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SKL701

A319CJ- PSS Gauge modif

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Guest vrandar

Below is an aircraft.cfg for the iFDG/PSS Privatair A319X-CJ from avsim.//LONG RANGE CENTRE TANK - DO NOT COPY TO OTHER A319s[fltsim.0]title=A319-100 IAE Privatairsim=A319_IAE_IFDG_011model=IAEpanel=sound=texture=PVTkb_checklists=kb_reference=atc_id=D-APACatc_airline=Privatairatc_flight_number=223atc_heavy=0ui_manufacturer=iFDG Airbus A319ui_type=A319-133X/CJui_variation=Privatair - for Lufthansadescription="The A320 was launched on March 2, 1984. It is the first subsonic commercial aircraft with fly-by-wire controls. First flight took place on February 22, 1987. The A320-100 was the initial version and was superseded by the A320-200 from the third quarter of 1988. The A320-200 differs from the A320-100 in having wingtip fences, a wing center-section fuel tank, and a higher MTOW. Model by Albaro Villegas and Ric Barker. Master Textures by Ben Jones. FDE by Eugene "Schitirlitz" Schneider."atc_id_color=0000000000visual_damage=0prop_anim_ratio=1.72[General]atc_type=Airbus atc_model=A319 editable=1 performance=EnginesnIAE V2527M-A5 rated at 24,800 lbsnnTypical Cruise Speedn0.78 Mach at 35,000 ftnnMax SpeednVmo 350 kts Mmo 0.82 MachnnRange(150 pax)n2,900 nm (5,374 km)nnMax Fueln42,230 lbs (6,303 US gal)nnMax Takeoff Weightn162,040 lbsnnMax Gross Weight (taxi weight)n162,900 lbsnnMax Payloadn42,370 lbs [pitot_static]vertical_speed_time_constant = 1[weight_and_balance]// ACM V2.3max_gross_weight = 154322empty_weight = 86421.1reference_datum_position = 0, 0, 0empty_weight_CG_position = 0, 0, 0empty_weight_pitch_MOI = 1312117empty_weight_roll_MOI = 578755empty_weight_yaw_MOI = 1392885empty_weight_coupled_MOI = 0max_number_of_stations = 6station_load.0 = 0450, 0.0, 0.0, 0.0, Pilotsstation_load.1 = 3000, 0.0, 0.0, 0.0, Galleysstation_load.2 = 4250, 0.0, 0.0, 0.0, Baggagestation_load.3 = 4920, 0.0, 0.0, 0.0, Mail and Cargostation_load.4 = 4320, 0.0, 0.0, 0.0, First Classstation_load.5 = 6960, 0, 0, 0, Meals[lights]//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landinglight.0 = 3, -15.888, -54.32, 3.11, iFDG_A320_rednavlight.1 = 3, -15.888, 54.32, 3.11, iFDG_A320_greennavlight.2 = 3, -64.88, 0, 5.09, iFDG_A320_whitenavlight.3 = 2, -64.88, 0, 5.07, iFDG_A320_whitestrobe_taillight.4 = 2, -16.41, -54.68, 3.15, iFDG_A320_whitestrobelight.5 = 2, -16.41, 54.68, 3.15, iFDG_A320_whitestrobelight.6 = 1, 2.90, 0, 9.20, iFDG_A320_redbeacon_toplight.7 = 1, 6.37, 0, -5.03, iFDG_A320_redbeacon_bottomlight.8 = 3, -56.73, 11.50, 5.86, iFDG_A320_logolight.9 = 3, -56.73, -11.5, 5.86, iFDG_A320_logolight.10 = 3, 22.03, 6.56, 1.79, iFDG_A320_inspectionlight.11 = 3, 21.777, -6.56, 1.79, iFDG_A320_inspection[GeneralEngineData]//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turbopropengine_type = 1fuel_flow_scalar = 0.94engine.0 = 11.25, -19, -4.96,engine.1 = 11.25, 19, -4.96,min_throttle_limit=-0.269958[smokesystem]smoke.0 = 0.80052, -18.00157, 43.23110, iFDG_A320_flapsmoke.1 = 0.80052, -18.00157, -43.23110, iFDG_A320_flap[effects]wake = fx_wakewater = fx_spraydirt = fx_tchdrtconcrete = fx_sparkstouchdown = ifdg_a320_touchdown, 1[fuel]//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)fuel_type = 2number_of_tank_selectors = 2Center1 = 0, 0, -4.11, 6613, 6.1LeftMain = -4, -19.01, -0.82, 2062, 15.6RightMain = -4, 19.01, -0.82, 2062, 15.6electric_pump=1[contact_points]static_pitch = 1.69static_cg_height = 10.2max_number_of_points = 11point.0 = 1, 29.1326, 0, -11.8209, 1574.8, 0, 1.68, 75, 1.33, 1.9, 0.7, 9, 9.4, 0, 0, 0point.1 = 1, -6.4, -12, -11.7, 1574.803, 1, 1.68, 0, 1.2, 2.1, 0.4, 11.7, 13, 2, 0, 0point.2 = 1, -6.4, 12, -11.7, 1574.803, 2, 1.68, 0, 1.2, 2.1, 0.4, 10.2, 12.9, 3, 0, 0point.3 = 2, 9.5, -19, -8.9019, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0point.4 = 2, -13.75, -55.1991, 1.8224, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0point.5 = 2, 9.5, 19, -8.9019, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0point.6 = 2, -13.75, 55.3538, 2.2868, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0point.7 = 2, -24.8662, 0, -4.7462, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0point.8 = 2, -65.3513, 0, 5.1893, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0point.9 = 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0point.10 = 2, 46.4048, 0, -0.1781, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0gear_system_type=1[keyboard_response]elevator = 150, 250aileron = 150, 250rudder = 150, 250[forcefeedback]gear_bump_nose_magnitude = 1000gear_bump_nose_direction = 18000gear_bump_nose_duration = 250000gear_bump_left_magnitude = 2000gear_bump_left_direction = 35500gear_bump_left_duration = 250000gear_bump_right_magnitude = 2000gear_bump_right_direction = 500gear_bump_right_duration = 250000ground_bumps_magnitude1 = 1250ground_bumps_angle1 = 8900ground_bumps_intercept1 = 5ground_bumps_slope1 = 0.48ground_bumps_magnitude2 = 450ground_bumps_angle2 = 9100ground_bumps_intercept2 = 0.075ground_bumps_slope2 = 1crash_magnitude1 = 10000crash_direction1 = 1000crash_magnitude2 = 10000crash_direction2 = 9000crash_period2 = 7500crash_duration2 = 2500000stick_shaker_magnitude = 8000stick_shaker_direction = 0stick_shaker_period = 111111[airplane_geometry]wing_area = 1317.503wing_span = 111.2529wing_root_chord = 17.07476wing_dihedral = 5.11wing_incidence = -0.784wing_twist = 0oswald_efficiency_factor = 0.75wing_winglets_flag = 1wing_sweep = 25wing_pos_apex_lon = 11.850wing_pos_apex_vert = -1.64htail_area = 333.6812htail_span = 40.84htail_pos_lon = -53.54htail_pos_vert = 4.40htail_incidence = -1htail_sweep = 34vtail_area = 231.4241vtail_span = 20.53vtail_sweep = 35vtail_pos_lon = -50.53vtail_pos_vert = 8.75elevator_area = 70.5aileron_area = 40.22rudder_area = 56.2elevator_up_limit = 28.0elevator_down_limit = 20.0aileron_up_limit = 26.0aileron_down_limit = 26.0rudder_limit = 25.0elevator_trim_limit = 18.5spoiler_limit = 35.0aileron_to_spoileron_gain = 1min_ailerons_for_spoilerons = 10min_flaps_for_spoilerons = 0spoilerons_available = 1[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 60electric_always_available = 0flap_motor = 0, 5, 17gear_motor = 0, 5, 17autopilot = 0, 5, 17avionics_bus = 0, 0, 17avionics = 1, 0, 17pitot_heat = 0, 2, 17additional_system = 0, 0, 17marker_beacon = 1, 2, 17gear_warning = 0, 2, 17fuel_pump = 0, 5, 17starter1 = 0, 20, 17light_nav = 0, 0, 17light_beacon = 0, 5, 17light_landing = 0, 5, 17light_taxi = 0, 5, 17light_strobe = 0, 5, 17light_panel = 0, 0, 17[Reference Speeds]flaps_up_stall_speed=128.0 full_flaps_stall_speed=102.0 cruise_speed=455.0 max_mach = 0.82max_indicated_speed = 350.0[Flaps.0]type=1span-outboard = 0.78extending-time = 14flaps-position.0 = 0.0, 0flaps-position.1 = 1.0, 230 //Conf. 1 Intermediate approachflaps-position.2 = 10.0, 215 //Conf. 1+F Take offflaps-position.3 = 15.0, 200 //Conf. 2 Take off and Approachflaps-position.4 = 20.0, 185 //Conf. 3 Take off, Approach, and Landingflaps-position.5 = 40.0, 177 //Conf "Full" Landingdamaging-speed = 230.0blowout-speed = 250.0lift_scalar = 0.547 //0.57drag_scalar = 1.25pitch_scalar = 0system_type = 1 //Hydraulic[flaps.1]type=2 // 1 - tail, 2 - leadspan-outboard = 0.85extending-time = 4flaps-position.0 = 0, 0flaps-position.1 = 18, 230 //Conf. 1 Intermediate approachflaps-position.2 = 22, 215 //Conf. 1+F Take offflaps-position.3 = 22, 200 //Conf. 2 Take off and Approachflaps-position.4 = 22, 185 //Conf. 3 Take off, Approach, and Landingflaps-position.5 = 27, 177 //Conf "Full" Landingdamaging-speed = 230blowout-speed = 250lift_scalar = 0.5 //0.55 drag_scalar = 0.4pitch_scalar = 0.2system_type = 1 //Hydraulic[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 [TurbineEngineData]fuel_flow_gain=0.004 inlet_area=22.22 rated_N2_rpm=14950 static_thrust=24800 //IAE V2527M-A5afterburner_available=0 reverser_available=1 [jet_engine]thrust_scalar=1.0 [autopilot]autopilot_available=1 flight_director_available=1 default_vertical_speed=700.000000 autothrottle_available=1 autothrottle_arming_required=1autothrottle_takeoff_ga=1autothrottle_max_rpm=113.000000pitch_takeoff_ga=10.000000 max_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=1.8max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control = 9.00nav_integrator_control = 0.25nav_derivative_control = 0.00nav_integrator_boundary = 2.50nav_derivative_boundary = 0.00gs_proportional_control = 9.52gs_integrator_control = 0.26gs_derivative_control = 0.00gs_integrator_boundary = 0.70gs_derivative_boundary = 0.00yaw_damper_gain = 1.00[gear_warning_system]gear_warning_available = 1 //Normalpct_throttle_limit = 0.125 //Percent throttle that activates warningflap_limit_idle = 5.0 //Flap angle that activates warning at idleflap_limit_power = 25.5 //Flap angle that activates warning at above idle[brakes]toe_brakes_scale=0.66parking_brake=1[hydraulic_system]normal_pressure=3000.0 //PSIelectric_pumps=0 //no electric pumpsengine_map=1,1,0,0 //pumps on Eng1,2[Views]eyepoint=43.22074,-1.723061,4.355627 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)[Radios]// Radio Type = availiable, standby frequency, has glide slopeAudio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [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 [attitude_indicators]//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyroattitude_indicator.0 = 2 attitude_indicator.1 = 1 [turn_indicators]//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyroturn_indicator.0=0,0[exits]number_of_exits = 2exit_rate.0 = 0.4 ;Percent per secondexit_rate.1 = 0.4 ;Percent per second[stall_warning]type=2[Views]eyepoint=43.22074,-1.723061,4.355627 ///(feet) longitudinal, lateral, vertical distance from reference datum3[TailHook]tailhook_length=1 ;(feet)tailhook_position=0, 0, 0 ;(feet) longitudinal, lateral, vertical positions from datumcable_force_adjust=1[folding_wings]wing_fold_system_type=4fold_rates=0.11,0.13Rob Elliott, EGPE InvernessPSS Airbus Support andAirbus Fleet Training Captain, British Airways Virtual airbus@speedbirdonline.co.ukhttp://www.speedbirdonline.co.uk/airbus.htmlhttp://www.bavirtual.co.uk

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Thank you Rob,but is not enough because i need to modified the gauge...CiaoFranco

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Rob,whit your aircraft.cfg the FMGS will accep the weigth?Sorry i lost my HD and i'm installing all on the new HD ...hard work!CiaoFranco

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NO Rob,it don't work like in the picture...I found the gouge patched and now work correct see the pictureThanksFranco

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Guest vrandar

Odd, it works for me. I'll have a look at this tomorrow.Edit: I've just loaded it up with a ZFW of 50 tonnes and fuel of 27.5 tonnes. This figure goes into the Block Fuel LSK without problem (see attached screenshot). You are entering the block fuel in the format 27.5 aren't you?Edit2: I've just seen your second screenshot and re-read your post: I see you got it sorted!Rob Elliott, EGPE InvernessPSS Airbus Support andAirbus Fleet Training Captain, British Airways Virtual airbus@speedbirdonline.co.ukhttp://www.speedbirdonline.co.uk/airbus.htmlhttp://www.bavirtual.co.uk

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Hello my friends,I'm an user of the models of iFDG, but my great passion is ACJ 319, in special, the model of the Brazilian Air Force. E would like to know of the friends if it does not have as to develop a proper FDE or one config for the ACJ. I have here the original manual of it with all the weight configurations. Until already I used this fuel configuration that was passed in the previous topic, but wanted to configure it correctly, with the number of passengers that is pertimito and the configurations in the panel of the PSS, since the FMGS of it only reads until 21.000Kg and the real ACJ supports until 32.000Kg.Please, they help me, is very important for me, since I only fly military aircraft and configs that they exist for the Airbus is all of the c

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Guest vrandar

It's deeply embarrassing to read now but in my earlier posts back at the end of '05 it's clear that at the time although I had the changes to the cfg I was not aware of the small program that changes the gauge. However I do have it and will send it to you if you email me (address below).Edit: Saul, I have now seen your email. The fuel tank modification will be sent to you today together with answers to your other questions.Rob Elliott, EGPE InvernessPSS Airbus Support andAirbus Fleet Training Captain, British Airways Virtual airbus@speedbirdonline.co.ukhttp://www.speedbirdonline.co.uk/airbus.htmlhttp://www.bavirtual.co.uk

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Hi Mister Rob,You still have that one gauge that she modifies the reading of weights of the fuel, in the FMGS of the Airbus?Best Regards,PS: My email is-> saulgaleno@hotmail.comSaul Galeno.

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I've started using the PSS Airbus again and also had this mod on my old HD but have since lost it. If anyone could e-mail it to me I would be most greatful. I've searched all over the web but had no luck.Many thanksGavine-mail: altecair@live.com

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