[fltsim.0] title=MB339 PAN sim=AerMacchi MB339 Pan model= panel= sound= texture= panel_alias = sound_alias = kb_checklists=AerMacchi MB339 Pan_check kb_reference=AerMacchi MB339 Pan_ref atc_id=RIVPAN atc_id_color = 0xffffffff atc_airline=Air Force atc_flight_number=Pony10 ui_manufacturer=Aermacchi ui_Type=MB339PAN ui_variation=Pony 10 visual_damage=1 description=The MB-339 jet trainer, produced by Aermacchi SpA of Varese, Italy, has been widely exported and is in service with the air forces of Argentina, Dubai, Eritrea, Ghana, Italy, Malaysia, New Zealand, Nigeria and Peru. The MB-339 jet trainer was initially developed to cover the basic and advanced training requirements of the Italian Air Force. Over 200 trainers are in service. The MB-339PAN is a special version for Italy's National Aerobatic Team, the Frecce Tricolori. The main modifications to the standard production planes are the removal of the wingtip fuel tanks and the addition of a two-color smoke system. atc_heavy=0 [fltsim.1] title=MB339 PAN with tanks sim=AerMacchi MB339 Pan model=tanks panel= sound= texture= panel_alias = sound_alias = kb_checklists=AerMacchi MB339 Pan_check kb_reference=AerMacchi MB339 Pan_ref atc_id=RIVPAN atc_id_color = 0xffffffff atc_airline=Air Force atc_flight_number=Pony 10 ui_manufacturer=Aermacchi ui_Type=MB339PAN ui_variation=Pony 10 with fuel tanks visual_damage=1 description=The MB-339 jet trainer, produced by Aermacchi SpA of Varese, Italy, has been widely exported and is in service with the air forces of Argentina, Dubai, Eritrea, Ghana, Italy, Malaysia, New Zealand, Nigeria and Peru. The MB-339 jet trainer was initially developed to cover the basic and advanced training requirements of the Italian Air Force. Over 200 trainers are in service. The MB-339PAN is a special version for Italy's National Aerobatic Team, the Frecce Tricolori. The main modifications to the standard production planes are the removal of the wingtip fuel tanks and the addition of a two-color smoke system. atc_heavy=0 //------------------------------------------------------------------------------------- [General] atc_type=MB339A PAN atc_model=PAN5 editable=0 performance="Lenght overall\t11.24m (36.8 ft) \nHeight overall\t3.9m (12.8 ft) \nWing span\t11.22m (36.8 ft) \n\nWeight (empty)\t3414Kg (7527 lb) \nWeight (clean t/o)\t5030Kg (11090 lb) \nWeight (maximum)\t6350 kts (14000 lb) \n\nMaximum speed\t496 kts (920 Km/h) \nApproach speed\t102kts (190 Km/h) \nTake off ground run\t550m (1805 ft) \nLanding ground run\t480m (1575 ft) \nLoad factor\t+7.33g,-4.0g" //------------------------------------------------------------------------------------- [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 //------------------------------------------------------------------------------------- [LIGHTS] // Types: 1=beacon 2=strobe 3=navigation 4=cockpit 5=landing 6=Taxi 7=recognition // 8=wing 9=logo light.0 = 1, -15.6, 0.00, 10.0, fx_beaconh light.1 = 3, -2.22, -17.6, 0.00, fx_navred // <== Sn light.2 = 2, -2.24, -17.6, 0.00, fx_strobe light.3 = 3, -2.22, 17.6, 0.00, fx_navgre light.4 = 2, -2.24, 17.6, 0.00, fx_strobe light.5 = 3, -19.5, 0.00, 1.8, fx_navwhi light.6 = 3, -2.08, 0.00, -2.20, fx_navwhi light.7 = 4, 10.23, 0.00, 0.229, Pz339_fx_vclight light.8 = 4, 5.23, 0.00, 0.229, Pz339_fx_vclight //------------------------------------------------------------------------------------- [SMOKESYSTEM] smoke.0=0.00, -22.00, 0.00, Pz339_fx_smoke_w //------------------------------------------------------------------------------------- [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 contrail=fx_contrail_s.fx //------------------------------------------------------------------------------------- [electrical] //BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) max_Battery_voltage = 24.5 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 70.0 flap_motor =0, 5 , 22.0 gear_motor =0, 5 , 22.0 autopilot =0, 5 , 22.0 avionics_bus =0, 10, 22.0 avionics =1, 5 , 23.0 pitot_heat =0, 2 , 22.0 additional_system =0, 14, 23.0 marker_beacon =1, 2 , 22.0 gear_warning =0, 2 , 22.0 fuel_pump =0, 5 , 22.0 hydraulic_pump =0, 5 , 22.0 starter1 =0, 10, 22.0 light_nav =0, 5 , 22.0 light_beacon =0, 2 , 22.0 light_landing =0, 2 , 22.0 light_taxi =0, 2 , 22.0 light_strobe =0, 2 , 22.0 light_panel =0, 5 , 22.0 //------------------------------------------------------------------------------------- [flight_tuning] //Flight Control effectiveness stability elevator_effectiveness =1.000 aileron_effectiveness =1.000 rudder_effectiveness =1.000 elevator_trim_effectiveness =1.000 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 //Stability parameters pitch_stability =1.000 roll_stability =1.000 yaw_stability =1.000 //Lift parameter cruise_lift_scalar =1.000 //High Angle Of Attack parameters hi_alpha_on_roll=1.0 hi_alpha_on_roll=1.0 //Drag Parameters parasite_drag_scalar =1.000 induced_drag_scalar =1.000 //------------------------------------------------------------------------------------- [pitot_static] vertical_speed_time_constant=2 //Increasing this value will cause a more instantaneous reaction in the VSI //------------------------------------------------------------------------------------- [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline) empty_weight_CG_position= 0.000, 0.000, 0.000 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations= 10 //Load Weight(lbs) longitudinal lateral vertical positions from datum (feet) station_load.0="200, 9.00, 0.00, -0.65, Pilot" // Pilot station_load.1="0.0, 4.00, 0.00, 0.00, CoPilot" // Co-Pilot station_load.2="0.0, 0.35, -11.50, -1.60, Free ExtLeftPyl" // Pyl station_load.3="0.0, 0.70, -9.02, -1.80, Free IntLeftPyl" // Pyl station_load.4="0.0, 0.70, 9.02, -1.80, Free IntRightPyl" // Pyl station_load.5="0.0, 0.35, 11.50, -1.60, Free ExtRightPyl" // Pyl //Moments of Inertia empty_weight= 6955.000 // (pounds) max_gross_weight= 13007.000 // (pounds) // FMW //empty_weight_pitch_MOI = 3746 //empty_weight_roll_MOI = 26228 //empty_weight_yaw_MOI = 28745 //FSEDIT empty_weight_pitch_MOI= 6668 empty_weight_roll_MOI= 6199 empty_weight_yaw_MOI= 12930 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 //------------------------------------------------------------------------------------- [fuel] //Tanks Position and capacity: //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux= -1.600, -17.420, 0.000, 132.000, 0.000 LeftMain= -0.300, -14.300, -1.000, 86.000, 0.000 Center1= 0.000, 0.000, 2.000, 206.000, 0.000 RightMain= -0.300, 14.300, -1.000, 86.000, 0.000 RightAux= -1.600, 17.420, 0.000, 132.000, 0.000 //Fuel type: 1 = Avgas, 2 = JetA fuel_type=2 number_of_tank_selectors=1 electric_pump=1 //------------------------------------------------------------------------------------- [airplane_geometry] wing_area= 208.000 //Square feet wing_span= 35.000 //Feet wing_root_chord= 8.0 //Feet wing_sweep= 10.6000 //Degrees, wing leading edge wing_dihedral= 3.500 //Degrees wing_incidence= 0.000 //Degrees wing_twist= 0.000 //Degrees //wing_pos_apex_lon= 1.486 // FMW wing_pos_apex_lon= 2.9 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert= -1.000 //Feet, vertical distance from reference point, positive going up wing_winglets_flag= 0 //Are winglets available? oswald_efficiency_factor= 0.8 //Measure of lift effeciency of wing htail_area= 38.000 //Square feet htail_span= 13.800 //Feet htail_pos_lon= -14.600 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert= 1.000 //Feet, vertical distance from reference point, positive going up htail_incidence= 0.000 //Degrees htail_sweep= 12.000 //Degrees, horizontal tail leading edge vtail_area= 22.000 //Square feet vtail_span= 6.600 //Feet, tip to body vtail_sweep= 52.000 //Degrees, vertical tail leading edge vtail_pos_lon= -10.5 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert= 2.45 //Feet, vertical distance from reference point, positive going up elevator_area= 14.400 //Square feet elevator_up_limit= 30.000 //Degrees elevator_down_limit= 24.000 //Degrees elevator_trim_limit= 19.500 //Degrees aileron_area= 14.400 //Square feet aileron_up_limit= 20.000 //Degrees aileron_down_limit= 20.000 //Degrees rudder_area= 10.000 //Square feet rudder_limit= 30.000 //Degrees spoiler_limit= 80.000 //Degrees spoilerons_available= 0 //Spoilerons Available? aileron_to_spoileron_gain= 0.000 //Aileron to spoileron gain min_ailerons_for_spoilerons= 0.000 //Degrees min_flaps_for_spoilerons= 0.000 //Minimum flap handle position when spoilerons activate //------------------------------------------------------------------------------------- [contact_points] //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) //GEAR // 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0= 1.000, 13.240, 0.000, -4.810, 1574.800, 0.000, 0.653, 56.000, 0.450, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000 point.1= 1.000, -1.428, -4.669, -4.850, 1574.800, 1.000, 0.891, 0.000, 0.500, 2.500, 0.850, 5.000, 5.000, 2.000, 0.000, 0.000 point.2= 1.000, -1.428, 4.669, -4.850, 1574.800, 2.000, 0.891, 0.000, 0.500, 2.500, 0.850, 5.000, 5.000, 3.000, 0.000, 0.000 //SCRAPES point.3= 2.000, -1.583, -15.920, 0.170, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -1.583, 15.920, 0.170, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -15.420, 0.000, -2.340, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 17.000, 0.000, -1.840, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= -0.051 static_cg_height= 4.460 gear_system_type=0 //------------------------------------------------------------------------------------- [GeneralEngineData] engine_type= 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0= -17.000, 0.000, -0.800 //(feet) longitudinal, lateral, vertical distance from reference datum // Spostare engine su aumenta VR fuel_flow_scalar= 1.280 //Scalar for fuel flow efficiency Regola il consumo di carburante min_throttle_limit= 0.00 //Minimum percent throttle. Generally negative for turbine reverser max_contrail_temperature=-30.0 master_ignition_switch=1 //------------------------------------------------------------------------------------- [TurbineEngineData] fuel_flow_gain= 0.020 //Gain on fuel flow Modifica il tempo per turbina al 100% inlet_area= 3.000 //Square Feet, engine nacelle inlet area rated_N2_rpm= 29920.000 //RPM, second stage compressor rated value static_thrust= 4400.000 //Lbs, max rated static thrust at Sea Level afterburner_available= 0 reverser_available= 0 //------------------------------------------------------------------------------------- [jet_engine] thrust_scalar=1.000 //------------------------------------------------------------------------------------- [Reference Speeds] flaps_up_stall_speed= 106.000 //Knots True (KTAS) full_flaps_stall_speed= 96.000 //Knots True (KTAS) cruise_speed= 400.000 //Knots True (KTAS) max_indicated_speed=520.000000 //Red line (KIAS) max_mach=0.88 //------------------------------------------------------------------------------------- [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=350.000000,500.000000 aileron =450.000000,1000.000000 rudder =200.000000,1000.000000 //------------------------------------------------------------------------------------- [Views] eyepoint= 10.40, 0.00, 1.40 //(feet) longitudinal, lateral, vertical distance from reference datum //------------------------------------------------------------------------------------- [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 use_no_default_bank=1 use_no_default_pitch=1 default_pitch_mode=0 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=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 // <== 9 nav_integrator_control=0.250000 // <== 0.25 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 //------------------------------------------------------------------------------------- [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=1,0 //------------------------------------------------------------------------------------- [Exits] number_of_exits=1 exit_rate.0=0.5 //------------------------------------------------------------------------------------- [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] parking_brake=1 //Parking brake available toe_brakes_scale=1.000000 //Brake scalar //------------------------------------------------------------------------------------- [gear_warning_system] gear_warning_available=1 //Normal pct_throttle_limit=0.1 //Percent throttle that activates warning flap_limit_idle=15 //Flap angle that activates warning at idle flap_limit_power=30 //Flap angle that activates warning at above idle //------------------------------------------------------------------------------------- [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 //------------------------------------------------------------------------------------- [stall_warning] type=2 //------------------------------------------------------------------------------------- [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0=1 //------------------------------------------------------------------------------------- [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,0 //------------------------------------------------------------------------------------- [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 2 flaps-position.0 = 0 flaps-position.1 = 20, 147 flaps-position.2 = 40, 140 damaging-speed = 200 blowout-speed = 240 system_type = 0 lift_scalar = 0 drag_scalar = 0 pitch_scalar = 1 [flaps.1] //Leading Edge Flaps - Lift type = 2 span-outboard = 0.5 extending-time = 2 flaps-position.0 = 0 flaps-position.1 = 20 flaps-position.2 = 40 damaging-speed = 200 blowout-speed = 240 system_type = 0 lift_scalar = 1 drag_scalar = 0 pitch_scalar = 0 [flaps.2] //Leading Edge Flaps - Drag type = 2 span-outboard = 0.5 extending-time = 2 flaps-position.0 = 0 flaps-position.1 = 4 flaps-position.2 = 40 damaging-speed = 200 blowout-speed = 240 system_type = 0 lift_scalar = 0 drag_scalar = 1 pitch_scalar = 0 //-------------------------------------------------------------------------------------