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747-100 posky merge pmdg

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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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