Sign in to follow this  
Guest CoolDead

Convert A319 to ACJ

Recommended Posts

Airbus ACJ is based in A319 body, but have very more range than A319. Is posible make changes in the config of the A319 in order to obtain the same characteristics of ACJ ???Thank's

Share this post


Link to post
Share on other sites
Help AVSIM continue to serve you!
Please donate today!

Yes the long range centre tank can be added. The aircraft.cfg for this is shown below. You will need to change the fltsim.0 section to the aircraft you are flying and make sure the sim= line gives the exact name of your air file. Other than that no changes should be necessary. The simulator will say in the Fuel and Payload menu that you are overweight but ignore that.//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=atc_id_color=0000000000visual_damage=0prop_anim_ratio=1.72[General]atc_type=Airbus atc_model=A319 editable=1 performance=[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[exits]number_of_exits = 2exit_rate.0 = 0.2 ;Percent per secondexit_rate.1 = 0.2 ;Percent per second[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=0.11,0.13

Share this post


Link to post
Share on other sites

The forum code changed chunks of that, sorry. I'll try again as plain text but any problem, just email me and I'll send the file.://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[exits]number_of_exits = 2exit_rate.0 = 0.2 ;Percent per secondexit_rate.1 = 0.2 ;Percent per second[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=0.11,0.13

Share this post


Link to post
Share on other sites

Thanks a lot Rob, but this is a cfg from IFDG plane and i want to use de cfg from my PSS A319, I only need to change the tank fuel caracteristics ?? or i need to make some other changes ?Thanks

Share this post


Link to post
Share on other sites
Sign in to follow this