Thanks for the wonderful a/c. You guys do wondeful work as usual.I'm wondering if the Posky Airbus is compatible with PSS A330 Panel.I've merged Pss Airfile and aircarft.cfg along with the Panel as one would normally do and altered the fltsim.xx to match that of the original Posky aircarft, but anytime I take a flight with the Posky jet, I can't seem to get passed 10,000FT...Any thoughts on this..ThanksTroy

BUMP!TROY

You might consider trying to copy over certain things from the POSKY aircraft.cfg file and replace whats in the PSS version. I recall somebody mentioning the contact points section as beeing one of them.Not sure if this is the cause of the errors in flight though.

Thanks for the feedback but I've already done this as well.The post you are talking about was originally created by me, but I thought I'd try again and hope to get some feed back from POSKY..Troy

Hi Troy,try this one for the A330-200, using the PSS airfile (sim=A332).[LIGHTS] Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landinglight.1 = 1, 7.800, 0.000, -5.500, fx_beaconb ,light.2 = 1, 0.200, 0.000, 14.500, fx_beaconh ,light.3 = 4, 73.000, 0.000, 8.000, fx_vclight ,light.4 = 2, -40.200, -93.100, 13.380, Opensky_airbus_strobe ,light.5 = 2, -40.200, 93.100, 13.380, Opensky_airbus_strobe ,light.6 = 5, 18.000, 27.000, -4.000, Opensky_wing_light,light.7 = 5, 19.933, 8.827, -4.368, Opensky_wing_light,light.8 = 5, 18.000, -27.000, -4.000, Opensky_wing_light,light.9 = 5, 19.933, -8.827, -5.368, Opensky_wing_light,light.10 = 5, 19.700, 19.000, -6.000, Opensky_nacelle_refl,light.11 = 5, 19.700, -19.000, -6.000, Opensky_nacelle_refl,light.12 = 3, -111.900, 0.000, 11.420, Opensky_nav_yellow , light.13 = 2, -111.900, 0.100, 11.300, fx_strobeh , [exits]number_of_exits=2exit_rate.0=0.25exit_rate.1=0.25[Views]eyepoint=78.0, -1.8, 5.5[General]atc_type=AIRBUSatc_model=A330performance=[pitot_static]vertical_speed_time_constant=99[GROUND_REACTION]MAX_STEERING_ANGLE=72[GeneralEngineData]engine_type=1Engine.0=12,-30,-6Engine.1=12, 30,-6fuel_flow_scalar=0.85min_throttle_limit=-0.499939[jet_engine]thrust_scalar = 1.0[EFFECTS]wake=fx_wakewater=fx_spraydirt=fx_tchdrtconcrete=fx_sparkstouchdown=fx_tchdwn, 1[direction_indicators]direction_indicator.0=3,0[Radios]Audio.1=1Com.1=1, 1Com.2=1, 1Nav.1=1, 1, 1Nav.2=1, 1, 0Adf.1=1Transponder.1=1Marker.1=1[Flaps.0]type=1span-outboard=1.0extending-time=20system_type=1flaps-position.0= 0 flaps-position.1= 2flaps-position.2= 8flaps-position.3=14flaps-position.4=22flaps-position.5=32damaging-speed = 240 blowout-speed = 260 lift_scalar = 1.0drag_scalar = 1.0pitch_scalar= 1.0[Flaps.1]type= 2span-outboard= 0.800extending-time= 12.000system_type= 1damaging-speed= 250.000blowout-speed= 300.000flaps-position.0= 0.000flaps-position.1= 20.000[forcefeedback]// default feedback.. change as you need.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[WEIGHT_AND_BALANCE]//do not changereference_datum_position=0.000000,0.000000,0.000000max_number_of_stations=50pss_num_class = THREE_CLASS // Load Editor Cfg Valuestation_load.0 = 450, 0.0, 0.0, 0.0 //Weight Crew (lbs) LEAVEstation_load.1 = 3000, 0.0, 0.0, 0.0 //Weight Galleys (lbs) LEAVEstation_load.2 = 33075, 0.0, 0.0, 0.0 //Weight Baggage (lbs)station_load.3 = 26980, 0.0, 0.0, 0.0 //Weight Cargo (lbs)station_load.4 = 1500, 0.0, 0.0, 0.0 //Weight First Class (lbs)station_load.5 = 5250, 0.0, 0.0, 0.0 //Weight Business Class (lbs)station_load.6 = 30750, 0.0, 0.0, 0.0 //Weight Economy Class (lbs)empty_weight = 264995.3empty_weight_roll_MOI = 3900000empty_weight_pitch_MOI = 13000000empty_weight_yaw_MOI = 11500000empty_weight_coupled_MO I= 0.000000empty_weight_CG_position =13.014977.000000,0.000000,0.000000max_gross_weight =509046.8empty_weight_coupled_MOI=0.000000***************************************************[airplane_geometry]wing_area=3892wing_span=197wing_root_chord=40wing_dihedral=6wing_incidence=0.7wing_twist=-0.8 oswald_efficiency_factor=0.6 wing_winglets_flag=1wing_sweep=29.7wing_pos_apex_lon=45wing_pos_apex_vert=0htail_area=333htail_span=134htail_pos_lon=-95.0htail_pos_vert=0htail_incidence=2.993774htail_sweep=0vtail_area=513vtail_span=134vtail_sweep=29vtail_pos_lon=-95.0vtail_pos_vert=8.5elevator_area=90.5aileron_area=36.8rudder_area=56.2elevator_up_limit=30elevator_down_limit=15aileron_up_limit=25aileron_down_limit=25rudder_limit=31.6elevator_trim_limit=30spoiler_limit=25spoilerons_available=1aileron_to_spoileron_gain=0.5min_ailerons_for_spoilerons=10min_flaps_for_spoilerons=0.0[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)point.0= 1.000, 51.233, 0.000, -10.625, 1181.102, 0.000, 4.845, 78.000, 0.500, 0.500, 0.510, 7.000, 9.000, 0.000, 280.000, 300.000 point.1= 1.000, -11.067, -17.750, -13.350, 1574.803, 2.000, 2.45, -8.000, 1.800, 1.600, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000 point.2= 1.000, -11.067, 17.750, -13.350, 1574.803, 1.000, 2.45, -8.000, 1.800, 1.600, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000 point.3= 2.000, -14.167, -84.717, 0.000, 787.402, 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, -14.167, 91.817, 0.000, 787.402, 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, -120.667, 0.000, 2.500, 787.402, 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, 88.417, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000point.7= 2.000, 14.167, -99.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000point.8= 2.000, 0.000, 44.750, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000point.9 = 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 2, 4, 0, 10, 30 point.10 = 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 4, 2, 0, 10, 30 static_pitch= 2.0static_cg_height= 10.420gear_system_type=0[TurbineEngineData]fuel_flow_gain=0.002inlet_area=28.72rated_N2_rpm=29920static_thrust=69690.77afterburner_available=0reverser_available=1max_contrail_temperature = -30[keyboard_response]elevator=150.000000,250.000000aileron=150.000000,250.000000rudder=150.000000,250.000000[autopilot]autopilot_available=1flight_director_available=1default_vertical_speed=800autothrottle_available=1autothrottle_arming_required=0autothrottle_takeoff_ga=8autothrottle_max_rpm=97pitch_takeoff_ga=4max_pitch=10.000000max_pitch_acceleration=1.000000max_pitch_velocity_lo_alt=2.000000max_pitch_velocity_hi_alt=1.500000max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=25.000000max_bank_acceleration=1.800000max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[Reference Speeds]flaps_up_stall_speed=155full_flaps_stall_speed=112cruise_speed=528max_indicated_speed=350.000000max_mach=0.841992[brakes]toe_brakes_scale=0.512497parking_brake=1[gear_warning_system]gear_warning_available=0pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=5.042029[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=1[turn_indicators]turn_indicator.0=1,0[flight_tuning]cruise_lift_scalar = 1.0parasite_drag_scalar = 0.5induced_drag_scalar = 3.0elevator_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[fuel]Center1 = 5.0, 0.0,-4.0,11020,1043LeftMain = -5.0, -19.0, 0.0,12060, 949RightMain = -5.0, 19.0, 0.0,12060, 949fuel_type=2.000000number_of_tank_selectors=1electric_pump=1ZFW is 365.0.Cheers,Gostahttp://hifi.avsim.net/activesky/images/wxrebeta.jpg

Thanks GostaTroy

Hi guys i've successfully modded the POSKY A330 with the PSS. I get a 4 engined E/WD display which is a problem, this was using the alias command.RegardsG-MIDYhttp://www.airliners.net/open.file/265713/L/

Hi there,change the aircraft title in the aircraft.cfg to reflect the PSS model, for example:[fltsim.0]title=PSS A330-200 RR Air Transat PoskyCheers,Gosta.http://hifi.avsim.net/activesky/images/wxrebeta.jpg

Thanks will try it out.RegardsG-MIDYhttp://www.airliners.net/open.file/265713/L/