[fltsim.0] title=Airbus A319-112 Skybus Airlines sim=pa319-cfm56 model=cfm panel= sound= texture=skybus_full checklists= description=Project Airbus A319. \n Visual model by Andy Warden and Derek Mayer. \n Base textures by Demetris Themistocleous and Alessandro Savarese. \n\n US Airways Carolina Panthers (N717UW) Repaint by Joe Shimmel. \n Flight model & Sounds by Peter Binamira. \n\n Copyright Project Airbus 2008.\n atc_id=N521VA atc_airline=Skybus atc_flight_number=58 atc_parking_codes=USA atc_parking_types=GATE ui_manufacturer=Airbus ui_type=A319-100 ui_variation=Skybus (Full Livery) visual_damage=1 atc_heavy=0 [fltsim.1] title=Airbus A319-112 Skybus Airlines "$10 Airfares. Only birds fly cheaper." sim=pa319-cfm56 model=cfm panel= sound= texture=skybus_fares checklists= description=Project Airbus A319. \n Visual model by Andy Warden and Derek Mayer. \n Base textures by Demetris Themistocleous and Alessandro Savarese. \n\n US Airways Carolina Panthers (N717UW) Repaint by Joe Shimmel. \n Flight model & Sounds by Peter Binamira. \n\n Copyright Project Airbus 2008.\n atc_id=N552SX atc_airline=Skybus atc_flight_number=58 atc_parking_codes=USA atc_parking_types=GATE ui_manufacturer=Airbus ui_type=A319-100 ui_variation=Skybus "$10 Airfares" visual_damage=1 atc_heavy=0 [fltsim.2] title=Airbus A319-112 Skybus Airlines White Livery sim=pa319-cfm56 model=cfm panel= sound= texture=skybus_plain checklists= description=Project Airbus A319. \n Visual model by Andy Warden and Derek Mayer. \n Base textures by Demetris Themistocleous and Alessandro Savarese. \n\n US Airways Carolina Panthers (N717UW) Repaint by Joe Shimmel. \n Flight model & Sounds by Peter Binamira. \n\n Copyright Project Airbus 2008.\n atc_id=N571SX atc_airline=Skybus atc_flight_number=58 atc_parking_codes=USA atc_parking_types=GATE ui_manufacturer=Airbus ui_type=A319-100 ui_variation=Skybus (Basic Livery) visual_damage=1 atc_heavy=0 [General] performance=A319-132\nIAE V2524-A5\n\nMZFW: 58,500 KG\nMTOW: 68,000 KG\nMLW: 62,500 KG\n atc_type=Airbus atc_model=A319 [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 [WEIGHT_AND_BALANCE] //A319-132 config //Pax Zonings station_load.0= "5705.3, 17.24, 0.000, 0.000, CAB OA (47)" station_load.1= "5808.6, -3.33, 0.000, 0.000, CAB OB (47)" station_load.2= "5003.1, -20.34, 0.000, 0.000, CAB OC (46)" //Cargo & Baggage station_load.3= "2021.1, 19.17, 0.000, -3.000, CPT 1" //Compartment 1 (5000lbs) 16.13 station_load.4= "2086.5, -14.13, 0.000, -3.000, CPT 4" //Compartment 4 (6660lbs) -16.34 station_load.5= "800.5, -24.85, 0.000, -2.000, CPT 5" //Compartment 5 (3300lbs) -31.19 //Basic Weight/Index= 39657 kgs | 48.5 //Crew 2/4 Cockpit 160 kgs | -1.9 // Cabin 280 kgs | 0.2 //Pantry - REGIONAL 612 kgs | -0.5 //Dry Operating Weight= 40709 kgs | 46.3 ----------------------------------------------------------- //DOW/DOI= 40709 kgs | 89748 lbs 46.3 ----------------------------------------------------------- empty_weight=89748.0 empty_weight_roll_MOI=931400.000000 empty_weight_pitch_MOI=1100000.000000 empty_weight_yaw_MOI=1000000.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight=166756 reference_datum_position=0.0000,0.000000,0.000000 empty_weight_CG_position=0.69,0.000000,0.000000 CG_forward_limit=0.17 CG_aft_limit=0.37 //Weight & Balance prepared by PB. (Version 150 Y) [airplane_geometry] wing_area=1317.503 wing_span=111.833333 wing_root_chord=13.76 wing_dihedral=3.298901 wing_incidence=-3.5 wing_twist=-1.600000 oswald_efficiency_factor=0.745 //.76 wing_winglets_flag=1 wing_sweep=25.0000 wing_pos_apex_lon=16.102 //17.655 //15.982 //13.3 wing_pos_apex_vert=0.90000 htail_area=333.681 htail_span=41.666667 htail_pos_lon=-50.703 htail_pos_vert=6.500000 htail_incidence=1.500000 htail_sweep=0.000000 vtail_area=231.424 vtail_span=17.991665 vtail_sweep=0.000000 vtail_pos_lon=-48.865 vtail_pos_vert=19.915 elevator_area=76.500000 aileron_area=57.0 rudder_area=56.200000 elevator_up_limit=25.0 elevator_down_limit=15.0 aileron_up_limit=25.0 aileron_down_limit=15.0 rudder_limit=25.0 elevator_trim_limit=13.5 spoiler_limit=35.0 spoilerons_available=1 aileron_to_spoileron_gain=1.5 min_ailerons_for_spoilerons=12 min_flaps_for_spoilerons=0 [GeneralEngineData] engine_type=1 fuel_flow_scalar=0.996 //CRZ SFC 1.086 Engine.0=6.500000,-18.95,-5.125 Engine.1=6.500000,18.95,-5.125 min_throttle_limit=-0.499939 //-0.4 [Reference Speeds] flaps_up_stall_speed=128.000 full_flaps_stall_speed=102.000 cruise_speed=462.0 max_indicated_speed=350.000000 max_mach=0.825 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 800 autothrottle_available= 1 //use_no_default_pitch= 1 //use_no_default_bank= 1 pitch_takeoff_ga= 18 autothrottle_arming_required= 1 autothrottle_takeoff_ga= 1 autothrottle_max_rpm= 92.5 default_pitch_mode= 0 default_bank_mode= 0 max_pitch= 10.00 max_pitch_acceleration= 2.00 max_pitch_velocity_lo_alt= 4.00 max_pitch_velocity_hi_alt= 1.50 //2.00 max_pitch_velocity_lo_alt_breakpoint= 20000 max_pitch_velocity_hi_alt_breakpoint= 24000 max_bank= 25.00 max_bank_acceleration= 2.0 max_bank_velocity= 3.0 max_throttle_rate= 0.20 nav_proportional_control= 12.00 nav_integrator_control= 0.05 nav_derivative_control= 0.01 nav_integrator_boundary= 0.5 nav_derivative_boundary= 0.35 gs_proportional_control= 15.0 //11.0 gs_integrator_control= 0.30 gs_derivative_control= 0.00 gs_integrator_boundary= 0.7 gs_derivative_boundary= 0.00 yaw_damper_gain= 1.00 [direction_indicators] direction_indicator.0=3,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn320, 1 [RADIOS] // Radio Type=avail?,sby freq?,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= 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) static_pitch=-0.319722 static_cg_height=11.60811023622 point.0=1.0, 32.83, 0.0000,-11.72, 800,0.0,1.5,68.0,0.70,1.4390000,0.68,13.200000,12.900000,0.000000,252.000000,282.000000 point.1=1.0,-4.160,-12.458,-12.22,1200,1.0,1.9,0.00,0.72,1.5419948,0.81,14.000000,13.700000,2.000000,252.000000,282.000000 point.2=1.0,-4.160, 12.458,-12.22,1200,2.0,1.9,0.00,0.72,1.5419948,0.80,14.200000,13.300000,3.000000,252.000000,282.000000 point.3=2.0,-13.750000,-54.583333,-0.500000,750.924659,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.0,-13.750000,54.583333,-0.500000,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0 point.5=2.0,-63.250000,0.0,4.050,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0 point.6=2.0,46.666667,0.0,-4.166667,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0 point.7=5.0,-3.000, 0,0000,0.0000, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 0.2, 0.2, 0, 0.0, 0.0 gear_system_type=0 [fuel] Center1= 1.95, 0.0, -4.00, 2179.6, 8.0 LeftMain= 2.35, -19.6, 1.40, 1829.6, 5.0 //3.45 RightMain= 2.35, 19.6, 1.40, 1829.6, 5.0 //3.45 LeftAux= -5.50, -36.4, 2.20, 232.5, 5.0 RightAux= -5.50, 36.4, 2.20, 232.5, 5.0 fuel_type=2.0 number_of_tank_selectors=1 electric_pump=0 [keyboard_response] aileron=180.000000,130.000000 [pitot_static] vertical_speed_time_constant=99 [Views] eyepoint=41.22074, -1.73061,4.155627 [Flaps.0] span-outboard=0.500000 extending-time=21.000000 system_type=1 type=1 flaps-position.0=0.000000,0.000000 flaps-position.1=0.0 flaps-position.2=13.0 flaps-position.3=20.0 flaps-position.4=29.0 flaps-position.5=40.0 lift_scalar=0.0 drag_scalar=0.0 [flaps.1] type=2 // slats span-outboard=0.95 // 0.0 .. 1.0 extending-time=21 // seconds flaps-position.0=0 flaps-position.1=18, flaps-position.2=18, flaps-position.3=22, flaps-position.4=22, flaps-position.5=27, blowout-speed=260 // KIAS lift_scalar=0.10 drag_scalar=0.43 pitch_scalar=0.3 system_type=1 [flaps.2] //ailerons type=2 span-outboard=0.85 extending-time=13.000 system_type=1 damaging-speed=233.000 blowout-speed=250.000 flaps-position.0=0.000, flaps-position.1=0.000, flaps-position.2=5.000, flaps-position.3=5.000, flaps-position.4=5.000, flaps-position.5=5.000, lift_scalar=0.25 drag_scalar=0.20 [flaps.3] //actual flaps type=1 span-outboard=0.85 extending-time=21.000 system_type=1 damaging-speed=233.000 blowout-speed=250.000 flaps-position.0=0.000, flaps-position.1=0.000, flaps-position.2=10.000, flaps-position.3=15.000, flaps-position.4=20.000, flaps-position.5=40.000, lift_scalar=0.66 //1.178 drag_scalar=0.75 [jet_engine] thrust_scalar=1.050 [TurbineEngineData] fuel_flow_gain=0.0021 //0.00194 inlet_area=21.3000 rated_N2_rpm=15183.000000 static_thrust=21640.000000 //More than CFM56-5B6 MCT 21630 5B5 20250 Underpower 24570 afterburner_available=0 reverser_available=1 bypass_ratio=4.90 [exits] number_of_exits=2 exit_rate.0=0.19 ;Percent per second exit_rate.1=0.17 ;Percent per second [flight_tuning] elevator_effectiveness=1.0 pitch_stability=1.2 roll_stability=1.0 yaw_stability=1.0 aileron_trim_effectiveness=0.9 rudder_trim_effectiveness=1.1 cruise_lift_scalar = 1.35 //36 parasite_drag_scalar=1.0 induced_drag_scalar=0.98 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //light.0=3, -14.00, -54.9, 2.45, fx_navred320pa , //light.1=3, -14.00, 54.9, 2.45, fx_navgre320pa , light.2=3, -62.00, 0.00, 4.70, fx_navwhi320pa , light.3=2, -62.10, 0.00, 4.70, fx_strobe2320pa , //light.4=2, -14.22, -54.91, 2.45, fx_strobe320pa , //light.5=2, -14.22, 54.91, 2.45, fx_strobe320pa , light.6=1, 6.8, 0.00, -5.80, fx_beacon320pa , light.7=1, 3.83, 0.00, 8.47, fx_beacon320pa , light.8=4, 44.41, 0.00, 3.50, fx_vclight , [SMOKESYSTEM] smoke.0=88.0,-17.3,-39.8, fx_contrail_320 smoke.1=88.0,-17.3,39.8, fx_contrail_320 [TailHook] tailhook_length=4 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0.9 [folding_wings] wing_fold_system_type=4 fold_rates=0.11,0.13 ;Percent per second [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 200 electric_always_available = 1 flap_motor = 0, 0 , 17.0 gear_motor = 0, 0 , 17.0 autopilot = 0, 0 , 17.0 avionics_bus = 0, 0 , 17.0 avionics = 0, 0 , 17.0 pitot_heat = 0, 0 , 17.0 additional_system = 0, 0 , 17.0 marker_beacon = 0, 0 , 17.0 gear_warning = 0, 0 , 17.0 fuel_pump = 0, 0 , 17.0 starter1 = 0, 0 , 17.0 starter2 = 0, 0 , 17.0 light_nav = 0, 0 , 17.0 light_beacon = 0, 0 , 17.0 light_landing = 0, 0 , 17.0 light_taxi = 0, 0 , 17.0 light_strobe = 0, 0 , 17.0 light_panel = 0, 0 , 17.0 light_cabin = 0, 0 , 17.0 auto_brakes = 0, 0 , 17.0 standby_vacuum = 0, 0 , 17.0 hydraulic_pump = 0, 0 , 17.0 fuel_transfer_pump = 0, 0 , 17.0 light_recognition = 0, 0 , 17.0 light_wing = 0, 0 , 17.0 light_logo = 0, 0 , 17.0 directional_gyro = 0, 0 , 17.0 directional_gyro_slaving = 0, 0 , 17.0 [brakes] toe_brakes_scale=0.58 //0.59 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 //FDE copyright Peter Binamira - //peter@philskies.net //Finalization by Derek Mayer - //mayerderek@hotmail.com //-For Project Airbus A319 0nly-