment_delta_rudder_trim_scalar=0.0 //Table 1534 aero_center_lift=-6.5 compute_aero_center=0 //Table 1535 roll_moment_delta_aileron_aoa_table=-15.000000:1.100000, 0.000000:1.000000, 13.000000:0.700000, 16.000000:0.550000, 20.000000:0.050000 //Table 1536 yaw_moment_delta_rudder_aoa_table=-15.000000:1.100000, 0.000000:1.000000, 13.000000:0.700000, 16.000000:0.550000, 20.000000:0.050000 //Table 1537 yaw_moment_aoa_table=0.000000:0.000000 //Table 1538 roll_moment_aoa_table=0.000000:0.000000 elevator_lift_coef = 1.0 rudder_lift_coef = 1.5 aileron_up_drag_coef = 0.4 aileron_down_drag_coef = 1.0 fuselage_lateral_cx = 0.4 presspt_fwd_Alpha0_pMAC=0 presspt_fwd_AlphaStall_pMAC=0 presspt_fwd_AlphaHiStall_pMAC=-0.25 [FLIGHT_TUNING] modern_fm_only = 1 /////////////////////////////////////////////////// cruise_lift_scalar = 1.0 /1.17//aircraft.cfg parasite_drag_scalar = 0.95 //1.0 induced_drag_scalar = 1.25 //1.33//aircraft.cfg //////////////////////////////////////////////////// flap_induced_drag_scalar = 1.2 /1.0 elevator_effectiveness = 0.95 //1.0//aircraft.cfg elevator_maxangle_scalar = 1.0//aircraft.cfg /////////////////////////////////////////////////// aileron_effectiveness = 1.15 /1.0//aircraft.cfg //////////////////////////////////////////////////// rudder_effectiveness = 1.0//aircraft.cfg rudder_maxangle_scalar = 0.55//aircraft.cfg ////////////////////////////////////////////////////////// pitch_stability = 3.5 //5.0 roll_stability = 1.2 //1.85 yaw_stability = 2.5 //4.0 ///////////////////////////////////////////////////////// pitch_gyro_stability = 2.0 roll_gyro_stability = 2.0 yaw_gyro_stability = 2.0 ////////////////////////////////////////////////////// elevator_trim_effectiveness = 1.025 //1.19 /////////////////////////////////////////////////////// aileron_trim_effectiveness = 1.0//aircraft.cfg rudder_trim_effectiveness = 1.0//aircraft.cfg hi_alpha_on_roll = 1.0 hi_alpha_on_yaw = 1.0 p_factor_on_yaw = 0.0 ///////////////////////////////////////////////////////// gyro_precession_on_yaw = 0.3 //0.5 gyro_precession_on_pitch=0.3 //0.5 ///////////////////////////////////////////////////////// wingflex_scalar = 1.08 wingflex_offset = 0.0 wingflex_surface_scalar =0.0 stall_coef_at_min_weight = 0.5 icing_scalar=0.32 elevator_chordangle_scalar=-1 htail_maxangle_scalar=-1 rudder_chordangle_scalar=-1 vtail_maxangle_scalar=-1 ground_high_speed_steeringwheel_static_friction_scalar=3.0 ground_high_speed_otherwheel_static_friction_scalar=2.5 [REFERENCE SPEEDS] full_flaps_stall_speed = 113//aircraft.cfg flaps_up_stall_speed = 142//aircraft.cfg cruise_speed = 477//aircraft.cfg cruise_mach = 0.785 crossover_speed = 0 max_mach = 0.82//aircraft.cfg max_indicated_speed = 340//aircraft.cfg max_flaps_extended = 250 normal_operating_speed = 310 airspeed_indicator_max = 450 rotation_speed_min = 95 climb_speed = 285 cruise_alt = 38000 takeoff_speed = 120 spawn_cruise_altitude = 5000 spawn_descent_altitude = 500 best_angle_climb_speed = 235 approach_speed = 135 best_glide = 220 max_gear_extended = 270 fly_assistant_use_dynamic_speeds = 0 [INTERACTIVE POINTS] number_of_interactive_points=9 interactive_point.0=0.400 , 40.4682,-5.4437, -1.5939, 0, 0.000000, 0.000000, -90.000000, 72, 16, 85, 3, -2, 33 // 0,Main exit-FWD Entry interactive_point.1=0.400 , 28.9189, 2.4250, -6.1920, 1, 0.000000, 0.000000, 90.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 1, Cargo exit/door-FWD Cargo interactive_point.2=0.400 , -47.6151, 4.5654, -1.5939, 0, 0.000000, 0.000000, 97.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 0, Main exit-AFT Service interactive_point.3=0.400 , 53.391604, 13.130946, -7.89732, 4, 0.000000, 0.000000, 45.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 4, Ground Power cable interactive_point.4=0.400 , -0.699505, 38.227005, -6.163185, 3, 0.000000, 0.000000, 90.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 3, Fuel hose interactive_point.5=0.400 , 7.72833, 0.00, -6.9299, 5, 0.000000, 0.000000, 90.000000 , 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 5, Air Start Unit interactive_point.6=0.400 , 41.6, 5.37906, -1.5939, 0, 0.000000, 0.000000, 97.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 0, Main exit-FWD Service interactive_point.7=0.400 , -47.6151, -4.5654, -1.5939, 0, 0.000000, 0.000000, 97.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 0, Main exit-AFT Entry interactive_point.8=0.400 , -34.6622, 2.4250, -6.1920, 1, 0.000000, 0.000000, 90.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 1, Cargo exit/door-AFT Cargo [STALL PROTECTION] stall_protection = 0 off_limit = 0 off_yoke_limit = 0 on_limit = 0 on_goal = 0 timer_trigger = 0 [FLAPS.0] type = 1//aircraft.cfg system_type = 1//aircraft.cfg system_type_index = 0 span-outboard = 0.8//aircraft.cfg extending-time = 27//aircraft.cfg damaging-speed = 250//aircraft.cfg blowout-speed = 300//aircraft.cfg maneuvering_flaps = 0 lift_scalar = 0.0//aircraft.cfg drag_scalar = 0.0//aircraft.cfg pitch_scalar = 0.0//aircraft.cfg max_on_ground_position = 8 delay_between_flap_index = 0 altitude-limit = -1 // flap position airspeed limit drag scalar, lift scalar, area scalar, add camber, add aft feet, add incidence flaps-position.0= 0.0, -1, 0.00000, 0.00000, 1, 0, 0.00, 0// 0 flaps-position.1= 1.0, 250, 0.00000, 0.00000, 1, 0, 0.00, 0// 1 flaps-position.2= 2.0, 250, 0.00000, 0.00000, 1, 0, 0.00, 0// 2 flaps-position.3= 5.0, 250, 0.00000, 0.00000, 1, 0, 0.00, 0// 5 flaps-position.4= 10.0, 210, 0.00000, 0.00000, 1, 0, 0.00, 0// 10 flaps-position.5= 15.0, 200, 0.00000, 0.00000, 1, 0, 0.00, 0// 15 flaps-position.6= 25.0, 190, 0.00000, 0.00000, 1, 0, 0.00, 0// 25 flaps-position.7= 30.0, 175, 0.00000, 0.00000, 1, 0, 0.00, 0// 30 flaps-position.8= 40.0, 166, 0.00000, 0.00000, 1, 0, 0.00, 0// 40 [FLAPS.1] type = 1//aircraft.cfg system_type = 1//aircraft.cfg system_type_index = 0 span-outboard = 0.8//aircraft.cfg extending-time = 27//aircraft.cfg damaging-speed = 250//aircraft.cfg blowout-speed = 300//aircraft.cfg maneuvering_flaps = 0 lift_scalar = 1.0//aircraft.cfg drag_scalar = 1.0//aircraft.cfg pitch_scalar = 1.0//aircraft.cfg max_on_ground_position = 8 delay_between_flap_index = 0 altitude-limit = -1 // flap position airspeed limit drag scalar, lift scalar, area scalar, add camber, add aft feet, add incidence flaps-position.0= 0.0, -1, 0.00000, 1.00000, 1, 0, 0.00, 0// 0 flaps-position.1= 7.5, 250, 0.10000, 1.00000, 1, 0, 0.00, 0// 1 flaps-position.2= 10.8, 250, 0.20000, 1.00000, 1, 0, 0.00, 0// 2 flaps-position.3= 14.9, 250, 0.30000, 1.10000, 1, 0, 0.00, 0// 5 flaps-position.4= 17.9, 210, 0.70000, 1.15000, 1, 0, 0.00, 0// 10 flaps-position.5= 23.0, 200, 1.00000, 1.20000, 1, 0, 0.00, 0// 15 flaps-position.6= 29.5, 190, 1.05000, 1.25000, 1, 0, 0.00, 0// 25 flaps-position.7= 32.5, 175, 1.10000, 1.35000, 1, 0, 0.00, 0// 30 flaps-position.8= 40.0, 166, 1.15000, 1.45000, 1, 0, 0.00, 0// 40 [FLAPS.2] type = 2//aircraft.cfg system_type = 1//aircraft.cfg system_type_index = 0 span-outboard = 0.8//aircraft.cfg extending-time = 7//aircraft.cfg damaging-speed = 250//aircraft.cfg blowout-speed = 300//aircraft.cfg maneuvering_flaps = 0 lift_scalar = 0.1//aircraft.cfg drag_scalar = 1.0//aircraft.cfg pitch_scalar = 0.0//aircraft.cfg max_on_ground_position = 8 delay_between_flap_index = 0 altitude-limit = -1 // flap position airspeed limit drag scalar, lift scalar, area scalar, add camber, add aft feet, add incidence flaps-position.0= 0.0, -1, 0.00000, 1.00000, 1, 0, 0.00, 0// 0 flaps-position.1= 5.0, 250, 0.15000, 1.05000, 1, 0, 0.00, 0// 1 flaps-position.2= 10.0, 250, 0.25000, 1.10000, 1, 0, 0.00, 0// 2 flaps-position.3= 20.0, 250, 0.45000, 1.10000, 1, 0, 0.00, 0// 5 flaps-position.4= 20.0, 210, 0.75000, 1.10000, 1, 0, 0.00, 0// 10 flaps-position.5= 20.0, 200, 0.95000, 1.10000, 1, 0, 0.00, 0// 15 flaps-position.6= 20.0, 190, 0.95000, 1.10000, 1, 0, 0.00, 0// 25 flaps-position.7= 20.0, 175, 0.95000, 1.10000, 1, 0, 0.00, 0// 30 flaps-position.8= 20.0, 166, 0.95000, 1.10000, 1, 0, 0.00, 0// 40 Edited August 22, 2025Aug 22 by LRBS 747 Captain for the last 39 years, and still learning.
August 22, 2025Aug 22 Are some of the AI and ATC voices new? Sounds like some of the other aircraft are talking through a tin can on a string (I think that's how some of the value airlines still do it) 🙂 ------------------------- Craig from KBUF
August 22, 2025Aug 22 14 hours ago, Jeff Nielsen said: Something has regressed. I used to be stutter free. Now it's just horrible. This is getting ridiculous. You want the good news or the bad news? Pending on what hardware setup you have it can be both good news ... or you may look at it as bad news. Probably not going to like what I have to report ... so you thought 64GB RAM would be enough? Think again ... LEMG (MK) + FSLabs A32x + GSX + AIG = 65.5 GB RAM (can see an FPS drop around the FSLabs A32x. Verified with Task Manager 63.3 GB used out of my 96 GB ... I don't know your graphics settings, but I'm using the same as before TAA=200 everything on Ultra. Slightly less RAM used with A2A Aerostar 600 - 59.3GB: I don't know if your hardware signature is still accurate, but if you are running 64GB RAM, then it's very likely you are swapping to disk which will cause significant stutters. I seem to recall a video somewhere on YouTube where MSFS 2024 performed better with 96GB of RAM which is why I went that route. Sorry don't have the FNX A320, but from my testing the RAM usage seems to be the issue not the aircraft selected as the A2A was 59GB and FSLabs 65GB. Rob. Extraordinary claims require extraordinary evidence. - Carl Sagan
August 22, 2025Aug 22 45 fps and stuttering with a 5090? Also: 7800X3D | 2x32 GB DDR5-6000 CL32 | RTX 5080 | Alienware OLED 34" | 1 Gbps fiber
August 22, 2025Aug 22 23 minutes ago, LRBS said: Try this and see if it is what you are looking for Ifly: [VERSION] major = 1 minor = 0 [WEIGHT_AND_BALANCE] max_gross_weight = 181700 ; Empty weight, (LBS) empty_weight = 99360 ; Empty weight, (LBS) reference_datum_position = 0,0,0 ; Position of reference datum relative to FS(0,0,0) (FEET), z, x, y empty_weight_CG_position = -6.171,0,0 ; Position of airplane empty weight CG relative to reference datum (FEET), z, x, y CG_forward_limit = 0.0 ; Gravity center forward limit (longitudinal offset) for longitudinal stability CG_aft_limit = 1.0 ; Gravity center after limit (longitudinal offset z) w.r.t reference datum for longitudinal stability (FEET) empty_weight_pitch_MOI = 3000000 ; 2148488 ; Empty pitch moment of inertia, Jxx (SLUG SQ FEET) empty_weight_roll_MOI = 1600000 ; 1470096 ; Empty roll moment of inertia, Jzz (SLUG SQ FEET) empty_weight_yaw_MOI = 1600000 ; Empty yaw moment of inertia, Jyy (SLUG SQ FEET) empty_weight_coupled_MOI = 0 ; Empty transverse moment of inertia, Jyz (SLUG SQ FEET) activate_mach_limit_based_on_cg = 0 ; Activate mach limitation depending on CG position (true if > 0 /false othewise). Mostly for Concorde). activate_cg_limit_based_on_mach = 0 ; Activate cg limitation depending on mach value (true if > 0 /false othewise). Mostly for Concorde). max_number_of_stations = 13 ; Number of payload stations station_load.0=220, 28.82, 0, 1, Pilot, 1 station_load.1=400, 25.10, 0, 1, FA fwd, 0 station_load.2=400, -29.38, 0, 1, FA aft, 0 station_load.3=2341, 18.91, 0, 1, PAX A, 3 station_load.4=5853, 6.10, 0, 1, PAX B, 3 station_load.5=1171, -6.28, 0, 1, PAX C, 3 station_load.6=3317, -10.00, 0, 1, PAX D, 3 station_load.7=3512, -13.00, 0, 1, PAX E, 3 station_load.8=3902, -18.00, 0, 1, PAX F, 3 station_load.9=2536, -22.30, 0, 1, PAX G, 3 station_load.10=5752, 12.10, 0, 1, Cargo fwd, 6 station_load.11=8018, -17.00, 0, 1, Cargo aft, 6 station_load.12=220, 28.82, 0, 1, Co-Pilot, 2 station_name.0=Pilot station_name.1=FA fwd station_name.2=FA aft station_name.3=PAX A station_name.4=PAX B station_name.5=PAX C station_name.6=PAX D station_name.7=PAX E station_name.8 =PAX F station_name.9 =PAX G station_name.10=Cargo fwd station_name.11=Cargo aft station_name.12=Co-Pilot [CONTACT_POINTS] static_pitch = -0 ; degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height = 11.7 ; feet, altitude of CG when at rest on the ground gear_system_type = 1 ; gear system type (betweeen 0 and 4) 0 = electrical, 1 = hydraulic, 2 = pneumatic, 3 = manual, 4 = none, 5 = undefined max_number_of_points = 14 ; Number of contact points point.0 = 1, 43.60, 0.000, -11.435, 1181, 0, 1.1333, 50.0, 0.388373, 1.5929, 0.99, 8.0, 8.0, 0, 265.0, 315.0, 2 point.1 = 1, -8.25, -9.35, -12.55, 1575, 1, 1.85, 0, 1.13648, 1.17318, 0.650, 9.0, 9.0, 2, 265.0, 315.0, 2 point.2 = 1, -8.25, 9.35, -12.55, 1575, 2, 1.85, 0, 1.13648, 1.17318, 0.650, 9.0, 9.0, 3, 265.0, 315.0, 2 point.3 = 2, -25.00,-58.5,-2.00,350,0,0.0001,0,0.0001,0.0001,0,0,0,5,0,0,1 point.4 = 2, -25.00,58.5,-2.00,350,0,0.0001,0,0.0001,0.0001,0,0,0,6,0,0,1 point.5 = 2, 44.35,-0,2.234,350,0,0.0001,0,0.0001,0.0001,0,0,0,4,0,0,1 point.6 = 2, 30.599,0,-2.126,500,0,0.0001,0,0.0001,0.0001,0,0,0,4,0,0,1 point.7 = 2, 22.65,0,11.483,1,0,0.0001,0,0.0001,0.0001,0,0,0,4,0,0,1 point.8 = 2, 9.43,-15.82,-8.526,500,0,0.0001,0,0.0001,0.0001,0,0,0,5,0,0,1 point.9= 2, 9.43,15.82,-8.526,500,0,0.0001,0,0.0001,0.0001,0,0,0,6,0,0,1 point.10= 2,-32.26,-0,-2.126,500,0,0.0001,0,0.0001,0.0001,0,0,0,4,0,0,1 point.11= 2,-71.5,0,4.1,750,0,0.0001,0,0.0001,0.0001,0,0,0,9,0,0,1 point.12= 2,-68.83,0,30.441999,350,0,0.0001,0,0.0001,0.0001,0,0,0,9,0,0,1 point.13= 2,-56.54,0.00,-2.61,350,0,0.0001,0,0.0001,0.0001,0,0,0,9,0,0,1 tailwheel_lock = 0 ; Is tailwheel lock available TRUE/FALSE gear_locked_on_ground = 0 ; Defines whether or not the landing gear handle is locked to down when the plane is on the ground. gear_locked_above_speed = -1 ; Defines the speed at which the landing gear handle becomes locked in the up position. (-1 = Disabled) ///////////////////////////////////////////////////////////////////////// max_speed_full_steering = 10 max_speed_decreasing_steering = 60 min_available_steering_angle_pct = 0.1 steering_time_constants= 8, 8 allow_stopped_steering=1 //////////////////////////////////////////////////////////////////////// emergency_extension_type = 0 hyd_need_power_to_function = 0 locked_tailwheel_max_range = 0 [fuel] Center1 = -1.00, 0.0, -1.5, 4274, 1.2 LeftMain = -5.75, -16.0, -0.4, 1273, 2.2 RightMain = -5.75, 16.0, -0.4, 1273, 2.2 leftaux = 0, 0, 0, 0, 0 rightaux = 0, 0, 0, 0, 0 center2 = 0, 0, 0, 0, 0 center3 = 0, 0, 0, 0, 0 lefttip = 0, 0, 0, 0, 0 righttip = 0, 0, 0, 0, 0 external1 = 0, 0, 0, 0, 0 external2 = 0, 0, 0, 0, 0 fuel_type = 2 number_of_tank_selectors = 2 electric_pump=1 fuel_dump_rate = 0.0167 engine_driven_pump=1 manual_transfer_pump=0 manual_pump=0 anemometer_pump=0 default_fuel_tank_selector.1=1 default_fuel_tank_selector.2=1 default_fuel_tank_selector.3=1 default_fuel_tank_selector.4=1 [AIRPLANE_GEOMETRY] wing_area = 1370//aircraft.cfg wing_span = 117.83//aircraft.cfg wing_root_chord = 18.9//aircraft.cfg wing_camber = 1 wing_thickness_ratio = 0.05 wing_dihedral = 6.2//aircraft.cfg wing_incidence = 1//aircraft.cfg wing_twist = -0.5//aircraft.cfg oswald_efficiency_factor = 0.74//aircraft.cfg wing_winglets_flag = 1//aircraft.cfg wing_sweep = 25.3//aircraft.cfg wing_pos_apex_lon = 9.28//aircraft.cfg wing_pos_apex_vert = -3//aircraft.cfg htail_area = 282.3//352.84//aircraft.cfg htail_span = 47.1//aircraft.cfg htail_pos_lon = -50.8//aircraft.cfg htail_pos_vert = 6.2//aircraft.cfg htail_incidence = 3.0//aircraft.cfg htail_sweep = 30.0//aircraft.cfg htail_thickness_ratio = 0.1 vtail_area = 284.0//aircraft.cfg vtail_span = 23.5//aircraft.cfg vtail_sweep = 35.0//aircraft.cfg vtail_pos_lon = -58.8//aircraft.cfg vtail_pos_vert = 12.6//aircraft.cfg vtail_thickness_ratio = 0.1 fuselage_length = 112 fuselage_diameter = 13 fuselage_center_pos = -7,0,5 elevator_area = 70.5//aircraft.cfg aileron_area = 26.9//aircraft.cfg rudder_area = 56.2//aircraft.cfg elevator_up_limit = 22.5//aircraft.cfg elevator_down_limit = 19.5//aircraft.cfg aileron_up_limit = 20.0//aircraft.cfg aileron_down_limit = 20.0//aircraft.cfg rudder_limit = 26.0//aircraft.cfg rudder_trim_limit = 10.0 elevator_trim_limit = 17.1//aircraft.cfg spoiler_limit = 60.0//aircraft.cfg spoiler_extension_time = 2.0//aircraft.cfg spoiler_handle_available = 1 auto_spoiler_available = 0//aircraft.cfg auto_spoiler_auto_retracts = 0 auto_spoiler_min_speed = 0 positive_g_limit_flaps_up = 4.0//aircraft.cfg positive_g_limit_flaps_down = 3.0//aircraft.cfg negative_g_limit_flaps_up = -3.0//aircraft.cfg negative_g_limit_flaps_down = -2.0//aircraft.cfg load_safety_factor = 1.5//aircraft.cfg spoilerons_available = 1//aircraft.cfg aileron_to_spoileron_gain = 1.5//aircraft.cfg min_ailerons_for_spoilerons = 10//aircraft.cfg min_flaps_for_spoilerons = 0//aircraft.cfg elevator_trim_neutral = 0 aileron_to_rudder_scale = 0 flap_to_aileron_scale = 0 fly_by_wire = 0 aileron_to_elevator_gain = 0 air_spoiler_limit = 60 spoiler_disabled_by_flaps = 0 fly_by_wire_from_flaps = 0 controls_reactivity_scalar = 0 ////////////////////////////////////////////////////////////////////////////////////////////////////////////// elevator_trim_elasticity_table = 0:0.7, 100:0.8, 250:0.7, 800:0.4, 1500:0.15 elevator_elasticity_table = 0:0.7, 80:0.9, 160:1.0, 250:0.9, 400:0.75 //0:0.6, 60:0.8, 120:0.9, 200:0.85, 400:0.7 aileron_elasticity_table = 0:0.7, 90:0.9, 180:1.0, 280:0.95, 400:0.85 //0:0.6, 70:0.8, 150:0.9, 250:0.95, 400:0.85 rudder_elasticity_table = 0:0.6, 100:0.8, 180:0.9, 280:0.8, 600:0.65, 1500:0.25 //0:0.5, 80:0.7, 150:0.9, 250:0.8, 600:0.6, 1500:0.2 //////////////////////////////////////////////////////////////////////////////////////////////////////////////// [AERODYNAMICS] //Table 341 elevator_scaling_table=-0.758:1.000000, -0.524000:0.900000, -0.175000:0.800000, 0.000000:0.700000, 0.175000:0.800000, 0.524000:0.900000, 0.785000:1.000000 //Table 342 aileron_scaling_table=-0.785000:1.000000, -0.524000:1.000000, -0.175000:0.975000, 0.000000:0.700000, 0.175000:0.975000, 0.524000:1.000000, 0.785000:1.000000 //Table 343 rudder_scaling_table=-0.785000:1.000000, -0.524000:1.000000, -0.175000:0.975000, 0.000000:0.900000, 0.175000:0.975000, 0.524000:1.000000, 0.785000:1.000000 //Table 400 lift_coef_ground_effect_mach_table=0.054000:1.060000, 0.100000:1.051500, 0.200000:1.039000, 0.300000:1.030000, 0.400000:1.024000, 0.500000:1.018000, 0.600000:1.013500, 0.700000:1.010000, 0.800000:1.006000, 0.900000:1.003000, 1.000000:1.00000 //Table 401 lift_coef_mach_table=0.000000:1.000000, 0.200000:1.020000, 0.400000:1.050000, 0.600000:1.115000, 0.800000:1.246000, 1.000000:1.180000, 1.200000:0.672100, 1.400000:0.434000, 1.600000:0.295200, 1.800000:0.235700, 2.000000:0.186400, 2.200000:0.156800, 2.400000:0.148100, 2.600000:0.137300, 2.800000:0.127400, 3.000000:0.127400, 3.200000:0.327400 //Table 404/1545 lift_coef_aoa_table=-3.141593:-0.000000, -2.792527:0.360000, -2.356194:0.500000, -1.919862:0.360000, -0349066:-0.400000, -0.087266:-0.250000, -0.034907:-0.020000, 0.034907:0.345000, 0.174533:1.060000, 0.226893:1.300000, 0.261799:1.450000, 0.296706:1.490000, 0.331613:1.490000, 0.383972:1.450000, 0.575959:0.200000, 1.570000:-0.080000, 1.960000:-0.140000, 2.360000:-0.200000, 3.140000:0.000000 //Table 430 drag_coef_zero_lift_mach_tab=0.000000:0.000000, 0.200000:0.000970, 0.400000:0.002440, 0.600000:0.004390, 0.800000:0.006830, 1.000000:0.039060, 1.200000:0.06250, 1.400000:0.047360, 1.600000:0.041010, 1.800000:0.036620, 2.000000:0.036620, 2.200000:0.036620, 2.400000:0.036620, 2.600000:0.036620, 2.800000:0.036620, 3.000000:0.036620, 3.200000:0.036620 //Table 410 lift_coef_delta_elevator_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:-0.010250, 0.600000:-0.040030, 0.800000:-0.120110, 1.000000:-0.120110, 1.200000:-0.100147, 1.400000:-0.080117, 1.600000:-0.060088, 1.800000:-0.040059, 2.000000:-0.020029, 2.200000:-0.020029, 2.400000:-0.020029, 2.600000:-0.020029, 2.800000:-0.020029, 3.000000:-0.020029, 3.200000:-0.020029 //Table 411 lift_coef_daoa_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.200190, 0.600000:0.500000, 0.800000:1.100090, 1.000000:1.700190, 1.200000:1.100090, 1.400000:0.500000, 1.600000:0.200190, 1.800000:0.200190, 2.000000:0.200190, 2.200000:0.200190, 2.400000:0.200190, 2.600000:0.200190, 2.800000:0.200190, 3.000000:0.200190, 3.200000:0.200190 //Table 412 lift_coef_pitch_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:-0.200190, 0.600000:-0.500000, 0.800000:-1.200190, 1.000000:-1.200190, 1.200000:-0.500000, 1.400000:-0.200190, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 413 lift_coef_horizontal_incidence_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.009760, 0.600000:0.040030, 0.800000:0.160150, 1.000000:0.160150, 1.200000:0.160150, 1.400000:0.160150, 1.600000:0.160150, 1.800000:0.160150, 2.000000:0.160150, 2.200000:0.160150, 2.400000:0.160150, 2.600000:0.160150, 2.800000:0.160150, 3.000000:0.160150, 3.200000:0.160150 //Table 420 pitch_moment_delta_elevator_mach_table=0.000000:0.000000, 0.200000:0.067870, 0.400000:0.135740, 0.600000:0.203610, 0.800000:0.303710, 1.000000:0.403800, 1.200000:0.403800, 1.400000:0.403800, 1.600000:0.403800, 1.800000:0.403800, 2.000000:0.403800, 2.200000:0.403800, 2.400000:0.403800, 2.600000:0.403800, 2.800000:0.403800, 3.000000:0.403800, 3.200000:0.403800 //Table 421 pitch_moment_daoa_mach_table=0.000000:0.000000, 0.200000:0.024900, 0.400000:0.100090, 0.600000:0.274900, 0.800000:0.750000, 1.000000:1.000000, 1.200000:0.000000, 1.400000:-3.000000, 1.600000:-4.000000, 1.800000:-4.500000, 2.000000:-5.000000, 2.200000:-5.000000, 2.400000:-5.000000, 2.600000:-5.000000, 2.800000:-5.000000, 3.000000:-5.000000, 3.200000:-5.000000 //Table 422 pitch_moment_pitch_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:-0.062500, 0.600000:-0.125000, 0.800000:-0.187500, 1.000000:-0.250000, 1.200000:-0.187500, 1.400000:-0.125000, 1.600000:-0.062500, 1.800000:0.000000, 2.000000:0.125000, 2.200000:0.250000, 2.400000:0.250000, 2.600000:0.250000, 2.800000:0.250000, 3.000000:0.250000, 3.200000:0.250000 //Table 423 pitch_moment_horizontal_incidence_mach_table=0.000000:0.000000, 0.200000:0.049800, 0.400000:0.100090, 0.600000:0.200190, 0.800000:0.500000, 1.000000:0.350090, 1.200000:0.350090, 1.400000:0.350090, 1.600000:0.350090, 1.800000:0.350090, 2.000000:0.350090, 2.200000:0.350090, 2.400000:0.350090, 2.600000:0.350090, 2.800000:0.350090, 3.000000:0.350090, 3.200000:0.350090 //Table 433 pitch_moment_aoa_0_mach_table=0.000000:0.000000, 0.200000:0.000480, 0.400000:0.000970, 0.600000:0.001950, 0.800000:0.003900, 1.000000:0.024410, 1.200000:0.012200, 1.400000:0.009760, 1.600000:0.009760, 1.800000:0.009760, 2.000000:0.009760, 2.200000:0.009760, 2.400000:0.009760, 2.600000:0.009760, 2.800000:0.009760, 3.000000:0.009760, 3.200000:0.009760 //Table 440 side_force_slip_angle_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 441 side_force_delta_rudder_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:-0.004880, 1.000000:-0.004880, 1.200000:-0.004880, 1.400000:-0.004880, 1.600000:-0.004880, 1.800000:-0.004880, 2.000000:-0.004880, 2.200000:-0.004880, 2.400000:-0.004880, 2.600000:-0.004880, 2.800000:-0.004880, 3.000000:-0.004880, 3.200000:-0.004880 //Table 442 side_force_yaw_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 443 side_force_roll_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 450 roll_moment_slip_angle_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 451 roll_moment_slip_angle_aoa_table=-180.000000:1.000000, -90.000000:0.200000, -18.000000:0.560000, -10.000000:0.940000, 0.000000:1.000000, 10.000000:0.950000, 18.000000:0.560000, 90.000000:0.200000, 180.000000:1.000000 //Table 452 roll_moment_delta_rudder_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 453 roll_moment_delta_aileron_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:-0.004880, 0.600000:-0.010250, 0.800000:-0.020010, 1.000000:-0.024900, 1.200000:-0.024900, 1.400000:-0.024900, 1.600000:-0.024900, 1.800000:-0.024900, 2.000000:-0.024900, 2.200000:-0.024900, 2.400000:-0.024900, 2.600000:-0.024900, 2.800000:-0.024900, 3.000000:-0.024900, 3.200000:-0.024900 //Table 454 roll_moment_yaw_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 455 roll_moment_roll_rate_mach_table=0.000000:0.000000, 0.200000:-0.004880, 0.400000:-0.020010, 0.600000:-0.049800, 0.800000:-0.100090, 1.000000:-0.109860, 1.200000:-0.109860, 1.400000:-0.109860, 1.600000:-0.109860, 1.800000:-0.109860, 2.000000:-0.109860, 2.200000:-0.109860, 2.400000:-0.109860, 2.600000:-0.109860, 2.800000:-0.109860, 3.000000:-0.109860, 3.200000:-0.109860 //Table 456 roll_moment_roll_rate_aoa_table=-180.000000:1.000000, -90.000000:0.300000, -18.000000:0.400000, -10.000000:0.650000, 0.000000:1.000000, 10.000000:0.650000, 18.000000:0.400000, 90.000000:0.300000, 180.000000:1.000000 //Table 459 yaw_moment_slip_angle_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 460 yaw_moment_slip_angle_aoa_table=-180.000000:1.000000, -90.000000:0.000000, -18.000000:0.200000, -10.000000:0.300000, 0.000000:1.000000, 10.000000:0.300000, 18.000000:0.200000, 90.000000:0.000000, 180.000000:1.000000 //Table 461 yaw_moment_delta_rudder_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 462 yaw_moment_delta_aileron_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:-0.000970, 0.600000:-0.001950, 0.800000:-0.002920, 1.000000:-0.002920, 1.200000:-0.002920, 1.400000:-0.002920, 1.600000:-0.002920, 1.800000:-0.002920, 2.000000:-0.002920, 2.200000:-0.002920, 2.400000:-0.002920, 2.600000:-0.002920, 2.800000:-0.002920, 3.000000:-0.002920, 3.200000:-0.002920 //Table 463 yaw_moment_yaw_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 464 yaw_moment_yaw_rate_aoa_table=-180.000000:1.000000, -90.000000:0.100000, -18.000000:0.700000, -10.000000:0.930000, 0.000000:1.000000, 10.000000:0.960000, 18.000000:0.700000, 90.000000:0.100000, 180.000000:1.000000 //Table 465 yaw_moment_roll_rate_mach_table=0.000000:0.000000, 0.200000:0.000000, 0.400000:0.000000, 0.600000:0.000000, 0.800000:0.000000, 1.000000:0.000000, 1.200000:0.000000, 1.400000:0.000000, 1.600000:0.000000, 1.800000:0.000000, 2.000000:0.000000, 2.200000:0.000000, 2.400000:0.000000, 2.600000:0.000000, 2.800000:0.000000, 3.000000:0.000000, 3.200000:0.000000 //Table 473/1546 pitch_moment_aoa_table=-3.141593:0.000000, -1.047198:-0.031416, -0.436332:-0.031416, -0.383972:-0.017453, -0.349066:-0.013090, -0.279253:-0.008727, 0.000000:0.000000, 0.279253:0.008727, 0.349066:0.013090, 0.383972:0.017453, 0.436332:0.031416, 1.047198:0.031416, 3.141593:0.000000 //Table 536 pitch_moment_delta_elevator_aoa_table=-25.000000:0.100000, -12.000000:1.000000, 12.000000:1.000000, 16.000000:0.560600, 25.000000:0.100000 //Table 537 pitch_moment_horizontal_incidence_aoa_table=0.000000:1.000000 //Table 538 pitch_moment_daoa_aoa_table=0.000000:1.000000 //Table 539 pitch_moment_pitch_alpha_table=0.000000:1.000000 //Table 546 aileron_load_factor_effectiveness_table=0.000000:1.000000 //Table 1101 lift_coef_pitch_rate=-10.25390625//Table 1101, CL_q lift_coef_daoa=2.197265625//Table 1101, CL_adot lift_coef_delta_elevator=-0.3564453125//Table 1101, CL_de lift_coef_horizontal_incidence=-1.46484375//Table 1101, CL_dh lift_coef_flaps=1.234000//Table 1101, CL_df lift_coef_spoilers=-0.045000//Table 1101, CL_ds lift_coef_air_spoilers=-0.045000//New lift_coef_at_drag_zero_flaps=0//New lift_coef_at_drag_zero=0//New drag_coef_zero_lift=0.02001953125//Table 1101, Cd0 drag_coef_flaps=0.0732421875//Table 1101, Cd_df drag_coef_gear=0.029296875//Table 1101, Cd_dg drag_coef_spoilers=0.01708984375//Table 1101, Cd_ds drag_coef_air_spoilers=0.01708984375//New side_force_slip_angle=-0.1220703125//Table 1101, CY_beta side_force_roll_rate=0.0146484375//Table 1101, CY_p side_force_yaw_rate=0//Table 1101, CY_r side_force_delta_rudder=-0.15869140625//Table 1101, CY_dr pitch_moment_horizontal_incidence=-6.591796875//Table 1101, Cm_dh pitch_moment_delta_elevator=-0.9765625//Table 1101, Cm_de pitch_moment_delta_trim=-2.0//Table 1101, Cm_dt //////////////////////////////////////////// pitch_moment_pitch_damping=-95.0 ; -120.0 /////////////////////////////////////////// pitch_moment_aoa_0=0.00//Table 1101, Cmo pitch_moment_daoa=9.27734375//Table 1101, Cm_adot pitch_moment_flaps=0.015//Table 1101, Cm_df pitch_moment_gear=0.0030//Table 1101, Cm_dg pitch_moment_spoilers=-0.005//Table 1101, Cm_ds pitch_moment_delta_elevator_propwash=0//Table 1101, Cm_de pitch_moment_pitch_propwash=-0.01//Table 1101, Cm_q roll_moment_slip_angle=0.0732421875//Table 1101, Cl_beta //////////////////////////////////////////////////////////////////// roll_moment_roll_damping=-1.2 ;-1.8 ///////////////////////////////////////////////////////////////////// roll_moment_yaw_rate=-0.01953125//Table 1101, Cl_r roll_moment_spoilers=0.050000//Table 1101, Cl_adot roll_moment_delta_aileron=-0.1953125//Table 1101, Cl_da roll_moment_delta_rudder=0.01953125//Table 1101, Cl_dr roll_moment_delta_aileron_trim_scalar=-0.2//Table 516 yaw_moment_slip_angle=0.1708984375//Table 1101, Cn_beta yaw_moment_roll=0.03662109375//Table 1101, Cn_p //////////////////////////////////////////////////////////////////////// yaw_moment_yaw_damping=-1.2 //-1.8 ///////////////////////////////////////////////////////////////////////// yaw_moment_yaw_propwash=0//Table 1101, damping yaw_moment_delta_aileron=-0.009765625//Table 1101, Cn_da yaw_moment_delta_rudder=0.1220703125//Table 1101, Cn_dr yaw_moment_delta_rudder_propwash=0//Table 1101, Cn_dp yaw_moment_delta_rudder_trim_scalar=0.0 //Table 1534 aero_center_lift=-6.5 compute_aero_center=0 //Table 1535 roll_moment_delta_aileron_aoa_table=-15.000000:1.100000, 0.000000:1.000000, 13.000000:0.700000, 16.000000:0.550000, 20.000000:0.050000 //Table 1536 yaw_moment_delta_rudder_aoa_table=-15.000000:1.100000, 0.000000:1.000000, 13.000000:0.700000, 16.000000:0.550000, 20.000000:0.050000 //Table 1537 yaw_moment_aoa_table=0.000000:0.000000 //Table 1538 roll_moment_aoa_table=0.000000:0.000000 elevator_lift_coef = 1.0 rudder_lift_coef = 1.5 aileron_up_drag_coef = 0.4 aileron_down_drag_coef = 1.0 fuselage_lateral_cx = 0.4 presspt_fwd_Alpha0_pMAC=0 presspt_fwd_AlphaStall_pMAC=0 presspt_fwd_AlphaHiStall_pMAC=-0.25 [FLIGHT_TUNING] modern_fm_only = 1 /////////////////////////////////////////////////// cruise_lift_scalar = 1.0 /1.17//aircraft.cfg parasite_drag_scalar = 0.95 //1.0 induced_drag_scalar = 1.25 //1.33//aircraft.cfg //////////////////////////////////////////////////// flap_induced_drag_scalar = 1.2 /1.0 elevator_effectiveness = 0.95 //1.0//aircraft.cfg elevator_maxangle_scalar = 1.0//aircraft.cfg /////////////////////////////////////////////////// aileron_effectiveness = 1.15 /1.0//aircraft.cfg //////////////////////////////////////////////////// rudder_effectiveness = 1.0//aircraft.cfg rudder_maxangle_scalar = 0.55//aircraft.cfg ////////////////////////////////////////////////////////// pitch_stability = 3.5 //5.0 roll_stability = 1.2 //1.85 yaw_stability = 2.5 //4.0 ///////////////////////////////////////////////////////// pitch_gyro_stability = 2.0 roll_gyro_stability = 2.0 yaw_gyro_stability = 2.0 ////////////////////////////////////////////////////// elevator_trim_effectiveness = 1.025 //1.19 /////////////////////////////////////////////////////// aileron_trim_effectiveness = 1.0//aircraft.cfg rudder_trim_effectiveness = 1.0//aircraft.cfg hi_alpha_on_roll = 1.0 hi_alpha_on_yaw = 1.0 p_factor_on_yaw = 0.0 ///////////////////////////////////////////////////////// gyro_precession_on_yaw = 0.3 //0.5 gyro_precession_on_pitch=0.3 //0.5 ///////////////////////////////////////////////////////// wingflex_scalar = 1.08 wingflex_offset = 0.0 wingflex_surface_scalar =0.0 stall_coef_at_min_weight = 0.5 icing_scalar=0.32 elevator_chordangle_scalar=-1 htail_maxangle_scalar=-1 rudder_chordangle_scalar=-1 vtail_maxangle_scalar=-1 ground_high_speed_steeringwheel_static_friction_scalar=3.0 ground_high_speed_otherwheel_static_friction_scalar=2.5 [REFERENCE SPEEDS] full_flaps_stall_speed = 113//aircraft.cfg flaps_up_stall_speed = 142//aircraft.cfg cruise_speed = 477//aircraft.cfg cruise_mach = 0.785 crossover_speed = 0 max_mach = 0.82//aircraft.cfg max_indicated_speed = 340//aircraft.cfg max_flaps_extended = 250 normal_operating_speed = 310 airspeed_indicator_max = 450 rotation_speed_min = 95 climb_speed = 285 cruise_alt = 38000 takeoff_speed = 120 spawn_cruise_altitude = 5000 spawn_descent_altitude = 500 best_angle_climb_speed = 235 approach_speed = 135 best_glide = 220 max_gear_extended = 270 fly_assistant_use_dynamic_speeds = 0 [INTERACTIVE POINTS] number_of_interactive_points=9 interactive_point.0=0.400 , 40.4682,-5.4437, -1.5939, 0, 0.000000, 0.000000, -90.000000, 72, 16, 85, 3, -2, 33 // 0,Main exit-FWD Entry interactive_point.1=0.400 , 28.9189, 2.4250, -6.1920, 1, 0.000000, 0.000000, 90.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 1, Cargo exit/door-FWD Cargo interactive_point.2=0.400 , -47.6151, 4.5654, -1.5939, 0, 0.000000, 0.000000, 97.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 0, Main exit-AFT Service interactive_point.3=0.400 , 53.391604, 13.130946, -7.89732, 4, 0.000000, 0.000000, 45.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 4, Ground Power cable interactive_point.4=0.400 , -0.699505, 38.227005, -6.163185, 3, 0.000000, 0.000000, 90.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 3, Fuel hose interactive_point.5=0.400 , 7.72833, 0.00, -6.9299, 5, 0.000000, 0.000000, 90.000000 , 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 5, Air Start Unit interactive_point.6=0.400 , 41.6, 5.37906, -1.5939, 0, 0.000000, 0.000000, 97.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 0, Main exit-FWD Service interactive_point.7=0.400 , -47.6151, -4.5654, -1.5939, 0, 0.000000, 0.000000, 97.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 0, Main exit-AFT Entry interactive_point.8=0.400 , -34.6622, 2.4250, -6.1920, 1, 0.000000, 0.000000, 90.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000 // 1, Cargo exit/door-AFT Cargo [STALL PROTECTION] stall_protection = 0 off_limit = 0 off_yoke_limit = 0 on_limit = 0 on_goal = 0 timer_trigger = 0 [FLAPS.0] type = 1//aircraft.cfg system_type = 1//aircraft.cfg system_type_index = 0 span-outboard = 0.8//aircraft.cfg extending-time = 27//aircraft.cfg damaging-speed = 250//aircraft.cfg blowout-speed = 300//aircraft.cfg maneuvering_flaps = 0 lift_scalar = 0.0//aircraft.cfg drag_scalar = 0.0//aircraft.cfg pitch_scalar = 0.0//aircraft.cfg max_on_ground_position = 8 delay_between_flap_index = 0 altitude-limit = -1 // flap position airspeed limit drag scalar, lift scalar, area scalar, add camber, add aft feet, add incidence flaps-position.0= 0.0, -1, 0.00000, 0.00000, 1, 0, 0.00, 0// 0 flaps-position.1= 1.0, 250, 0.00000, 0.00000, 1, 0, 0.00, 0// 1 flaps-position.2= 2.0, 250, 0.00000, 0.00000, 1, 0, 0.00, 0// 2 flaps-position.3= 5.0, 250, 0.00000, 0.00000, 1, 0, 0.00, 0// 5 flaps-position.4= 10.0, 210, 0.00000, 0.00000, 1, 0, 0.00, 0// 10 flaps-position.5= 15.0, 200, 0.00000, 0.00000, 1, 0, 0.00, 0// 15 flaps-position.6= 25.0, 190, 0.00000, 0.00000, 1, 0, 0.00, 0// 25 flaps-position.7= 30.0, 175, 0.00000, 0.00000, 1, 0, 0.00, 0// 30 flaps-position.8= 40.0, 166, 0.00000, 0.00000, 1, 0, 0.00, 0// 40 [FLAPS.1] type = 1//aircraft.cfg system_type = 1//aircraft.cfg system_type_index = 0 span-outboard = 0.8//aircraft.cfg extending-time = 27//aircraft.cfg damaging-speed = 250//aircraft.cfg blowout-speed = 300//aircraft.cfg maneuvering_flaps = 0 lift_scalar = 1.0//aircraft.cfg drag_scalar = 1.0//aircraft.cfg pitch_scalar = 1.0//aircraft.cfg max_on_ground_position = 8 delay_between_flap_index = 0 altitude-limit = -1 // flap position airspeed limit drag scalar, lift scalar, area scalar, add camber, add aft feet, add incidence flaps-position.0= 0.0, -1, 0.00000, 1.00000, 1, 0, 0.00, 0// 0 flaps-position.1= 7.5, 250, 0.10000, 1.00000, 1, 0, 0.00, 0// 1 flaps-position.2= 10.8, 250, 0.20000, 1.00000, 1, 0, 0.00, 0// 2 flaps-position.3= 14.9, 250, 0.30000, 1.10000, 1, 0, 0.00, 0// 5 flaps-position.4= 17.9, 210, 0.70000, 1.15000, 1, 0, 0.00, 0// 10 flaps-position.5= 23.0, 200, 1.00000, 1.20000, 1, 0, 0.00, 0// 15 flaps-position.6= 29.5, 190, 1.05000, 1.25000, 1, 0, 0.00, 0// 25 flaps-position.7= 32.5, 175, 1.10000, 1.35000, 1, 0, 0.00, 0// 30 flaps-position.8= 40.0, 166, 1.15000, 1.45000, 1, 0, 0.00, 0// 40 [FLAPS.2] type = 2//aircraft.cfg system_type = 1//aircraft.cfg system_type_index = 0 span-outboard = 0.8//aircraft.cfg extending-time = 7//aircraft.cfg damaging-speed = 250//aircraft.cfg blowout-speed = 300//aircraft.cfg maneuvering_flaps = 0 lift_scalar = 0.1//aircraft.cfg drag_scalar = 1.0//aircraft.cfg pitch_scalar = 0.0//aircraft.cfg max_on_ground_position = 8 delay_between_flap_index = 0 altitude-limit = -1 // flap position airspeed limit drag scalar, lift scalar, area scalar, add camber, add aft feet, add incidence flaps-position.0= 0.0, -1, 0.00000, 1.00000, 1, 0, 0.00, 0// 0 flaps-position.1= 5.0, 250, 0.15000, 1.05000, 1, 0, 0.00, 0// 1 flaps-position.2= 10.0, 250, 0.25000, 1.10000, 1, 0, 0.00, 0// 2 flaps-position.3= 20.0, 250, 0.45000, 1.10000, 1, 0, 0.00, 0// 5 flaps-position.4= 20.0, 210, 0.75000, 1.10000, 1, 0, 0.00, 0// 10 flaps-position.5= 20.0, 200, 0.95000, 1.10000, 1, 0, 0.00, 0// 15 flaps-position.6= 20.0, 190, 0.95000, 1.10000, 1, 0, 0.00, 0// 25 flaps-position.7= 20.0, 175, 0.95000, 1.10000, 1, 0, 0.00, 0// 30 flaps-position.8= 20.0, 166, 0.95000, 1.10000, 1, 0, 0.00, 0// 40 Much appreciated man, like always. SN737
August 22, 2025Aug 22 12 hours ago, Bunchy said: This results in blurry textures for me. Not a great solution. Not true for my 3060ti. I can even use it at altitude. 1080p Just use it for landing. Thing is, I can't fly without it. Also, is there a penalty if you post more than 100 liines. dd dd Edited August 22, 2025Aug 22 by Sky_Pilot071
August 22, 2025Aug 22 1 hour ago, SayAgain said: so you thought 64GB RAM would be enough? Think again ... AFAIK, Windows will use as much memory as you give it if there are things to put in that memory. You'd need to run your same test on 64 and 32GB of RAM to see if the extra memory actually improves performance. Back in the 2020 days, when I upgraded from 32 to 64GB of RAM, the decreased memory timings had a larger impact than the increase in memory (and the impact was only a few FPS). I confirmed this by removing half of the new memory to bring me down to 32GB, and noticed the performance was still better than that of my older, slower 32GB sticks.
August 22, 2025Aug 22 15 minutes ago, Funky D said: if there are things to put in that memory. There are apparently "things" to put in memory ... are you saying those "things" aren't important? Not sure I'd agree with that. Going to I/O is to be avoided. AMD 9950X3D's IMC is 2 channel ... I'm running two 48GB modules at 6400MT/s What I suspect is really happening here is my MSFS scenery cache is 32GB and it's being loaded into memory (this is a good thing for performance as RAM is considerably faster than any I/O, even my Samsung 9100 nVME). 1 hour ago, MrFuzzy said: Also: Yep, and several other things, like AI aircraft with no wheels until you get close enough (object culling needs some tuning by Asobo even at the cost of FPS). Not an FPS chaser, perfectly happy with 30 so long as image quality is good ... I just don't rapidly twirl my view around frequently when doing normal flight and not testing ... so it's a non-event for me. Edited August 22, 2025Aug 22 by SayAgain Extraordinary claims require extraordinary evidence. - Carl Sagan
August 22, 2025Aug 22 47 minutes ago, SayAgain said: There are apparently "things" to put in memory ... are you saying those "things" aren't important? Not sure I'd agree with that. Going to I/O is to be avoided. Those things aren't important if they don't affect performance. Re: I/O, if it's something that isn't accessed again, or is only accessed when you reload the flight and saves a few seconds of loading, is it worth that data being retained in memory? My point was this test doesn't mean much unless you perform the same test with less memory and can actually record a performance benefit with more memory installed. And for 2020 (albeit it was with limited testing), the extra memory did not make a measurable difference. You could get a workstation with 512GB of memory and load the entirety of MSFS onto a RAM disk and will likely quickly find the bottlenecks of MSFS lie outside of memory and disk I/O, assuming it's tested against a system with NVMe storage and 64GB of memory.
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