[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