[fltsim.0] title=Super Etendard n°31 sim=super_etendard model= panel= sound= texture= kb_checklists=super_etendard_check kb_reference=super_etendard_ref atc_id=31 atc_airline=Navy atc_flight_number=31 ui_manufacturer=Dassault ui_type=Super Etendard ui_variation=Aéronavale n°31 visual_damage=1 description=Updated version of the Etendard IV, the Super Etendard is a carrier-based single-seat strike fighter which flew for the first time in October 1974 and was introduced into service in June 1978. In France, about 50 planes out of the 71 serving in the 11F, 14F and 17F squadrons of the French Navy were modernized with updated avionics and a new Anémone radar. The first of them flew in October 1990. This model is painted like the former Super Etendard n°31. It has a camouflage painting now.\n\nNo external fuel tanks.\nRealistic right/left aux tank max level : 0%.\n [fltsim.1] title=Super Etendard n°15 sim=super_etendard model=cm panel= sound= texture= kb_checklists=super_etendard_check kb_reference=super_etendard_ref atc_id=15 atc_airline=Navy atc_flight_number=15 ui_manufacturer=Dassault ui_type=Super Etendard ui_variation=Aéronavale n°15 visual_damage=1 description=Updated version of the Etendard IV, the Super Etendard is a carrier-based single-seat strike fighter which flew for the first time in October 1974 and was introduced into service in June 1978. In France, about 50 planes out of the 71 serving in the 11F, 14F and 17F squadrons of the French Navy were modernized with updated avionics and a new Anémone radar. The first of them flew in October 1990. Nowadays, the Super Etendard is the main attack force aboard the French carrier "Charles de Gaulle". A second modernization program of 54 Super Etendard began in 1992 and will allow them to serve in the 11F and 17F squadrons until they are replaced by Rafale M in 2008. This model is the n°15 of the 17F squadron based at the BAN of Landivisiau.\n\nHeavy fuel tanks.\nRealistic right/left aux tank max level : 100%.\n [fltsim.2] title=Super Etendard 3-A-203 sim=super_etendard model=argentina panel= sound= texture= kb_checklists=super_etendard_check kb_reference=super_etendard_ref atc_id=203 atc_airline=Navy atc_flight_number=203 ui_manufacturer=Dassault ui_type=Super Etendard ui_variation=Armada 3-A-203 visual_damage=1 description=Updated version of the Etendard IV, the Super Etendard is a carrier-based single-seat strike fighter which flew for the first time in October 1974 and was introduced into service in June 1978. 14 Super Etendard were delivered to Argentina in and after November 1981. Five of them took part in the Falklands War of 1982. Argentine aircrafts carrying Exocet missiles sank two British ships : the destroyer "Sheffield" (4,500 tons) and the "Atlantic Conveyor" (15,000 tons).\n\nLight fuel tanks.\nRealistic right/left aux tank max level : 54%.\n [General] atc_heavy=0 atc_type=Dassault atc_model=SEM editable=0 performance=CONFIGURATION\t\nLength 14.30 m\t\nWingspan 9.60 m\t\nWing area 28.40 m²\n\nWEIGHT\t\nEmpty weight 6,450 kg\t\nTypical weight 9,450 kg\t\nMax takeoff weight 12,000 kg\t\nInternal fuel capacity 2,591 kg\n\nENGINE\t\nAtar 8K50\t\nThrust 48.6 kN\n\nPERFORMANCE\t\nMax Mach in level flight Mach 1.15\t\nApproach speed 126 kts\t\nOperational ceiling 45,000 ft\t\nRange with external tanks 750 - 1,080 nm Category=airplane [WEIGHT_AND_BALANCE] max_gross_weight=23803.0 // (pounds) empty_weight=14220.0 // (pounds) reference_datum_position=36.90, 0, 1.64 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline) empty_weight_CG_position=-35.79, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170, -17.0, 0.0, 0.0 //Pilot Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=60000 empty_weight_roll_MOI=45000 empty_weight_yaw_MOI=100000 empty_weight_coupled_MOI=0.0 [electrical] max_battery_voltage=12.0 generator_alternator_voltage=13.8 max_generator_alternator_amps=40.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus=0, 10, 9.5 avionics=1, 5 , 9.5 additional_system=0, 20, 9.5 marker_beacon=1, 2 , 9.0 fuel_pump=0, 5 , 9.0 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=0.9 elevator_effectiveness=1.7 aileron_effectiveness=1.3 rudder_effectiveness=1.0 pitch_stability=1.2 roll_stability=1.5 yaw_stability=1.2 elevator_trim_effectiveness=1.7 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=-42.8, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.0015 //Gain on fuel flow inlet_area=10.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=11265 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=0 //Thrust reverser available? [jet_engine] thrust_scalar=1.0 //0 Class //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 [contact_points] point.0=1, -22.6, 0.00, -7.0, 1481.1, 0, 0.79, 46.8, 0.5, 2.2, 0.7, 5.0, 5.0, 0, 0.0, 0.0 point.1=1, -38.4, -5.3, -6.7, 1974.8, 1, 1.08, 0.0, 0.5, 2.0, 0.9, 5.0, 6.0, 2, 0.0, 0.0 point.2=1, -38.4, 5.3, -6.7, 1974.8, 2, 1.08, 0.0, 0.5, 2.0, 0.9, 5.0, 6.0, 3, 0.0, 0.0 point.3=2, -46.1, -15.7, -3.1, 987.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -46.1, 15.7, -3.1, 987.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -51.5, 0.00, -4.0, 987.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, -11.7, 0.00, -0.5, 987.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch=0.5 static_cg_height=4.36 gear_system_type=0 [Views] eyepoint=-21.80, 0, 1.96 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees flaps-position.1=0 // degrees flaps-position.2=40 // degrees damaging-speed=180 // KIAS blowout-speed=220 // KIAS [flaps.1] type=2 // 1 - tail, 2 - lead span-outboard=1.0 // 0.0 .. 1.0 extending-time=3 // seconds flaps-position.0=0 // degrees flaps-position.1=15 // degrees flaps-position.2=30 // degrees damaging-speed=550 // KIAS blowout-speed=600 // KIAS [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=150, 250 aileron=150, 250 rudder=150, 250 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain=-41.4, -1.0, -1.5, 426.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-41.4, 1.0, -1.5, 426.0, 0.0 LeftAux=-37.0, -8.0, -1.5, 289.000, 0.000 RightAux=-37.0, 8.0, -1.5, 289.000, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=306.0 //Square feet wing_span=31.5 //Feet wing_root_chord=10.0 //Feet wing_dihedral=0.5 //Degrees wing_incidence=2.0 //Degrees wing_twist=-1.5 //Degrees oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=47.0 //Degrees, wing leading edge wing_pos_apex_lon=-28.0 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_area=87.0 //Square feet htail_span=17.2 //Feet htail_pos_lon=-59.1 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=2.0 //Degrees htail_sweep=25.0 //Degrees, horizontal tail leading edge vtail_area=52.0 //Square feet vtail_span=7.4 //Feet, tip to body vtail_sweep=30.0 //Degrees, vertical tail leading edge vtail_pos_lon=-55.0 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=4.1 //Feet, vertical distance from reference point, positive going up elevator_area=34.0 //Square feet aileron_area=19.5 //Square feet rudder_area=15.3 //Square feet elevator_up_limit=14.0 //Degrees elevator_down_limit=13.5 //Degrees aileron_up_limit=15.0 //Degrees aileron_down_limit=15.0 //Degrees rudder_limit=30.0 //Degrees elevator_trim_limit=15.0 //Degrees spoiler_limit=65.0 //Degrees spoilerons_available=0 //Spoilerons Available? aileron_to_spoileron_gain=4.6 //Aileron to spoileron gain min_ailerons_for_spoilerons=5 //Degrees min_flaps_for_spoilerons=0.0 //Minimum flap handle position when spoilerons activate auto_spoiler_available=0 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=6.136752 positive_g_limit_flaps_down=5.205128 negative_g_limit_flaps_up=-2.000000 negative_g_limit_flaps_down=-2.000000 [Reference Speeds] flaps_up_stall_speed=132.0 //Knots True (KTAS) full_flaps_stall_speed=118.0 //Knots True (KTAS) cruise_speed=464.0 //Knots True (KTAS) max_indicated_speed=860.000000 max_mach=1.510010 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_max_rpm=95 autothrottle_takeoff_ga=0 pitch_takeoff_ga=8; use_no_default_pitch = 0 use_no_default_bank = 1 default_bank_mode=0 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_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 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.15,0.14 ;Percent per second [TailHook] tailhook_length=3.0 ;(feet) tailhook_position=-46.9, 0.0, -0.5 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 [LIGHTS] //Position Order: Z, X, Y //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=2, -40.00, 0.00, 1.22, fx_strobe , // feu anticollision light.1=3, -31.13, 0.12, -2.67, fx_navwhi , //feu de reconnaissance light.2=4, -20.57, 0.0, 1.40, fx_vclight , // cockpit [SMOKESYSTEM] smoke.0=-3.1, -50.2, 15.7, fx_contrail_s.fx smoke.1=-3.1, -50.2, -15.7, fx_contrail_s.fx [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 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 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=15.011494 [brakes] toe_brakes_scale=1.000000 parking_brake=1 [pitot_static] pitot_heat=1.000000 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=3000.000000 [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 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [deice_system] structural_deice_type=0
