[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, -16.00, 0.00, 9.5, 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, 1.0, fx_navwhi
light.6 = 3, -2.08, 0.00, -2.50, 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, -4.650, 1574.800, 0.000, 0.653, 56.000, 0.500, 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
//-------------------------------------------------------------------------------------