pstlpete Posted April 11, 2015 Share Posted April 11, 2015 Can someone post the aircraft.cfg file from the "Commercial_Airliner" folder in P3D. I am trying to fix an AI traffic problem in P3D & I may have boogered up that .cfg file. Link to comment Share on other sites More sharing options...
Penz Posted April 11, 2015 Share Posted April 11, 2015 This should be a totally unmodified version: [fltsim.0] title=Commercial Airliner Paint2 sim=Commercial_Airliner model= panel= sound= texture=2 kb_checklists= kb_reference= atc_id=F-MSAB atc_airline=World Travel atc_flight_number= ui_manufacturer="ACME" ui_type="Commercial Jet" ui_variation="World Travel Airlines" ui_typerole="Commercial Airliner" ui_createdby="Lockheed Martin" description="Commercial Airliner" [fltsim.1] title=Commercial Airliner Paint4 sim=Commercial_Airliner model= panel= sound= texture=4 kb_checklists= kb_reference= atc_id=I-HKSN atc_airline=Orbit atc_flight_number= ui_manufacturer="ACME" ui_type="Commercial Jet" ui_variation="Orbit Airlines" ui_typerole="Commercial Airliner" ui_createdby="Lockheed Martin" description="Commercial Airliner" [fltsim.2] title=Commercial Airliner Paint5 sim=Commercial_Airliner model= panel= sound= texture=5 kb_checklists= kb_reference= atc_id=JA-3297 atc_airline=Pacifica atc_flight_number= ui_manufacturer="ACME" ui_type="Commercial Jet" ui_variation="Pacifica Airlines" ui_typerole="Commercial Airliner" ui_createdby="Lockheed Martin" description="Commercial Airliner" [fltsim.3] title=Commercial Airliner sim=Commercial_Airliner model= panel= sound= texture=0 kb_checklists= kb_reference= atc_id=F-X395 atc_airline= atc_flight_number= ui_manufacturer="ACME" ui_type="Commercial Jet" ui_variation="White" ui_typerole="Commercial Airliner" ui_createdby="Lockheed Martin" description="Commercial Airliner" [General] atc_type=AIRBUS atc_model=A321 editable=0 performance="Cruise Speed\n0.80 Mach 530 mph 828 km\/h\n\nEngine options\nGeneral Electric CFM56-5B3 30,000 lb thrust\n\nMaximum Range\n2,454 nm 4,352 km\n\nService Ceiling\n41,000 ft 12,497 m\n\nFuel Capacity\n52,500 lb 198,675 kg\n\nEmpty Weight\n105,906 lb 48,139 kg\n\nMaximum Gross Weight\n205,000 lb 93,181 kg\n\nLength\n146 ft 44.51 m\n\nWingspan\n111 ft, 10 in 34.09 m\n\nHeight\n38 ft, 7 in 11.76 m\n\nSeating (typical configuration)\n186" Category = airplane [CameraDefinition.0] Title = "Right Side Window" Guid = {54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC} Description = View of the right wing from the passenger cabin Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.9 ShowWeather = Yes InitialXyz = 3.2, 1.8, -5 InitialPbh = 5, 0, 100 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.1] Title = "Left Side Window" Guid = {0ae3f864-da10-4e5a-977c-b9bba47d6f7a} Description = View of the left wing from the passenger cabin Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 1.0 ShowWeather = Yes InitialXyz = -3.2, 1.8, -5 InitialPbh = 5, 0, 260 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.2] Title = "Landing Gear" Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051} Description = View of the landing gear and left wing inboard flaps Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = .52 ShowWeather = Yes InitialXyz = -3.6, -1.8, -11 InitialPbh = 0, 0, 18 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.3] Title = "Tail" Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c} Description = Looking forward from behind the aircraft Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = .75 ShowWeather = Yes InitialXyz = 0, 5.5, -52.0 InitialPbh = 5, 0, 0 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.4] Title = "Right Wing" Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59} Description = View from the right wing tip looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = 30.8, 1.6, 4.0 InitialPbh = 6, 0, 280 XyzAdjust = TRUE Category=Aircraft MomentumEffect = FALSE ClipMode=Minimum [CameraDefinition.5] Title = "Left Wing" Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de} Description = View from the left wing tip looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = -30.8, 1.6, 4.0 InitialPbh = 6, 0, 80 XyzAdjust = TRUE Category=Aircraft MomentumEffect = No ClipMode=Minimum [CameraDefinition.001] Title = "Right Seat" Guid = {8ff6c134-098d-409f-baec-caba3f683f98} Origin = Virtual Cockpit MomentumEffect = YES SnapPbhAdjust = Swivel SnapPbhReturn = False PanPbhAdjust = Swivel PanPbhReturn = False Track = None ShowAxis = YES AllowZoom = TRUE InitialZoom = .7 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=1.35, 0.0, 0.0 InitialPbh=2, 0, 0 [CameraDefinition.002] Title = "Center Console" Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = None PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.9 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.65, 0.50, -0.2 InitialPbh=70, 0, 0 [CameraDefinition.003] Title = "Overhead Panel" Guid = {4ca337db-ae88-4c5f-96ea-ddebbd2a86fe} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = None PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.8 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.7, -0.58, -0.31 InitialPbh=-58.0, 0, 0 [WEIGHT_AND_BALANCE] max_gross_weight = 187392 // (pounds) empty_weight = 93662 // (pounds) reference_datum_position = -4.5, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -4.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 170.0, 52.0, -3.0, 2.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 170.0, 52.0, 3.0, 2.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = 3500.0, 18.5, -3.0, 2.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = 3500.0, 18.5, 3.0, 2.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = 3500.0, -26.0, -3.0, 2.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = 3500.0, -26.0, 3.0, 2.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_name.0 = "Pilot" station_name.1 = "Co-Pilot" station_name.2 = "First Class A-C" station_name.3 = "First Class D-F" station_name.4 = "Coach A-C" station_name.5 = "Coach D-F" ;Moments of Inertia empty_weight_pitch_MOI = 835131.26 empty_weight_roll_MOI = 198749.02 empty_weight_yaw_MOI = 806087.52 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [GeneralEngineData] engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 5.2, -18.6, -4.6 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = 5.2, 18.6, -4.6 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 1 //Scalar for fuel flow efficiency min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear [TurbineEngineData] fuel_flow_gain = 0.002 //Gain on fuel flow inlet_area = 19.6 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 30000 //Lbs, max rated static thrust at Sea Level afterburner_available = 0 //Afterburner available? reverser_available = 1 //Thrust reverser available? [jet_engine] thrust_scalar = 1.0 [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 30.0 max_generator_alternator_amps = 400.0 //0 Class //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) [contact_points] point.0=1, 43.00, 0.00, -9.70, 1600, 0, 1.442, 55.92, 0.6, 2.5, 0.9, 4.0, 4.0, 0, 220.0, 250.0 point.1=1, -11.20, -12.45, -10.30, 1600, 1, 1.442, 0.00, 1.0, 2.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0 point.2=1, -11.20, 12.45, -10.30, 1600, 2, 1.442, 0.00, 1.0, 2.5, 0.9, 7.1, 7.1, 3, 220.0, 250.0 point.3=2, -19.00, -55.00, 4.00, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -19.00, 55.00, 4.00, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -51.00, 0.00, -2.00, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 54.00, 0.00, -2.00, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 point.7=2, -75.00, 0.00, 31.00, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 max_number_of_points = 21 static_pitch=0.3 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=9.2 //feet, altitude of CG when at rest on the ground gear_system_type=1 //Hydraulic [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 = 25.5 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.885 //Brake scalar auto_brakes = 3 hydraulic_system_scalar = 1 //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 1 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint = 53.0, -1.8, 4.3 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] //Trailing Edge Flaps type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 20 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 10 // degrees flaps-position.2 = 15 // degrees flaps-position.3 = 20 // degrees flaps-position.4 = 40 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.7 drag_scalar = 0.2 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.1] //Leading Edge Slats type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 10 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 18.0 // degrees flaps-position.2 = 22.0 // degrees flaps-position.3 = 22.0 // degrees flaps-position.4 = 27.0 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.3 drag_scalar = 0.2 pitch_scalar= 0.0 system_type = 1 //Hydraulic [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 1, 1 Nav.2 = 1, 1, 0 Adf.1 = 1, 1 Transponder.1 = 1 Marker.1 = 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -19.10, -54.15, 5.85, fx_navredm , light.1 = 3, -19.10, 54.15, 5.85, fx_navgrem , light.2 = 3, -83.60, 0.00, 7.60, fx_navwhih , light.3 = 2, -18.60, -53.50, 5.75, fx_strobeh , light.4 = 2, -18.60, 53.50, 5.75, fx_strobeh , light.5 = 2, 3.70, 0.00, -2.80, fx_beaconb , light.6 = 1, -3.30, 0.00, 11.50, fx_beaconh , //light.7 = 4, 53.41, 0.00, 4.50, fx_vclighth , [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 [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 direction_indicator.1=3,0 [airspeed_indicators] airspeed_indicator.0=1 airspeed_indicator.1=1 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 attitude_indicator.1 = 2 [altimeters] altimeter.0=1 altimeter.1=1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [vacuum_system] max_pressure=5.15 // PSI vacuum_type=2 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [exits] number_of_exits = 3 exit.0 = 0.4, 45.50, -6.0, 7.0, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) exit.1 = 0.4, -33.50, 5.85, 0.0, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) exit.2 = 0.4, 29.90, 6.0, 1.0, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm = 90 autothrottle_takeoff_ga=1 pitch_takeoff_ga = 8; max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=12.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=25.0 gs_integrator_control=0.53 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 yaw_slip_control_gain=0.000000 yaw_control_uses_trim=0.000000 [fuel] Center1 = -4.0, 0.0, 0.0, 2150, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -6.4, -16.8, 0.0, 2040, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -6.4, 16.8 0.0, 2040, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux = -15.2, -37.6, 2.0, 780, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux = -15.2, 37.6, 2.0, 780, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=1 fuel_dump_rate = 0.0167 //Percent of max quantity per second, i.e. about 1 minute for full fuel [airplane_geometry] wing_area = 1320.0 //Square feet wing_span = 112.04 //Feet wing_root_chord = 20.0 //Feet wing_dihedral = 6.5 //Degrees wing_incidence = 1.0 //Degrees wing_twist = -0.5 //Degrees oswald_efficiency_factor= 0.67 //Measure of lift effeciency of wing wing_winglets_flag = 1 //Are winglets available? wing_sweep = 25.0 //Degrees, wing leading edge wing_pos_apex_lon = 8.4 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = -1.6 //Feet, vertical distance from reference point, positive going up htail_area = 280.0 //Square feet htail_span = 39.2 //Feet htail_pos_lon = -69.0 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 3.2 //Feet, vertical distance from reference point, positive going up htail_incidence = 0.0 //Degrees htail_sweep = 34.0 //Degrees, horizontal tail leading edge vtail_area = 288.0 //Square feet vtail_span = 25.6 //Feet, tip to body vtail_sweep = 44.0 //Degrees, vertical tail leading edge vtail_pos_lon = -35.8 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 12.0 //Feet, vertical distance from reference point, positive going up elevator_area = 70.5 //Square feet aileron_area = 26.9 //Square feet rudder_area = 56.2 //Square feet elevator_up_limit = 22.5 //Degrees elevator_down_limit = 19.5 //Degrees aileron_up_limit = 20.0 //Degrees aileron_down_limit = 20.0 //Degrees rudder_limit = 26.0 //Degrees elevator_trim_limit = 20.0 //Degrees spoiler_limit = 60.0 //Degrees spoiler_extension_time = 2.0 //Seconds spoilerons_available = 1 //Spoilerons Available? aileron_to_spoileron_gain = 3 //Aileron to spoileron gain min_ailerons_for_spoilerons = 10 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate auto_spoiler_available = 1 positive_g_limit_flaps_up = 4.0 //Design G load tolerance (positive, flaps up) positive_g_limit_flaps_down= 3.0 //Design G load tolerance (positive, flaps down) negative_g_limit_flaps_up = -3.0 //Design G load tolerance (negative, flaps up) negative_g_limit_flaps_down= -2.0 //Design G load tolerance (negative, flaps down) load_safety_factor = 1.5 //Design G load safety factor fly_by_wire = 1 [Reference Speeds] flaps_up_stall_speed = 142.0 //Knots True (KTAS) full_flaps_stall_speed = 113.0 //Knots True (KTAS) cruise_speed = 477.0 //Knots True (KTAS) max_mach = 0.82 max_indicated_speed = 340 //Red line (KIAS) [stall_warning] type=2 stick_shaker=1 [deice_system] structural_deice_type=1 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots Hope you solve your boogering up! :) - Jens Peter "Penz" Pedersen Link to comment Share on other sites More sharing options...
pstlpete Posted April 12, 2015 Author Share Posted April 12, 2015 Thanx, JP. Appreciate it. Link to comment Share on other sites More sharing options...
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