Globe Cargo

"Hi, just installed all liveries for RFP and PMDG aicrafts. All nice, but get a problem with Atlas for RFP. Probably is a known bug, but I've been looking for in the forum and didn't find it. The problem is when I select 747-200F Atlas aircraft, the noise goes up and the back touch the ground as if the aircraft load was moved to the back part of the aircraft. I know the problem is in the aircraft.cfg file cause replaced it by Polar aircraft and worked fine. Anyone has the cfg file fixed?. regards."

"This has happened to me also. If anyone has any idea on the cause of this, I would love to know. I too have a feeling that it's some problem in the aircraft.cfg ... perhaps in the weight & balance section but I don't know much about that part of the aircraft.cfg Jerry Lauderbaugh 1505"

"Here,s a Copy of my Atlas cfg to check against your own Mike [fltsim.0] title=Vmax 747-200 VMAX ATLAS AIR N508 sim=Vmax_Classic_2 model= panel= sound= texture=1 kb_checklists=Boeing747-200_check kb_reference=Boeing747-200_ref atc_type=Boeing atc_model=B742 atc_id_enable=1 atc_id=N508MC atc_id_color=0xffffffff editable=0 atc_airline=ATLAS atc_flight_number=636 atc_parking_types=CARGO atc_parking_codes=GTI atc_heavy=1 ui_manufacturer=Ready For Pushback ui_type=747-200(SF) ui_variation=ATLAS AIR N508MC visual_damage=1 description=Vmax Classic 747-200Manufactured between 1970 and 1986
Powered by 4 GE CF6-50E2 Engines Copyright of Ralph's Panel Shop and Vmax Flight Systems //FS2004 Version 2 [FORCEFEEDBACK] GEAR_BUMP_NOSE_MAGNITUDE=6000 GEAR_BUMP_NOSE_DIRECTION=18000 GEAR_BUMP_NOSE_DURATION=250000 GEAR_BUMP_LEFT_MAGNITUDE=6000 GEAR_BUMP_LEFT_DIRECTION=35500 GEAR_BUMP_LEFT_DURATION=250000 GEAR_BUMP_RIGHT_MAGNITUDE=6000 GEAR_BUMP_RIGHT_DIRECTION=00500 GEAR_BUMP_RIGHT_DURATION=250000 GROUND_BUMPS_MAGNITUDE1=3250 GROUND_BUMPS_ANGLE1=8900 GROUND_BUMPS_INTERCEPT1=5.0 GROUND_BUMPS_SLOPE1=0.48 GROUND_BUMPS_MAGNITUDE2=750 GROUND_BUMPS_ANGLE2=9100 GROUND_BUMPS_INTERCEPT2=0.075 GROUND_BUMPS_SLOPE2=1.0 CRASH_MAGNITUDE1=10000 CRASH_DIRECTION1=01000 CRASH_MAGNITUDE2=10000 CRASH_DIRECTION2=9000 CRASH_PERIOD2=75000 CRASH_DURATION2=2500000 [ELECTRICAL] ;BUSTYPE, MAXAMPLOAD, MINVOLTAGE ;BUSTYPES:0=MAINBUS,1=AVIONICSBUS,2=BATTERYBUS,3=HOTBATTERYBUS,4-7=GENERATOR/ALTERNATORBUS(1-4) ;BUS TYPES: ;0=MAIN BUS(MOST COMPONENTS CONNECTED HERE) ;1=AVIONICS BUS ;2=BATTERY BUS ;3=HOT BATTERY BUS(BYPASSESE MASTER SWITCH) ;4=GENERATOR/ALTERNATOR BUS1 ;5=GENERATOR/ALTERNATOR BUS2 ;6=GENERATOR/ALTERNATOR BUS3 ;7=GENERATOR/ALTERNATOR BUS4 ;BUSTYPE, MAXAMPLOAD, MINVOLTAGE MAX_BATTERY_VOLTAGE = 30.0 GENERATOR_ALTERNATOR_VOLTAGE = 30.0 GENERATOR_ALTERNATOR_AMPS = 100.0 FLAP_MOTOR = 0, 15, 17.0 GEAR_MOTOR = 0, 15, 17.0 AUTOPILOT = 0, 12, 0.0 AVIONICS_BUS = 0, 10, 17.0 AVIONICS = 1, 10, 10.0 PITOT_HEAT = 0, 15, 10.0 ADDITIONAL_SYSTEM = 0, 10, 4.0 MARKER_BEACON = 1, 10, 6.0 GEAR_WARNING = 0, 2, 10.0 FUEL_PUMP = 0, 15, 5.0 STARTER1 = 0, 20, 15.0 STARTER2 = 0, 20, 15.0 STARTER3 = 0, 20, 15.0 STARTER4 = 0, 20, 15.0 LIGHT_NAV = 0, 10, 5.0 LIGHT_BEACON = 0, 10, 5.0 LIGHT_LANDING = 0, 25, 15.0 LIGHT_TAXI = 0, 25, 15.0 LIGHT_STROBE = 0, 10, 10.0 LIGHT_PANEL = 0, 5, 10.0 AUTO_BRAKES = 0, 1, 5.0 HYDRAULIC_PUMP = 0, 5, 5.0 FUEL_TRANSFER_PUMP = 0, 5, 5.0 LIGHT_RECOGNITION = 0, 5, 5.0 LIGHT_WING = 0, 10, 10.0 LIGHT_LOGO = 0, 10, 10.0 [GROUND_REACTION] MAIN_GEAR_STATIC_COMPRESSION = 1.54 // (FEET), THE DISTANCE THE MAIN GEAR STRUT IS COMPRESSED WHEN AT REST ON THE GROUND CENTER_GEAR_STATIC_COMPRESSION = 1.54 // (FEET), THE DISTANCE THE CENTER GEAR STRUT IS COMPRESSED WHEN AT REST ON THE GROUND MAIN_GEAR_DAMPING_RATIO = 0.9 // MAIN GEAR STRUT DAMPING, 0 = UNDAMPED OSCIALLATIONS, 1 = CRITICALLY DAMPED CENTER_GEAR_DAMPING_RATIO = 0.9 // CENTER GEAR STRUT DAMPING, 0 = UNDAMPED OSCIALLATIONS, 1 = CRITICALLY DAMPED MAX_STEERING_ANGLE =70.0 [PITOT_STATIC] VERTICAL_SPEED_TIME_CONSTANT = 999.0 //INCREASING THIS VALUE WILL CAUSE A MORE INSTANTANEOUS REACTION IN THE VSI [WEIGHT_AND_BALANCE] // Cargo Load Data empty_weight =342000 max_number_of_stations = 62 //station_load.0 = 246400.00, 20.20, 0.00, 2.00 station_load.0 = 98000.00, 20.20, 0.00, 2.00 //station_load.0 = 58000.00, 20.20, 0.00, 2.00 // END of Cargo Load Data reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=10.000000,0.000000,0.000000 max_gross_weight=790180.000000 //CG_forward_limit=0.140 //CG_aft_limit=0.420 empty_weight_roll_MOI=19618435.000000 empty_weight_pitch_MOI=40143699.000000 empty_weight_yaw_MOI=36447449.000000 empty_weight_coupled_MOI=0.000000 [General] performance=Length: 225'-2"'
Wingspan: 195'-8"
MTOW: 775,000 LBS
MLW: 564,000 LBS
Cruise: Max 523knts/Economical 470knts
Accomodation: 385 (Basic)
Range: 5150 NM


atc_type=Boeing atc_model=B742 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) [fuel] Center1= 38.0, 0.00, -6.00, 16689.000000, 3.00 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center2= 45.0, 0.00, -6.00, 50.000000, 3.00 LeftMain= 17.0, -29.00, 0.00, 4421.000000, 3.00 LeftAux= -7.0, -54.00, 0.00, 12240.000000, 3.00 RightMain=-17.0, 29.00, 0.00, 4421.000000, 3.00 RightAux= -7.0, 54.00, 0.00, 12240.000000, 3.00 LeftTip= -27.0, -85.00, 0.00, 440.000000, 3.00 RightTip= -27.0, 85.00, 0.00, 440.000000, 3.00 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=5503.000000 wing_span=195.666667 wing_root_chord=28.166667 wing_dihedral=6.998291 wing_incidence=1.320 wing_twist=-0.999756 oswald_efficiency_factor=1.100000 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=1470.000000 htail_span=73.166667 htail_pos_lon=-180.000000 htail_pos_vert=0.000000 htail_incidence=3.000000 htail_sweep=0.000000 vtail_area=1290.000000 vtail_span=40.951190 vtail_sweep=0.000000 vtail_pos_lon=-116.000000 vtail_pos_vert=5.833333 elevator_area=352.000000 aileron_area=220.120000 rudder_area=219.300000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available = 1 //Spoilerons Available? aileron_to_spoileron_gain = 3 //Aileron to spoileron gain min_ailerons_for_spoilerons = 10 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate //[contact_points] //0 Class <0=none,1=wheel, 2=scrape, 3=float> //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) // -- 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 //------------------------------------------------------------------------------------------------------------------------------------------------------- [contact_points] point.0=1.00,92.0, 0.00, -18.2, 1574.8, 0.000000, 5.826899, 70.0, 1.450000, 2.500000, 0.900000, 14.000000, 14.000000, 0.000000, 0.000000, 0.000000 //point.1=1.00, 1.1, -6.20, -18.2, 1574.8, 1.000000, 5.826899, 0.00, 1.540000, 2.500000, 0.900000, 18.000000, 18.000000, 2.000000, 0.000000, 0.000000 //point.2=1.00, 1.1, 6.40, -18.2, 1574.8, 2.000000, 5.826899, 0.00, 1.540000, 2.500000, 0.900000, 18.000000, 18.000000, 2.000000, 0.000000, 0.000000 point.1=1.00, -3.6, 28.02, -19.1, 1574.8, 2.000000, 5.826899, 0.00, 1.540000, 2.500000, 0.900000, 18.000000, 18.000000, 2.000000, 0.000000, 0.000000 point.2=1.00, -3.6, -28.02, -19.1, 1574.8, 2.000000, 5.826899, 0.00, 1.540000, 2.500000, 0.900000, 18.000000, 18.000000, 2.000000, 0.000000, 0.000000 //scrape points point.3=2, -70.7, -102.0, 6.0, 1574.8, 0.000000, 0.000000, 0.00000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 5.000000, 0.000000, 0.000000 point.4=2, -70.7, 102.0, 6.0, 1574.8, 0.000000, 0.000000, 0.00000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 6.000000, 0.000000, 0.000000 point.5=2,-126.6, 0.0, 5.8, 1574.8, 0.000000, 0.000000, 0.00000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 9.000000, 0.000000, 0.000000 point.6=2, 66.8, 0.0, 5.8, 1574.8, 0.000000, 0.000000, 0.00000, 0.000000, 0.000000, 0.000000, 0.000000, 0.000000, 4.000000, 0.000000, 0.000000 static_pitch=0.00 static_cg_height=16.50000 //gear_system_type=0 gear_system_type=0 [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 49 // seconds flaps-position.0=0.000000,0.000000 flaps-position.1=6.665409,0.000000 flaps-position.2=13.330818,0.000000 flaps-position.3=19.996227,0.000000 flaps-position.4=26.661636,0.000000 flaps-position.5=33.327045,0.000000 flaps-position.6=39.992454,0.000000 damaging-speed = 200 // KIAS blowout-speed = 250 // KIAS lift_scalar = 0.25 drag_scalar = 1.00 pitch_scalar= 1.00 system_type = 1 //Hydraulic [Flaps.1] type = 1 // 1 - tail, 2 - lead span-outboard = 0.2 extending-time = 49 // seconds flaps-position.0=0.000000,0.000000 flaps-position.1=6.665409,0.000000 flaps-position.2=13.330818,0.000000 flaps-position.3=19.996227,0.000000 flaps-position.4=26.661636,0.000000 flaps-position.5=33.327045,0.000000 flaps-position.6=39.992454,0.000000 damaging-speed = 200 // KIAS blowout-speed = 250 // KIAS lift_scalar = 0.23 drag_scalar = 1.000 pitch_scalar=-15.00 system_type = 1 //Hydraulic [Flaps.2] type= 2 span-outboard= 0.800 extending-time= 3.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar=-1.00 drag_scalar= 0.000 pitch_scalar=-15.25 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 flaps-position.2= 1.000, 0.000 [Flaps.3] type= 2 span-outboard= 0.800 extending-time= 3.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar=-1.00 drag_scalar= 0.000 pitch_scalar=0.00 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.000, 0.000 flaps-position.2= 1.000, 0.000 [GeneralEngineData] engine_type=1 Engine.0= 5.333333,-70.083333,-7.233333 Engine.1= 25.833333,-40.916667,-7.000000 Engine.2= 25.833333, 40.916667,-7.000000 Engine.3= -5.333333, 70.083333,-7.233333 fuel_flow_scalar=0.988000 min_throttle_limit=-0.349915 [TurbineEngineData] fuel_flow_gain=0.002170 inlet_area=54.843840 rated_N2_rpm=29920.000000 static_thrust=44703.200000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=173.000000 full_flaps_stall_speed=138.400000 cruise_speed=527.744626 max_indicated_speed=396.000000 max_mach=0.920000 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=95.678662,-1.499446,12.816150 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=00.10000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=1 autothrottle_max_rpm=94.000000 pitch_takeoff_ga=13.000000 autoland_available=0 use_no_default_bank=1 use_no_default_pitch=1 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=16.00 nav_integrator_control=0.17 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control = 18.0 gs_integrator_control = 0.33 gs_derivative_control = 0.00 gs_integrator_boundary = 0.70 gs_derivative_boundary = 0.00 yaw_damper_gain = 1.0 default_pitch_mode=0 default_bank_mode=0 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.2 induced_drag_scalar = 1.2 elevator_effectiveness = 0.85 aileron_effectiveness = 1.0 rudder_effectiveness = 1.5 pitch_stability = 1.27 roll_stability = 1.0 yaw_stability = 1.2 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [direction_indicators] direction_indicator.0=3,0 [turn_indicators] turn_indicator.0=1,0 [airspeed_indicators] airspeed_indicator.0=0.9827, -3.0 [attitude_indicators] attitude_indicator.0=1 [Radios] Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 1, 1 Nav.2 = 1, 1, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [LIGHTS] light.0 = 1, 78.50, 0.00, 16.25, VM742_beacon , light.1 = 1, 35.00, 0.00, -11.30, VM742_beacon , light.2 = 2, -111.00, 0.00, 7.25, VM742_strobes , light.3 = 8, -10.00, -50.827, 10.90, VM742_wing_l, light.4 = 8, -10.00, 50.827, 10.90, VM742_wing_r, light.5 = 4, 93.55, 0.00, 10.00, VM742_vclight_1, [SMOKESYSTEM] smoke.0=0.00, 0.00,-96.50, fx_contrail_l.fx smoke.1=0.00, 0.00, 96.50, fx_contrail_l.fx [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits = 2 exit_rate.0 = 0.2 ;Percent per second exit_rate.1 = 0.2 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;Percent per second [TailHook] tailhook_length=4 ;(feet) tailhook_position = -15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust = 0.0 [brakes] toe_brakes_scale=0.694815 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=1145.915590 flap_limit_idle=572.957795 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=3000.000000 [stall_warning] type=1"