//Revisione dinamiche di volo del 16/05/2009 - Flight Dynamics revised on the 16th  of may 2009.

[fltsim.0]
title			=MB339_CD RS-26
sim			=MB339_CD
model			=
panel			=
sound			=
texture			=RS
kb_checklists		=Aermacchi MB339 CD_CHECK.TXT
kb_reference		=Aermacchi MB339 CD_REF.TXT

atc_model		=
atc_parking_codes	=
atc_id			=MM-55062
atc_airline		=Air Force
atc_flight_number	= RS-01
ui_manufacturer		=AerMacchi
ui_Type			=MB339CD
ui_variation		=Aermacchi MB339CD "Reparto Sperimentale"
ui_createdby   		= Massimo Taccoli
visual_damage		=1

description=AerMacchi MB.339CD\nAdvanced Trainer used by AMI, Italian Air Force\n Flight Dynamics: Paolo Zamparo \nAircraft and Panel design: Massimo Taccoli\Sounds: Aaron Swindle

atc_heavy=0
atc_id_color		=0x00000000
atc_id_font		=Verdana,-11,1,600,0
atc_parking_types	=MIL_COMBAT

[fltsim.1]
title		=MB339_CD 36-01
sim		=MB339_CD
model		=
panel		=
sound		=
texture		=36
kb_checklists	=Aermacchi MB339 CD_CHECK.TXT
kb_reference	=Aermacchi MB339 CD_REF.TXT
atc_model	=
atc_parking_codes=
atc_id		=MM-55073
atc_airline	=Air Force
atc_flight_number=36-01
ui_manufacturer	=AerMacchi
ui_Type		=MB339CD
ui_variation	=Aermacchi MB339CD "36° Stormo"
ui_createdby    =Massimo Taccoli
visual_damage	=1
description=AerMacchi MB.339CD\nAdvanced Trainer used by AMI, Italian Air Force\n Flight Dynamics: Paolo Zamparo \nAircraft and Panel design: Massimo Taccoli\Sounds: Aaron Swindle

atc_heavy=0
atc_id_color		=0x00000000
atc_id_font		=Verdana,-11,1,600,0
atc_parking_types	=MIL_COMBAT

[General]
atc_type		=MB339_CD 
atc_model		=339CD 
editable		=0 

performance=Aircraft infoes are on the Knee-Board\nEnjoy !!!!!!! 
Category=airplane

//-------------------------------------------------------------------------------------

[Radios]
// Radio Type=available, 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 
//-------------------------------------------------------------------------------------

[flight_tuning]

//Flight Control effectiveness stability
elevator_effectiveness		=1.000 
aileron_effectiveness		=1.600
rudder_effectiveness		=1.000 
elevator_trim_effectiveness	=1.500
aileron_trim_effectiveness	=1.000 
rudder_trim_effectiveness	=1.200

//Stability parameters
pitch_stability			=2.000
roll_stability			=2.000
yaw_stability			=2.000

//Lift parameter
cruise_lift_scalar		=1.000 

//High Angle Of Attack parameters
hi_alpha_on_roll		=1.000
hi_alpha_on_yaw			=1.000

//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 
pitot_heat=1.000000
                                          reaction in the VSI
//-------------------------------------------------------------------------------------

[weight_and_balance]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
empty_weight=6955.000000
empty_weight_roll_MOI=0.000000
empty_weight_pitch_MOI=0.000000
empty_weight_yaw_MOI=0.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=10432.500000

[WEIGHT_AND_BALANCE]
reference_datum_position	=0.00,0.00,0.00 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position	=2.00,0.00,0.00 // (feet) longitudinal, lateral, vertical distance from specified datum

empty_weight	= 7350.000          // (pounds) 
max_gross_weight=14000.000         // (pounds)


max_number_of_stations 	= 2
station_load.0 = 170, 9.00,   0,     -0.65     // 1ST pilot
station_load.1 = 170, 4.00,   0,      0.00     // 2nd pilot


empty_weight_pitch_MOI	=58733		
empty_weight_roll_MOI	=48560		
empty_weight_yaw_MOI	=92943
empty_weight_coupled_MOI=0.0
CG_forward_limit	=0.000
CG_aft_limit		=1.000


//-------------------------------------------------------------------------------------

[LIGHTS]

//   Types: 1=beacon 2=strobe 3=navigation 4=cockpit 5=landing 6=Taxi 7=recognition
//          8=wing 9=logo 10=cabinlight 

light.0 = 1, -16.64,    0.00,   9.15,  fx_beaconh
light.1 = 3,  -1.81,  -18.76,   0,     fx_navred
light.2 = 2,  -2.01,  -18.76,   0,     fx_strobe
light.3 = 3,  -1.81,   18.73,   0,     fx_navgre
light.4 = 2,  -2.01,   18.73,   0,     fx_strobe
light.5 = 3, -20.22,    0.00,   1.16,  fx_navwhi
light.6 = 3,  -2.04,    0.00,  -2.40,  fx_navwhi
light.7 = 3,  -6.44,    0.00,   2.62,  fx_navwhi
light.8 = 4,   8.89,    0,      0.71,  Pz339_fx_vclight
light.9 = 4,   4.62,    0,      1.26,  Pz339_fx_vclight
light.10= 10, -4.90,  -17.06,   0,     Pz339_fx_WVortex
light.11= 10, -4.90,   17.06,   0,     Pz339_fx_WVortex



[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type 		= 1
fuel_flow_scalar 	= 1.80
min_throttle_limit 	= 0.00
max_contrail_temperature=-30.0
master_ignition_switch 	= 1
Engine.0	        =-7.00 , 0.0 , 0.416667


//-------------------------------------------------------------------------------------

[SMOKESYSTEM]

[smokesystem]
smoke.0 = 0, -21.8, 0, Pz339_fx_smoke_engin   // <== Exhaust


//-------------------------------------------------------------------------------------


[EFFECTS]

wake		=fx_wake
water		=fx_spray
dirt		=fx_tchdrt
concrete	=fx_sparks
touchdown	=fx_tchdwn, 1
contrail	=fx_contrail_s

//-------------------------------------------------------------------------------------

[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1		=  0.0,	   0.0,	 -1.0,	177.0,	0.8 
LeftAux		=  1.0,	  -9.5,	 -2.0,	 37.7,	0.5
RightAux	=  1.0,	   9.5,	 -2.0,	 37.7,	0.5

External1 	= -1.88, -17.97,  0,    109,    0.8
External2 	= -1.88,  17.97,  0,    109,    0.8

fuel_type                =2
number_of_tank_selectors =1
electric_pump            =1            

//-------------------------------------------------------------------------------------

//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]
static_pitch   		= -0.051
static_cg_height   	= 4.55
tailwheel_lock 		= 0
gear_system_type 	= 0
max_number_of_points 	= 7

//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., 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., 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., 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., 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., 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., 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., 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


[keyboard_response]
elevator 	= 350.000,  500.00
aileron 	= 450.000, 1000.00
rudder 		= 200.000, 1000.00


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111


[airplane_geometry]
wing_area   		=207		
wing_span		=37.08
wing_root_chord		=7.48
wing_dihedral		=3.49
wing_incidence		=-0.08
wing_twist		=-0.5
oswald_efficiency_factor=0.845
wing_winglets_flag	=0
wing_sweep		=10.78
wing_pos_apex_lon	=3.05
wing_pos_apex_vert	=-1.15
htail_area		=32.00
htail_span		=13.94
htail_pos_lon		=-14.36
htail_pos_vert		=1.03
htail_incidence		=0.000
htail_sweep		=11.40
vtail_area		=32.00
vtail_span		=6.44
vtail_sweep		=0.000
vtail_pos_lon		=-10.62
vtail_pos_vert		=2.49
elevator_area		=13.76
elevator_up_limit	=19.48
elevator_down_limit	=20.00
elevator_trim_limit	=19.48
aileron_area		=21.63
aileron_up_limit	=19.480
aileron_down_limit	=19.480
rudder_area		=11.200
rudder_limit		=23.49
spoiler_limit		=60.00
spoilerons_available	=0
aileron_to_spoileron_gain  =0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons   =0.000000
auto_spoiler_available=0
spoiler_extension_time=1.000000
positive_g_limit_flaps_up=10.000000
positive_g_limit_flaps_down=8.000000
negative_g_limit_flaps_up=-6.000000
negative_g_limit_flaps_down=-4.000000

[electrical]
max_battery_voltage 		= 24.5
generator_alternator_voltage 	= 28
max_generator_alternator_amps 	= 70
engine_generator_map 		= 1
electric_always_available 	= 0
flap_motor 			= 0, 5, 22
gear_motor 			= 0, 5, 22
autopilot 			= 0, 5, 22
avionics_bus 			= 0, 10, 22
avionics 			= 1, 5, 23
pitot_heat 			= 0, 2, 22
additional_system 		= 0, 14, 23
marker_beacon 			= 1, 2, 22
gear_warning 			= 0, 2, 22
fuel_pump 			= 0, 5, 22
starter1 			= 0, 10, 22
light_nav 			= 0, 5, 22
light_beacon 			= 0, 2, 22
light_landing 			= 0, 2, 22
light_taxi 			= 0, 2, 22
light_strobe 			= 0, 2, 22
light_panel 			= 0, 5, 22
hydraulic_pump 			= 0, 5, 22

[TurbineEngineData]
fuel_flow_gain		= 0.0033
inlet_area		= 4.5
rated_N2_rpm		= 29920
static_thrust		= 4500
afterburner_available	= 0
reverser_available	= 0



//-------------------------------------------------------------------------------------

[jet_engine]
thrust_scalar=1.000 

[Reference Speeds]
flaps_up_stall_speed	=106.000000
full_flaps_stall_speed	=84.000000
cruise_speed		=420
max_indicated_speed	=450.000000
max_mach		=0.989990


//-------------------------------------------------------------------------------------

[Views]

eyepoint= 8.80, 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		=0			//era 1
autothrottle_takeoff_ga			=0			//era 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   
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
//-------------------------------------------------------------------------------------

[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      
//-------------------------------------------------------------------------------------

[Exits]
number_of_exits		=1
exit_rate.0		=0.5
//-------------------------------------------------------------------------------------

[brakes]
parking_brake		=1           	//Parking brake available
toe_brakes_scale	=0.85	 	//Brake scalar  (era 1.0)
differential_braking_scale = 1.0        //Delta on the amount of brake when the rudder pedals deflected

//-------------------------------------------------------------------------------------
[gear_warning_system]
gear_warning_available	=0          //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 = 1500.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2
//-------------------------------------------------------------------------------------
[stall_warning]
type			=2
stick_shaker=1
//-------------------------------------------------------------------------------------
[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]
type		=1
span-outboard	=0.5
extending-time	=7
system_type	=0
flaps-position.0	=0.000
flaps-position.1	=20.000
flaps-position.2	=40.000
damaging-speed	=290
blowout-speed	=330
lift_scalar	=1.000
drag_scalar	=1.000

//-------------------------------------------------------------------------------------

[jet_engine]
thrust_scalar	=1.0



[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=4.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[deice_system]
structural_deice_type=0