[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\[email protected]\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