[fltsim.0] title=DSB A-7 Corsair II (VA146) Clean sim=A-7 model=clean panel= sound= texture=va146 kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=311 ui_manufacturer=Vought A-7E Corsair II ui_type=VA-146 "Blue Diamonds" ui_variation= Clean description= [fltsim.1] title=DSB A-7 Corsair II (VA83)Clean sim=A-7 model=clean panel= sound= texture=va83 kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=310 ui_manufacturer=Vought A-7E Corsair II ui_type=VA-83 "Rampagers" ui_variation= Clean description= [fltsim.2] title=DSB A-7 Corsair II (NATC)Clean sim=A-7 model=clean panel= sound= texture=natc kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=403 ui_manufacturer=Vought A-7E Corsair II ui_type=Naval Air Test Centre "Pax River" ui_variation= Clean description= [fltsim.3] title=DSB A-7 Corsair II (VA146)Ferry sim=A-7 model=ferry panel= sound= texture=va146 kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=311 ui_manufacturer=Vought A-7E Corsair II ui_type=VA-146 "Blue Diamonds" ui_variation= Ferry description= [fltsim.4] title=DSB A-7 Corsair II (VA83) Ferry sim=A-7 model=ferry panel= sound= texture=va83 kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=310 ui_manufacturer=Vought A-7E Corsair II ui_type=VA-83 "Rampagers" ui_variation= Ferry description= [fltsim.5] title=DSB A-7 Corsair II (NATC) Ferry sim=A-7 model=ferry panel= sound= texture=natc kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=403 ui_manufacturer=Vought A-7E Corsair II ui_type=Naval Air Test Centre "Pax River" ui_variation= Ferry description= [fltsim.6] title=DSB A-7 Corsair II (VA146) Strike sim=A-7 model=strike panel= sound= texture=va146 kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=311 ui_manufacturer=Vought A-7E Corsair II ui_type=VA-146 "Blue Diamonds" ui_variation= Strike description= [fltsim.7] title=DSB A-7 Corsair II (VA83) Strike sim=A-7 model=strike panel= sound= texture=va83 kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=310 ui_manufacturer=Vought A-7E Corsair II ui_type=VA-83 "Rampagers" ui_variation= Strike description= [fltsim.8] title=DSB A-7 Corsair II (NATC) Strike sim=A-7 model=strike panel= sound= texture=natc kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=403 ui_manufacturer=Vought A-7E Corsair II ui_type=Naval Air Test Centre "Pax River" ui_variation= Strike description= //----V1.20 Ammendments [fltsim.9] title=DSB A-7 Corsair II (VA146) CAS sim=A-7 model=cas panel= sound= texture=va146 kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=311 ui_manufacturer=Vought A-7E Corsair II ui_type=VA-146 "Blue Diamonds" ui_variation= Close Air Support description= [fltsim.10] title=DSB A-7 Corsair II (VA83) CAS sim=A-7 model=cas panel= sound= texture=va83 kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=310 ui_manufacturer=Vought A-7E Corsair II ui_type=VA-83 "Rampagers" ui_variation= Close Air Support description= [fltsim.11] title=DSB A-7 Corsair II (NATC) AI sim=A-7 model=ai panel= sound= texture=natc kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=403 ui_manufacturer=Vought A-7E Corsair II ui_type=Naval Air Test Centre "Pax River" ui_variation= Air Interdiction description= [fltsim.12] title=DSB A-7 Corsair II (VA146) AI sim=A-7 model=ai panel= sound= texture=va146 kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=311 ui_manufacturer=Vought A-7E Corsair II ui_type=VA-146 "Blue Diamonds" ui_variation= Air Interdiction description= [fltsim.13] title=DSB A-7 Corsair II (VA83) AI sim=A-7 model=ai panel= sound= texture=va83 kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=310 ui_manufacturer=Vought A-7E Corsair II ui_type=VA-83 "Rampagers" ui_variation= Air Interdiction description= [fltsim.14] title=DSB A-7 Corsair II (NATC) CAS sim=A-7 model=cas panel= sound= texture=natc kb_checklists=a7_check kb_reference=a7_ref atc_airline=NAVY atc_flight_number=403 ui_manufacturer=Vought A-7E Corsair II ui_type=Naval Air Test Centre "Pax River" ui_variation= Close Air Support description= //-----END OF AIRCRAFT [General] atc_type=Vought atc_model=A7 editable=0 performance="Cruise Speed\t\nMach 0.81\n\nEngines\t\nGeneral Electric TF-34-GE-400B Turbofan Engines 9275 lb thrust\n\nMaximum Range\t\n2,335 nm\n\nService Ceiling\t\n40,000 ft\n\nFuel Capacity\t\n937 U.S. gal \n\nMaximum Gross Weight\t\n52,539 lb \n\nLength\t\n53.4 ft\t 16.0 m\n\nWingspan\t\n68.8 ft\t 20.6 m\n\nHeight\t\n22.9 ft\t6.9 m Category=airplane [WEIGHT_AND_BALANCE] max_gross_weight = 20450.0 // (pounds) empty_weight = 11700.0 // (pounds) reference_datum_position = 34.5, 0, 0 // (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, -23.5, -1.2, 0.0, Pilot" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 50000 empty_weight_roll_MOI = 45000 empty_weight_yaw_MOI = 70000 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, 5 , 9.5 avionics = 1, 5 , 9.5 additional_system = 0, 2 , 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 = 1.0 elevator_effectiveness = 1.5 aileron_effectiveness = 2.5 rudder_effectiveness = 1.0 pitch_stability = 2.0 roll_stability = 2.0 yaw_stability = 2.0 elevator_trim_effectiveness = 1.0 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 = -50.0, 0.0, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency min_throttle_limit = 0.00 //Minimum percent throttle. Generally negative for turbine reverser [TurbineEngineData] fuel_flow_gain = 0.0025 //Gain on fuel flow inlet_area = 4.2895 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 6000 //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, -21.00, 0.00, -7.50, 2000.1, 0, 0.6349, 46.8, 0.8000, 1.5, 0.5100, 4.0, 4.0, 0, 260.0, 260.0 point.1=1, -42.00, -5.75, -6.80, 1574.8, 1, 0.6349, 0.0, 0.7798, 1.5, 0.5456, 4.0, 4.0, 2, 260.0, 260.0 point.2=1, -42.00, 5.75, -6.80, 1574.8, 2, 0.6349, 0.0, 0.7798, 1.5, 0.5456, 4.0, 4.0, 3, 260.0, 260.0 point.3=2, -44.00, -35.00, 2.00, 1500.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -44.00, 35.00, 2.00, 1500.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -65.50, 0.00, -0.50, 1500.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, -14.00, 0.00, -1.50, 1500.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 point.7=5.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 3.0, 3.0, 0.000, 0.000, 0.000 static_pitch=0.0 static_cg_height=7.5 gear_system_type=0 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 15.0 //Flap angle that activates warning at idle flap_limit_power = 30.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 3.0 //Brake scalar auto_brakes=4 [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint = -19.5, 0.0, 2.5, Pilot Seat [Folding_wings] wing_fold_system_type=4 fold_rates=0.14,0.13 [exits] number_of_exits=2 exit_rate.0=0.4 //******************************************************************* [LIGHTS] //#1=beacon #2=strobe #3=nav //#4=cockpit #5=landing #6=taxi //#7=recog #8=wing #9=logo //index,type, long, lat, vert, fx_filename //---------------------------------------------------------- light.0= 3, -57.25, 0.00, 10.25, fx_navwhi light.1= 4, 0.50, 0.00, 1.50, fx_vclight light.2= 1, -30.00, 0.00, 3.70, fx_beacon light.3= 1, -27.30, 0.00, -4.50, fx_beacon light.4= 5, -20.30, -4.00, -1.50, fx_llight light.5= 5, -20.30, 4.00, -1.50, fx_llight light.6= 2, -45.00, -19.50, 1.00, fx_Vortices light.7= 2, -45.00, 19.50, 1.00, fx_Vortices light.8= 4, -19.0, 0, 2.0, fx_dsb_vclight_red, light.9= 4, -18.0, 0, 3.0, fx_dsb_vclight_red, //************************************************************************ [Tailhook] tailhook_length=3.0 tailhook_position=-30.5,0.0,0.0 cable_force_adjust=1.0 [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 5 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 10 // degrees flaps-position.2 = 25 // degrees flaps-position.3 = 40 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // 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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 attitude_indicator.1 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [fuel] LeftMain = -36.3, -10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -36.3, 10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux = -36.3, -10.0, -1.5, 200.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux = -36.3, 10.0, -1.5, 200.0, 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 = 312.0 //Square feet wing_span = 45.8 //Feet wing_root_chord = 9.9 //Feet wing_dihedral = 2.5 //Degrees wing_incidence = 0.5 //Degrees wing_twist = -1.5 //Degrees oswald_efficiency_factor= 0.8 //Measure of lift effeciency of wing wing_winglets_flag = 1 //Are winglets available? wing_sweep = 13.4 //Degrees, wing leading edge wing_pos_apex_lon = -31.5 //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 = 67.0 //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 = 42.0 //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 = 17.0 //Square feet aileron_area = 13.5 //Square feet rudder_area = 7.3 //Square feet elevator_up_limit = 17.0 //Degrees elevator_down_limit = 15.5 //Degrees aileron_up_limit = 18.0 //Degrees aileron_down_limit = 18.0 //Degrees rudder_limit = 30.0 //Degrees elevator_trim_limit = 15.0 //Degrees spoiler_limit = 60.0 //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=1 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=4.273504 positive_g_limit_flaps_down=4.273504 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-3.000000 [Reference Speeds] flaps_up_stall_speed = 112.0 //Knots True (KTAS) full_flaps_stall_speed = 102.0 //Knots True (KTAS) cruise_speed = 450.0 //Knots True (KTAS) max_mach = 0.92 max_indicated_speed = 620 //Red line (KIAS) [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1500.0 autothrottle_available= 0 autothrottle_arming_required= 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga= 0 pitch_takeoff_ga = 8; max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=20.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=11.00 nav_integrator_control=0.20 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [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 [stall_warning] type=2 stick_shaker=1 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 startup=fx_dsb_heat [SMOKESYSTEM] smoke.0 = -60, -0, -0, fx_dsb_smoke [pitot_static] pitot_heat=1.000000 [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 [deice_system] structural_deice_type=0