[fltsim.0]
title=PAJERO IO
sim=Pajero
model=pajero
panel=""
sound=""
texture=
kb_checklists=Wright_Flyer_check
kb_reference=Wright_Flyer_ref
atc_id=N9FLY
atc_id_color=0xffffffff
ui_manufacturer=MITSUBISHI MOTORS
ui_type=PAJERO IO
ui_variation=
description=


[General]
atc_type=Wright Flyer
atc_model=""
editable=0
performance=\n

[WEIGHT_AND_BALANCE]
max_gross_weight=6000                         // (pounds)
empty_weight=2500                             // (pounds)

reference_datum_position=3.6, 0, 0       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-3.0, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0="170, -3.0, -1.5, -2.0, "                    // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1="170, -3.0,  1.5, -2.0, "          // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2="0, -3.2, -1.5, -2.0, "           // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3="0, -6.2,  1.5, -2.0, "           // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4="0, -8.0,  0.0, -2.0, "                  // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI=8400.0
empty_weight_roll_MOI=1137.0
empty_weight_yaw_MOI=2000.0
empty_weight_coupled_MOI=0.0


[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.6
yaw_stability=1.0
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=-10.0, 0.0, -3.0                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=0.88                          //Fuel flow scalar
min_throttle_limit=0.0                        //Minimum percent throttle.  Generally negative for turbine reverser

[piston_engine]
power_scalar=1.0                             //Piston power scalar
cylinder_displacement=90.0                     //Cubic inches per cylinder
compression_ratio=8.5                          //Compression ratio
number_of_cylinders=6                          //Number of cylinders
max_rated_rpm=3700                             //Max rated RPM
max_rated_hp=260                               //Max rated HP
fuel_metering_type=0                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3                 //Starter torque factor
turbocharged=0                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=0                                //Max design manifold pressure, (inHg)
min_design_mp=0                                //Min design manifold pressure, (inHg)
critical_altitude=0                            //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=1                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=6.3                         //Propeller Diameter, (feet)
propeller_blades=2                             //Number of propeller blades
propeller_moi=5.0                              //Propeller moment of inertia
beta_max=0                                     //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=0                                     //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=0                                  //Miminum governed RPM
prop_tc=0                                      //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=0                         //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, 5 , 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 2 , 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,  2.50,  -2.61, -1.62 , 9500, 0, 2.0, 38.0, 0.3,1.5, 1.8, 0.0, 0.0, 0
point.1=1,  2.50,   2.61, -1.62 , 9500, 0, 2.0, 38.0, 0.3,1.5, 1.8, 0.0, 0.0, 0
point.2=1, -5.8, -2.65, -1.83, 9500, 1, 1.5,  0.0, 0.5, 1.5, 1.8, 0.0, 0.0, 2
point.3=1, -5.8  2.65, -1.83, 9500, 2, 1.5,  0.0, 0.5, 1.5, 1.8, 0.0, 0.0, 3
point.4=2, 3.0, -2.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.5=2, 3.0   2.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.6=2,-10.23,   0.0,  0.30, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.7=2,  1.48,   0.0, 1.70, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.8=2,-12.80,   0.0,  5.83, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7
point.9=2, -4.90,   0.0, 1.70, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8

max_number_of_points=21

static_pitch=0.0               //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=1.5           //feet, altitude of CG when at rest on the ground

[brakes]
parking_brake=1.4        //Parking brake available
toe_brakes_scale=1.0  //Brake scalar

[hydraulic_system]
normal_pressure=0.0    //PSI

[Views]
eyepoint=-3.8, 1.4, 3.35        //(feet) longitudinal, lateral, vertical distance from reference datum

[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

//[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0=5,  2.8, -1.95, -1.34, fx_landing,
light.1=5,  2.8,  1.95, -1.34, fx_landing,
light.2=4,  -3.25, 0.0, 0.89, fx_vclight,

[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

[attitude_indicators]
;/Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=1

[turn_indicators]
;/Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,1    //Turn AND Bank

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

[fuel]
LeftMain=-3.0, 0.0, -0.0, 139.0, 0.0       //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=10.0                 //Square feet
wing_span=10.1                  //Feet
wing_root_chord=0.9                   //Feet
wing_dihedral=1.7                   //Degrees
wing_incidence=1.5                   //Degrees
wing_twist=-3.0                  //Degrees
oswald_efficiency_factor=0.68                  //Measure of lift effeciency of wing
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=0                     //Degrees, wing leading edge
wing_pos_apex_lon=-2.4                  //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=9.0                  //Square feet
htail_span=11.7                  //Feet
htail_pos_lon=-18.3                 //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=3.2                   //Degrees
htail_sweep=10.0                  //Degrees, horizontal tail leading edge
vtail_area=18.0                  //Square feet
vtail_span=4.8                   //Feet, tip to body
vtail_sweep=40.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-16.2                 //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=0.1                  //Square feet
rudder_area=0.7                   //Square feet
elevator_up_limit=28.0                  //Degrees
elevator_down_limit=21.0                  //Degrees
aileron_up_limit=90.0                  //Degrees
aileron_down_limit=90.0                  //Degrees
rudder_limit=34.0                  //Degrees
elevator_trim_limit=19.5                  //Degrees
spoiler_limit=0.0                   //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


[flaps.0]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.5                                  // 0.0 .. 1.0
extending-time=7                                    // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=12.7                                 // degrees
flaps-position.2=25.3                                 // degrees
flaps-position.3=38                                   // degrees
damaging-speed=120                                  // KIAS
blowout-speed=150                                  // 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


[Reference Speeds]
flaps_up_stall_speed=53.0                  //Knots True (KTAS)
full_flaps_stall_speed=48.0                  //Knots True (KTAS)
cruise_speed=115.0                 //Knots True (KTAS)
max_indicated_speed=263                   //Red line (KIAS)

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.0
autothrottle_available=0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.0


[forcefeedback]
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=6000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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

[stall_warning]
type=1

[exits]
number_of_exits=2
exit_rate.0=0.5                               ;Percent per second
exit_rate.1=0.7                               ;Percent per second

[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.7,0.7	                          ;Percent per second