[fltsim.0]
title =Piaggio P-166DL3
sim =P-166DL3
model =
panel =
sound =
texture =
panel_alias =
sound_alias =
kb_checklists = CheckList_Piaggio_P-166DL3
kb_reference =
atc_id =I-PJAG
atc_id_color = 0xffffffff
atc_airline =
atc_flight_number =
ui_manufacturer =Piaggio
ui_type =P-166DL-3
ui_variation =Prototype
description=The Piaggio P-166A is a light small twin. An Exotic two-engined prop that sold all over the world including America, UK, and Australia. The P-166DL3 is the actual production version of a plane that firt flew in 1957, now with turboprop engines, new avionics, increased fuel capacity, and completly new hydraulic and electric system. Its origin is traced Back to the Piaggio P-136, a light anphibian, which the P-166 keeps the wings, the engines and the tailplanes. The first P-166A flew in November 1957, and the DL3 is dated 1976. It has newer versions for special roles, like anti-submarine patrols, cargo and similar. The aircraft waits to be repalced by a new version, the P-166DP-1.
atc_parking_types=RAMP,CARGO
atc_parking_codes=
visual_damage=1
atc_heavy=0
prop_anim_ratio=-1.00
[fltsim.1]
title =Piaggio P-166DL3 I-PIAE
sim =P-166DL3
model =
panel =
sound =
texture = ipiae
panel_alias =
sound_alias =
kb_checklists = CheckList_Piaggio_P-166DL3
kb_reference =
atc_id =I-PIAE
atc_id_color = 0xffffffff
atc_airline =
atc_flight_number =
ui_manufacturer =Piaggio
ui_type =P-166DL-3
ui_variation =Demonstrator DL3#2
ddescription=The Piaggio P-166A is a light small twin. An Exotic two-engined prop that sold all over the world including America, UK, and Australia. The P-166DL3 is the actual production version of a plane that firt flew in 1957, now with turboprop engines, new avionics, increased fuel capacity, and completly new hydraulic and electric system. Its origin is traced Back to the Piaggio P-136, a light anphibian, which the P-166 keeps the wings, the engines and the tailplanes. The first P-166A flew in November 1957, and the DL3 is dated 1976. It has newer versions for special roles, like anti-submarine patrols, cargo and similar. The aircraft waits to be repalced by a new version, the P-166DP-1.
atc_parking_types=RAMP,CARGO
atc_parking_codes=
visual_damage=1
atc_heavy=0
prop_anim_ratio=-1.00
description=Piaggio P-166DL3
[fltsim.2]
title =Piaggio P-166DL3 Alitalia
sim =P-166DL3
model =
panel =
sound =
texture = Alitalia
panel_alias =
sound_alias =
kb_checklists = CheckList_Piaggio_P-166DL3
kb_reference =
atc_id =I-PIAE
atc_id_color = 0xffffffff
atc_airline = Alitalia
atc_flight_number = 166
ui_manufacturer =Piaggio
ui_type =P-166DL-3
ui_variation =Alitalia Flying School
description=The Piaggio P-166A is a light small twin. An Exotic two-engined prop that sold all over the world including America, UK, and Australia. The P-166DL3 is the actual production version of a plane that firt flew in 1957, now with turboprop engines, new avionics, increased fuel capacity, and completly new hydraulic and electric system. Its origin is traced Back to the Piaggio P-136, a light anphibian, which the P-166 keeps the wings, the engines and the tailplanes. The first P-166A flew in November 1957, and the DL3 is dated 1976. It has newer versions for special roles, like anti-submarine patrols, cargo and similar. The aircraft waits to be repalced by a new version, the P-166DP-1.
atc_parking_types=RAMP,CARGO
atc_parking_codes=
visual_damage=1
atc_heavy=0
prop_anim_ratio=-1.00
[fltsim.3]
title =Piaggio P-166DL3 I-PIAC
sim =P-166DL3
model =
panel =
sound =
texture = ipiac
panel_alias =
sound_alias =
kb_checklists = CheckList_Piaggio_P-166DL3
kb_reference =
atc_id =I-PIAC
atc_id_color = 0xffffffff
atc_airline =
atc_flight_number =
ui_manufacturer =Piaggio
ui_type =P-166DL-3
ui_variation =Prototype #2
description=The Piaggio P-166A is a light small twin. An Exotic two-engined prop that sold all over the world including America, UK, and Australia. The P-166DL3 is the actual production version of a plane that firt flew in 1957, now with turboprop engines, new avionics, increased fuel capacity, and completly new hydraulic and electric system. Its origin is traced Back to the Piaggio P-136, a light anphibian, which the P-166 keeps the wings, the engines and the tailplanes. The first P-166A flew in November 1957, and the DL3 is dated 1976. It has newer versions for special roles, like anti-submarine patrols, cargo and similar. The aircraft waits to be repalced by a new version, the P-166DP-1.
atc_parking_types=RAMP,CARGO
atc_parking_codes=
visual_damage=1
atc_heavy=0
prop_anim_ratio=-1.00
[fltsim.4]
title =Piaggio P-166DL3 Somalia
sim =P-166DL3
model =
panel =
sound =
texture = somalia
panel_alias =
sound_alias =
kb_checklists = CheckList_Piaggio_P-166DL3
kb_reference =
atc_id =60-SBJ
atc_id_color = 0xffffffff
atc_airline =
atc_flight_number =
ui_manufacturer =Piaggio
ui_type =P-166DL-3
ui_variation =Somaila AF
description=The Piaggio P-166A is a light small twin. An Exotic two-engined prop that sold all over the world including America, UK, and Australia. The P-166DL3 is the actual production version of a plane that firt flew in 1957, now with turboprop engines, new avionics, increased fuel capacity, and completly new hydraulic and electric system. Its origin is traced Back to the Piaggio P-136, a light anphibian, which the P-166 keeps the wings, the engines and the tailplanes. The first P-166A flew in November 1957, and the DL3 is dated 1976. It has newer versions for special roles, like anti-submarine patrols, cargo and similar. The aircraft waits to be repalced by a new version, the P-166DP-1.
atc_parking_types=RAMP,CARGO
atc_parking_codes=
visual_damage=1
atc_heavy=0
prop_anim_ratio=-1.00
[General]
atc_type =PIAGGIO
atc_model =p66p
editable = 1
performance=Weight: 6500 lbs Max 9950 lbs\nEngines:2 Avco Lycoming LTP-101A (570 SHP)\n3.3g Corner speed: 150 Kts\nMax speed @ SL: 225 Kts\nMax speed: 220 Kts @ 10000 ft\nClimb rate: 2400 ft\/min @ 200 Kts\nFlight Model By: Mario Noriega\nPlane built with Aircraft Designer 2002, www.actpub.com\nFlight Model Workbook V2.82.105
[pitot_static]
vertical_speed_time_constant = 2
[WEIGHT_AND_BALANCE]
max_gross_weight = 9920
empty_weight = 6320
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.8, 0, 0
CG_forward_limit = 0
CG_aft_limit = 1
max_number_of_stations = 7
station_load.0 = "100, 4.4, -0.88, 1, Pilot"
station_load.1 = "100, 4.4, 0.88, 1, Co-pilot"
station_load.2 = "100, 2.32, 0.72, 0, Passenger 1
station_load.3 = "100, 0.87, 0.72, 0, Paseenger 2"
station_load.4 = "100, -0.58, 0.72, 0, Passenger 3"
station_load.5 = "100, 2.32, -0.72, 0, Passenger 4
station_load.6 = "50, 0, 0, 0, Cargo Load"
empty_weight_pitch_MOI = 22078
empty_weight_roll_MOI = 19967
empty_weight_yaw_MOI = 25412
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
[folding_wings]
wing_fold_system_type = 0
fold_rates = 0, 0
[TailHook]
tailhook_length = 0
tailhook_position = 0, 0, 0
cable_force_adjust = 1
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//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)
[contact_points]
max_number_of_points = 15
point.0 = 1, 9.53, 0, -4.05, 1181.1, 0, 0.571217, 33.66, 0.727981, 2.5, 1.082096, 4, 5, 0, 176, 220
point.1 = 1, -2.65, -4.35, -4.05, 1574.8, 1, 0.571217, 0, 0.873911, 2.5, 0.948861, 5.5, 6, 2, 176, 220
point.2 = 1, -2.65, 4.35, -4.05, 1574.8, 2, 0.571217, 0, 0.873911, 2.5, 0.948861, 6, 6.5, 3, 176, 220
point.3 = 2, -3, -22.9, 4.5, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5 //left wing front
point.4 = 2, -3, 22.9, 4.5, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 6 //right wing front
point.5 = 2, -11.8, -22.9, 4.5, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5 //left wing rear
point.6 = 2, -11.8, 22.9, 4.5, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 6 //right wing rear
point.7 = 2, -22.8, 0, 1.7, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9 //tail lower
point.8 = 2, -25.7, 0, 3.5, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9 //tail rear
point.9 = 2, -24.7, 0, 13.5, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9 //vertical fin
point.10 = 2, 0.8, 0, 4.6, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4 //fuselage top
point.11 = 2, 0.8, 0, -2, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4 //fuselage Belly
point.12 = 2, 12.8, 0, 0, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4 //nose
point.13 = 2, -21.9, 8.5, 5.2, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 8 //right Hstab
point.14 = 2, -21.9, -8.5, 5.2, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 7 //left Hstab
static_pitch= 2.8
static_cg_height= 3.0
gear_system_type=1
[Views]
eyepoint= 4.325, -0.91, 2.15
[flaps.0] //Trailing Edge Flaps
type = 1
span-outboard = 0.5
extending-time = 5
flaps-position.0 = 0
flaps-position.1 = 11, 165
flaps-position.2 = 22, 160
flaps-position.3 = 33, 155
flaps-position.4 = 45, 150
damaging-speed = 170
blowout-speed = 180
system_type = 1
lift_scalar = 1
drag_scalar = 1.5
pitch_scalar = 1.5
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 160
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
starter3 = 0, 20, 17
starter4 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
prop_sync = 0, 15, 17
auto_feather = 0, 15, 17
auto_brakes = 0, 15, 17
standby_vacuum = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
[LIGHTS]
light.0 = 3, -0.612, -22.168, 4.53, fx_navred
light.1 = 3, -0.612, 22.168, 4.53, fx_navgre
light.2 = 2, -22.8, 0, 13.36, fx_strobe
light.3 = 1, -25.25, 0, 3.518, fx_beacon
light.4 = 4, 5.05, 0, 2.4, fx_vclight
light.5 = 4, 1.4, 0, 1.9, fx_vclight
[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_tchdwn_s, 1
[autopilot]
autopilot_available = 1
flight_director_available = 0
default_vertical_speed = 1000
autothrottle_available = 0
autothrottle_arming_required = 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga = 1
pitch_takeoff_ga = 8
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
[fuel]
Center1 = -5, 0, -0.5, 112, 0
LeftMain = -6.2, -10.7, 4.1, 56.5, 0
RightMain = -6.2, 10.7, 4.1, 56.5, 0
LeftAux = -7.2, -22.1, 4.4, 88.2, 0
RightAux = -7.2, 22.1, 4.4, 88.2, 0
fuel_type = 2
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 572
wing_span = 48.25
wing_root_chord = 11.8549222797927
wing_dihedral = 4
wing_incidence = 1
wing_twist = -2
oswald_efficiency_factor = 0.897197885440908
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2.96373056994819
wing_pos_apex_vert = 0
htail_area = 135
htail_span = 16.73
htail_pos_lon = -31.79
htail_pos_vert = 0
htail_incidence = 0
htail_sweep = 0
vtail_area = 31
vtail_span = 7.02
vtail_sweep = 0
vtail_pos_lon = -31.39
vtail_pos_vert = 0
elevator_area = 22.8
aileron_area = 10.49
rudder_area = 10.55
elevator_up_limit = 26
elevator_down_limit = 16
aileron_up_limit = 25
aileron_down_limit = 15
rudder_limit = 27
elevator_trim_limit = 18
spoiler_limit = 0
spoilerons_available = 0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
[Reference Speeds]
flaps_up_stall_speed = 65.2
full_flaps_stall_speed = 56.5
cruise_speed = 200
max_indicated_speed=360.796875
max_mach=0.538770
[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
[brakes]
toe_brakes_scale=0.640889
parking_brake=1
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=6.930556
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1,1
[turn_indicators]
turn_indicator.0=1,1
\\please don't edit: this turboprop settings drove me NUTS!!!!!
[GeneralEngineData]
engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -9.8, -5.88, 2.5
Engine.1 = -9.8, 5.88, 2.5
fuel_flow_scalar = 0.54 //Scalar for fuel flow efficiency
min_throttle_limit = -0.01 //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature=-27
[propeller]
thrust_scalar = 2.08 //Propeller thrust scalar
propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter = 8.8 //Propeller Diameter, (feet)
propeller_blades = 4 //Number of propeller blades
propeller_moi = 24 //Propeller moment of inertia
beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min = 15.2 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm = 10520 //Miminum governed RPM
prop_tc = 0.004 //Prop time-constant
gear_reduction_ratio = 17.6 //Propeller gear reduction ratio
fixed_pitch_beta = 0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit = 80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available = 1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available = 1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather = 700 //Minimum RPM for prop feathering
beta_feather = 79.3 //Feathering pitch angle (degrees)
power_absorbed_cf = 0.9 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available = 1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta = 1.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta = -1.0 //Minimum pitch angle in reverse, (degrees)
[TurbineEngineData]
fuel_flow_gain = 0.011 //Gain on fuel flow
inlet_area = 1.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 158 //Lbs, max rated static thrust at Sea Level
[turboprop_engine]
power_scalar = 1.00 //Scalar on Turboprop power
maximum_torque = 3270 //Maximum torque available (ft-lbs)