[fltsim.0] title=Breda Zappata BZ308 sim=BZ308 model= panel= sound= texture= kb_checklists= ui_manufacturer=BREDA ui_type=BZ308 ui_variation=STATO MAGGIORE atc_heavy=0 atc_id=BZ308 atc_airline=AIR FORCE atc_flight_number=SM5 ui_typerole="4 Engines Piston" ui_createdby="I. D'Attomo & G. Quai" description=Called the italian Constellation, the B.Z.308 was a large low-wing monoplane of all-metal construction, the fuselage had an oval cross-section. It had a large tailplane with endplate fins and rudders, retractable landing gear. Powered by four Bristol Centaurus radial engines driving five-bladded propellers, it was designed for a flightcrew of five, and 55 passengers in two cabins, a high-density model was planned with seats for 80. Although flight testing went well, financial problems and the realisation that competition from American-built airliners would take a major share of the post-war airliner market, along with the pressures to close down the Aeronautical section of the Breda, led to the project being abandoned. Breda stopped producing airplanes subsequently. [fltsim.1] title=Breda Zappata BZ308PAINT1 sim=BZ308 model= panel= sound= texture=1 kb_checklists= ui_manufacturer=BREDA ui_type=BZ308 ui_variation=Factory Paint atc_heavy=0 atc_id=BZ308 atc_airline=I-BREZ atc_flight_number=BEZ ui_typerole="4 Engines Piston" ui_createdby="I. D'Attomo & G. Quai" description=Called the italian Constellation, the B.Z.308 was a large low-wing monoplane of all-metal construction, the fuselage had an oval cross-section. It had a large tailplane with endplate fins and rudders, retractable landing gear. Powered by four Bristol Centaurus radial engines driving five-bladded propellers, it was designed for a flightcrew of five, and 55 passengers in two cabins, a high-density model was planned with seats for 80. Although flight testing went well, financial problems and the realisation that competition from American-built airliners would take a major share of the post-war airliner market, along with the pressures to close down the Aeronautical section of the Breda, led to the project being abandoned. Breda stopped producing airplanes subsequently. [General] ui_type=BZ308 ui_model=BZ308 performance=Wing span: 42.10 mt\ Length: 33.5 mt\ Weight: 88,185 lbs (max)\ Power:4x 2500 HP Bristol Centaurus radial piston. Max Speed: 357 mph (575 Km/h). Category=airplane [WEIGHT_AND_BALANCE] reference_datum_position=0,0,0 empty_weight_CG_position=0,0,0 max_number_of_stations=50 station_load.0=340.00,0.00,0.00,0.00 station_load.1=170.00,-6.00,0.00,0.00 empty_weight=60000 empty_weight_roll_MOI=1066725 empty_weight_pitch_MOI=1417509 empty_weight_yaw_MOI=1786469 empty_weight_coupled_MOI=1 max_gross_weight=120000 [airplane_geometry] wing_area=1736 wing_span=141 wing_root_chord=11 wing_dihedral=4.5 wing_incidence=2.2 wing_twist=0 oswald_efficiency_factor=0.36 wing_winglets_flag=0 wing_sweep=0 wing_pos_apex_lon=4 wing_pos_apex_vert=-1 htail_area=356 htail_span=43 htail_pos_lon=-60 htail_pos_vert=6 htail_incidence=0.0 htail_sweep=0 vtail_area=333 vtail_span=20 vtail_sweep=25 vtail_pos_lon=-58 vtail_pos_vert=8 elevator_area=183 aileron_area=198 rudder_area=116 elevator_up_limit=27 elevator_down_limit=27 aileron_up_limit=25 aileron_down_limit=25 rudder_limit=25 elevator_trim_limit=26 spoiler_limit=0 spoilerons_available=0 aileron_to_spoileron_gain=0 min_ailerons_for_spoilerons=0 min_flaps_for_spoilerons=0 //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) auto_spoiler_available=0 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-1.500000 negative_g_limit_flaps_down=-1.500000 //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type [contact_points] point.0=1, 30.63, 0, -13.5, 1100, 0, 1.35, 30, 1, 2.5, 0.7, 4.5, 5, 0, 0, 0 point.1=1, -10, -20.66, -13.8, 1575, 1, 2.65, 0, 1, 2.5, 0.7, 5.5, 6, 0, 0, 0 point.2=1, -10, 20.66, -13.8, 1575, 2, 2.65, 0, 1, 2.5, 0.7, 4.5, 5, 0, 0, 0 point.3=2, -1.2,-47.33, 0, 787.40,0,0,0,0,0,0,0,0,5,0,0 point.4=2, -1.2, 47.33, 0, 787.40,0,0,0,0,0,0,0,0,6,0,0 point.5=2, -64, 0, 16.83, 787.40,0,0,0,0,0,0,0,0,9,0,0 point.6=2, 29.2, 0, -3.75, 787.40,0,0,0,0,0,0,0,0,4,0,0 static_pitch=0.0 static_cg_height=11 gear_system_type=0 [Flaps.0] type=1 system_type=1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None span-outboard=0.50 extending-time=5.0 flaps-position.0=0.00 flaps-position.1=15.00 flaps-position.2=30.00 flaps-position.3=45.00 damaging-speed=290 // KIAS blowout-speed=360 // KIAS lift_scalar=0.1 drag_scalar=3.0 pitch_scalar=1.0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=1 ;Percent per second [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 0 fuel_flow_scalar = 1.000 engine.0 = 12.167, -30.000, 1.00 engine.1 = 14.167, -13.750, -1.00 engine.2 = 14.160, 13.750, -1.00 engine.3 = 12.167, 30.000, 1.00 min_throttle_limit=0.00 [piston_engine] cylinder_displacement=186.110 compression_ratio=6.850 number_of_cylinders=18 max_rated_rpm=2700 max_rated_hp=2500 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.035 turbocharged=1 max_design_mp=47 min_design_mp=9.5 critical_altitude=25000 emergency_boost_type=0 emergency_boost_mp_offset=0.000 emergency_boost_gain_offset=0.000 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 power_scalar=1.000 [propeller] propeller_type=0 propeller_diameter=15.1 propeller_blades=5 propeller_moi=60.000 beta_max=65.000 beta_min=15.000 min_gov_rpm=700.00 prop_tc=0.010 gear_reduction_ratio=1.80 fixed_pitch_beta=0.000 low_speed_theory_limit=80.000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000 beta_feather=0.000 power_absorbed_cf=0.9 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000 minimum_reverse_beta=0.000 thrust_scalar=1.65 [flight_tuning] cruise_lift_scalar=2.5 parasite_drag_scalar=1.0 induced_drag_scalar=2.0 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=1.8 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [Reference Speeds] flaps_up_stall_speed=94.00 full_flaps_stall_speed=75.00 cruise_speed=170 max_indicated_speed=400.00 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 11.36, -69.49, 0.84, fx_navredh , light.1 = 3, 11.36, 69.49, 0.84, fx_navgreh , light.2 = 3, -55.10, 0.00, -0.50, fx_navwhih , light.3 = 4, 50.10, -0.10, 2.55, fx_vclighth , light.4 = 4, 50.10, 0.10, 2.55, fx_vclighth , light.5 = 4, 25.00, 0.00, 2.55, fx_vclighth , light.6 = 4, 5.00, 0.00, 2.55, fx_vclighth , light.7 = 4, -10.00, 0.00, 2.55, fx_vclighth , light.8 = 4, -25.00, 0.00, 2.55, fx_vclighth , [keyboard_response] elevator=150.00,250.00 aileron=150.00,250.00 rudder=150.00,250.00 [Views] eyepoint=49.0,-0.8,2.80 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1,0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=800.00 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.00 pitch_takeoff_ga=8.00 max_pitch=10.00 max_pitch_acceleration=1.00 max_pitch_velocity_lo_alt=2.00 max_pitch_velocity_hi_alt=1.50 max_pitch_velocity_lo_alt_breakpoint=20000.00 max_pitch_velocity_hi_alt_breakpoint=28000.00 max_bank=25.00 max_bank_acceleration=1.80 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=0.00 [direction_indicators] direction_indicator.0=1,0 [fuel] Center1=0,0,-6,312,60 LeftMain=-2,-22,0,1502,15 RightMain=-2,22,0,1502,15 fuel_type=1 number_of_tank_selectors=1 electric_pump=1 [brakes] toe_brakes_scale=1.00 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.00 flap_limit_power=0.00 flap_limit_idle=0.00 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=3000.00 [stall_warning] type=0 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [tailhook] tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=1.0 [pitot_static] pitot_heat=1.00 [vacuum_system] max_pressure=5.00 vacuum_type=1 electric_backup_pressure=0.00 engine_map=1,1,0,0 [pneumatic_system] max_pressure=0.00 bleed_air_scalar=1.00 [deice_system] structural_deice_type=0
