; Localized	06/21/2007 02:00 AM (GMT)	4:4.2.169 	aircraft.cfg
[fltsim.0]
title=Piper Cherokee 180
sim=Piper_PA28_180
model=""
panel=""
sound=""
texture=""
kb_checklists=""
kb_reference=""
atc_id=N700MS
ui_manufacturer=Пайпер
ui_type=Чероки-180
ui_variation=Классика-1
ui_typerole=Одномоторный винтовой
ui_createdby=Корпорация Майкрософт

[fltsim.1]
title=Piper Cherokee 180 Paint1
sim=Piper_PA28_180
model=""
panel=""
sound=""
texture=1
kb_checklists=""
kb_reference=""
atc_id=N700MS
ui_manufacturer=Пайпер
ui_type=Чероки-180
ui_variation=Классика-2
ui_typerole=Одномоторный винтовой
ui_createdby=Корпорация Майкрософт

[fltsim.2]
title=Piper Cherokee 180 Paint2
sim=Piper_PA28_180
model=""
panel=""
sound=""
texture=2
kb_checklists=""
kb_reference=""
atc_id=N700MS
ui_manufacturer=Пайпер
ui_type=Чероки-180
ui_variation=Классика-3
ui_typerole=Одномоторный винтовой
ui_createdby=Корпорация Майкрософт

[General]
atc_type=Piper
atc_model=ARCHER
editable=0
performance=""
Category=airplane

[WEIGHT_AND_BALANCE]
max_gross_weight=2400                         // (pounds)
empty_weight=1330                             // (pounds)

reference_datum_position=7.70, 0, 0      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-6.0, 0, 0      // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50

station_load.0=170,  -7.125, -0.81, 0.0       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170,  -7.125,  0.81, 0.0       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=170,  -9.842, -0.81, 0.0       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=170,  -9.842,  0.81, 0.0       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=97, -11.900,  0.00, 0.0       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_name.0=Пилот
station_name.1=Пер. пассажир
station_name.2=Задний пассажир
station_name.3=Задний пассажир
station_name.4=Багаж

;Moments of Inertia
empty_weight_pitch_MOI=829
empty_weight_roll_MOI=602
empty_weight_yaw_MOI=1168
empty_weight_coupled_MOI=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=1.0
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=-2.4, 0.0, 0.0                       //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0                           //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=90.3                     //Cubic inches per cylinder
compression_ratio=8.5                          //Compression ratio
number_of_cylinders=4                           //Number of cylinders
max_rated_rpm=2700                             //Max rated RPM
max_rated_hp=180                               //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=4.4                              //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=0.1                                    //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=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                        <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]
point.0=1,  -3.80,   0.00, -4.20, 1500, 0, 0.433, 25.0, 0.500, 2.5, 1.0, 0.0, 0.0, 0, 0, 150
point.1=1,  -10.1,  -5.25, -4.35, 3000, 1, 0.433,  0.0, 0.500, 2.5, 0.9, 0.0, 0.0, 2, 0, 150
point.2=1,  -10.1,   5.25, -4.35, 3000, 2, 0.433,  0.0, 0.500, 2.5, 0.9, 0.0, 0.0, 3, 0, 150
point.3=2,  -8.89, -14.95,  0.16, 1200, 0, 0.000,  0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5
point.4=2,  -8.89,  14.95,  0.16, 1200, 0, 0.000,  0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6
point.5=2, -22.29,   0.00, -0.65, 1200, 0, 0.000,  0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9
point.6=2,  -1.33,   0.00, -1.62, 1200, 0, 0.000,  0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4
 
max_number_of_points=21


static_pitch=1.9              //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=3.75         //feet, altitude of CG when at rest on the ground

[brakes]
parking_brake=1        //Parking brake available
toe_brakes_scale=0.94  //Brake scalar
auto_brakes=0

[hydraulic_system]
normal_pressure=0.0    //PSI

[Views]
eyepoint=-6.9, -0.81, 1.5     //(feet) longitudinal, lateral, vertical distance from reference datum

[flaps.0]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.587                                // 0.0 .. 1.0
extending-time=5                                    // seconds
flaps-position.0=0                                    // degrees, KIAS
flaps-position.1=10                                   // degrees, KIAS
flaps-position.2=25                                   // degrees, KIAS
flaps-position.3=40                                   // degrees, KIAS
damaging-speed=100                                  // KIAS
blowout-speed=120                                  // KIAS
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
system_type=3                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None

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

[direction_indicators]
direction_indicator.0=1,0  //Gyro

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

[vacuum_system]
max_pressure=5.15   //PSI
vacuum_type=1   //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
engine_map=1

[pneumatic_system]
max_pressure=0.000000

[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.0    //Scalar on heat effectiveness, 0 = not available

[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0=3,  -9.00, -15.11, 0.05, fx_navred
light.1=3,  -9.00,  15.11, 0.05, fx_navgre
light.2=3, -23.30,   0.00, 4.55, fx_navwhi
light.3=2, -16.30,   0.00,-1.65, fx_strobe
light.4=2, -23.30,   0.00, 4.55, fx_strobe
light.5=1, -21.85,   0.00, 5.00, fx_beacon
light.6=4,  -8.00,   0.00, 2.15, fx_vclight

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

[fuel]
LeftMain=-7.8, -5.8, -0.8, 25.0, 0.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-7.8,  5.8, -0.8, 25.0, 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=160.0                 //Square feet
wing_span=30.0                  //Feet
wing_root_chord=5.3                   //Feet
wing_dihedral=7.2                   //Degrees
wing_incidence=2.0                   //Degrees
wing_twist=-2.0                  //Degrees
oswald_efficiency_factor=0.9                   //Measure of lift effeciency of wing
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=0.0                   //Degrees, wing leading edge
wing_pos_apex_lon=-6.4                  //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=27.0                  //Square feet
htail_span=10.8                  //Feet
htail_pos_lon=-20.5                 //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=0.0                   //Degrees, horizontal tail leading edge
vtail_area=11.0                  //Square feet
vtail_span=3.8                   //Feet, tip to body
vtail_sweep=40.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-17.6                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=1.3                   //Feet, vertical distance from reference point, positive going up
elevator_area=24.4                  //Square feet
aileron_area=10.6                  //Square feet
rudder_area=4.9                   //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=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
auto_spoiler_available=0
positive_g_limit_flaps_up=4.0               //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down=2.0               //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up=-1.5               //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down=-1.5               //Design G load tolerance (negative, flaps down)
load_safety_factor=1.5               //Design G load safety factor

[Reference Speeds]
flaps_up_stall_speed=61.0                  //Knots True (KTAS)
full_flaps_stall_speed=50.0                  //Knots True (KTAS)
cruise_speed=124.0                 //Knots True (KTAS)
max_indicated_speed=148                   //Red line (KIAS)

[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=100.0, 180.0
aileron=200.0, 1000.0
rudder=200.0, 1000.0

[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
stick_shaker=0

[deice_system]
structural_deice_type=0     //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots