[fltsim.0]
title=Piper Malibu Mirage
sim=PA46-350p_2k4
model=
panel=
sound=
texture=
kb_checklists=pipmir_Check
kb_reference=pipmir_ref
atc_id=N3308S
ui_manufacturer=Piper
ui_type=Mirage
ui_variation=Blue/White
description=Piper Malibu Mirage PA46-350P, Lycoming TIO-540-AE2A turbocharged, pressurized

[General]
atc_type=Piper
atc_model=Mirage
editable=1
performance=High Speed Cruise:  213 kt\nCeiling:  25,000 ft\nDesigner:  Chuck Dome\nDate:  May 2003\nVisual Model and FDE Modified by John Cillis: July 2003

[WEIGHT_AND_BALANCE]
max_gross_weight=3368                         // (pounds)
empty_weight=2189                             // (pounds)

reference_datum_position=3.9, 0, 0       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-3.7, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=170, -3.1, -1.5, 0.0           //Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170, -3.1,  1.5, 0.0           //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI=12706
empty_weight_roll_MOI=12131
empty_weight_yaw_MOI=13932
empty_weight_coupled_MOI=0.0

[pitot_static]
vertical_speed_time_constant=1.0              //Increasing this value will cause a more instantaneous reaction in the VSI

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.5
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=4.0
rudder_effectiveness=1.0
pitch_stability=3.0
roll_stability=3.0
yaw_stability=3.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[GeneralEngineData]
engine_type=0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=2.1, 0.0, 0.0                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=0.45                          //Fuel flow scalar
min_throttle_limit=0.000000

[piston_engine]
power_scalar=1.0                              //Piston power scalar
cylinder_displacement=175.0                     //Cubic inches per cylinder
compression_ratio=8.0                          //Compression ratio
number_of_cylinders=6                           //Number of cylinders
max_rated_rpm=2575                             //Max rated RPM
max_rated_hp=350                               //Max rated HP
fuel_metering_type=0                           //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type=0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3                  //Starter torque factor
turbocharged=1                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=38                               //Max design manifold pressure, (inHg)
min_design_mp=1                                //Min design manifold pressure, (inHg)
critical_altitude=18000                        //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.0                   //Scalar on idle RPM friction

[propeller]
thrust_scalar=1.0                             //Propeller thrust scalar
propeller_type=0                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=7.55                         //Propeller Diameter, (feet)
propeller_blades=3                             //Number of propeller blades
propeller_moi=8.0                              //Propeller moment of inertia
beta_max=55                                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=12.5                                    //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1400                               //Miminum governed RPM
prop_tc=0.1                                    //Prop time-constant
gear_reduction_ratio=1.0                       //Propeller gear reduction ratio
fixed_pitch_beta=20                             //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=0                          //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=0                          //Minimum RPM for prop feathering
beta_feather=0                                 //Feathering pitch angle (degrees)
power_absorbed_cf=0                            //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available=0                       //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=0                       //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0                         //Minimum pitch angle in reverse, (degrees)

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
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



//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


[contact_points]
point.0=1,   1.18,   0.0, -3.80, 1181.1, 0, 0.523, 33.66, 0.170, 2.5, 0.794, 4.0, 4.0, 0, 0.0, 0.0
point.1=1,  -5.48,  -4.5, -3.40, 1574.8, 1, 0.523,  0.00, 0.286, 2.5, 0.808, 4.0, 4.0, 2, 0.0, 0.0
point.2=1,  -5.48,   4.5, -3.40, 1574.8, 2, 0.523,  0.00, 0.286, 2.5, 0.808, 4.0, 4.0, 3, 0.0, 0.0
point.3=2,  -3.90, -18.0, -0.67, 1574.8, 0, 0.000,  0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2,  -3.90   18.0, -0.67, 1574.8, 0, 0.000,  0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -20.23,   0.0,  0.83, 1574.8, 0, 0.000,  0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2,  -1.48,   0.0, -2.17, 1574.8, 0, 0.000,  0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 4, 0.0, 0.0
point.7=2, -20.23,   0.0,  6.83, 1574.8, 0, 0.000,  0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 7, 0.0, 0.0
point.8=2,  -4.90,   0.0, -1.83, 1574.8, 0, 0.000,  0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 8, 0.0, 0.0

max_number_of_points=21

static_pitch=0
static_cg_height=3.54
gear_system_type=0



[Views]
eyepoint=-0.3, -1.25, 2.2    //long,lat,vert

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3,  -0.90, -21.60,  0.32, fx_navred ,
light.1=3,  -0.90,  21.60,  0.32, fx_navgre ,
light.2=2,  -1.10, -21.60,  0.32, fx_strobe ,
light.3=2,  -1.10,  21.60,  0.32, fx_strobe ,
light.4=2, -16.80,   0.00,  7.70, fx_beacon ,

[flaps.0]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.5                                  // 0.0 .. 1.0
extending-time=5                                    // seconds
flaps-position.0=0                                    // degrees, KIAS
flaps-position.1=12                                   // degrees, KIAS
flaps-position.2=24                                   // degrees, KIAS
flaps-position.3=36                                   // degrees, KIAS
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=1.0                                       
drag_scalar=1.0
pitch_scalar=1.0
system_type=0                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
elevator=100,  180
aileron=200, 1000
rudder=200, 1000

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type=4
direction_indicator.0=1,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[fuel]
LeftMain=-4.1, -7.9, -0.8, 47.5, 3.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-4.1,  7.9, -0.8, 47.5, 3.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=1                                 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1                    
electric_pump=1

[airplane_geometry]
wing_area=175.0                 //Square feet
wing_span=36.1                  //Feet
wing_root_chord=5.1                   //Feet
wing_dihedral=5.5                   //Degrees
wing_incidence=2.5                   //Degrees
wing_twist=-1.5                  //Degrees
oswald_efficiency_factor=0.6                   //Measure of lift effeciency of wing
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=5.0                   //Degrees, wing leading edge
wing_pos_apex_lon=-2.6                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0                   //Feet, vertical distance from reference point, positive going up
htail_area=34.0                  //Square feet
htail_span=11.8                  //Feet
htail_pos_lon=-18.6                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence=1.0                   //Degrees
htail_sweep=0.0                   //Degrees, horizontal tail leading edge
vtail_area=10.0                  //Square feet
vtail_span=3.6                   //Feet, tip to body
vtail_sweep=0.0                   //Degrees, vertical tail leading edge
vtail_pos_lon=-16.5                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=1.5                   //Feet, vertical distance from reference point, positive going up
elevator_area=16.6                  //Square feet
aileron_area=18.3                  //Square feet
rudder_area=6.7                   //Square feet
elevator_up_limit=28.0                  //Degrees
elevator_down_limit=21.0                  //Degrees
aileron_up_limit=20.0                  //Degrees
aileron_down_limit=15.0                  //Degrees
rudder_limit=24.0                  //Degrees
elevator_trim_limit=19.5                  //Degrees
spoiler_limit=90.0                  //Degrees
spoilerons_available=0                     //Spoilerons Available?
aileron_to_spoileron_gain=0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons=0                 //Degrees
min_flaps_for_spoilerons=0                    //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed=66.0                  //Knots True (KTAS)
full_flaps_stall_speed=52.8                  //Knots True (KTAS)
cruise_speed=195.0                 //Knots True (KTAS)
max_indicated_speed=2010.000000

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=700.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
use_no_default_pitch=1
use_no_default_bank=1
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
default_pitch_mode=0
default_bank_mode=0


[forcefeedback]
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds

[brakes]
toe_brakes_scale=1.000000
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=15.996982
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