[fltsim.0]
title=FIAT G-18V MVG 1
sim=FIAT_G18_MVG
model=
panel=
sound=
texture=NCALI
kb_checklists=
kb_reference=FIAT_G18_MVG_ref
atc_id=
atc_id_color=0xffffffff
ui_manufacturer=FIAT
ui_type="G-18V"
ui_variation=N.C.A.L.I.
description=Nucleo Comunicazioni Avio Linee Italiane I-EION. The "Nucleo Comunicazioni Avio Linee" was established on 10 June 1940, the flying equipment was commandeered and their personal redrafted.These machines soon began special liaison fights first to France (within the Italian Armistice Commission) and later to Albania during the war against Greece.By Manuele Villa on January 2009.
visual_damage=0

[fltsim.1]
title=FIAT G-18V MVG 2
sim=FIAT_G18_MVG
model=NR
panel=
sound=
texture=RA
kb_checklists=
kb_reference=FIAT_G18_MVG_ref
atc_id=
atc_id_color=0xffffffff
ui_manufacturer=FIAT
ui_type="G-18V"
ui_variation=Regia Aeronautica
description=Nucleo Comunicazioni Avio Linee Italiane I-ELCE/Regia Aeronautica. In June 1940, ALI was brought under control of the Regia Aeronautica (Italian Air Force), and the G.18s were put to use as transports. Among other operations, they flew troops to Albania in November 1940 as part of the campaign against Greece. During 1942 the remaining G.18V were painted in the standard Regia Aeronautica's two colors camouflage (Dark Green/Light Gray).By Manuele Villa on January 2009.
visual_damage=0

[fltsim.2]
title=FIAT G-18V MVG 3
sim=FIAT_G18_MVG
model=
panel=
sound=
texture=ALI_PW
kb_checklists=
kb_reference=FIAT_G18_MVG_ref
atc_id=
atc_id_color=0xffffffff
ui_manufacturer=FIAT
ui_type="G-18V"
ui_variation=A.L.I.Pre-War
description=Avio Linee Italiane I-ENEA. The first G.18V, was flown in Turin on 11 March 1937, exhibited at the 2nd International Air Saloon in Milan and operated since December of that year by Avio Linee Italiane together with other five examples (registered I-ELFO, I-ELCE, I-ERME, I-ENEA and l-EURE, respectively).A.L.I.operated them on its European routes until the outbreak of war.By Manuele Villa on January 2009.
visual_damage=0



[General]
atc_type=FIAT 
atc_model=G-18 
editable=0

performance=Press F10 and select lowest icon for on screen handling notes. Read 'Understanding the Fiat G.18.txt' and 'Navigating the Fiat G.18.txt' before flight.

[Views]
eyepoint=14.2, -1.1, 2.9 

[fuel]

1980 litres = c2300 lbs

Oil c330lbs is included in 'empty' weight below.

electric_pump=0
fuel_type = 1
number_of_tank_selectors = 2

LeftMain  = 0, -4.6, 0, 64, 0
LeftAux   = 0, -4.6, 0, 64, 0
LeftTip =   0, -4.6, 0, 64, 0
RightMain = 0,  4.6, 0, 64, 0
RightAux =  0,  4.6, 0, 64, 0
RightTip =  0,  4.6, 0, 64, 0

[weight_and_balance]

max_gross_weight = 22063
empty_weight     = 16359 //including oil

reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0

empty_weight_pitch_MOI =  86000
empty_weight_roll_MOI  = 290000
empty_weight_yaw_MOI   = 340000

empty_weight_coupled_MOI = 0

station_load.0 =  600,0,0,0 //3 crew and bags
station_load.1 = 2800,0,0,0 //14 pax plus bags is max payload with full fuel

[GeneralEngineData]

engine_type = 0
fuel_flow_scalar = 1.0
engine.0 = 10.66, -8.98, -2.45
engine.1 = 10.66,  8.98, -2.45

[piston_engine]

Fiat A80RC41

critical_altitude=11000		//adjusted for RC41 supercharger running at rated = 2100 RPM
cylinder_displacement=154.89
compression_ratio=6.7
number_of_cylinders=18
max_rated_rpm=2200		//TOGA
max_rated_hp=1000		//TOGA
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.8   //0.2
turbocharged=1
max_design_mp=28.96		//1.0 C2 (kg/cm^2)
min_design_mp=0
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=1
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000


[propeller]
propeller_type=0
propeller_blades=3
gear_reduction_ratio=1.0			
propeller_diameter=7.7	
propeller_moi=6	
beta_max=43.0					
beta_min=16.0					
prop_sync_available=1                        
prop_deice_available=1                      
prop_feathering_available=1
feathering_switches = 1                         
prop_auto_feathering_available=0 
min_rpm_for_feather=0                     
beta_feather=88
defeathering_accumulators_available=0     
prop_reverse_available=0                                
power_absorbed_cf=0.9                          
minimum_on_ground_beta=0.000000    				
minimum_reverse_beta=0.000000                    
min_gov_rpm=0.000000
prop_tc=0.1
low_speed_theory_limit=80.000000
fixed_pitch_beta=0


[airplane_geometry]

oswald_efficiency_factor = 0.74
wing_area = 950
wing_span = 82
wing_root_chord = 7.67
wing_pos_apex_lon = 2.9
wing_pos_apex_vert = -2
htail_area = 95.8
htail_span = 28.25
htail_pos_lon = -52.7
htail_pos_vert = -52.7
htail_incidence = 0
htail_sweep = 0
vtail_area = 37.9
vtail_span = 11.49
vtail_sweep = 0
vtail_pos_lon = -51.4
vtail_pos_vert = 6.7
elevator_area = 83.4
aileron_area = 102.8
rudder_area = 46.7
elevator_up_limit = 30.0
elevator_down_limit = 20.0
aileron_up_limit = 27.0
aileron_down_limit = 18.0
rudder_limit = 30.0
elevator_trim_limit = 20.0
spoiler_limit = 60
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
wing_dihedral = 0
wing_incidence = 0
wing_twist = 0
wing_winglets_flag = 0
wing_sweep = 0

[flaps.0]       
type             = 1 
system_type      = 1                                   
span-outboard    = 0                                 
extending-time   = 15                                    
flaps-position.0 = 0 ,0                                  
flaps-position.1 = 10,108                                  
flaps-position.2 = 25,97                                  
flaps-position.3 = 40,97                                  
                            
[Reference Speeds]

flaps_up_stall_speed  =  66           
full_flaps_stall_speed=  59       //Vref=77 KIAS at MLW=MTOW <> 140 KmIAS
cruise_speed          = 188	  //KTAS at 5500M full throttle cruising at 1900 RPM is design condition           max_indicated_speed   = 173       //KIAS Vc but MSFS assigns Vc as Vno
max_indicated_speed=228.000000

[contact_points]

Tailwheel steering implemented for convenience in FS9; alter 40 to 0 within point.0 for max realism.

point.0 = 1, -30.8,  0,  -2.4, 1200, 0, 0.8,  40, 0.19, 2, 0.8,  8,  8, 0, 108, 108
point.1 = 1,   2.0, -9, -10.4, 1200, 1, 1.8,   0, 0.22, 2, 0.8, 11, 12, 2, 108, 108
point.2 = 1,   2.0,  9, -10.4, 1200, 2, 1.8,   0, 0.22, 2, 0.8, 12, 13, 3, 108, 108

point.3 = 2, -0.15, -41, -5.7, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -0.15,  41, -5.7, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -31  ,   0,  1  , 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2,  14.2,   0, -4.3, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0

static_pitch = 13.9
static_cg_height = 9.8
tailwheel_lock = 1
gear_system_type=0

[electrical]
electric_always_available = 1  //simulates compressed air starting not dependent on battery state

[gear_warning_system]
gear_warning_available = 1    
pct_throttle_limit =  0.1     
flap_limit_idle    =  0.0     
flap_limit_power   = 26.0     

[brakes]
parking_brake = 1       
toe_brakes_scale = 0.25  

[hydraulic_system]
normal_pressure = 2850.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.000000

[vacuum_system]
max_pressure=3.800000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,0,0

[Radios]

Audio.1=1 
Com.1=1, 0 
Nav.1=1, 0
Adf.1=1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
direction_indicator.0=1,0 
direction_indicator.1=2,0

[attitude_indicators]
attitude_indicator.0 = 1 
attitude_indicator.1 = 2 

[turn_indicators]
turn_indicator.0=2,0

[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 0
autothrottle_available= 0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=20
max_bank_acceleration=1.8
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 = 0.0


[stall_warning]
type=1

[exits]
number_of_exits = 1
exit_rate.0 = 0.4                               ;Percent per second

[lights]

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

light.0 = 3, 3.54, -36.45, -1.12, fx_shockwave_navred
light.1 = 3, 3.54, 36.45, -1.12, fx_shockwave_navgre
light.2 = 3, -40.33, 0, 2.8, fx_shockwave_navwhi_l_old
light.3 = 4, 15.97, -1.19, 2.53, fx_shockwave_vclight
light.4 = 5, 2.72, -26.67, -2.74, fx_shockwave_landing_light_tail_old
light.5 = 5, 2.72, 26.67, -2.74, fx_shockwave_landing_light_tail_old

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

[forcefeedback]	//not tested

ground_bumps_magnitude1 = 2600
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 3500000

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1