[fltsim.0] title=INTER A319 sim=A319 model= panel= sound= texture= checklists= panel_alias= sound_alias= kb_checklists= kb_reference= atc_id=CS-AFR atc_airline=INTER atc_flight_number=319 atc_heavy=0 ui_manufacturer=Airbus ui_type=INTER A319 ui_variation= INTER TransAir description=The Airbus A319 is a highly sophisticated, all electric medium jet. The state-of-the-art flight deck features multiple color displays and a highly advanced flight contol system. The pilot flys the plane with a "sidestick", a joystick mounted to the side, rather than the conventional yoke. With advanced aerodynamics and electronic engine control systems, it can cruise at mach 0.8 with excellent fuel efficiency. Plane built with AD2000 v2.1 by Mike Stone and repaint for the Virtual Aero Club Belgium by Michel Melchior.\nFS2002 - A319 version 0.8 [General] performance=Cruise Speed\t.80 Mach\nMaximum Range\t3,400 miles\nService Ceiling\t36,000\nMax Takeoff Weigh 161,000 lb\nSeating\t\t150 to 179\nCargo Capacity\t1,322 CU ft\n\n atc_type=AIRBUS atc_model=A319 [flight_tuning] pitch_stability=2.5 [Radios] Radio type=availeble, stanby, 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 Transponder.1=1 Marker.1=1 [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=100 station_load.0=170, 51.86, -3.21,7.46 //Pilot Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, 51.86, 3.21,7.46 //Co-Pilot Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=170, 41.68, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=170, 41.68, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=170, 41.68, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=170, 41.68, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6=170, 38.47, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7=170, 38.47, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8=170, 38.47, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.9=170, 38.47, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.10=170, 31.67, -3.21,6.93 //Stewardess Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.11=170, 31.67, 0.00,6.93 //Stewardess Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.12=170, 31.67, 3.21,6.93 //Stewardess Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.13=170, 24.88, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.14=170, 24.88, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.15=170, 24.88, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.16=170, 24.88, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.17=170, 24.88, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.18=170, 22.61, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.19=170, 22.61, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.20=170, 22.61, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.21=170, 22.61, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.22=170, 22.61, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.23=170, 20.34, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.24=170, 20.34, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.25=170, 20.34, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.26=170, 20.34, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.27=170, 20.34, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.28=170, 18.07, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.29=170, 18.07, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.30=170, 18.07, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.31=170, 18.07, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.32=170, 18.07, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.33=170, 15.80, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.34=170, 15.80, -1.07,6.93 //Stewardess Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.35=170, 15.80, 0.00,6.93 //Stewardess Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.36=170, 15.80, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.37=170, 15.80, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.38=170, 13.53, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.39=170, 13.53, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.40=170, 13.53, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.41=170, 13.53, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.42=170, 13.53, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.43=170, 11.26, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.44=170, 11.26, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.45=170, 11.26, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.46=170, 11.26, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.47=170, 11.26, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.48=170, 8.99, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.49=170, 8.99, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.50=170, 8.99, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.51=170, 8.99, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.52=170, 8.99, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.53=170, 6.72, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.54=170, 6.72, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.55=170, 6.72, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.56=170, 6.72, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.57=170, 6.72, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.58=170, 4.45, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.59=170, 4.45, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.60=170, 4.45, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.61=170, 4.45, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.62=170, 4.45, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.63=170, 2.18, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.64=170, 2.18, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.65=170, 2.18, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.66=170, 2.18, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.67=170, 2.18, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.68=170, -0.09, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.69=170, -0.09, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.70=170, -0.09, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.71=170, -0.09, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.72=170, -0.09, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.73=170, -2.36, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.74=170, -2.36, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.75=170, -2.36, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.76=170, -2.36, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.77=170, -2.36, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.78=170, -4.63, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.79=170, -4.63, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.80=170, -4.63, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.81=170, -4.63, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.82=170, -4.63, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.83=170, -6.90, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.84=170, -6.90, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.85=170, -6.90, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.86=170, -6.90, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.87=170, -6.90, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.88=170, -9.17, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.89=170, -9.17, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.90=170, -9.17, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.91=170, -9.17, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.92=170, -9.17, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.93=170,-11.44, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.94=170,-11.44, -1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.95=170,-11.44, 0.00,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.96=170,-11.44, 1.07,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.97=170,-11.44, 3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.98=170,-13.71, -3.21,6.93 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.99=12258, 15.51, 0.0 ,1.61 //Baggage/Cargo Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.100=12258,-15.51, 0.0 ,1.61 empty_weight=91500.000 empty_weight_roll_MOI=2480000.000 empty_weight_pitch_MOI=3480000.000 empty_weight_yaw_MOI=3660000.000 empty_weight_coupled_MOI=1000.000 max_gross_weight=133709.999 CG_forward_limit=0.000 CG_aft_limit=1.000 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain=-3.000, -19.000, 0.000, 3150.000, 0.000 RightMain=-3.000, 19.000, 0.000, 3150.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=1320.000 wing_span=111.833 wing_root_chord=10.500 wing_dihedral=4.999 wing_incidence=0.000 wing_twist=-0.500 oswald_efficiency_factor=0.500 wing_winglets_flag=65535 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=315.000 htail_span=42.000 htail_pos_lon=-63.000 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=0.000 vtail_area=286.000 vtail_span=19.282 vtail_sweep=0.000 vtail_pos_lon=-63.000 vtail_pos_vert=22.000 elevator_area=42.000 aileron_area=40.000 rudder_area=77.000 elevator_up_limit=26.001 elevator_down_limit=26.001 aileron_up_limit=30.000 aileron_down_limit=30.000 rudder_limit=30.000 elevator_trim_limit=19.996 spoiler_limit=59.989 spoilerons_available=0 aileron_to_spoileron_gain=3.000 min_ailerons_for_spoilerons=9.969 min_flaps_for_spoilerons=0.000 [contact_points] point.0=1.000, 36.000, 0.000, -12.167, 1181.102, 0.000, 1.427, 55.920, 0.983, 2.500, 0.807, 4.000, 4.000, 0.000, 0.000, 0.000 point.1=1.000, -4.750, -8.583, -12.167, 1574.803, 1.000, 1.427, 0.000, 0.983, 2.500, 0.706, 6.900, 6.900, 2.000, 0.000, 0.000 point.2=1.000, -4.750, 8.583, -12.167, 1574.803, 2.000, 1.427, 0.000, 0.983, 2.500, 0.706, 7.100, 7.100, 3.000, 0.000, 0.000 point.3=2.000, -14.167, -47.333, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4=2.000, -14.167, 47.333, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5=2.000, -54.000, 0.000, 2.833, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6=2.000, 42.667, 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, 0.000 static_pitch=0.000 static_cg_height=11.014 [GeneralEngineData] engine_type=1 Engine.0=4.417, -19.000, 0.000 Engine.1=4.417, 19.000, 0.000 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_scalar=1.000 fuel_flow_gain=0.002 inlet_area=19.600 rated_N2_rpm=29920.000 static_thrust=26500.000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=140.000 full_flaps_stall_speed=112.000 cruise_speed=429.032 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=43.317339,-1.499446,5.164760 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 autoland_available=1 use_no_default_bank=1 use_no_default_pitch=1 [direction_indicators] direction_indicator.0=3,0 [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [Flaps.0] type=1 span-outboard=0.500 extending-time=7.000 system_type=0 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=1.000 flaps-position.0=0.000, 0.000 flaps-position.1=13.331, 0.000 flaps-position.2=26.662, 0.000 flaps-position.3=39.992, 0.000
