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