[fltsim.0]
title=P50_II
sim=P50_II
model=
panel=
sound=
texture=
kb_checklists=

ui_manufacturer=Piaggio
ui_type= P50
ui_variation= II-MM370
atc_heavy=0
atc_id= 
atc_airline= 
atc_flight_number= 
description=Notes:Prototype with 4 radial engines in traditional position\nfirst flight in 1938\nFather of the more famouse Piaggio P108B\nfor description see file 

[General]
performance=Length: 64.11 ft\nSpan: 84.71 ft\nWeight: empty 29,040 lbs \nPower: 4 x Piaggio P XI RC40-1,000 hp each\nAverage climb rate to 13,100 ft in 15 min\nMax speed 279 mph.
atc_type= 
atc_model= 
editable=1  




[WEIGHT_AND_BALANCE]
reference_datum_position=0.000,  0.000, -0.200
empty_weight_CG_position=0.000,  0.000, -0.200

max_number_of_stations=50
station_load.0=   0.000000,0.000000,0.000000,0.000000 ; upkeep weapon use 10000 lbs
/station_load.1=   0.000000,0.000000,0.000000,0.000000 ; 

empty_weight_roll_MOI=388864.000
empty_weight_pitch_MOI=448839.000
empty_weight_yaw_MOI=629754.000
empty_weight_coupled_MOI=400.000

empty_weight=39000.000

max_gross_weight=65000.000

CG_forward_limit=0.000
CG_aft_limit=1.000


[tailhook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=1.0



[folding_wings]
wing_fold_system_type =1                     ;0=None
fold_rates = 0.12,0.11    


[flight_tuning]
cruise_lift_scalar=1.50
parasite_drag_scalar=3.00
induced_drag_scalar=3.00
elevator_effectiveness=1.000
aileron_effectiveness=1.250
rudder_effectiveness=1.000
pitch_stability=1.700
roll_stability=1.000
yaw_stability=1.100
elevator_trim_effectiveness=1.750
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000




[Reference Speeds] ;TAS
flaps_up_stall_speed=95.000
full_flaps_stall_speed=76.000
cruise_speed=138.00 ; Heavily loaded
cruise_speed=150.00 ; lightly loaded
max_indicated_speed=274.765625




[GeneralEngineData]
engine_type=0
Engine.0=14.167, -24.583, 0.000
Engine.1=15.833, -11.833, 0.000
Engine.2=15.833, 11.833, 0.000
Engine.3=14.167, 24.583, 0.000
fuel_flow_scalar=1.288
min_throttle_limit=0.000000




[piston_engine]
cylinder_displacement=137.400000
compression_ratio=6.000000
number_of_cylinders=12
max_rated_rpm=3000.000000
turbocharged=1
min_design_mp=1.000000

emergency_boost_type=1
emergency_boost_mp_offset=1.000000
emergency_boost_gain_offset=1.000000

fuel_metering_type=0
cooling_type=1
normalized_starter_torque=12.0350000
fuel_air_auto_mixture=1
auto_ignition=0

max_rpm_friction_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.00000
idle_rpm_friction_scalar=1.000000

//==================================



max_rated_hp=1460.000
power_scalar=0.562
max_design_mp=52.5000000  ;58.4-5.9 lost due to altitude
critical_altitude=6000 ; M Gear 
max_rpm_mechanical_efficiency_scalar=1.1372





[fuel]

RightMain= 0.000000,0.000000,0.000000,1392.000000,0.000000  ;#1




LeftMain=  0.000000,0.000000,0.000000,920.000000,0.000000  ;DB #2

fuel_type=1.000
number_of_tank_selectors=1
electric_pump=0




[airplane_geometry]
wing_area=1301.000
wing_span=102.000
wing_root_chord=12.750
wing_dihedral=4.999
wing_incidence=0.000
wing_twist=0.500
oswald_efficiency_factor=5.007
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=0.000
wing_pos_apex_vert=0.000
htail_area=237.000
htail_span=45.000
htail_pos_lon=-41.667
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=0.000
vtail_area=248.000
vtail_span=17.956
vtail_sweep=0.000
vtail_pos_lon=-42.333
vtail_pos_vert=1.500
elevator_area=101.910
aileron_area=130.100
rudder_area=86.800
elevator_up_limit=27.502
elevator_down_limit=20.626
aileron_up_limit=19.481
aileron_down_limit=14.897
rudder_limit=23.491
elevator_trim_limit=19.481
spoiler_limit=59.989
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000




[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                (0=Undamped, 1=Critically                                               Damped)
//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)

point.0=1.000, -35.917, 0.000, -5.333, 1574.803, 0.000, 0.862, 55.860, 0.340, 2.500, 0.708, 15.000, 10.000, 0.000, 0.000, 0.000
point.1=1.000, 5.917, -11.917, -10.333, 1574.803, 1.000, 0.862, 0.000, 0.453, 2.500, 0.708, 15.000, 10.000, 2.000, 0.000, 0.000
point.2=1.000, 5.917, 11.917, -10.333, 1574.803, 2.000, 0.862, 0.000, 0.453, 2.500, 0.708, 15.000, 10.000, 3.000, 0.000, 0.000

point.3=2.000, -2.833, -50.583, 3.583, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4=2.000, -2.833, 50.583, 3.583, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5=2.000, -35.917, 0.000, -4.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6=2.000, 23.833, 0.000, -2.083, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch=6.800
static_cg_height= 9.3000

static_pitch=6.900
static_cg_height= 9.5000

gear_system_type=0





[propeller]
propeller_type=0
propeller_diameter=10.333
propeller_blades=3

thrust_scalar=2.100
propeller_moi=28.963
beta_max=49.000
beta_min=15.000
min_gov_rpm=600.000
prop_tc=0.100
gear_reduction_ratio=1.300
fixed_pitch_beta=20.000
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=0.000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000
minimum_reverse_beta=0.000





[electrical]
electric_always_available=1
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0





[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
// x, z, y 

light.0=4,22.46,-0.50,-1.30, fx_vclight_s403.fx






[keyboard_response]
elevator=150.000, 250.000
aileron=150.000, 250.000
rudder=150.000, 250.000




[Views]
//eyepoint=22.46,-1.10,-1.30
eyepoint=22.46,-0.50,-1.30





[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=500.000
autothrottle_available=0
pitch_takeoff_ga=8.000
use_no_default_bank=1
default_bank_mode=0
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




[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=0
Com.1=1, 0
Com.2=0, 0
Nav.1=1, 0, 1
Nav.2=0, 0, 1 ; with glide slope, not activated for PD Lancaster
Adf.1=1
Adf.2=0
Transponder.1=1
Marker.1=1 




[Flaps.0] 
type=1
span-outboard=0.500
extending-time=8.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=0.900
drag_scalar=1.000

flaps-position.0 = 0
flaps-position.1 =  8, 200
flaps-position.2 = 20, 200
flaps-position.3 = 30, 180
flaps-position.4 = 42, 150






[direction_indicators]
direction_indicator.0=1,0





[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=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000




[brakes]
toe_brakes_scale=1.0000
parking_brake=1




[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000




[hydraulic_system]
normal_pressure=0.000000




[stall_warning]
type=1




[attitude_indicators]
attitude_indicator.0=1




[turn_indicators]
turn_indicator.0=1,0