// Lublin R-XIIID configuration file
// Copyright (c) 2007 Michal Puto.  All rights reserved.
// www.simhangar.com

[fltsim.0]
title=Lublin R-XIII D 26 Eskadra
sim=LublinRXIII
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=
atc_id_color=
ui_manufacturer=Plage & Laskiewicz
ui_type="Lublin R-XIIID"
ui_typerole=Њmigіowy jednosilnikowy
ui_createdby=Michal Puto
ui_variation="26 Eskadra Obserwacyjna 2 Puіku Lotniczego"
description="\n\n\nPolish observation, close reconnaissance and army cooperation plane, designed in early-1930s in Plage i Laskiewicz factory in Lublin. \nR-XIII D variant introduced visible changes, like a Townend ring on a radial engine, and a new engine cowling. It also had new type of a machine gun ring mounting. The first R-XIIID was tested in February, 1933. All aircraft were given to the Air Force by March 2, 1935. During repairs, older models A, B and C were modified to R-XIIID standard as well. (source: en.wikipedia.org/wiki/Lublin_RXIII)"

[fltsim.1]
title=Lublin R-XIII D
sim=LublinRXIII
model=
panel=
sound=
texture=1
kb_checklists=
kb_reference=
atc_id=
atc_id_color=
ui_manufacturer=Plage & Laskiewicz
ui_type="Lublin R-XIIID"
ui_typerole=Њmigіowy jednosilnikowy
ui_createdby=Michal Puto
ui_variation="26 Eskadra Obserwacyjna 2 Puіku Lotniczego"
description="\n\n\nPolish observation, close reconnaissance and army cooperation plane, designed in early-1930s in Plage i Laskiewicz factory in Lublin. \nR-XIII D variant introduced visible changes, like a Townend ring on a radial engine, and a new engine cowling. It also had new type of a machine gun ring mounting. The first R-XIIID was tested in February, 1933. All aircraft were given to the Air Force by March 2, 1935. During repairs, older models A, B and C were modified to R-XIIID standard as well. (source: en.wikipedia.org/wiki/Lublin_RXIII)"

[fltsim.2]
title=Lublin R-XIII D SP-ANG
sim=LublinRXIII
model=1
panel=
sound=
texture=2
kb_checklists=
kb_reference=
atc_id=
atc_id_color=
ui_manufacturer=Plage & Laskiewicz
ui_type="Lublin R-XIIID"
ui_typerole=Њmigіowy jednosilnikowy
ui_createdby=Michal Puto
ui_variation="SP-ANG"
description="\n\n\nPolish observation, close reconnaissance and army cooperation plane, designed in early-1930s in Plage i Laskiewicz factory in Lublin. \nR-XIII D variant introduced visible changes, like a Townend ring on a radial engine, and a new engine cowling. It also had new type of a machine gun ring mounting. The first R-XIIID was tested in February, 1933. All aircraft were given to the Air Force by March 2, 1935. During repairs, older models A, B and C were modified to R-XIIID standard as well. (source: en.wikipedia.org/wiki/Lublin_RXIII)"

[CameraDefinition.001]
Title=Tylne siedzenie
Guid={2B86D24F-303F-4c87-A1EB-EFEBC3328A53}
Origin=Virtual Cockpit
MomentumEffect=Yes
SnapPbhAdjust=Swivel
SnapPbhReturn=False
PanPbhAdjust=Swivel
PanPbhReturn=False
Track=None
ShowAxis=YES
AllowZoom=TRUE
InitialZoom=0.45
SmoothZoomTime=2.0
ZoomPanScalar=1
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.0, 0.1, -0.7
InitialPbh=0, 0, 0

[General]
atc_type=
atc_model=
editable=0
performance="Maximum Speed\n185 km\/h\n\nEngine\nLicensed Wright Whirlwind J5, 162kW (220hp)\n\nService Ceiling\n4,450m\n\nMaximum Range\n600 km\n\nFuel Capacity\n200 L\n\nEmpty Weight\n912kg (2,010lb)\n\nGross Weight\n1332 kg (2936lb)\n\nLength\n8.46 m\n\nWingspan\n13.25 m\n\nHeight\n2.76m\n\nSeating\n2"
Category=airplane

[weight_and_balance]
max_gross_weight =2936.5 
empty_weight =2010.60000

reference_datum_position     = 10.150, 0.000, 0.620
empty_weight_CG_position     = -7.433, 0.000, -0.600

max_number_of_stations =2


;Moments of Inertia
empty_weight_pitch_MOI   =1913.00000
empty_weight_roll_MOI    =2032.00000
empty_weight_yaw_MOI     =3312.00000
empty_weight_coupled_MOI =0.00000
station_load.0= 170, -11.300, 0.000, 0.400, Pilot
station_load.1= 170, -13.900, 0.000, 0.500, Navigator

[flight_tuning]
cruise_lift_scalar     =1.00000
parasite_drag_scalar   =1.00000
induced_drag_scalar    =1.00000
elevator_effectiveness =1.00000
aileron_effectiveness  =1.00000
rudder_effectiveness   =1.00000
pitch_stability        =1.00000
roll_stability         =1.00000
yaw_stability          =1.00000
elevator_trim_effectiveness =1.00000
aileron_trim_effectiveness  =1.00000
rudder_trim_effectiveness   =1.00000
p_factor_on_yaw          =0.30000
torque_on_roll           =0.30000
gyro_precession_on_yaw   =0.30000
gyro_precession_on_pitch = 0.3
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
gyro_precession_on_roll=1.00000

[Flaps.0]
type= 0

[GeneralEngineData]
engine_type =0
Engine.0 =0.000, 0.000, 0.000
fuel_flow_scalar=1.00000
min_throttle_limit = 0.0                        //Minimum percent throttle.  Generally negative for turbine reverser

[piston_engine]
power_scalar =1.00000
cylinder_displacement=87.46667
compression_ratio=5.10000
number_of_cylinders=9
max_rated_rpm=1800.00000
max_rated_hp=223.00000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.25320
turbocharged=0
max_design_mp=29.92000
min_design_mp=0.00000
critical_altitude=0.00000
emergency_boost_type=0
emergency_boost_mp_offset=0.00000
emergency_boost_gain_offset=0.00000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.00000
idle_rpm_mechanical_efficiency_scalar=1.00000
max_rpm_friction_scalar=1.00000
idle_rpm_friction_scalar=1.00000
emergency_boost_duration=0.00000

[propeller]
thrust_scalar =1.00000
propeller_type=1
propeller_diameter=8.86000
propeller_blades=2
propeller_moi=12.30000
beta_max=14.75000
beta_min=12.75000
min_gov_rpm=0.00000
prop_tc=0.10000
gear_reduction_ratio=1.00000
fixed_pitch_beta=13.75000
low_speed_theory_limit=80.00000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.00000
beta_feather=0.00000
power_absorbed_cf=0.00000
defeathering_accumulators_available=0 
prop_reverse_available=0
minimum_on_ground_beta=0.00000
minimum_reverse_beta=0.00000


        //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]
static_pitch = 14.200
static_cg_height = 4.900
max_number_of_points=7
gear_system_type=0
tailwheel_lock=0
point.0= 3, -25.809, 0.000, -1.404, 1200, 0, 0.238, 0.000, 0.160, 2.500, 0.200, 0.000, 0.000, 0
point.1= 1, -7.050, -4.300, -5.700, 1600, 1, 1.250, 0.000, 0.480, 1.250, 0.650, 0.000, 0.000, 2
point.2= 1, -7.050, 4.300, -5.700, 1600, 2, 1.250, 0.000, 0.480, 1.250, 0.650, 0.000, 0.000, 3
point.3= 2, -8.400, -22.000, 2.900, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, -8.400, 22.000, 2.900, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -27.200, 0.000, 4.461, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2, -0.900, 0.000, -3.300, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale =0.50000
differential_braking_scale = 1.0        //Delta on the amount of brake when the rudder pedals deflected

[hydraulic_system]
normal_pressure =0.00000

[Views]
eyepoint = -12.2, 0.000, 2.100

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -8.2, -21.23, 3.17, fx_navred
light.1 = 3, -8.2, 21.23, 3.17, fx_navgre
light.2 = 3, -25.45, 0, 4.7, fx_navwhi

[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
magnetic_compass=0
induction_compass.0=2       //1=Electric, 2=Anemometer Driven

[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=2,0

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

[electrical]
max_battery_voltage = 0
generator_alternator_voltage = 0

[fuel]
Center1 = -3.350, 0.000, -0.230, 52.000, 0.000
fuel_type =1                    
number_of_tank_selectors =1                    
electric_pump=0

[airplane_geometry]
wing_area               =263.70000
wing_span               =43.47000
wing_root_chord         =7.15000
wing_dihedral           =0.00000
wing_incidence          =0.00000
wing_twist              =0.00000
oswald_efficiency_factor=0.60000
wing_winglets_flag      =0
wing_sweep              =0.00000
wing_pos_apex_lon       =-5.90030
wing_pos_apex_vert      =2.80000

htail_area              =17.43000
htail_span              =8.30000
htail_pos_lon           =-22.10000
htail_pos_vert          =0.80000
htail_incidence         =0.00000
htail_sweep             =15.00000

vtail_area              =6.35000
vtail_span              =3.00000
vtail_sweep             =20.00000
vtail_pos_lon           =-22.10000
vtail_pos_vert          =0.96000

elevator_area           =19.16000
aileron_area            =30.10000
rudder_area             =10.41000
elevator_up_limit       =30.00000
elevator_down_limit     =20.00000
aileron_up_limit        =20.00000
aileron_down_limit      =20.00000
rudder_limit            =28.00000
elevator_trim_limit     =10.00000
spoiler_limit           =0.00000
spoilerons_available    =0
aileron_to_spoileron_gain =0.00000
min_ailerons_for_spoilerons =0.00000
min_flaps_for_spoilerons =0.00000
spoiler_handle_available=0
auto_spoiler_available=0
positive_g_limit_flaps_up=3.70000
negative_g_limit_flaps_up=-2.96000
positive_g_limit_flaps_down=2.59000
negative_g_limit_flaps_down=-2.22000
load_safety_factor=1.00000

[Reference Speeds]
flaps_up_stall_speed    =48.57577
full_flaps_stall_speed  =48.57577
cruise_speed            =89.07006
max_indicated_speed     =106.00000
max_mach=0.14500

[autopilot]
autopilot_available=0
flight_director_available=0
autothrottle_available=0
autothrottle_arming_required=0
default_pitch_mode=0
default_bank_mode=0
use_no_default_bank=1
use_no_default_pitch=1
default_vertical_speed=1000.00000
autothrottle_takeoff_ga=1.00000
autothrottle_max_rpm=90.00000
pitch_takeoff_ga=8.00000
max_pitch=10.00000
max_pitch_acceleration=1.00000
max_pitch_velocity_lo_alt=2.00000
max_pitch_velocity_hi_alt=1.50000
max_pitch_velocity_lo_alt_breakpoint=20000.00000
max_pitch_velocity_hi_alt_breakpoint=28000.00000
max_bank=25.00000
max_bank_acceleration=1.80000
max_bank_velocity=3.00000
max_throttle_rate=0.10000
nav_proportional_control=9.00000
nav_integrator_control=0.25000
nav_derivative_control=0.00000
nav_integrator_boundary=2.50000
nav_derivative_boundary=0.00000
gs_proportional_control=9.52000
gs_integrator_control=0.26000
gs_derivative_control=0.00000
gs_integrator_boundary=0.70000
gs_derivative_boundary=0.00000
yaw_damper_gain=0.00000

[forcefeedback]
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

[stall_warning]
type=1
stick_shaker=1

[AirWrench]
Aircraft_Length=27.76000
nose_position_lon=0.00000
Vmax_sl=114.00000
Vmax_ca=114.00000
V_rc=74.50000
Climb_Rate=826.70000
Climb_Weight=2662.60000
Max_gforce=3.70000
Emergency_hp=223.00000
VSI_Weight=2350.60000
ActualIncidence=2.00000
ActualTwist=0.00000
ActualTailIncidence=0.00000
Aircraft_Type=2
FlowCorrection=1.00000
Power_Calibration=1.00000
JetAltitude=0.00000
turboprop_critical_altitude=0.00000
target_roll_Vopt=523.20000
target_roll_rate=185.80000
pitch_damping=1.00000
yaw_damping=1.00000
elevator_scalar=1.00000
rudder_scalar=1.00000
dihedral_scalar=1.00000
Elevator_FF=130.00000
Aileron_FF=-150.00000
Roll_Response=30.00000
Adverse_Yaw=100.00000
Control_Response=100.00000
V_Max_Control=121.98257
V_Zero_Control=243.96515
Spin_Stability=100.00000
Stall_Stability=100.00000
ClAoA_S0=1.00000
ClAoA_S1=1.00000
ClAoA_S2=1.00000
Elevator_Propwash=1.00000
Rudder_Propwash=1.00000
spoiler_time=0.00000
afterburner_thrust=0.00000
mach_scale=1.00000
prop_design_altitude=5000.00000
protect_airfile=0
spoiler_type=0
spoiler_cd=0.00000
spoiler_cl=0.00000
spoiler_cm=0.00000
flaps_type=0
flaps_cd_scalar=0.00000
flaps_cm_scalar=0.00000
vfe_enabled=0
gear_cd_scalar=0.00000
gear_cm_scalar=0.00000
cylinder_head_temperature=501.00000
exhaust_gas_temperature=1201.00000
fuel_pressure=16.50000
oil_pressure=60.00000
oil_temperature=241.00000
radiator_temperature=211.00000
exhaust_pressure_ratio=0.00000
interstage_turbine_temperature=-459.00000
knots_flag=0
cfs1_flag=0
cfs2_flag=0
ai_flag=0
fs8_flag=1
laminar_flow=1
edit_tp_torque=0
direct_edit_mach=0
fixed_wing_pos=0
AirWrenchVersion=1.01.38
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.00000
flap_limit_idle=0.00000
flap_limit_power=0.00000
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[deice_system]
structural_deice_type=0