There are so many post on what is best for the PW model of the iFDG that I just simply got lost. I saw everything from using the RR airfile, static thrust settings, etc. Could someone post there CFG for a good setup. I noticed the iFDG PW model climbs real slow above FL250. Is there a way to fix that also. Also what is the best ZFW option to use. I saw several. Sorry for all the questions. I just got behind the times with all the updates and changes.

Rolls Royce is the way to go for the 757. this config will use the pic's logic for electricalsenjoy[General]atc_type=BOEING AIRCRAFTatc_model=B752editable=1performance=Cruise Speedt.80 - .84 MachnNever Exceed .86 MachnMaximum Ranget3,960 nmnMTOW 255,500 lbnSeatingtt192 to 239nCargo Capacityt1,670 CU ftn[pitot_static]vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI[WEIGHT_AND_BALANCE]max_gross_weight = 249150.000empty_weight = 170000.000reference_datum_position = 0.000, 0.000, 0.000empty_weight_CG_position = 0.000, 0.000, 0.000max_number_of_stations =50station_load.0 =0.000000,0.000000,0.000000,0.000000;Moments of Inertiaempty_weight_pitch_MOI = 3172439.000empty_weight_roll_MOI = 2262183.000empty_weight_yaw_MOI = 3337024.000empty_weight_coupled_MOI = 0.000CG_forward_limit= 0.000CG_aft_limit= 1.000[flight_tuning]cruise_lift_scalar = 1.0parasite_drag_scalar = 1.0induced_drag_scalar = 1.0elevator_effectiveness = 1.0aileron_effectiveness = 1.0rudder_effectiveness = 1.0pitch_stability = 1.0roll_stability = 1.0yaw_stability = 1.0elevator_trim_effectiveness = 1.0aileron_trim_effectiveness = 1.0rudder_trim_effectiveness = 1.0[GeneralEngineData]engine_type = 1Engine.0 = 4.750, -16.100, -2.500Engine.1 = 4.750, 16.100, -2.500fuel_flow_scalar = 0.794[TurbineEngineData]fuel_flow_gain = 0.002inlet_area = 40.000rated_N2_rpm = 29920.000static_thrust = 40100.000afterburner_available = 0reverser_available = 1[jet_engine]thrust_scalar = 1.0[electrical];BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)// FS Systems tied to PIC logic avionics_bus=0,0,1avionics=0,0,1flap_motor=1,0,1gear_motor=4,0,1starter1=0,0,1starter2=0,0,1light_nav=0,0,1light_beacon=0,0,1light_landing=0,0,1light_taxi=0,0,1light_strobe=0,0,1light_recognition=0,0,1light_wing=0,0,1light_logo=0,0,1marker_beacon=0,0,1standby_vacuum=0,0,1 [contact_points]point.0= 1.000, 60.167, 0.000, -10.000, 1181.102, 0.000, 2.188, 73.320, 0.239, 2.500, 1.933, 4.000, 4.000, 0.000, 0.000, 0.000point.1= 1.000, -1.667, -14.000, -12.083, 1574.803, 1.000, 2.188, 0.000, 1.972, 2.500, 0.498, 6.900, 6.900, 2.000, 0.000, 0.000point.2= 1.000, -1.667, 14.000, -12.083, 1574.803, 2.000, 2.188, 0.000, 1.972, 2.500, 0.498, 7.100, 7.100, 3.000, 0.000, 0.000point.3= 2.000, -14.170, -47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000point.4= 2.000, -14.170, 47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000point.5= 2.000, -54.000, 0.000, 2.830, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000point.6= 2.000, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000max_number_of_points = 21static_pitch= 0.000static_cg_height= 9.862[Views]eyepoint=43.7, -1.31, 3.55 //(feet) longitudinal, lateral, vertical distance from reference datum[Radios]// Radio Type = availiable, standby frequency, has glide slopeAudio.1 = 1Com.1 = 1, 1Com.2 = 1, 1Nav.1 = 1, 1, 1Nav.2 = 1, 1, 0Adf.1 = 1Transponder.1 = 1Marker.1 = 1[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, 250rudder = 150, 250[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 = 4direction_indicator.0=3,0[exits]number_of_exits = 2exit_rate.0 = 0.4 ;Percent per secondexit_rate.1 = 0.4 ;Percent per second[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=1800autothrottle_available=1autothrottle_arming_required=1autothrottle_max_rpm = 90autothrottle_takeoff_ga=1pitch_takeoff_ga = 8;use_no_default_bank=1use_no_default_pitch=1[fuel]Center1 = 0.000, 0.000, 0.000, 6984.000, 0.000LeftMain = -3.000, -19.000, 0.000, 2185.000, 0.000RightMain = -3.000, 19.000, 0.000, 2185.000, 0.000fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetAnumber_of_tank_selectors = 1 [airplane_geometry]wing_area = 1994.000wing_span = 124.000wing_root_chord = 18.000wing_dihedral = 6.200wing_incidence = 1.000wing_twist = -0.500oswald_efficiency_factor= 0.750wing_winglets_flag = 0wing_sweep = 25.000wing_pos_apex_lon = 8.000wing_pos_apex_vert = 0.000htail_area = 338.000htail_span = 41.700htail_pos_lon = -35.000htail_pos_vert = 0.000htail_incidence = 0.000htail_sweep = 30.000vtail_area = 224.000vtail_span = 20.000vtail_sweep = 35.000vtail_pos_lon = -35.800vtail_pos_vert = 5.800elevator_area = 70.500aileron_area = 26.900rudder_area = 56.200elevator_up_limit = 22.500elevator_down_limit = 19.500aileron_up_limit = 20.000aileron_down_limit = 20.000rudder_limit = 26.000elevator_trim_limit = 20.000spoiler_limit = 60.000spoilerons_available = 1aileron_to_spoileron_gain = 3.000min_ailerons_for_spoilerons = 10.000min_flaps_for_spoilerons = 0.000[Reference Speeds]flaps_up_stall_speed = 142.000full_flaps_stall_speed = 113.000cruise_speed = 505.000[forcefeedback]gear_bump_nose_magnitude=3000 ; 0 - 10000gear_bump_nose_direction=18000 ; 0 - 35999 degreesgear_bump_nose_duration=250000 ; in microsecondsgear_bump_left_magnitude=2700 ; 0 - 10000gear_bump_left_direction=35500 ; 0 - 35999 degreesgear_bump_left_duration=250000 ; in microsecondsgear_bump_right_magnitude=2700 ; 0 - 10000gear_bump_right_direction=00500 ; 0 - 35999 degreesgear_bump_right_duration=250000 ; in microsecondsground_bumps_magnitude1=1300 ; 0 - 10000ground_bumps_angle1=08900 ; 0 - 35999 degreesground_bumps_intercept1=3.0ground_bumps_slope1=0.20ground_bumps_magnitude2=200 ; 0 - 10000ground_bumps_angle2=09100 ; 0 - 35999 degreesground_bumps_intercept2=1.075ground_bumps_slope2=0.035crash_magnitude1=10000 ; 0 - 10000crash_direction1=01000 ; 0 - 35999 degreescrash_magnitude2=10000 ; 0 - 10000crash_direction2=9000 ; 0 - 35999 degreescrash_period2=75000 ; in microsecondscrash_duration2=2500000 ; in microseconds[LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landinglight.0 = 3, -10.34, -62.95, 6.50, fx_navredm ,light.1 = 3, -10.34, 62.95, 6.50, fx_navgrem ,light.2 = 3, -76.31, 0.00, 7.58, fx_navwhih ,light.3 = 2, -13.14, -63.23, 6.50, fx_strobeh ,light.4 = 2, -13.14, 63.23, 6.50, fx_strobeh ,light.5 = 2, 36.09, 0.00, 12.31, fx_beaconb ,light.6 = 1, 17.72, 0.00, -3.61, fx_beaconh ,light.7 = 2, -15.74, -63.23, 6.50, fx_navwhih ,light.8 = 2, -15.74, 63.23, 6.50, fx_navwhih ,[TailHook] // #1 Doortailhook_length=1 tailhook_position = 0.0, 0.0, 0.0 [folding_wings] // #3 door on 3 door version, #4 door on 4 door version.wing_fold_system_type = 4 fold_rates = 0.4,0.4 cable_force_adjust = 1.0[Flaps.0]type= 1span-outboard= 0.800extending-time= 20.000system_type= 1damaging-speed= 250.000blowout-speed= 300.000lift_scalar= 1.000drag_scalar= 1.000pitch_scalar= 1.000flaps-position.0= 0.000, 0.000flaps-position.1= 1.000, 0.000flaps-position.2= 5.000, 0.000flaps-position.3= 15.000, 0.000flaps-position.4= 20.000, 0.000flaps-position.5= 25.000, 0.000flaps-position.6= 30.000, 0.000[Flaps.1]type= 2span-outboard= 0.800extending-time= 2.000system_type= 1damaging-speed= 250.000blowout-speed= 300.000lift_scalar= 1.000drag_scalar= 1.000pitch_scalar= 1.000flaps-position.0= 0.000, 0.000flaps-position.1= 1.000, 0.000[Flaps.2]type= 2span-outboard= 0.800extending-time= 3.000system_type= 1damaging-speed= 250.000blowout-speed= 300.000lift_scalar= 1.000drag_scalar= 1.000pitch_scalar= 1.000flaps-position.0= 0.000, 0.000flaps-position.1= 0.500, 0.000flaps-position.2= 1.000, 0.000