Atlas RFP Liveries problem
Moderators: Staff, HR, Flight Ops
-
Gustavo
- www.meble-kuchenne.warszawa.pl
Atlas RFP Liveries problem
"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."
-
lauderj
-
Brogs
"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"
[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 1986Powered 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"