[fltsim.0]
title=Ilyushin IL-14
sim=IL14_2
model=
panel=7
sound=
texture=
kb_checklists=
kb_reference=
atc_id=11738
atc_airline=AEROFLOT
atc_flight_number=6AP
atc_heavy=0
ui_manufacturer=Ilyushin
ui_type="Il-14"
ui_variation=AEROFLOT
visual_damage=0
description=paint by Andrey Maslov
atc_parking_types=
atc_parking_codes=
[General]
atc_type=Ilyushin
atc_model=Il14
editable=1
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
[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=-2.0, 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" //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, 17.5, 1.5, 0.5, Co-Pilot" //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "170, 11.1, -2.8, 0.5, Navigator" //Navigator Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "170, 11.1, 2.8, 0.5, Technik"
station_load.4 = "520, 10.1, 0.0, 0.5, Passenger Row1" //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "520, 2.0, 0.0, 0.5, Passenger Row2"
station_load.6 = "520, -0.5, 0.0, 0.5, Passenger Row3"
station_load.7 = "520, -3.0, 0.0, 0.5, Passenger Row4"
station_load.8 = "520,-5.5, 0.0, 0.5, Passenger Row5"
station_load.9 = "520,-8.0, 0.0, 0.5, Passenger Row6"
station_load.10 = "520,-10.5, 0.0, 0.5, Passenger Row7"
station_load.11 = "400, 8.0, 0.0, 0.0, Forvard Cargo" //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.12 = "400, -16.9, 0.0, 0.5, Rear Cargo"
;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=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
[airplane_geometry]
wing_area=1076.0 //Square feet
wing_span=104 //Feet
wing_root_chord=10.3 //Feet
wing_dihedral=3.0 //Degrees
wing_incidence=2.0 //Degrees
wing_twist=0.0 //Degrees
oswald_efficiency_factor=0.65 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=2.0 //Degrees, wing leading edge
wing_pos_apex_lon=3.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=-2.0 //Feet, vertical distance from reference point, positive going up
htail_area=229.5 //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=-2.2 //Degrees
htail_sweep=24.0 //Degrees, horizontal tail leading edge
vtail_area=136.6 //Square fee
vtail_span=16.9 //Feet, tip to body
vtail_sweep=15.0 //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=74.38 //Square feet
aileron_area=77.5 //Square feet
rudder_area=62.86 //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=15.0 //Degrees
spoiler_limit=90.0 //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
[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, 5, 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]
LeftMain=-5.4, -16.0, -1.0, 462.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-5.4, 16.0, -1.0, 462.0, 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=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= 7.2 //Propeller moment of inertia
beta_max= 22.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 2.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1100 //Miminum governed RPM
//max_gov_rpm=2600.0
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.13 //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= 1 //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= 1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering
beta_feather= 89.5 //Feathering pitch angle (degrees)
power_absorbed_cf= 0.9 //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= 0.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees)
feathering_switches = 1 //Switches which invoke feathering
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=200 //Cubic inches per cylinder
compression_ratio=6.9 //Compression ratio
number_of_cylinders=14 //Number of cylinders
max_rated_rpm=2600.0 //Max rated RPM
max_rated_hp=1900.0 //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=0.1 //Starter torque factor
turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=52.0 //Max design manifold pressure, (inHg)
min_design_mp=10.0 //Min design manifold pressure, (inHg)
critical_altitude=0.0 //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=0.0 //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
Adf.2=1
Transponder.1=1
Marker.1=1
[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=1.000000
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=0
use_no_default_bank=2
[Reference Speeds]
flaps_up_stall_speed=96.0 //Knots True (KTAS)
full_flaps_stall_speed=76.0 //Knots True (KTAS)
cruise_speed=145.0 //Knots True (KTAS)
//-------------------------------------------------------------------------------
max_indicated_speed=220.000000
[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=1,0
direction_indicator.1=2,0
[brakes]
parking_brake=1 //Parking brake available
toe_brakes_scale=0.3 //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
[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
[attitude_indicators]
attitude_indicator.0=1
attitude_indicator.1=2
[turn_indicators]
turn_indicator.0=2,0
