[fltsim.0]
title=F6MZ
sim=F6MZ
model=
panel=
sound=
texture=
kb_checklists=

ui_manufacturer=Caproni Vizzola
ui_type= F6MZ
ui_variation= Protoype- MM498

description=Caproni Vizzola F6Mz Fighter-First flight august 1943\n Only one aircraft build with MM 498 with the "Continental" camouflage\nFor description see file 

[General]
performance=Lenth 9,25m\nWingspan 11,82 m\nEmpty weight 2,238Kg\nPower plant: 1 × Isotta-Fraschini R.C.25/60 Zeta 24-cylinder X-type piston, 1,118 kW (1,500 hp)\nMax speed:630Km/h\nrange:1,060Km\nService ceiling 9,000 m


[WEIGHT_AND_BALANCE]
empty_weight = 6331

reference_datum_position=0.0, 0.0, 0.0	// (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.095, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=10

station_load.0=200,  -3.0, 0.0, 3.0		//Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI  = 6193
empty_weight_roll_MOI  = 5511
empty_weight_yaw_MOI  = 10832
empty_weight_coupled_MOI=0.000000
max_gross_weight=9796.500000





[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0





[piston_engine]
power_scalar=1.0
cylinder_displacement=181.500000
compression_ratio=8.500000
number_of_cylinders=12
max_rated_rpm=2800.000000
max_rated_hp=1350.000000
fuel_metering_type=0
cooling_type=1
normalized_starter_torque=0.035000
turbocharged=1
max_design_mp=39.869999
min_design_mp=9.000000
critical_altitude=22966.000000
emergency_boost_type=2
emergency_boost_mp_offset=2.210000
emergency_boost_gain_offset=0.185178
fuel_air_auto_mixture=0
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]
thrust_scalar=1.0
propeller_type=0
propeller_diameter=11.000000
propeller_blades=2
propeller_moi=27.580348
beta_max=65.000000
beta_min=15.000000
min_gov_rpm=420.000000
prop_tc=0.010000
gear_reduction_ratio=2.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=70.000000
beta_feather=88.500000
power_absorbed_cf=0.900000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=1.000000
minimum_reverse_beta=-14.000000





[exits]
number_of_exits=3
exit_rate.0=0.4	 				;Percent per second
exit_rate.1=0.4	 
exit_rate.2=0.4	 





[electrical]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0





[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)
point.0=1.0,-12.30, 0.0,     -2.06,   2165.354400,0.0,0.557255,12.0,0.292829,2.50,0.462118,3.0,3.0,0.0,0.0,0.0
point.1=1.0,  3.250,   -5.916667,-6.40,   2165.354400,1.0,0.557255,0.0,0.965931,2.50,0.649925,5.50,5.0,2.0,0.0,0.0
point.2=1.0,  3.250,    5.916667,-6.40,   2165.354400,2.0,0.557255,0.0,0.965931,2.50,0.649925,5.50,5.0,3.0,0.0,0.0
point.3=2.0,  0.0,    -18.50,     0.0,    1181.102400,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,5.0,0.0,0.0
point.4=2.0,  0.0,     18.50,     0.0,    1181.102400,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0
point.5=2.0,-14.166667,0.0,      -0.50,   1181.102400,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0
point.6=2.0,  9.250,   0.0,      -1.916667,1181.102400,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0

static_pitch=12.0
static_cg_height=4.8
gear_system_type=1






[forcefeedback]
gear_bump_nose_magnitude=6000		; 0 - 10000
gear_bump_nose_direction=18000		; 0 - 35999 degrees
gear_bump_nose_duration=250000		; in microseconds
gear_bump_left_magnitude=6000		; 0 - 10000
gear_bump_left_direction=35500		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=6000		; 0 - 10000
gear_bump_right_direction=00500		; 0 - 35999 degrees
gear_bump_right_duration=250000		; in microseconds
ground_bumps_magnitude1=3250		; 0 - 10000
ground_bumps_angle1=8900		; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750		; 0 - 10000
ground_bumps_angle2=9100		; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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






[Views]
eyepoint=3.10,0.035,2.52






[LIGHTS]
light.0=4,3.10,0.035,2.52, fx_vclight_s403







[fuel]
Center1=0.010000,0.000000,0.000000,65.000000,0.000000
LeftMain=0.000000,-4.000000,-2.000000,25.000000,0.000000
RightMain=0.000000,4.000000,-2.000000,25.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=1




[airplane_geometry]
wing_area=227.000000
wing_span=38.916667
wing_root_chord=5.833333
wing_dihedral=4.998779
wing_incidence=0.999756
wing_twist=0.000000
oswald_efficiency_factor=0.889527
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=27.000000
htail_span=15.583333
htail_pos_lon=-16.916667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=13.000000
vtail_span=4.110961
vtail_sweep=0.000000
vtail_pos_lon=-16.916667
vtail_pos_vert=5.833333
elevator_area=18.100000
aileron_area=21.900000
rudder_area=9.800000
elevator_up_limit=30.000000
elevator_down_limit=20.000000
aileron_up_limit=15.000000
aileron_down_limit=15.000000
rudder_limit=30.000000
elevator_trim_limit=18.000000
spoiler_limit=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000




[brakes]
toe_brakes_scale=0.640889
parking_brake=1




[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000




[Flaps.0]
type=1
span-outboard=0.500000
extending-time=2.000000
system_type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=15.000000,0.000000
flaps-position.2=30.000000,0.000000
flaps-position.3=45.000000,0.000000




[GeneralEngineData]
engine_type=0
Engine.0=9.250000,0.000000,-0.083333
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000




[Reference Speeds]
flaps_up_stall_speed=97.000000
full_flaps_stall_speed=77.600000
cruise_speed=250.000000
max_indicated_speed=387.000000




[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000




[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
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




[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.930556




[stall_warning]
type=1




[attitude_indicators]
attitude_indicator.0=1




[turn_indicators]
turn_indicator.0=1,0




[direction_indicators]
direction_indicator.0=1,0