[fltsim.0]
title=Ilyushin IL-14 Red
sim=IL14
model=
panel=
sound=
texture=red
kb_checklists=
kb_reference=
atc_id=11735
atc_airline=AEROFLOT
atc_flight_number=6AP
atc_heavy=0
ui_manufacturer=Ilyushin IL14
ui_type="Il-14"
ui_variation=AEROFLOT RED
visual_damage=0
description=paint by Andrey Maslov

[fltsim.1]
title=Ilyushin IL-14
sim=IL14
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=61611
atc_airline=AEROFLOT
atc_flight_number=61611
atc_heavy=0
ui_manufacturer=Ilyushin IL14
ui_type="Il-14"
ui_variation=AEROFLOT
visual_damage=0
description=paint by Andrey Maslov

[General]  
atc_type=Ilyushin
atc_model=Il14
editable=0
performance=Function: transport \nYear: 1953 \nCrew 2 \nEngines: 1900hp Shvetsov ASh-82T \nWing Span: 31.70m \nLength: 22.30m \nHeight: 7.90m \nWing Area: 99.70m2 \nEmpty Weight: 12600kg \nMaximum Weight: 18000kg \nMaximum Speed: 430 km/h \nCruising Speed: 350 km/h \nCeiling: 7400m \nRange: 1086mls \nPayLoad: 26 seats or 4800 kg
Category=airplane


[WEIGHT_AND_BALANCE]
max_gross_weight=38030                        // (pounds)
empty_weight=26621                             // (pounds)
reference_datum_position=0.0, 0.0, 0.0     // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-1.0, 0.0, -1.8
//empty_weight_CG_position=2.5, 0.0, -1.8

max_number_of_stations=50
station_load.0=170, 17.5, -1.5, 0.5         //Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170, 17.5,  1.5, 0.5         //Co-Pilot        Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=170, 11.1,  -2.8, 0.5         //Navigator       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=000, 0.0,  0.0, 0.0
//station_load.3=1200, 0.0,  0.0, 0.0         //Passenger        Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=400, 0.0,  0.0, 0.0         //Baggage         Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI=325000
empty_weight_roll_MOI=239000
empty_weight_yaw_MOI=488000
//empty_weight_pitch_MOI=700000
//empty_weight_roll_MOI=500000
//empty_weight_yaw_MOI=900000
empty_weight_coupled_MOI=0

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=2.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=5.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0


[airplane_geometry]
wing_area=1076.0                 //Square feet
wing_span=104                  //Feet
wing_root_chord=10.3                   //Feet
wing_dihedral=-2.0                   //Degrees
wing_incidence=1.0                   //Degrees
wing_twist=-3.0                  //Degrees
oswald_efficiency_factor=0.70                   //Measure of lift effeciency of wing
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=15.0                   //Degrees, wing leading edge
wing_pos_apex_lon=3.0                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=5.0                   //Feet, vertical distance from reference point, positive going up
htail_area=620.0                  //Square feet
htail_span=31.0                  //Feet
htail_pos_lon=-39.5                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.5                   //Feet, vertical distance from reference point, positive going up
htail_incidence=0.0                  //Degrees
htail_sweep=20.0                   //Degrees, horizontal tail leading edge
vtail_area=208.0                  //Square feet
vtail_span=16.9                  //Feet, tip to body
vtail_sweep=25.0                   //Degrees, vertical tail leading edge
vtail_pos_lon=-39.0                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=7.2                   //Feet, vertical distance from reference point, positive going up
elevator_area=60.0                  //Square feet
aileron_area=44.0                  //Square feet
rudder_area=96.0                  //Square feet
elevator_up_limit=17.0                  //Degrees
elevator_down_limit=15.0                  //Degrees
aileron_up_limit=13.0                  //Degrees
aileron_down_limit=18.0                  //Degrees
rudder_limit=25.0                  //Degrees
elevator_trim_limit=20.0                  //Degrees
spoiler_limit=20.0                   //Degrees
spoilerons_available=0                     //Spoilerons Available?
aileron_to_spoileron_gain=0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons=10                 //Degrees
min_flaps_for_spoilerons=20                    //Minimum flap handle position when spoilerons activate
auto_spoiler_available=0
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.350427
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000


[contact_points]
point.0=1,   14.5,     0,  -10.8, 1600,   0,   0.633,    55,  0.42,   2.5,   0.90,     3,    3,   0,  0,  180
point.1=1,  -4.0, -12.7, -10.5, 1600,   1,   0.886,      0,   0.50,   2.5,   0.85,  4.1, 4.3,  2,  0,  200
point.2=1,  -4.0,  12.7, -10.5, 1600,   2,   0.886,      0,   0.50,   2.5,   0.85,  4.3, 4.1,  3,  0,  200
point.3=2,  -2.9,-50.0,  0.11,  600, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4=2,  -2.9, 50.0,  0.11,  600, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5=2,  26.0, 0.00, -3.60,  1200, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6=2,  -7.6, 0.00, -3.60,  1200, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7=2, -46.0, 0.00,  0.60,  800, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0
static_pitch=1.0             //Degrees
static_cg_height=10.5         //Feet
gear_system_type=0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3,  -0.2,   -51.0,  0.95, fx_navredm ,
light.1=3,  -4.9,   -51.0,  0.80, fx_navredm ,
light.2=3,  -0.2,    51.0,  0.95, fx_navgrem ,
light.3=3,  -4.9,    51.0,  0.80, fx_navgrem ,
light.4=3, -46.4,    0.00,  0.70, fx_navwhi ,
light.5=1, -40.0,   0.00,   16.5, fx_beaconh ,
light.6=4, 17.00,   0.00,   3.40, fx_vclighth,

[SMOKESYSTEM]
smoke.0=0.00, -30.00, 13.00, fx_smoke_rx
smoke.1=0.00, -30.00, -13.00, fx_smoke_rx  

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

[electrical]
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0
BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus=0, 10, 17.0
avionics=1, 5, 17.0
autopilot=1, 2, 17.0
pitot_heat=0, 2, 17.0
additional_system=0, 1, 16.0
marker_beacon=1, 2, 9.0
fuel_pump=0, 0.1 , 17.0
starter1=0, 20, 15.0
starter2=0, 20, 15.0
light_nav=0, 5, 17.0
light_landing=0, 5, 17.0
light_strobe=0, 1.5 , 17.0
light_panel=0, 2, 17.0

[fuel]
RightMain=-1.237, 7.000, 2.264, 198.12913, 0.000    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)                               
LeftMain=-1.237, -7.000, 2.264, 198.12913, 0.000  //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)  
fuel_type=1.000000                            //Fuel type: 1 = Avgas, 2 = JetA  
number_of_tank_selectors=2
electric_pump=1

[GeneralEngineData]
engine_type=0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=9.0, -12.7, -1.8                      //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=9.0,  12.7, -1.8                      //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=0.9                           //Fuel flow scalar
min_throttle_limit=0.000000

[propeller]
thrust_scalar=1.0                             //Propeller thrust scalar
propeller_type=0                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=12.4                         //Propeller Diameter, (feet)
propeller_blades=4                             //Number of propeller blades
propeller_moi=67                              //Propeller moment of inertia
beta_max=45.0                                  //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15.2                                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1100.0                             //Miminum governed RPM
prop_tc=0.1                                    //Prop time-constant
gear_reduction_ratio=1.0                       //Propeller gear reduction ratio
fixed_pitch_beta=0.0                           //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80.0                    //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=1                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=700.0                      //Minimum RPM for prop feathering
beta_feather=82.5                              //Feathering pitch angle (degrees)
power_absorbed_cf=0.9                          //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=0.0                     //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0.0                       //Minimum pitch angle in reverse, (degrees)


[piston_engine]
power_scalar=1.0                              //Piston power scalar
cylinder_displacement=150                 //Cubic inches per cylinder
compression_ratio=6.900                         //Compression ratio
number_of_cylinders=18                         //Number of cylinders
max_rated_rpm=2700.0                           //Max rated RPM
max_rated_hp=800.0                             //Max rated HP
fuel_metering_type=0                          //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type=0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.4                  //Starter torque factor
turbocharged=1                                //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 48                              //Max design manifold pressure, (inHg)
min_design_mp= 11                             //Min design manifold pressure, (inHg)
critical_altitude=16000                          //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=0.0                  //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0.0                //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=1                        //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

[flaps.0]       //Trailing Edge Flaps
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=11                                   // degrees
flaps-position.2=23                                   // degrees
flaps-position.3=34                                   // degrees
flaps-position.4=45.0                                 // degrees
damaging-speed=140                                  // KIAS
blowout-speed=175                                  // KIAS
lift_scalar=1.0                                       
drag_scalar=1.0
pitch_scalar=1.0
system_type=1                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None


[exits]
number_of_exits=2
exit_rate.0=0.6                               ;Percent per second
exit_rate.1=0.6 

[Radios]
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1,0
Adf.2=1,0
Transponder.1=1
Marker.1=1

[Reference Speeds]
flaps_up_stall_speed=96.0                  //Knots True (KTAS)
full_flaps_stall_speed=76.0                  //Knots True (KTAS)
cruise_speed=180.0                 //Knots True (KTAS)


//-------------------------------------------------------------------------------
max_indicated_speed=259.000000

[autopilot]
autopilot_available=1
flight_director_available=0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
attitude_indicator=1
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=0.0
default_bank_mode=2     //Default to Heading Hold

[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=3,0

[brakes]
parking_brake=1       //Parking brake available
toe_brakes_scale=0.6  //Brake scalar
differential_braking_scale=1.0        //Delta on the amount of brake when the rudder pedals deflected

[hydraulic_system]
normal_pressure=732.0    //PSI
electric_pumps=0         //no electric pumps
engine_map=1,1,0,0   //pumps on Eng1,2

[Views]
eyepoint=0,0,0    //Longitudinal, Lateral, Vertical (feet)

[pitot_static]
vertical_speed_time_constant=1.0  
pitot_heat=1.000000

[keyboard_response]
//elevator=350.0,500.0
//aileron=450.0,1000.0
//rudder=200.0,1000.0
elevator=150, 250
aileron=150, 250
rudder=150, 250

[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                ; in microseconds

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=31.512679
flap_limit_idle=31.512679

[stall_warning]
type=1
stick_shaker=0

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=4.900000
engine_map=1,1,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0