[fltsim.0] title=Airbus A340-600 Etihad Airways - Grand Prix 2011 Abu Dhabi sim=a346 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=A6-EHH atc_airline=Etihad atc_flight_number=EY17 atc_heavy=1 ui_manufacturer=Airbus ui_type=A340-600 ui_variation=Etihad Airways - Grand Prix 2011 Abu Dhabi visual_damage=1 description= fly.afsalzain © 2011 Re-paints - www.fly.afsalzain.com [General] atc_type=AIRBUS atc_model=A340 editable=1 performance=Maximum Cruise: Mach .86\nEngines: Four (4) RR Trent 556 Turbofans\nThrust: 56,000 lbs or 20,901 KG\nMaximum Range: 7480 NM or 13,853 KM\nPax Capacity: 380 - 475 Passengers\nSimuBuild Freeware Group\nDesigner: Herve Dongmo\nFlight Dynamics: SimuBuild FDX Engineering Department\nTextureing: SimuBuild Texture Department\nFlight Deck: SimuBuild Flightdeck Engineering.\n Visit us at simubuild.cjb.net\nV1K-2 Category=airplane [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [WEIGHT_AND_BALANCE] max_gross_weight= 804675 // (pounds)920000 empty_weight=391000 // (pounds) reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-2, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 //PASSENGER WEIGHT LOADOUT station_load.0=10620, 0.0, 0.0,0.0 //PAX SEC 1 (DEFAULT:10620)78, 0,0.98 / station_load.1=18360, 0.0, 0.0,0.0 //PAX SEC 2 (DEFAULT:18360)-0.55, 0,0.98 station_load.2=8100, 0.0, 0.0,0.0 //PAX SEC 3 (DEFAULT:8100)-55.7, 0,0.98 //station_load.3=139074,0,0,0 //AFT Galley Payload (MAX: MIN: DEFAULT:) Rick added //CARGO AND FRIEGHT LOADOUT station_load.4=4037, 0.0, 0.0,0.0 //FORE CARGO COMPARTMENT (DEFAULT: 4037) 96.03,0,-4.26 station_load.5=3131, 0.0, 0.0,0.0 //AFT LARGE CARGO COMPARTMENT(DEFAULT:3131)-69.16,0,-4.26 station_load.6=1071, 0.0, 0.0,0.0 //AFT SMALL CARGO COMPARTMENT(DEFAULT:1071)-76.96,0,-4.26 //PILOT AND RELIEF WEIGHT station_load.7=180, 0.0, 0.0,0.0 //CAPTAIN WEIGHT (DEFAULT: 180)-1.6,118.1,1.6 station_load.8=180, 0.0, 0.0,0.0 //FIRST OFFICER WEIGHT (DEFAULT: 180)1.6,118.1,1.6 station_load.9=220, 0.0, 0.0,0.0 //JUMPSEAT/RELIEF PILOT(S) (DEFAULT: 220)2.2,114.8,1.6 ;Moments of Inertia empty_weight_roll_MOI=15352310 empty_weight_pitch_MOI=24223159 empty_weight_yaw_MOI=39531785 empty_weight_coupled_MOI=0 ;2142 [fuel] Center1=21.3, 0.0, -7.0, 18786.0, 7.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center1=21.3, 0.0, -7.0, 14788.0, 7.0 Center2=-37.0, 0.0, 6.5, 2177.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center2=-107.0, LeftMain=20, -50.1, -4.0, 15588.0, 9.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux=-2.3, -63.0, -3.0, 1680.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=20, 50.1, -4.0, 15588.0, 9.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux=-2.3, 63.0, -3.0, 1680.0, 0.0 //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 [airplane_geometry] wing_area=4729.16 //Square feet wing_span=208.5 //Feet wing_root_chord=45.3 //Feet wing_dihedral=7.0 //Degrees wing_incidence=2.0 //Degrees wing_twist=-1.0 //Degrees oswald_efficiency_factor=0.81 //Measure of lift effeciency of wing wing_winglets_flag=1 //Are winglets available? wing_sweep=37.5 //Degrees, wing leading edge wing_pos_apex_lon=-68.2 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0 //Feet, vertical distance from reference point, positive going up htail_area=1470 //1470 Square feet, Rick htail_span=72.8 //72.8 Feet, Rick htail_pos_lon=-210.0 //-210.0 long, Rick htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=-6.0 //0.0 Degrees, Rick -6.0 worked but a bit too "down" htail_sweep=37.5 //37.5 Degrees, horizontal tail leading edge vtail_area=1060 //Square feet vtail_span=37.1 //Feet, tip to body vtail_sweep=45.0 //Degrees, vertical tail leading edge vtail_pos_lon=-198.5 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=26.1 //Feet, vertical distance from reference point, positive going up elevator_area=327 //Square feet aileron_area=225 //Square feet rudder_area=230 //Square feet elevator_up_limit=30 //30 Degrees Rick elevator_down_limit=17 //17 Degrees Rick aileron_up_limit=30 //Degrees aileron_down_limit=20 //Degrees rudder_limit=35 //Degrees elevator_trim_limit=16 //Degrees spoiler_limit=35 //Degrees spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=2 //Aileron to spoileron gain min_ailerons_for_spoilerons=15 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate auto_spoiler_available=1 spoiler_extension_time=1.100000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 [Reference Speeds] flaps_up_stall_speed=224.0 //Knots True (KTAS) full_flaps_stall_speed=155.0 //Knots True (KTAS) cruise_speed=500.0 //Knots True (KTAS) max_indicated_speed=370.671875 max_mach=0.904980 // [flaps.0] //Inboard Trailing Edge Flaps type=1 // 1 - tail, 2 - lead span-outboard=0.2 // 0.0 .. 1.0 extending-time=25 // seconds flaps-position.0=0 // degrees flaps-position.1=0 // degrees flaps-position.2=17.5 // degrees flaps-position.3=22.5 // degrees flaps-position.4=26.5 // degrees flaps-position.5=32 // degrees damaging-speed=269 // KIAS blowout-speed=327 // KIAS lift_scalar=0.38 drag_scalar=0.25 pitch_scalar=0.17 system_type=1 //Hydraulic [flaps.1] //Outboard Trailing Edge Flaps type=1 // 1 - tail, 2 - lead span-outboard=0.2 // 0.0 .. 1.0 extending-time=25 // seconds flaps-position.0=0 // degrees flaps-position.1=0 // degrees flaps-position.2=17.5 // degrees flaps-position.3=22.5 // degrees flaps-position.4=26.5 // degrees flaps-position.5=32 // degrees damaging-speed=269 // KIAS blowout-speed=327 // KIAS lift_scalar=0.38 drag_scalar=0.25 pitch_scalar=0.17 system_type=1 //Hydraulic [flaps.2] //Leading Edge Slats type=2 // 1 - tail, 2 - lead span-outboard=0.2 // 0.0 .. 1.0 extending-time=11 // seconds flaps-position.0=0 // degrees flaps-position.1=21 // degrees flaps-position.2=21 // degrees flaps-position.3=24 // degrees damaging-speed=260 // KIAS blowout-speed=300 // KIAS lift_scalar=0.33 drag_scalar=0.11 pitch_scalar=0.35 system_type=1 //Hydraulic [flight_tuning] cruise_lift_scalar=1.1 parasite_drag_scalar=1.1 //2.1 Rick induced_drag_scalar=1.8 //1.8 Rick elevator_effectivenes=2.0 //1.0 Rick aileron_effectiveness=2.0 //0.7 rick rudder_effectiveness=1.0 pitch_stability=1.15 //1.0 Rick roll_stability=1.0 //1.0 Rick yaw_stability=1.0 //1.0 Rick elevator_trim_effectiveness=2.0 //1.0 Rick 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=-107.5, -73.0, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-76.0, -38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.2=-76.0, 38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.3=-107.5, 73.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.05 //Scalar for fuel flow efficiency min_throttle_limit=-0.250000 max_contrail_temperature = -27 [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=56.2 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=56000 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=0.9 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=99 //96 Rick autothrottle_takeoff_ga=1 pitch_takeoff_ga=8; max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [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) //Main and Nose Gear Contact Points point.0=1, 102.5, 0.0, -17.1, 1500.0, 0, 1.584, 85, 0.6, 3, 2.100, 9.0, 8.0, 0, 220, 262 point.1=1, -9, 0.0, -18.90, 2000.0, 0, 1.837, 0, 1, 1, 0.900, 11.0, 9.0, 2, 220, 262 point.2=1, -9, -17.536, -18.90, 2000.0, 1, 1.837, 0, 1, 1, 0.900, 11.0, 9.0, 3, 220, 262 point.3=1, -9, 17.536, -18.90, 2000.0, 2, 1.837, 0, 1, 1, 0.900, 11.0, 9.0, 3, 220, 262 //Tail Scrape Points point.4=2, -72.178, 0.0, -9.51, 430.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0 //Crest point.5=2, -131.23, 0.0, 6.8, 430.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0 //Peak //Nose Scrape Points point.6=2, 112.762, 0.0, 7.217, 430.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0 //Break for NG Door //Fairing Scrape Points point.7=2, 0.75, 0.0, 10.465, 430.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 //Center Faring Bottom //Wing Scrape Points point.8=2, 40.48, -103.83, 4.845, 430.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 //Left Wing point.9=2, 40.48, 103.83, 4.845, 430.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 //Right Wing static_pitch=-0.2 static_cg_height=16.7 gear_system_type=0 [Views] eyepoint=42.00, -7.30, 3.00 //Pilots View [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 //[Radios] [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 =1, 18.207, 0, 9.4, fx_beaconb, light.1 =1, 18.225, 0, -10.8, fx_beaconh, light.2 =3, -123.839, -0.151, 6.819, fx_navwhih , light.3 =2, -123.839, 0.151, 6.819, fx_strobeh , light.4 =5, 18, 27.464, -4, A340_wingscan, light.5=5, -1.933, 60.827, -0.368, A340_wingscan, light.6=5, 18, -27.464, -4, A340_wingscan, light.7=5, -1.933, -60.827, -0.368, A340_wingscan, light.8 =4, 117.038, 0, 2.812, A340_cockpit, light.9=6, 97.0, 0.00, -10.0, noselight , light.10 = 3, -115.94, -6.58, 30.36, Newll , light.11 = 3, -115.94, 6.58, 30.36, Newll , light.12 = 3, 40.94, -15.58, -3.36, Newll , light.13 = 3, 40.94, 15.58, -3.36, Newll , //longitudinal, lateral, vertical distance from reference datum [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 [keyboard_response] elevator=150, 250 aileron=150, 250 rudder=150, 250 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 //contrail=fx_A_I_Contrail //Rick removed [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second ;1660 [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 [brakes] toe_brakes_scale=0.91 //1.241798 parking_brake=1 differential_braking_scale = 1.0 auto_brakes=4 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=3000.000000 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=1
