[fltsim.0] title =Piaggio PD-808 RM 1 sim = PD808 model = panel = sound = texture = RM panel_alias = sound_alias = kb_checklists =../PD808_shared/Documents/PD808_check kb_reference =../PD808_shared/Documents/PD808_Ref atc_id = MM62015 atc_id_color = atc_parking_types = atc_parking_code = atc_airline= atc_flight_number= ui_manufacturer = Piaggio ui_type = PD-808 ui_variation = RM - Early description =PD-808 Radio Misiure: Navaid Calibrator Version.\nMM62015 Early RM Livery\nInitially a joint venture beween Douglas and Piaggio, and later only manufatured by Piaggio as Douglas withdrew from the project after the merger with McDonnell. Piaggio continued with the project, but the subsequent delays gave time for the Learjet 23 and the HS-125 to enter the market. This left Piaggio with an aircraft with very little commercial interest. In fact only 2 civilian PD-808s were manufactured. One served as private jet for Piaggio itself, the other crashed due to bad weather while demostrating to it's only civilian buyer. The italian air force ordered 25 examples anyway, therefore saving Piaggio from bankruptcy. They were used as trainers, VIP transports, Navaid calibrators and ECM platforms. All the 25 units are now disbanded as have reached the maximum flying hours. The last PD-808 flew on May 17, 2003 after more than 25 years of valuable service. visual_damage = 0 [fltsim.1] title =Piaggio PD-808 RM 2 sim = PD808 model = panel = sound = texture = RM2 panel_alias = sound_alias = kb_checklists =../PD808_shared/Documents/PD808_check kb_reference =../PD808_shared/Documents/PD808_Ref atc_id = MM62015 atc_id_color = atc_parking_types = atc_parking_code = atc_airline= atc_flight_number= ui_manufacturer = Piaggio ui_type = PD-808 ui_variation = RM - Late description =PD-808 Radio Misiure: Navaid Calibrator Version.\nMM62015 Late RM Livery\nInitially a joint venture beween Douglas and Piaggio, and later only manufatured by Piaggio as Douglas withdrew from the project after the merger with McDonnell. Piaggio continued with the project, but the subsequent delays gave time for the Learjet 23 and the HS-125 to enter the market. This left Piaggio with an aircraft with very little commercial interest. In fact only 2 civilian PD-808s were manufactured. One served as private jet for Piaggio itself, the other crashed due to bad weather while demostrating to it's only civilian buyer. The italian air force ordered 25 examples anyway, therefore saving Piaggio from bankruptcy. They were used as trainers, VIP transports, Navaid calibrators and ECM platforms. All the 25 units are now disbanded as have reached the maximum flying hours. The last PD-808 flew on May 17, 2003 after more than 25 years of valuable service. visual_damage = 0 [fltsim.2] title =Piaggio PD-808 RM Batman sim = PD808 model = panel = sound = texture = RM_Batman panel_alias = sound_alias = kb_checklists =../PD808_shared/Documents/PD808_check kb_reference =../PD808_shared/Documents/PD808_Ref atc_id = MM62016 atc_id_color = atc_parking_types = atc_parking_code = atc_airline= atc_flight_number= ui_manufacturer = Piaggio ui_type = PD-808 ui_variation = RM - Special livery "Batman" description =PD-808 Radio Misiure: Navaid Calibrator Version.\nMM62016 RM "Batman" Special Livery\nInitially a joint venture beween Douglas and Piaggio, and later only manufatured by Piaggio as Douglas withdrew from the project after the merger with McDonnell. Piaggio continued with the project, but the subsequent delays gave time for the Learjet 23 and the HS-125 to enter the market. This left Piaggio with an aircraft with very little commercial interest. In fact only 2 civilian PD-808s were manufactured. One served as private jet for Piaggio itself, the other crashed due to bad weather while demostrating to it's only civilian buyer. The italian air force ordered 25 examples anyway, therefore saving Piaggio from bankruptcy. They were used as trainers, VIP transports, Navaid calibrators and ECM platforms. All the 25 units are now disbanded as have reached the maximum flying hours. The last PD-808 flew on May 17, 2003 after more than 25 years of valuable service. visual_damage = 0 [General] atc_type = Piaggio atc_model = P808 performance =Mario noriega Designs\nwww.mariopilot.6x.to\nmario@norcex.com\nRead Notes before flying!\nEmpty Weight: 10648 lbs\nMax T\O Weight: 18001 lbs\nPower:2x 3330 lbs thrust Bristol Siddeley (Piaggio) Viper MK.526 Turbojets\n Maximum load factor: 5.0 g\nMax speed at sea-level: 350 KIAS\nFull flaps Stall speed: 90 KIAS\nInit. Climb rate: 5415 ft/min\nFlight Dynamics By: Mario Noriega Designs based on Flight Dynamics Workbook V2005.12 by Jerry Beckwith editable = 1 prop_anim_ratio = 1 [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 18001 empty_weight = 10648 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 11 station_load.0 = "101, 12.1, -1.51, 2.7, Pilot" station_load.1 = "102, 12.1, 1.51, 2.7, Co-Pilot" station_load.2 = "107, 0.2, -1.51, 2.7, Operator 1" station_load.3 = "105, 0.2, 1.51, 2.7, Operator 2" station_load.4 = "112, 3.31, -1.51, 2.7, Passenger 1" station_load.5 = "112, 3.31, 1.51, 2.7, Passenger 2" station_load.6 = "111, 6, 1.51, 2.7, Passenger 3" station_load.7 = "75, -11, 0, 1.0, Cargo Load" empty_weight_pitch_MOI = 22707 empty_weight_roll_MOI = 7997 empty_weight_yaw_MOI = 16828 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 hi_alpha_on_roll = 1 hi_alpha_on_yaw = 1 p_factor_on_yaw = 1 torque_on_roll = 1 gyro_precession_on_roll = 1 gyro_precession_on_yaw = 1 [GeneralEngineData] engine_type = 1 Engine.0 = -9.87, -3.55, 0 Engine.1 = -9.87, 3.55, 0 fuel_flow_scalar =2.057 min_throttle_limit = -0.25 [TurbineEngineData] fuel_flow_gain=0.012500 inlet_area=4.2895 rated_N2_rpm=13760.000000 static_thrust=3330.000000 afterburner_available=1 reverser_available=6.0 [jet_engine] thrust_scalar = 1 [folding_wings] wing_fold_system_type = 0 fold_rates = 0.12, 0.11 [TailHook] tailhook_length = 0 tailhook_position = -15, 0, -1 cable_force_adjust = 1 [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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal //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) max_number_of_points = 19 point.0 = 1, 12.19, 0.0, -3.68, 650, 0, 0.52, 40, 0.18, 2.1, 0.85, 5.0, 5.2, 0, 200, 223 point.1 = 1, -0.875, -6.1, -4.57, 950, 1, 0.9, 0, 1.1, 2.0, 0.95, 5.3, 5.4, 2, 200, 223 point.2 = 1, -0.875, 6.1, -4.57, 950, 2, 0.9, 0, 1.1, 2.0, 0.95, 5.2, 5.5, 3, 200, 223 //gear point.3 = 2, -7.61, -20.4, -0.29, 787, 0, 0, 0, 0, 0, 0, 0, 0, 5 //L wing tank front point.4 = 2, -7.05, -21.4, -0.29, 787, 0, 0, 0, 0, 0, 0, 0, 0, 5 //L wing tank back point.5 = 2, 7.61, 20.4, -0.29, 787, 0, 0, 0, 0, 0, 0, 0, 0, 6 //R wing tank front point.6 = 2, 7.05, 21.4, -0.29, 787, 0, 0, 0, 0, 0, 0, 0, 0, 6 //R wing tank back point.7 = 2, 21, 0, 1.37, 787, 0, 0, 0, 0, 0, 0, 0, 0, 8 //nose point.8 = 2, 14.6, 0, -0.2, 1550, 0, 0, 0, 0, 0, 0, 0, 0, 8 //front fuselage scrape point.9 = 2, -9.9, 0, 0.03, 1550, 0, 0, 0, 0, 0, 0, 0, 0, 9 //tail scrape point.10 = 2, -21, 0, 2.1, 1550, 0, 0, 0, 0, 0, 0, 0, 0, 8 //tail extreme point.11 = 2, -18.4, 0, 11.31, 787, 0, 0, 0, 0, 0, 0, 0, 0, 8 //vertical empennage point.12 = 2, -19, -8.9, 5.34, 787, 0, 0, 0, 0, 0, 0, 0, 0, 7 //L horizontal empennage point.13 = 2, -19, 8.9, 5.34, 787, 0, 0, 0, 0, 0, 0, 0, 0, 7 //R horizontal empennage point.14 = 2, -0.95, -5.47, -0.95, 1550, 0, 0, 0, 0, 0, 0, 0, 0, 4 // gear blisters (fuselage scrape) point.15 = 2, -0.95, 5.47, -0.95, 1550, 0, 0, 0, 0, 0, 0, 0, 0, 4 //R gear blister static_pitch= 0 static_cg_height= 4.02 gear_system_type = 1 [Views] eyepoint= 11.61, -1.4927, 3.643 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 20, 220 flaps-position.2 = 40, 185 damaging-speed = 225 blowout-speed = 245 system_type = 1 lift_scalar = 1 drag_scalar = 1 pitch_scalar = 1 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 300 electric_always_available = 0 flap_motor = 0, 25, 17 gear_motor = 0, 25, 17 autopilot = 1, 15, 17 avionics_bus = 0, 45, 17 avionics = 1, 25, 17 pitot_heat = 0, 0, 0 additional_system = 0, 75, 17 marker_beacon = 1, 10, 17 gear_warning = 0, 10, 17 fuel_pump = 0, 25, 17 starter1 = 0, 115, 17 starter2 = 0, 115, 17 light_nav = 0, 25, 17 light_beacon = 0, 25, 17 light_landing = 0, 25, 17 light_taxi = 0, 10, 17 light_strobe = 0, 10, 17 light_panel = 0, 5, 17 light_recognition = 0, 10, 17 light_wing = 0, 25, 17 light_logo = 0, 10, 17 light_cabin = 0, 10, 17 auto_brakes = 0, 85, 17 standby_vacuum = 0, 85, 17 hydraulic_pump = 0, 7, 17 fuel_transfer_pump = 0, 25, 17 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=Landing, 6=Taxi,7=Recog ,8=Wing, 9=Logo, 10=Cabin light.0 = 3, 7.217, -20.3084, 0.81, fx_PD808_Navred //NAV light.1 = 3, 7.217, 20.3084, 0.81, fx_PD808_navgre //NAV light.2 = 1, -7.85, 0, -0.177, fx_PD808_beacon //BCN light.3 = 1, -18.307, 0, 11.361, fx_PD808_beacon //BCN light.4 = 7, 12.303, 0, 3.93, fx_PD808_whitecockpit //Cockpit (white) light.5 = 9, 12.303, 0, 3.93, fx_PD808_redcockpit //Cockpit (RED) light.6 = 2, 12.303, 0, 3.93, fx_PD808_thunderlight //Cockpit (thunderstorm) light.7 = 10, 1.28, 0, 3.28, fx_PD808_cabinlight //cabin light (1) light.8 = 10, 5.28, 0, 3.28, fx_PD808_Cabinlight //cabin light (2) light.9 = 8, 8.43, 1.348, 0.045, fx_PD808_winsp //wing inspection light.10 = 8, 8.43, -1.348, 0.045, fx_PD808_winsp //wing inspection light.11 = 8, 5.43, 10.348, 0.545, fx_PD808_winsp_LE //wing inspection (LE lighting) light.12 = 8, 5.43, -10.348, 0.545, fx_PD808_winsp_LE //wing inspection (LE Lighting) light.13 = 4, 0, 0, 0, fx_PD808_panel_light //panel (Electrical_placeholder) light.14 = 5, 7.509, 19.875, 0.81, fx_PD808_LL //landing light light.15 = 5, 7.509, -19.875, 0.81, fx_PD808_LL //landing light light.16 = 6, 1.886, -5.426, -0.246, fx_PD808_TL //taxi light [Radios] // 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 [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_PD808_tchdn, 1 startup=fx_PD808_startup [autopilot] autopilot_available = 1 use_no_default_bank = 0 use_no_default_pitch = 0 flight_director_available = 0 default_vertical_speed = 0 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_takeoff_ga = 0 autothrottle_max_rpm = 90 pitch_takeoff_ga = 8 default_pitch_mode = 1 default_bank_mode = 1 max_pitch = 10 max_pitch_acceleration = 5.5 max_pitch_velocity_lo_alt = 3.0 max_pitch_velocity_hi_alt = 2.5 max_pitch_velocity_lo_alt_breakpoint = 20000 max_pitch_velocity_hi_alt_breakpoint = 28000 max_bank= 25 max_bank_acceleration = 2 max_bank_velocity = 5 max_throttle_rate = 0.1 nav_proportional_control = 11.0 nav_integrator_control = 0.20 nav_derivative_control = 0.1 nav_integrator_boundary = 2.5 nav_derivative_boundary = 0.2 gs_proportional_control = 15.0 gs_integrator_control = 0.35 gs_derivative_control = 0.10 gs_integrator_boundary = 0.7 gs_derivative_boundary = 0.2 yaw_damper_gain = 1.0 [fuel] LeftMain = 0.78, -12.1, 0.42, 248, 0 RightMain = 0.78, 12.1, 0.42, 248, 0 LeftAux = 0, -20, 0.75, 237, 0 RightAux = 0, 20, 0.75, 237, 0 fuel_type = 2 number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 224.97 wing_span = 37.75 wing_root_chord = 5.9594701986755 wing_dihedral = 3 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.891839831461859 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 1.28986754966887 wing_pos_apex_vert = 1 htail_area = 31.7 htail_span = 17.7 htail_pos_lon = -19.5 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 26.1 vtail_span = 8 vtail_sweep = 0 vtail_pos_lon = -19.24 vtail_pos_vert = 0 elevator_area = 25.04 aileron_area = 24.097 rudder_area = 16.84 elevator_up_limit = 20 elevator_down_limit = 10 aileron_up_limit = 16 aileron_down_limit = 16 rudder_limit = 27 elevator_trim_limit = 22 spoiler_limit = 60 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 101.7 full_flaps_stall_speed = 90.4 cruise_speed = 339 max_indicated_speed = 350 max_mach = 0.75 [forcefeedback] gear_bump_nose_magnitude = 6000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 6000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 6000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 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 = 75000 crash_duration2 = 2500000 stick_shaker_magnitude = 5000 stick_shaker_direction = 0 stick_shaker_period = 111111 [gear_warning_system] gear_warning_available = 1 pct_throttle_limit = 0.1 flap_limit_idle = 50 flap_limit_power = 50 [brakes] toe_brakes_scale = 0.640888698995941 parking_brake = 1 [stall_warning] // 0 = None, 1 = Suction, 2 = Electric. type = 1 [hydraulic_system] electric_pumps = 0 engine_map = 1, 1, 0, 0 normal_pressure = 3000 [attitude_indicators] // 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] // 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0 = 1, 0 [direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind direction_indicator.0 = 1, 0 [airspeed_indicators] airspeed_indicator.0 = 1, 0 [smokesystem] smoke.0 = 3.5, -9.87, 3.55, fx_PD808_engsmoke smoke.1 = 3.5, -9.87, -3.55, fx_PD808_engsmoke