August 31, 201411 yr I tried to merge 747pmdg with posky 747-100. When I accelerate the plane turns slightly right and when I flying slowly bends to the right. Can you help me? This is the Aircraft.CFG: [fltsim.1] title=Project Opensky - Boeing 747-100B Tower Air sim=747-100B-PW-JT9D-7R4G2 model= panel= sound= texture=ff kb_checklists=boeing747_check kb_reference=boeing747_ref atc_airline=TOWER atc_flight_number=2 atc_parking_types=GATE, RAMP, CARGO atc_parking_code=TWR ui_typerole=Commercial Airliner ui_createdby=Project Opensky ui_manufacturer=Project Opensky ui_type=747-100 ui_variation=Tower Air visual_damage=1 atc_heavy=1 atc_id= description=Project Opensky \nBoeing 747-100\nVersion 2006.9.6-FSX\n\nEngine Type PW JT9D-7A\n\n747-100 Commercial Version \n\nModel Designer\n Hiroshi Igami\n\nFlight Dynamics Designer\n Warren C. Daniel\n\nMaster Texture Designer\n Corey Ford\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 6,100 statute miles (9,800 km) \n\nTypical city pairs: \n NY-Madrid\n LA-Honolulu\n Seattle-Tokyo\n\nFor proper operation: See B747 manual at: \n www.projectopensky.com [General] atc_type=BOEING atc_model=B744 editable=0 performance="Cruise: 0.86 Mach/565 mph/910 km/h\nEngine: General Electric CF6-80C2B1F, Rolls Royce RB211 or Pratt & Whitney PW4000\nMaximum Range : 7,325 nm [13,570 km]\nMaximum Certified Altitude : 45,100 ft [13,747 m]\nFuel Capacity : 57,285 gal [216,840 L]\nBasic Operating Weight : 394,088 lb [178,755 kg]\nMax Gross Weight : 875,000 lb [396,893 kg]\nLength : 231 ft 10 in [70.6 m]\nWingspan : 211 ft 5 in [64.4 m]\nHeight : 63 ft 8 in [19.4 m]\nSeating : Typical 3-class configuration - 416\nTypical 2-class configuration - 524" [pitot_static] vertical_speed_time_constant = 99 [WEIGHT_AND_BALANCE] empty_weight = 394088.0 // 3-Class max_gross_weight = 875000.0 // 800, 833, 850, 870, 875 x 10^3 lbs [+2000 for max ramp] max_landing_weight = 630000.0 // 574, 630 x 10^3 lbs max_zerofuel_weight = 542500.0 // 535, 542.5 x 10^3 lbs CG_forward_limit=0.130 // 11% 572000-775000 lbs CG_aft_limit=0.331 // WARNING : DO NOT EDIT ! reference_datum_position = 112.714, 0.0, 5.502 // (feet) Boeing Section2.0 reference position (RefPos) empty_weight_CG_position = -97.85, 0, 0 // (feet) from RefPos 19.75% MAC max_number_of_stations =50 ;Moments of Inertia empty_weight_pitch_MOI = 17018677.379279 empty_weight_roll_MOI = 15962454.863936 empty_weight_yaw_MOI = 16890566.121607 empty_weight_coupled_MOI = 2048.0 station_load.0=1236, -95.55, 3.00, 0.00, First Deck station_load.1=5119, -97.85, 0.31, 8.00, Upper Deck station_load.2=4413, -97.85, 0.13, 0.00, Busn Deck station_load.3=42011, -98.00, -0.29, 0.00, Econ Deck station_load.4=78291, -97.11, 0.00, -8.00, Cargo Deck [GeneralEngineData] engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -107.5, -53.3, -6.9 //(feet) from RefPos Engine.1 = -76.0, -30.0, -10.4 //(feet) from RefPos Engine.2 = -76.0, 30.0, -10.4 //(feet) from RefPos Engine.3 = -107.5, 53.3, -6.9 //(feet) from RefPos fuel_flow_scalar = 1.07 // sfc [...] min_throttle_limit = -0.20 // reverse [TurbineEngineData] // // Model : CF6-80C2B1F ~58K // fuel_flow_gain = 0.0036 //Gain on fuel flow inlet_area = 61.283 //Square Feet, engine nacelle inlet area [d=106 in] rated_N2_rpm = 13635.0 //max RPM HPC static_thrust = 58000.0 //Lbs, nominal SLS adjusted thru EEC afterburner_available = 0 //Afterburner available? reverser_available = 1 //Thrust reverser available? [jet_engine] thrust_scalar = 1.0 [fuel] // LeftAux = -112.0, -36.5, -3.0, 4420.0, 0.0 // Main 1 LeftMain = -96.0, -28.0, -4.0, 12240.0, 0.0 // Main 2 RightMain = -96.0, 28.0, -4.0, 12240.0, 0.0 // Main 3 RightAux = -112.0, 36.5, -3.0, 4420.0, 0.0 // Main 4 LeftTip = -130.0, -73.0, 0.0, 500.0, 0.0 // R2 RightTip = -130.0, 73.0, 0.0, 500.0, 0.0 // R3 Center1 = -83.5, 0.0, -7.0, 12240.0, 0.0 // CWT Center2 = -193.5, 0.0, 6.0, 50.0, 0.0 // STAB fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 4 electric_pump=0 [airplane_geometry] wing_area = 5825.0 //Square feet wing_span = 211.4 //Feet [Jig Position (213.0 at full weight)] wing_root_chord = 47.298 //Feet wing_dihedral = 7.0 //Degrees wing_incidence = 0.0 //Degrees [inop in FS9] wing_twist = 0.0 //Degrees [inop in FS9] oswald_efficiency_factor = 0.504 //[...] wing_winglets_flag = 1 //Winglet flag [0:false/1:true] wing_sweep = 37.5 //Degrees at 25% MAC wing_pos_apex_lon = -60.606 //Feet from RefPos wing_pos_apex_vert = 0.0 //Feet from RefPos htail_area = 1470.0 //Square feet htail_span = 75.75 //Feet htail_pos_lon = -210.0 //Feet, from RefPos htail_pos_vert = 7.32 //Feet, from RefPos htail_incidence = 0.0 //Degrees [inop in FS9] htail_sweep = 37.5 //Degrees, horizontal tail leading edge vtail_area = 1060.0 //Square feet vtail_span = 37.1 //Feet, tip to body vtail_sweep = 45.0 //Degrees, vertical tail leading edge vtail_pos_lon = -198.5 //Feet from RefPos vtail_pos_vert = 26.1 //Feet from RefPos elevator_area = 342.0 //Square feet aileron_area = 225.0 //Square feet rudder_area = 230.0 //Square feet elevator_up_limit = 28.0 //Degrees elevator_down_limit = 20.0 //Degrees aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit = 31.5 //Degrees elevator_trim_limit = 20.0 //Degrees spoiler_limit = 70.0 //Degrees spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 3. //Aileron to spoileron gain min_ailerons_for_spoilerons = 10.0 //Degrees min_flaps_for_spoilerons = 0.0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed = 174.55 //Stall clean KTAS @450,000 lbs full_flaps_stall_speed = 122.0 //Stall flaps KTAS cruise_speed = 485.0 //Cruise KTAS max_mach = 0.920 //Barber pole MACH max_indicated_speed = 372.0 // KIAS / modified provision for CAS->KIAS [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 = 0.23 drag_scalar = 1.20 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 = 1.20 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 [autopilot] autopilot_available = 0 autothrottle_available = 0 default_pitch_mode=0 default_bank_mode=0 [contact_points] static_pitch = 1 static_cg_height = 12.5 tailwheel_lock = 0 gear_system_type = 0 max_number_of_points = 5 point.0 = 1, -24.194, 0, -19.335, 1500, 0, 1.932, 56, 1.45, 0.128, 0.78, 9, 12, 0, 270, 320 point.1 = 1, -102.496, -16.009, -20.905, 1500, 1, 1.932, 0, 1.54, 1.171, 0.88, 16, 21, 2, 270, 320 point.2 = 1, -102.496, 16.009, -20.905, 1500, 2, 1.932, 0, 1.54, 1.171, 0.88, 15, 20, 3, 270, 320 point.3 = 1, -115.277, -4.253, -20.905, 1700, 1, 1.932, 0, 1.5, 1.203, 0.82, 15, 18, 2, 270, 320 point.4 = 1, -115.277, 4.253, -20.905, 1700, 1, 1.932, 0, 1.5, 1.203, 0.82, 15, 18, 2, 270, 320 static_pitch = -0.29 static_cg_height = 12.09 gear_system_type=0 static_pitch = -0.29 static_cg_height = 12.09 gear_system_type=0 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 5.0 //Flap angle that activates warning at idle flap_limit_power = 31.5 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.78 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,1,1 //pumps on Eng1,2,3,4 [Views] eyepoint = -19.100, -1.312, 11.122 ; Longitude, Latitude and Vertical position from Reference Point, (FEET) //eyepoint= -18.848, -1.312, 11.122 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 avionics_bus = 0, 5 , 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 17.0 light_nav = 0, 5 , 17.0 light_beacon = 0, 5 , 17.0 light_landing = 0, 5 , 17.0 light_taxi = 0, 5 , 17.0 light_strobe = 0, 5 , 17.0 light_panel = 0, 5 , 17.0 [Radios] Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 1 Adf.1 = 1 Adf.2 = 1 Transponder.1 = 1 Marker.1 = 1 [LIGHTS] light.0 = 1, 65.200, 0.600, 19.100, Opensky_beacon , light.1 = 1, 13.900, 0.000, -7.080, Opensky_beacon , light.4 = 3, -122.3, -0.250, 12.300, Opensky_nav_yellow , light.5 = 3, -122.3, 0.250, 12.300, Opensky_nav_yellow , light.7 = 3, 83.55, 0.000, 14.850, fx_vclighth , light.8 = 9, -111.1, -4.500, 43.750, Opensky_wing_light , // <-----3 previously light.9 = 9, -111.1, 4.500, 43.750, Opensky_wing_light , // <-----3 previously light.10= 5, 17.7, -29.200, -2.000, Opensky_nacelle_refl , light.11= 5, 17.7, 29.200, -2.000, Opensky_nacelle_refl , light.12= 5, 50.9, -11.700, 0.000, Opensky_nacelle_refl , light.13= 5, 50.9, 11.700, 0.000, Opensky_nacelle_refl , light.14= 5, 56.9, -13.700, 1.900, Opensky_nacelle_refl , light.15= 5, 56.9, 13.700, 1.900, Opensky_nacelle_refl , light.16= 5, 83.067, 0.000, -2.000, Opensky_nacelle_refl , light.17= 3, 79.1, -6.500, 6.000, Opensky_nacelle_refl , light.18= 3, 44.79, -4.500, 6.000, Opensky_nacelle_refl , light.19= 3, -47.11, 0.000, -3.000, Opensky_wing_light , [sMOKESYSTEM] smoke.0 = 0.00, -20.5, 0.00, fx_pmdg744_cockpit, [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=3,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 attitude_indicator.1 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [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 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [stall_warning] type=2 Attilio Cardone
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