[fltsim.0] title=FIAT G91Y sim=G91Y model= panel= sound= texture= kb_checklists= atc_heavy=0 atc_airline=Air Force atc_flight_number= B306 ui_manufacturer=FIAT ui_type=G91Y ui_variation=32° Stormo Caccia description=Designed by italian Ing. Giuseppe Gabrielli and derived from the single engine G91R this aircraft, designated G.91Y and nicknamed "Yankee", replaced the original Bristol-Siddeley Orpheus engine with two General Electric J85 units. The G.91Y, first flown on December/12/1966, displayed an improvement in speed, range, payload, and maneuverability. It increased maximum speed to 600 kts (1,110 km/h, 690 mph, Mach 0.91). The machine guns were replaced by a pair of DEFA 552 30mm cannon with 125 rpg. All the aircraft built served with the Aeronautica Militare Italiana (Italian Air Force). ui_typerole="Modern Military" ui_createdby="I. D'Attomo & G. Quai" [fltsim.1] title=FIAT G91YPAINTVigna sim=G91Y model= panel= sound= texture=Vigna kb_checklists= atc_heavy=0 atc_airline=Air Force atc_flight_number= S21 ui_manufacturer=FIAT ui_type=G91Y ui_variation=Vigna di Valle Museum description=Designed by italian Ing. Giuseppe Gabrielli and derived from the single engine G91R this aircraft, designated G.91Y and nicknamed "Yankee", replaced the original Bristol-Siddeley Orpheus engine with two General Electric J85 units. The G.91Y, first flown on December/12/1966, displayed an improvement in speed, range, payload, and maneuverability. It increased maximum speed to 600 kts (1,110 km/h, 690 mph, Mach 0.91). The machine guns were replaced by a pair of DEFA 552 30mm cannon with 125 rpg. All the aircraft built served with the Aeronautica Militare Italiana (Italian Air Force). ui_typerole="Modern Military" ui_createdby="I. D'Attomo & G. Quai" [fltsim.2] title=FIAT G91YPAINTAluminium sim=G91Y model= panel= sound= texture=Aluminium kb_checklists= atc_heavy=0 atc_airline=Air Force atc_flight_number= B306 ui_manufacturer=FIAT ui_type=G91Y ui_variation=Aluminium description=Designed by italian Ing. Giuseppe Gabrielli and derived from the single engine G91R this aircraft, designated G.91Y and nicknamed "Yankee", replaced the original Bristol-Siddeley Orpheus engine with two General Electric J85 units. The G.91Y, first flown on December/12/1966, displayed an improvement in speed, range, payload, and maneuverability. It increased maximum speed to 600 kts (1,110 km/h, 690 mph, Mach 0.91). The machine guns were replaced by a pair of DEFA 552 30mm cannon with 125 rpg. All the aircraft built served with the Aeronautica Militare Italiana (Italian Air Force). ui_typerole="Modern Military" ui_createdby="I. D'Attomo & G. Quai" [General] atc_type=FIAT G91Y atc_model=FIAT G91Y editable=1 performance=Max Speed: 600 Kts\nCruise Speed: Mach n° 0.91\nMax Ceiling: 41000ft\nRange: 2.000 Km.\nMax Mach: 1.01 in steep dive. Category=airplane [WEIGHT_AND_BALANCE] max_gross_weight=17000.00 empty_weight=8100.00 reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, -1.000 max_number_of_stations=50 ;Moments of Inertia empty_weight_pitch_MOI=320000.000 empty_weight_roll_MOI=50000.000 empty_weight_yaw_MOI=120000.000 empty_weight_coupled_MOI=0.000 CG_forward_limit=0.000 CG_aft_limit=1.000 station_load.0 = 200, 12, 0, 3, Pilot [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 1 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 ;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=1.0 elevator_effectiveness=0.7 aileron_effectiveness=3.8 rudder_effectiveness=1.00 pitch_stability=3.4 roll_stability=1.00 yaw_stability=1.00 elevator_trim_effectiveness=0.5 aileron_trim_effectiveness=1.10 rudder_trim_effectiveness=1.10 [GeneralEngineData] engine_type=1 Engine.0=-19.000, -2.000, 0.000 Engine.1=-19.000, 2.000, 0.000 fuel_flow_scalar=1.000 min_throttle_limit=-0.25 [TurbineEngineData] fuel_flow_gain=0.003 inlet_area=3.000 rated_N2_rpm=29000.0 static_thrust=4100.00 afterburner_available=0 reverser_available=0 [jet_engine] thrust_scalar=0.55 //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) 45 //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=1.00, 13.50, 0.00, -5.65, 3120.00, 0.00, 0.80, 55.00, 0.25, 2.50, 0.80, 3.00, 4.00, 0.00, 0.00, 0.00 point.1=1.00, -2.00, -4.00, -5.81, 3160.00, 1.00, 1.00, 0.00, 0.50, 2.50, 0.90, 6.00, 5.00, 2.00, 0.00, 0.00 point.2=1.00, -2.00, 4.00, -5.81, 3160.00, 2.00, 1.00, 0.00, 0.50, 2.50, 0.90, 5.00, 6.00, 3.00, 0.00, 0.00 point.3=2.0, -3.30, -23.90, -3.00, 787.40, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00 point.4=2.0, -3.30, 23.90, -3.00, 787.40, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00 point.5=2.0, -22.60, 0.00, 0.00, 787.40, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00 point.6=2.0, 13.03, 0.00, -1.50, 787.40, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00 static_pitch=-0.750 static_cg_height=5.200 gear_system_type=0 [Views] eyepoint=9.00, 0.00, 1.64 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, -6.72, -14.75, -1.45, fx_navred , light.1 = 3, -6.72, 14.75, -1.45, fx_navgre , light.2 = 3, -17.95, 0.00, 2.55, fx_navwhi , light.3=2,-15.00,-0.90,0.80,fx_afterburner_f3 light.4=2,-15.00,0.90,0.80,fx_afterburner_f3 light.5 = 4, 10.85,-0.1,1.3, fx_vclighth light.6 = 4, 10.85, 0.1,1.3, fx_vclighth [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,0.0 [fuel] Center1=0.000, 0.000, 0.000, 300.000, 0.000 LeftMain=0.000, -5.000, 0.000, 135.000, 0.000 RightMain=0.000, 5.000, 0.000, 135.000, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=220.00 wing_span=39.000 wing_root_chord=9.500 wing_dihedral=3.000 wing_incidence=-0.500 wing_twist=-1.000 oswald_efficiency_factor=0.800 wing_winglets_flag=0 wing_sweep=37.000 wing_pos_apex_lon=8.000 wing_pos_apex_vert=-2.000 htail_area=70.000 htail_span=12.800 htail_pos_lon=-25.000 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=35.000 vtail_area=60.000 vtail_span=7.000 vtail_sweep=35.000 vtail_pos_lon=-25.000 vtail_pos_vert=2.000 elevator_area=25.000 aileron_area=26.000 rudder_area=6.500 elevator_up_limit=20.0 elevator_down_limit=20.0 aileron_up_limit=18.000 aileron_down_limit=18.000 rudder_limit=30.000 elevator_trim_limit=16.000 spoiler_limit=66.0 spoilerons_available=0 aileron_to_spoileron_gain=4.600 min_ailerons_for_spoilerons=5.000 min_flaps_for_spoilerons=0.000 auto_spoiler_available=0 spoiler_extension_time=1.00 positive_g_limit_flaps_up=3.00 positive_g_limit_flaps_down=2.00 negative_g_limit_flaps_up=-2.00 negative_g_limit_flaps_down=-2.00 [Reference Speeds] flaps_up_stall_speed=130.00 full_flaps_stall_speed=100.00 cruise_speed=590.00 max_indicated_speed=700.00 max_mach=1.02 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_max_rpm=90 autothrottle_takeoff_ga=0 pitch_takeoff_ga=8; max_pitch=10.00 max_pitch_acceleration=1.00 max_pitch_velocity_lo_alt=2.00 max_pitch_velocity_hi_alt=1.50 max_pitch_velocity_lo_alt_breakpoint=20000.00 max_pitch_velocity_hi_alt_breakpoint=28000.00 max_bank=30.00 max_bank_acceleration=1.80 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 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=0.00 [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 [brakes] toe_brakes_scale=1.30 parking_brake=1 differential_braking_scale =0.1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099 flap_limit_power=30.023 flap_limit_idle=15.011 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=3000.0 [TailHook] tailhook_length = 5 ;(feet) tailhook_position = -17, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust = 1 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.50,0.50 ;Percent per second [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [Flaps.0] type=1 span-outboard=0.500 extending-time=5.000 system_type=0 damaging-speed=250.000 blowout-speed=300.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=0.10 flaps-position.0=0.00 flaps-position.1=10.00 flaps-position.2=35.00 [Flaps.1] type=2 span-outboard=0.65 extending-time=5.0 system_type=0 damaging-speed=250.0 blowout-speed=290.0 lift_scalar=1.0 drag_scalar=1.0 pitch_scalar=0.0 flaps-position.0=0.0 flaps-position.1=25.0 [SMOKESYSTEM] smoke.0=-15.0, 0.0, 0.0, fx_smoke_w //smoke.0=0.0, -18.0, 0.0, fx_smoke_w --OK for FS2k4-- [pitot_static] pitot_heat=1.00 [vacuum_system] max_pressure=5.15 vacuum_type=2 electric_backup_pressure=0.00 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.00 bleed_air_scalar=1.00 [deice_system] structural_deice_type=0
