; Localized	06/21/2007 02:00 AM (GMT)	4:4.2.169 	aircraft.cfg
[fltsim.0]
title=Piper Cub
sim=Piper_J3Cub
model=""
panel=""
sound=""
texture=""
kb_checklists=Piper_J3Cub_check
kb_reference=Piper_J3Cub_ref
atc_id=NC77583
atc_id_color=""
ui_manufacturer=Пайпер
ui_type=J-3 Каб
ui_variation=Классика-желтый
ui_typerole=Одномоторный винтовой
ui_createdby=Корпорация Майкрософт
description=Простой и недорогой "Пайпер J-3 Каб" был первым самолетом для целого поколения пилотов. Выпущенный в 1938 году, он стал пропуском в небо для множества людей. 75 процентов американских летчиков времен Второй мировой войны учились летать именно на нем. Медленный полет на низкой высоте - настоящее возвращение к истокам авиации.

[fltsim.1]
title=Piper Cub Paint1
sim=Piper_J3Cub
model=""
panel=""
sound=""
texture=1
kb_checklists=Piper_J3Cub_check
kb_reference=Piper_J3Cub_ref
atc_id=NC77584
atc_id_color=""
ui_manufacturer=Пайпер
ui_type=J-3 Каб
ui_variation=Кремовый с темно-красным
ui_typerole=Одномоторный винтовой
ui_createdby=Корпорация Майкрософт
description=Простой и недорогой "Пайпер J-3 Каб" был первым самолетом для целого поколения пилотов. Выпущеный в 1938 году, он стал пропуском в небо для множества людей. 75 процентов американских летчиков времен Второй мировой войны учились летать именно на нем. Медленный полет на низкой высоте - настоящее возвращение к истокам авиации.

[fltsim.2]
title=Piper Cub Paint2
sim=Piper_J3Cub
model=""
panel=""
sound=""
texture=2
kb_checklists=Piper_J3Cub_check
kb_reference=Piper_J3Cub_ref
atc_id=NC77585
atc_id_color=""
ui_manufacturer=Пайпер
ui_type=J-3 Каб
ui_variation=Красный с белым
ui_typerole=Одномоторный винтовой
ui_createdby=Корпорация Майкрософт
description=Простой и недорогой "Пайпер J-3 Каб" был первым самолетом для целого поколения пилотов. Выпущеный в 1938 году, он стал пропуском в небо для множества людей. 75 процентов американских летчиков времен Второй мировой войны учились летать именно на нем. Медленный полет на низкой высоте - настоящее возвращение к истокам авиации.

[General]
atc_type=Piper
atc_model=J3
editable=1
performance=Максимальная скорость: 74 узла (85 миль/ч, или 137 км/ч)\n\nДвигатель: Continental, с воздушным охлаждением, 65 л.с.\n\nРабочий потолок: 11500 фт. (3505 м)\n\nМаксимальная дальность: 300 миль (480 км)\n\nЗапас топлива: 12 галл. (45,4 л)\n\nВес без нагрузки: 680 фнт. (308 кг)\n\nМаксимальный вес: 1220 фнт. (553 кг)\n\Длина: 22 фт. (6,7 м)\n\nРазмах крыла: 35 фт. (10,6 м)\n\nВысота: 6,7 фт. (2 м)\n\nПосадочных мест: 2\n\nПолезная нагрузка: 340 фнт. (154 кг)
Category=airplane

[CameraDefinition.0]
Title=Правое крыло
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description=Вид на кабину с кончика правого крыла
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=1.0
ShowWeather=Yes
InitialXyz=9.0, 0.38, -1.5
InitialPbh=5, 0, 280
XyzAdjust=TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.1]
Title=Левое крыло
Guid={3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
Description=Вид на кабину с кончика левого крыла
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=1.0
ShowWeather=Yes
InitialXyz=-9.0, 0.38, -1.5
InitialPbh=5, 0, 80
XyzAdjust=TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.2]
Title=Хвост
Guid={D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description=Вид прямо по курсу с вертикального стабилизатора
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.75
ShowWeather=Yes
InitialXyz=0, 1.9, -10.75
InitialPbh=11, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.001]
Title=Пер. сиденье
Guid={195EAB58-9E4A-4E2A-A34C-A8D9D948F078}
Origin=Virtual Cockpit
MomentumEffect=Yes
SnapPbhAdjust=Swivel
SnapPbhReturn=False
PanPbhAdjust=Swivel
PanPbhReturn=False
Track=None
ShowAxis=YES
AllowZoom=TRUE
InitialZoom=.7
SmoothZoomTime=2.0
ZoomPanScalar=0.75
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.0, -0.1, 0.7
InitialPbh=0, 0, 0

[WEIGHT_AND_BALANCE]
max_gross_weight=1220                         // (pounds)
empty_weight=680                             // (pounds)

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

max_number_of_stations=50

station_load.0=170.0, -3.25, 0.00, 0.00   //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=0.0, -0.75, 0.00, 0.00   //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=20.0, -4.40, 0.00, 0.00   //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_name.0=Пилот
station_name.1=Пассажир
station_name.2=Багаж


;Moments of Inertia
empty_weight_pitch_MOI=313.8
empty_weight_roll_MOI=313.9
empty_weight_yaw_MOI=642.2
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=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
p_factor_on_yaw=0.2
torque_on_roll=0.3
gyro_precession_on_yaw=0.3
gyro_precession_on_pitch=0.3

[Flaps.0]
type=0

[GeneralEngineData]
engine_type=0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=5.8, 0.0, 0.0                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=0.6                           //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=42.75                    //Cubic inches per cylinder
compression_ratio=7.5                          //Compression ratio
number_of_cylinders=4                           //Number of cylinders
max_rated_rpm=2300                             //Max rated RPM
max_rated_hp=65                                //Max rated HP
fuel_metering_type=1                           //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
magneto_order_left_right_both=1		//sets the order of the magneto switch direction

[propeller]
thrust_scalar=1.0                             //Propeller thrust scalar
propeller_type=1                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=6.0                         //Propeller Diameter, (feet)
propeller_blades=2                             //Number of propeller blades
propeller_moi=3.78                             //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=13.75                            //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 in feather
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)


;/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,  -15.00,   0.0, -1.05, 1800, 0, 0.238,  60.0, 0.300, 2.5, 0.40, 0.0, 0.0, 0.0, 0.0, 0.0
point.1=1,    1.24,  -3.0, -5.25, 1600, 1, 0.728,   0.0, 0.540, 2.5, 0.65, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=1,    1.24,   3.0, -5.25, 1600, 2, 0.728,   0.0, 0.540, 2.5, 0.65, 0.0, 0.0, 3.0, 0.0, 0.0
point.3=2,   -1.00, -17.7,  1.80,  800, 0, 0.000,   0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2,   -1.00,  17.7,  1.80,  800, 0, 0.000,   0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2,  -14.40,   0.0,  4.50,  800, 0, 0.000,   0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2,    5.40,   0.0, -2.20,  800, 0, 0.000,   0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4.0, 0.0, 0.0

static_pitch=15.2
static_cg_height=4.3

[brakes]
parking_brake=1       //Parking brake available
toe_brakes_scale=0.5  //Brake scalar
differential_braking_scale=1.0        //Delta on the amount of brake when the rudder pedals deflected
auto_brakes=0

[hydraulic_system]
normal_pressure=0.0    //PSI

[Views]
eyepoint=-2.884, 0.000, 1.230

[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=4,  -1.1,   0.00,  1.50, fx_vclight,

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

[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=200, 1000
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=0,0

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

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

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

[pneumatic_system]
max_pressure=0

[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=0.0    //Scalar on heat effectiveness, 0 = not available

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

[electrical]
max_battery_voltage=0
generator_alternator_voltage=0

[fuel]
Center1=2.8, 0.0, 0.0, 12.0, 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=0
engine_driven_pump=0

[airplane_geometry]
wing_area=178.5                 //Square feet
wing_span=35.2                  //Feet
wing_root_chord=5.25                  //Feet
wing_dihedral=1.1                   //Degrees
wing_incidence=2.5                   //Degrees
wing_twist=-1.0                  //Degrees
oswald_efficiency_factor=0.6                   //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=1.31                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=2.1                   //Feet, vertical distance from reference point, positive going up

htail_area=18.2                  //Square feet
htail_span=9.6                   //Feet
htail_pos_lon=-13.4                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=1.3                   //Feet, vertical distance from reference point, positive going up
htail_incidence=-0.8                   //Degrees
htail_sweep=30.0                  //Degrees, horizontal tail leading edge

vtail_area=13.0                  //Square feet
vtail_span=4.44                  //Feet, tip to body
vtail_sweep=38.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-13.5                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=1.6                   //Feet, vertical distance from reference point, positive going up

elevator_area=10.64                 //Square feet
aileron_area=9.6                   //Square feet
rudder_area=6.55                  //Square feet
elevator_up_limit=30.0                  //Degrees
elevator_down_limit=20.0                  //Degrees
aileron_up_limit=20.0                  //Degrees
aileron_down_limit=20.0                  //Degrees
rudder_limit=28.0                  //Degrees
elevator_trim_limit=10.0                   //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=33.0                  //Knots True (KTAS)
full_flaps_stall_speed=33.0                  //Knots True (KTAS)
cruise_speed=55.0                  //Knots True (KTAS)
max_indicated_speed=106                   //Red line (KIAS)

[autopilot]
autopilot_available=0
flight_director_available=0

[forcefeedback]
ground_bumps_magnitude1=2600            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200            ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000                 ; 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