//FD files by Massimo Taccoli with revision and update by G.Quai , 30 June 2013.

[fltsim.0]
title=Nardi FN 305 pre 1962(tail wheel)
sim=nardi305
panel=
model=
sound=
texture=1
prop_anim_ratio	=2  
kb_checklists=
kb_reference=
atc_id=I-DASM
description=Two Seat Basic Trainer and Liaison
ui_type=Nardi FN 305
ui_manufacturer="Nardi (Piaggio)"
ui_variation="With tail wheel pre 1962"
ui_createdby="Massimo Taccoli"

visual_damage=1
atc_flight_number=
atc_id_color=0x00000000
atc_parking_types=RAMP
atc_id_font=Verdana,-11,1,600,0

[fltsim.1]
title=Nardi FN 305 after 1962(tail wheel)
sim=nardi305
panel=
model=
sound=
texture=2
prop_anim_ratio	=2   
kb_checklists=
kb_reference=
atc_id=I-DASM
description=Two Seat Basic Trainer and Liaison
ui_type=Nardi FN 305
ui_manufacturer="Nardi (Piaggio)"
ui_variation="With tail wheel after 1962"
ui_createdby="Massimo Taccoli"

visual_damage=1
atc_flight_number=
atc_id_color=0x00000000
atc_parking_types=RAMP
atc_id_font=Verdana,-11,1,600,0

[General]
performance=Powerplant: One 200 hp (149.14 kW) Alfa Romeo 115 6-cylinder inline piston engine. Wing Span 8.476 m. 27.79ft. Lenght 6.985 m. 22.91 ft. Wing Area 12 mq. 129.17 sq.ft. Accommodation/Crew: Pilot & Student sitting in tandem fully enclosed cockpits with dual controls. 

atc_type	=Nardi FN305 
atc_model	=FN305 
Category	=airplane
editable	=1

[weight_and_balance]

// ACM V2.5
max_gross_weight 			= 2128
empty_weight 				= 1521
reference_datum_position 	= 0, 0, 0
empty_weight_CG_position 	= 0, 0, 0

CG_forward_limit 			= 0.000
CG_aft_limit 				= 1.000

max_number_of_stations 		= 2

station_load.0 = "170, 0.000, 0.000, 0.469, Pilota"      			// Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, 0.000, 0.000, 0.341, Passenger/student"   // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI 		= 948.09
empty_weight_roll_MOI 		= 640.91
empty_weight_yaw_MOI 		= 1261.43
empty_weight_coupled_MOI 	= 0


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3,   0.510, -12.610, -0.690, fx_navred
light.1 = 3,   0.510,  12.610, -0.690, fx_navgre
light.2 = 3, -14.850,  -0.020,  4.800, fx_navwhi
light.3 = 4, -1.470,    0.000,  1.490, fx_vclight
light.4 = 4, -4.590,    0.000,  1.460, fx_vclight

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type 		= 0
fuel_flow_scalar 	= 1.00000
min_throttle_limit 	= 0.00000
engine.0 			= 5.81, 0, 0.64, 

[smokesystem]
smoke.0 			= -1.61, 4.04, 0.07, fx_engstrt

[effects]
dirt 			= fx_tchdrt
concrete 		= fx_sparks
touchdown 		= fx_tchdwn_s, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type 					= 1
number_of_tank_selectors 	= 1
electric_pump 				= 1

Center1 = 0, 0, 0.920, 10.00, 9.20
Center2 = 0, 0, 0.381, 10.50, 9.70


[contact_points]
static_pitch 		= 10.52
static_cg_height 	= 4.01
tailwheel_lock 		= 1
gear_system_type 	= 3
max_number_of_points = 7

point.0 = 1, -15.072,   0,     -1.3019, 1601, 0, 0.29, 60, 0.1,   2.5, 0.95, 0,   0, 0, 0, 0
point.1 = 1,   0.7508, -3.035, -4.2981, 1601, 1, 0.781, 0, 0.249, 2.5, 0.9,  4,   6, 2, 0, 0
point.2 = 1,   0.7508,  3.035, -4.2981, 1601, 2, 0.781, 0, 0.249, 2.5, 0.9,  4.5, 7, 3, 0, 0
point.3 = 2,  -0.653, -13.809, -0.692,  1575, 0, 0.000, 0, 0.000, 0.0, 0.0,  0.0, 0, 5
point.4 = 2,  -0.653,  13.809, -0.692,  1575, 0, 0.000, 0, 0.000, 0.0, 0.0,  0.0, 0, 6
point.5 = 2, -14.564,  0.000,   4.856,  1575, 0, 0.000, 0, 0.000, 0.0, 0.0,  0.0, 0, 9
point.6 = 2,   5.597,  0.000,  -1.558,  1575, 0, 0.000, 0, 0.000, 0.0, 0.0,  0.0, 0, 4


[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000


[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 10000
crash_direction1 = 1000
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 			= 129.17
wing_span 			= 27.80
wing_root_chord 	= 7.05
wing_dihedral 		= 3.27
wing_incidence 		= 0.00000
wing_twist 			= 0.00000
oswald_efficiency_factor = 0.75000
wing_winglets_flag	 	= 0
wing_sweep 				= 7.90
wing_pos_apex_lon 		= 2.07
wing_pos_apex_vert 		= -1.36
htail_area 				= 16.146
htail_span 				= 9.52
htail_pos_lon 			= -12.58
htail_pos_vert 			= 1.00
htail_incidence 		= 0.00000
htail_sweep 			= 16.39
vtail_area 				= 12.48
vtail_span 				= 3.19
vtail_sweep 			= 37.39
vtail_pos_lon 			= -11.98
vtail_pos_vert 			= 1.66
elevator_area 			= 21.74
aileron_area 			= 5.87
rudder_area 			= 7.42
elevator_up_limit 		= 25.00000
elevator_down_limit 	= 25.00000
aileron_up_limit 		= 22.00000
aileron_down_limit 		= 22.00000
rudder_limit 			= 20.00
elevator_trim_limit 	= 20.00000
spoiler_limit 			= 0.00000
aileron_to_spoileron_gain = 0.00000
spoiler_handle_available 	= 0
min_ailerons_for_spoilerons = 0.00000
min_flaps_for_spoilerons 	= 0.00000
spoilerons_available 		= 0
auto_spoiler_available=0
positive_g_limit_flaps_up=4.047009
positive_g_limit_flaps_down=2.833333
negative_g_limit_flaps_up=-3.238248
negative_g_limit_flaps_down=-2.428419

[electrical]
max_battery_voltage 			= 24
generator_alternator_voltage 	= 28
max_generator_alternator_amps 	= 60
engine_generator_map 			= 1
electric_always_available 		= 0
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
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

[Exits]
number_of_exits	= 4 			// Canopy part front and back, sliding window front and back seat.
exit_rate.0    	= 0.5
exit_rate.1   	= 0.5
exit_rate.2    	= 0.5
exit_rate.3   	= 0.5

[piston_engine]
max_rpm_mechanical_efficiency_scalar	=1.00000 
idle_rpm_mechanical_efficiency_scalar	=1.00000 
max_rpm_friction_scalar					=1.00000 
idle_rpm_friction_scalar				=1.00000 
cylinder_displacement					=93.42735
compression_ratio						=6.50
number_of_cylinders						=6 
max_rated_rpm							=2205
max_rated_hp							=200
fuel_metering_type						=1 
cooling_type							=1 
normalized_starter_torque				=0.30327 
turbocharged							=0 
max_design_mp							=29.91978 
min_design_mp							=2.992
critical_altitude						=0.00000 
emergency_boost_type					=0 
emergency_boost_mp_offset				=0.00000 
emergency_boost_gain_offset				=0.00000 
fuel_air_auto_mixture					=0 
auto_ignition							=0 
power_scalar							=1.00000 
emergency_boost_duration				=0.00000 
BestPowerSpecificFuelConsumption		=0.50000
detonation_onset						=32.91117

[propeller]
thrust_scalar							=1.00000 
propeller_type							=1 
propeller_diameter						=7.22
propeller_blades						=2 
propeller_moi							=1.15   
beta_max								=21.00000       
beta_min								=19.00000     	
min_gov_rpm								=0.00000 
prop_tc									=0.10000 
gear_reduction_ratio					=1.00000 
fixed_pitch_beta						=20.00000 
low_speed_theory_limit					=80.00000 
prop_sync_available						=0 
prop_deice_available					=0 
prop_feathering_available				=0 
prop_auto_feathering_available			=0 
min_rpm_for_feather						=0.00000 
beta_feather							=0.00000 
power_absorbed_cf						=0.00000 
defeathering_accumulators_available		=0 
prop_reverse_available					=0 
minimum_on_ground_beta					=0.00000 
minimum_reverse_beta					=0.00000 
rotation 								=-1

[Reference Speeds]
flaps_up_stall_speed			=64 
full_flaps_stall_speed			=58 
cruise_speed					=107.99140 
max_indicated_speed				=178.99568  
max_mach						=0.40000

[Views]
eyepoint					=-2.887, 0.00, 1.978   //(feet) longitudinal, lateral, vertical distance from reference datum

[autopilot]
autopilot_available				=1
flight_director_available		=0 
default_vertical_speed			=700 
autothrottle_available			=0 
pitch_takeoff_ga				=8 
max_pitch									=10
max_pitch_acceleration						=1
max_pitch_velocity_lo_alt					=2
max_pitch_velocity_hi_alt					=1.5
max_pitch_velocity_lo_alt_breakpoint		=20000
max_pitch_velocity_hi_alt_breakpoint		=28000
max_bank									=25
max_bank_acceleration						=1.8
max_bank_velocity							=3
max_throttle_rate							=0.1
nav_proportional_control					=9
nav_integrator_control						=0.25
nav_derivative_control						=0
nav_integrator_boundary						=2.5
nav_derivative_boundary						=0
gs_proportional_control						=9.52
gs_integrator_control						=0.26
gs_derivative_control						=0
gs_integrator_boundary						=0.7
gs_derivative_boundary						=0
yaw_damper_gain								=1
default_pitch_mode							=0
default_bank_mode							=0
autothrottle_arming_required				=0
autothrottle_takeoff_ga						=1
autothrottle_max_rpm						=90
use_no_default_bank							=1
use_no_default_pitch						=1


// Radio Type = availiable, standby frequency, has glide slope

[Radios]
Audio.1       = 0
Com.1         = 1, 0
Nav.1         = 0, 0, 0
Adf.1         = 0
Transponder.1 = 0
Marker.1      = 0

[direction_indicators]
direction_indicator.0=1,0 

[flight_tuning]
cruise_lift_scalar			=1.00000 
pitch_stability				=1.00000 
roll_stability				=1.00000 
yaw_stability				=1.00000 
parasite_drag_scalar		=1.00000 
induced_drag_scalar			=1.00000 
elevator_effectiveness		=1.00000 
aileron_effectiveness		=1.00000 
rudder_effectiveness		=1.00000 
elevator_trim_effectiveness	=0.82000 
aileron_trim_effectiveness	=1.00000 
rudder_trim_effectiveness	=1.00000 
p_factor_on_yaw          	=0.25000
torque_on_roll           	=0.80000
gyro_precession_on_yaw   	=1.00000
gyro_precession_on_pitch 	=1.00000
hi_alpha_on_roll			=1.00000
hi_alpha_on_yaw				=1.00000
gyro_precession_on_roll		=0.70000

[Flaps.0]
type				= 1
system_type			= 3
span-outboard		= 0.500
extending-time		= 3.0
damaging-speed		=102.6
blowout-speed		=124.2
flaps-position.0	=0.00
flaps-position.1	=15.00
flaps-position.2	=35.00
lift_scalar			=0.90
drag_scalar			=1.30
pitch_scalar		=0.01

[brakes]
toe_brakes_scale			=0.60000
parking_brake				=1
differential_braking_scale 	=1.00000     
auto_brakes					=0
hydraulic_system_scalar		=0.00000

[hydraulic_system]
normal_pressure				=986.25666
engine_map					=1,0,0,0

[stall_warning]
type						=1
stick_shaker				=0

[attitude_indicators]
attitude_indicator.0		=1

[turn_indicators]
turn_indicator.0			=1,0

[pitot_static]
pitot_heat					=1.0

[vacuum_system]
max_pressure				=5.15
vacuum_type					=1
electric_backup_pressure	=0
engine_map					=1, 0, 0, 0

[pneumatic_system]
max_pressure				=0
bleed_air_scalar			=0

[deice_system]
structural_deice_type		=0

[gear_warning_system]
gear_warning_available		=0
pct_throttle_limit			=0.00000
flap_limit_power			=16.87500
flap_limit_idle				=33.75000