[fltsim.0]
title=CRDA Cant.Z 506A I-LERO
sim=Z506AC
model=A
panel=
sound=
texture=I-LERO
ui_manufacturer=C.R.D.A.
ui_type=Cant Z.506 A
ui_variation=Ala Littoria I-LERO
description=Cant Z.506 A 'Ala Littoria'I-LERO, 1937. Developed from a design of Ing. Zappata, the first prototype of this seaplane, flown by test pilot Stoppani, did its maiden flight, powered by three  American made Wright Cyclone, in August 1936 and gained immediately eight world records in speed and two in altitude in the seaplane  category. Successive versions, powered by three Alfa Romeo 126 RC10 (later RC34), gained another 16 world records. These airplanes (A or  C) were intended for commercial transport of 12/14 passengers and were employed by Ala Littoria Company on mediterranean routes. During  WWII all the civilian aircraft, aquired by Regia Aeronautica (Royal Italian Air Force), were used in communication and SAR roles.Created by Manuele Villa , July 2007.
atc_id_color=0000000000
visual_damage=0

[fltsim.1]
title=CRDA Cant.Z 506A I-RODI
sim=Z506AC
model=A
panel=
sound=
texture=I-RODI
ui_manufacturer=C.R.D.A.
ui_type=Cant Z.506 A
ui_variation=Ala Littoria I-RODI
description=Cant Z.506 A 'Nucleo Comunicazioni Ala Littoria'I-RODI, 1939. Developed from a design of Ing. Zappata, the first prototype of this seaplane, flown by test pilot Stoppani, did its maiden flight, powered by three  American made Wright Cyclone, in August 1936 and gained immediately eight world records in speed and two in altitude in the seaplane  category. Successive versions, powered by three Alfa Romeo 126 RC10 (later RC34), gained another 16 world records. These airplanes (A or  C) were intended for commercial transport of 12/14 passengers and were employed by Ala Littoria Company on mediterranean routes. During  WWII all the civilian aircraft, aquired by Regia Aeronautica (Royal Italian Air Force), were used in communication and SAR roles.Created by Manuele Villa , July 2007.
atc_id_color=0000000000
visual_damage=0

[fltsim.2]
title=CRDA Cant.Z 506A SOCCORSO
sim=Z506AC
model=A
panel=
sound=
texture=SOCCORSO
ui_manufacturer=C.R.D.A.
ui_type=Cant Z.506 A
ui_variation=Regia Aeronautica Soccorso
description=Cant Z.506 A 'Regia Aeronautica',612th Squadriglia Soccorso, 1941. Developed from a design of Ing. Zappata, the first prototype of this seaplane, flown by test pilot Stoppani, did its maiden flight, powered by three  American made Wright Cyclone, in August 1936 and gained immediately eight world records in speed and two in altitude in the seaplane  category. Successive versions, powered by three Alfa Romeo 126 RC10 (later RC34), gained another 16 world records. These airplanes (A or  C) were intended for commercial transport of 12/14 passengers and were employed by Ala Littoria Company on mediterranean routes. During  WWII all the civilian aircraft, aquired by Regia Aeronautica (Royal Italian Air Force), were used in communication and SAR roles.Created by Manuele Villa , July 2007.
atc_id_color=0000000000
visual_damage=0

[fltsim.3]
title=CRDA Cant.Z 506C I-PAUL
sim=Z506AC
model=C
panel=
sound=
texture=I-PAUL
ui_manufacturer=C.R.D.A.
ui_type=Cant Z.506 C
ui_variation=Ala Littoria I-PAUL
description=Cant Z.506 C 'Nucleo Comunicazioni Ala Littoria'I-PAUL, personal aircraft of Italo Balbo,1939. Developed from a design of Ing. Zappata, the first prototype of this seaplane, flown by test pilot Stoppani, did its maiden flight, powered by three  American made Wright Cyclone, in August 1936 and gained immediately eight world records in speed and two in altitude in the seaplane  category. Successive versions, powered by three Alfa Romeo 126 RC10 (later RC34), gained another 16 world records. These airplanes (A or  C) were intended for commercial transport of 12/14 passengers and were employed by Ala Littoria Company on mediterranean routes. During  WWII all the civilian aircraft, aquired by Regia Aeronautica (Royal Italian Air Force), were used in communication and SAR roles.Created by Manuele Villa , July 2007.
atc_id_color=0000000000
visual_damage=0

[fltsim.4]
title=CRDA Cant.Z 506C I-DITO
sim=Z506AC
model=C
panel=
sound=
texture=I-DITO
ui_manufacturer=C.R.D.A.
ui_type=Cant Z.506 C
ui_variation=Ala Littoria I-DITO
description=Cant Z.506 C 'Nucleo Comunicazioni Ala Littoria'I-DITO,1939. Developed from a design of Ing. Zappata, the first prototype of this seaplane, flown by test pilot Stoppani, did its maiden flight, powered by three  American made Wright Cyclone, in August 1936 and gained immediately eight world records in speed and two in altitude in the seaplane  category. Successive versions, powered by three Alfa Romeo 126 RC10 (later RC34), gained another 16 world records. These airplanes (A or  C) were intended for commercial transport of 12/14 passengers and were employed by Ala Littoria Company on mediterranean routes. During  WWII all the civilian aircraft, aquired by Regia Aeronautica (Royal Italian Air Force), were used in communication and SAR roles.Created by Manuele Villa , July 2007.
atc_id_color=0000000000
visual_damage=0

[fltsim.5]
title=CRDA Cant.Z 506C I-DOTE
sim=Z506AC
model=C_NR
panel=
sound=
texture=I-DOTE
ui_manufacturer=C.R.D.A.
ui_type=Cant Z.506 C
ui_variation=Ala Littoria I-DOTE
description=Cant Z.506 C 'Nucleo Comunicazioni Ala Littoria'I-DOTE,1940. Developed from a design of Ing. Zappata, the first prototype of this seaplane, flown by test pilot Stoppani, did its maiden flight, powered by three  American made Wright Cyclone, in August 1936 and gained immediately eight world records in speed and two in altitude in the seaplane  category. Successive versions, powered by three Alfa Romeo 126 RC10 (later RC34), gained another 16 world records. These airplanes (A or  C) were intended for commercial transport of 12/14 passengers and were employed by Ala Littoria Company on mediterranean routes. During  WWII all the civilian aircraft, aquired by Regia Aeronautica (Royal Italian Air Force), were used in communication and SAR roles.Created by Manuele Villa , July 2007.
atc_id_color=0000000000
visual_damage=0

[weight_and_balance]

// ACM V2.3
max_gross_weight = 26455
empty_weight = 17637
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 144665
empty_weight_roll_MOI = 231750
empty_weight_yaw_MOI = 294911
empty_weight_coupled_MOI = 0
max_number_of_stations = 6

station_load.0 = 170, 4.20, 0.98, 0.90
station_load.1 = 170, 4.16, -1.01, 0.90
station_load.2 = 170, -7.72, 1.26, 1.18
station_load.3 = 170, -10.71, 1.29, 1.18
station_load.4 = 170, -10.74, -1.29, 1.23
station_load.5 = 170, -7.76, -1.20, 1.18
station_load.6 = 170, -13.86, 1.23, 1.15
station_load.7 = 170, -13.85, -1.32, 1.15
station_load.8 = 170, -17.57, 1.23, 1.20
station_load.9 = 170, -17.57, -1.29, 1.15
station_load.10 = 170, -20.32, 1.23, 1.20
station_load.11 = 170, -20.36, -1.37, 1.20
station_load.12 = 170, -23.10, 1.23, 1.20
station_load.13 = 170, -23.10, -1.32, 1.20
station_load.14 = 170, -4.70, 1.29, 1.11
station_load.15 = 170, -4.73, -1.29, 1.11
station_load.16 = 170, -0.04, 1.08, 0.93
station_load.17 = 170, -0.04, -1.06, 0.93


[lights]

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

light.0 = 3, -1.40, -42.72, 3.39, fx_navredsml
light.1 = 3, -1.40, 42.79, 3.41, fx_navgresml
light.2 = 3, -45.11, 0.01, 2.22, fx_navwhisml
light.3 = 4, 3.38, 0, 3.33, fx_vclight_ju

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.000000
engine.0 = 15.05, 0, 0.31,
engine.1 = 9.75, 11.31, 0,
engine.2 = 9.75, -11.32, 0,
min_throttle_limit=0.000000

[smokesystem]
smoke.0 = 0.25, 11.76, 0, fx_nicks_watrsnoland_s
smoke.1 = 0, 6.5, -11.2, fx_nicks_watrsnoland_s
smoke.2 = 0, 6.5, 11.2, fx_nicks_watrsnoland_s

[effects]
wake = fx_wakeju
water = fx_sprayju
waterspeed = fx_sprayju
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s

[fuel]

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

fuel_type = 1
number_of_tank_selectors = 1

LeftMain = -2.2, -8, -0.1, 220, 0
LeftAux = -2.2, -4.5, -0.34, 220, 0
RightMain = -2.2, 8, -0.1, 220, 0
RightAux = -2.2, 4.5, -0.34, 220, 0
electric_pump=0


[contact_points]
static_pitch = -1
static_cg_height = 11.8
max_number_of_points = 10

point.0 = 4, -21.5888, -11.17, -9.18, 4000.504, 0, 0.654205, 48.24, 1.271411, 2.5, 0.299433, 0, 0, 0, 0, 0
point.1 = 4, 15.9013, -11.17, -10, 4000.504, 0, 0.654205, 48.24, 1.271411, 2.5, 0.299433, 0, 0, 0, 0, 0
point.2 = 4, 15.9031, 11.17, -10, 4000.504, 0, 0.654205, 48.24, 1.271411, 2.5, 0.299433, 0, 0, 0, 0, 0
point.3 = 4, -21.5932, 11.17, -9.18, 4000.504, 0, 0.654205, 48.24, 1.271411, 2.5, 0.299433, 0, 0, 0, 0, 0
point.4 = 2,-5.666667,-44.166667,2.72562,2200.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,5.0,0.0,0.0
point.5 = 2,-5.666667,44.166667,2.72562,2200.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0
point.6 = 2,-49.0,0.0,-0.774377,2200.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0
point.7 = 2,22.75,0.0,-7.21043,2200.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0
point.8 = 2,0.0,-11.166667,-7.44104,2200.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,5.0,0.0,0.0
point.9 = 2,0.0,11.166667,-7.44104,2200.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0


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


[forcefeedback]
gear_bump_nose_magnitude = 7000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 9000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 9000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 7500
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 2300
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 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 8000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0,0,-1.3990,4.7828,1.4594,1.4594,-1.2719,3.1070,2.7697,2.7697
//ACM_AREAW2// -1.1835,3.0274,4.2357,4.2357,-1.0210,2.9553,6.1044,6.1044,-0.8597,2.8824
//ACM_AREAW3// 7.8081,7.8081,-0.7110,2.7973,8.9188,8.9188,-0.6118,2.7362,10.4238,10.4238
//ACM_AREAW4// -0.4413,2.6245,12.1996,12.1996,-0.0702,2.1719,13.0424,13.0424,0.4713,1.4084
//ACM_AREAH1// -0.0174,-0.0174,-1.6066,0.2124,0.2915,0.2915,-1.5714,0.3433,0.5479,0.5479
//ACM_AREAH2// -1.5190,0.8058,0.9444,0.9444,-1.4493,0.8144,1.3932,1.3932,-1.3621,0.8054
//ACM_AREAH3// 1.8415,1.8415,-1.2747,0.8141,2.4827,2.4827,-1.0477,0.8051,2.8965,2.8965
//ACM_AREAH4// -0.8381,0.7789,3.5548,3.5548,-0.4189,0.6653,3.8986,3.8986,0.0522,0.3770
//ACM_AREAV1// -2.0185,-2.0185,-2.2190,1.3789,-1.5898,-1.5898,-1.7446,1.3271,-1.3171,-1.3171
//ACM_AREAV2// -1.6517,1.2984,-0.9620,-0.9620,-1.5785,1.2733,-0.5726,-0.5726,-1.5075,1.2401
//ACM_AREAV3// -0.2293,-0.2293,-1.3832,1.1878,0.1040,0.1040,-1.2480,1.0994,0.4821,0.4821
//ACM_AREAV4// -1.0425,0.8719,0.8295,0.8295,-0.7462,0.5705,1.0578,1.0578,-0.3677,0.1395
//ACM_CAREAW1// 6.6336,6.6336,2.2846,2.8615,8.0038,8.0038,2.2465,2.7829,8.9181,8.9181
//ACM_CAREAW2// 2.2193,2.7290,9.6653,9.6653,2.2039,2.6865,10.4167,10.4167,2.1809,2.6105
//ACM_CAREAW3// 11.1525,11.1525,2.1596,2.4900,11.4299,11.4299,2.1596,2.4268,11.6597,11.6597
//ACM_CAREAW4// 2.1477,2.3714,11.8815,11.8815,2.1407,2.3287,12.1576,12.1576,2.1517,2.1860
//ACM_CAREAH1// 0.0307,0.0307,0.1448,0.2352,0.6065,0.6065,0.1254,0.8238,0.9980,0.9980
//ACM_CAREAH2// 0.1254,0.8381,1.3875,1.3875,0.1254,0.8299,1.8659,1.8659,0.1254,0.8105
//ACM_CAREAH3// 2.5009,2.5009,0.1448,0.8136,3.3280,3.3280,0.1650,0.7379,3.4082,3.4082
//ACM_CAREAH4// -0.5284,0.7074,3.6809,3.6809,-0.2903,0.5982,3.9061,3.9061,0.0153,0.3429
//ACM_CAREAV1// -1.7460,-1.7460,-0.1207,1.4212,-1.3602,-1.3602,-0.1207,1.3020,-0.9498,-0.9498
//ACM_CAREAV2// -0.1207,1.2704,-0.6460,-0.6460,-0.1084,1.2482,-0.3865,-0.3865,-0.1084,1.2042
//ACM_CAREAV3// -0.1088,-0.1088,-0.1206,1.1555,0.1782,0.1782,-0.1084,1.0700,0.4693,0.4693
//ACM_CAREAV4// -0.0926,0.8917,0.7842,0.7842,0.0344,0.5835,0.9782,0.9782,0.1699,0.2289
wing_area = 1008.700000
wing_span = 87.460
wing_root_chord = 6.666667
wing_dihedral = 2.499390
wing_incidence = 2.499390
wing_twist = 0.000000
oswald_efficiency_factor = 0.667098
wing_winglets_flag = 0
wing_sweep = 0.000000
wing_pos_apex_lon = 0.000000
wing_pos_apex_vert = 0.000000
htail_area = 331.000000
htail_span = 43.000000
htail_pos_lon = -39.333333
htail_pos_vert = 0.000000
htail_incidence = -0.499878
htail_sweep = 0.000000
vtail_area = 220.000000
vtail_span = 16.911535
vtail_sweep = 0.000000
vtail_pos_lon = -39.333333
vtail_pos_vert = 9.833333
elevator_area = 101.400000
aileron_area = 61.210000
rudder_area = 50.100000
elevator_up_limit = 28.000447
elevator_down_limit = 22.998526
aileron_up_limit = 26.000825
aileron_down_limit = 18.999280
rudder_limit = 28.000447
elevator_trim_limit = 19.996227
spoiler_limit = 57.295780
aileron_to_spoileron_gain = 0.000000
min_ailerons_for_spoilerons = 0.000000
min_flaps_for_spoilerons = 0.000000
spoilerons_available = 1

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

[piston_engine]
power_scalar=1.0 
cylinder_displacement=181.844000 
compression_ratio=6.400000 
number_of_cylinders=9 
max_rated_rpm=2300.000000 
max_rated_hp=800.000000 
fuel_metering_type=2 
cooling_type=0 
normalized_starter_torque=0.035000 
turbocharged=1 
max_design_mp=44.499999 
min_design_mp=1.000000 
critical_altitude=21000.000000 
emergency_boost_type=0 
emergency_boost_mp_offset=0.000000 
emergency_boost_gain_offset=0.000000 
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=0.85 
propeller_type=0 
propeller_diameter=12 
propeller_blades=3 
propeller_moi=40 
beta_max=60 
beta_min=18 
min_gov_rpm=1200 
prop_tc=0.003 
gear_reduction_ratio=1.8 // 1.85
fixed_pitch_beta=0.000000 
low_speed_theory_limit=80.000000 
prop_sync_available=0 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=1200.000000 
beta_feather=12.000000 
power_absorbed_cf=0.300000 
defeathering_accumulators_available=0 
prop_reverse_available=0 
minimum_on_ground_beta=0.0 
minimum_reverse_beta=0.0 

[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 

[Views]
eyepoint=2.6,-1.0,3.5 

[General]
performance=Wingspan: 87 ft. 6.5 in. \nLength: 62 ft. 5.5 in. \nHeight: 23 ft. 6 in.  \nAlfa Romeo AR126 RC-10\nMax Horsepower (each): 800\nCrew: 4\nMaximum Speed: 200 mph. \nCeiling: 20,000 ft. \nMaximum Range: 1,242 miles \nPassengers 14-16 \n 
editable=0 

[brakes]
toe_brakes_scale=0.000000
parking_brake=0
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=20.330853,0.000000
flaps-position.2=40.661706,0.000000
flaps-position.3=60.992559,0.000000

[Reference Speeds]
flaps_up_stall_speed=60.000000 
full_flaps_stall_speed=48.000000 
cruise_speed=168.819890 
max_indicated_speed=250.000000

[autopilot]
autopilot_available=1 
flight_director_available=0 
default_vertical_speed=700.000000 
autothrottle_available=0 
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=1,1,1,0
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