[fltsim.0]
title=R-5
sim=R-5
model=
panel=
sound=
texture=
kb_checklists=
prop_anim_ratio=0.5

atc_id=L-1579
ui_manufacturer=Policarpov
ui_type=R-5
ui_variation=USSR L-1579
description=version 2009.08.12

[General]
atc_type=R-5
atc_model=R-5
editable=0
performance="version 2009.08.10"

[WEIGHT_AND_BALANCE]
max_gross_weight = 8389                         // (pounds)
empty_weight =  4788                            // (pounds)
reference_datum_position    = 0.0, 0.0, 0.0     // (feet) distance from FlightSim Ref. (1/4 chord, centerline).
empty_weight_CG_position    = 0.0, 0.0, 0.0

max_number_of_stations =3

station_load.0 = "200.0,  -4.65, 0.0,  1.31, Pilot"                 //Weight, longitudinal, lateral, vertical distance from specified datum
station_load.1 = "200.0,  -8.29, 0.0,  0.46, Navigator"             //Weight, longitudinal, lateral, vertical distance from specified datum
station_load.2 = "200.0, -11.80, 0.0,   0.0, Cargo"                 //Weight, longitudinal, lateral, vertical distance from specified datum

;Moments of Inertia
empty_weight_roll_MOI    	=  8464.0
empty_weight_pitch_MOI   	= 10136.0
empty_weight_yaw_MOI     	= 16082.0
empty_weight_coupled_MOI 	= 0.0



[flight_tuning]
cruise_lift_scalar     	=1.0
parasite_drag_scalar   	=1.165
induced_drag_scalar    	=1.0
elevator_effectiveness	=1.0
aileron_effectiveness  	=1.0
rudder_effectiveness   	=1.0
pitch_stability        	=1.1
roll_stability         	=1.1
yaw_stability          	=1.0
elevator_trim_effectiveness 	=1.0
aileron_trim_effectiveness  	=1.0
rudder_trim_effectiveness   	=1.0
p_factor_on_yaw          	= 0.5
hi_alpha_on_roll		=1.0
hi_alpha_on_yaw		=1.0
torque_on_roll		=1.0
gyro_precession_on_roll	=1.0
gyro_precession_on_yaw	=1.0


[GeneralEngineData]
engine_type 	= 0
Engine.0 		= 9.51, 0.0, 0.0
fuel_flow_scalar	= 1.0666
min_throttle_limit 	= 0.005                      	// Minimum percent throttle.

[piston_engine]
power_scalar 		= 1.0
cylinder_displacement	= 233.8
compression_ratio	= 6.0
number_of_cylinders	= 12
max_rated_rpm		= 1800.0
max_rated_hp		= 730.0
fuel_metering_type	= 1
cooling_type		= 1
normalized_starter_torque = 0.3
turbocharged		= 1                                //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp		= 30                               //Max design manifold pressure, (inHg)
min_design_mp		= 10                               //Min design manifold pressure, (inHg)
critical_altitude	= 8000.0

emergency_boost_type		=0
emergency_boost_mp_offset	=0.0
emergency_boost_gain_offset	=0.0
fuel_air_auto_mixture		=0
auto_ignition			=0

max_rpm_mechanical_efficiency_scalar	=0.98
idle_rpm_mechanical_efficiency_scalar	=1.0
max_rpm_friction_scalar			=1.0
idle_rpm_friction_scalar		=1.0
emergency_boost_duration		=0.0
power_scalar				=1.0


[propeller]
thrust_scalar 		= 1.0
propeller_type		= 1.0
propeller_diameter	= 13.0
propeller_blades	= 2
propeller_moi		= 14.0
gear_reduction_ratio	= 1.135
fixed_pitch_beta	= 13.5
low_speed_theory_limit	= 80.0
beta_max		=0
beta_min		=0
min_gov_rpm		=0
prop_tc			=0
prop_sync_available	=0
prop_deice_available	=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather	=0
beta_feather		=0
power_absorbed_cf	=0
defeathering_accumulators_available=0
prop_reverse_available	=0
minimum_on_ground_beta	=0
minimum_reverse_beta	=0


[contact_points]


        //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

max_number_of_points=7

; Ref:...0......1.....2......3......4.....5..6......7....8....9...10...11...12..13
point.0= 3, -18.69,  0.0,  -2.50,  1200,  0, 0.1, 30.0, 0.3, 1.5, 0.8, 0.0, 0.0, 7
point.1= 1,  1.49, -3.42,  -6.56,  1600,  1, 1.1,  0.0, 0.6, 1.5, 0.8, 0.0, 0.0, 2
point.2= 1,  1.49,  3.42,  -6.56,  1600,  2, 1.1,  0.0, 0.6, 1.5, 0.8, 0.0, 0.0, 3
;  Scrapes
point.3= 2,   -1.6, -28.0,  4.00,   800, 0, 0.0,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.4= 2,   -1.6,  28.0,  4.00,   800, 0, 0.0,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.5= 2, -29.5,    0.0,  2.00,   800, 0, 0.0,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.6= 2,   8.5,    0.0, -2.10,   800, 0, 0.0,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4

static_pitch 	= 12.8
static_cg_height =  5.7
gear_system_type =4


[brakes]
parking_brake 		= 1       	// Parking brake available?
toe_brakes_scale 		= 0.3
differential_braking_scale 	= 0    	// Delta on the amount of brake when the rudder pedals deflected.


[hydraulic_system]
normal_pressure =0.0


[Views]
eyepoint = -5, 0.0, 2.75


[LIGHTS]
//Types: 4=cockpit.
//light.0 = 4,   -5.00,  0.00,   2.00,NULL
; Remainder done by FSDS3 / fs9 materials.

[Radios]
// Radio Type = availiable, standby frequency, has glide slope.
Audio.1       	= 1
Com.1         	= 1, 0
Nav.1         	= 0, 0, 0
Adf.1         	= 1
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.
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0= 1,0
direction_indicator.1= 2,0


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


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


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


[electrical]
autopilot= 		0,  0.0, 17.0
avionics_bus=		4, 20.0, 20.0
avionics=		4, 20.0, 20.0
pitot_heat=		4,  0.0, 17.0
light_nav=		4,  0.1, 17.0
light_beacon=		4,  0.1, 17.0
light_landing=		4,  1.0, 17.0
light_panel=		4,  0.1, 17.0
starter1=               3, 20.0, 17.0
avionics=		4,  1.0, 17.0

electric_always_available=0
max_battery_voltage 		= 28
generator_alternator_voltage 	= 30
max_generator_alternator_amps 	= 60


[fuel]
Center1   =  2.13,  0.00, 2.13,   1.5, 0.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  =  0.00,  0.00, 5.88,  82.0, 0.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain =  0.82,  0.00, 0.69, 138.0, 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
manual_transfer_pump=0


[airplane_geometry]
wing_area               	= 539.64
wing_span               	= 50.82
wing_root_chord         	= 6.62
wing_dihedral           	= 2.5
wing_incidence          	= 0.0
wing_twist              	= 0.0
oswald_efficiency_factor	= 1.0
wing_winglets_flag      	= 0
wing_sweep              	=  2.3
wing_pos_apex_lon       	=  0.0
wing_pos_apex_vert      	=  1.0

htail_area              	=  71.4
htail_span              	=  15.7
htail_pos_lon           	= -20.6
htail_pos_vert          	=  0.0
htail_incidence         	=  0.0
htail_sweep             	=  0.0

vtail_area              	=   7.5
vtail_span              	=   5.0
vtail_sweep             	=   0.0
vtail_pos_lon           	= -20.6
vtail_pos_vert          	=   0.0

elevator_area           	= 31.4
aileron_area            	= 38.7
rudder_area             	= 17.2
elevator_up_limit       	= 20.0
elevator_down_limit     	= 19.0
aileron_up_limit        	= 32.0
aileron_down_limit      	= 10.5
rudder_limit            	= 22.0
elevator_trim_limit     	= 20.0

spoiler_limit=0.0
spoilerons_available=0
aileron_to_spoileron_gain =0.0
min_ailerons_for_spoilerons =0.0
min_flaps_for_spoilerons =0.0
spoiler_handle_available=0
auto_spoiler_available=0
positive_g_limit_flaps_up=4.0
negative_g_limit_flaps_up=-3.20000
positive_g_limit_flaps_down=2.80000
negative_g_limit_flaps_down=-2.40000
load_safety_factor=1.0


[Reference Speeds] 			// Knots True (KTAS)
flaps_up_stall_speed    	=45		// = 51 mph
full_flaps_stall_speed  	=45
cruise_speed            	=87		// = 100mph
max_indicated_speed 	=130		// (KIAS) = 150 mph.

[stall_warning]
type=1

[smokesystem]
smoke.0=0

[gear_warning_system]
gear_warning_available=0

[autopilot]
autopilot_available=1
flight_director_available=0
autothrottle_available=0
default_vertical_speed=0.000000
pitch_takeoff_ga=8.000000
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

[forcefeedback]	// You are on your own here!
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
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
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=0.300000
system_type=4
flaps-position.0=0.000000,0.000000
flaps-position.1=40.000001,0.000000