[fltsim.0]
title=Ilyushin-IL4
sim=Ilyushin-IL4
model=
panel=
sound=
texture=
kb_reference=CheckList__Ilyushin IL4
atc_id=78
atc_airline=VVS USSR
atc_flight_number=78
ui_manufacturer=Ilyushin
ui_type="Il-4"
ui_variation="USSR"
description="In 1938 the variant of plane DB-3 with absolutely new, easily gathering glider was developed. As a result of its appearance has absolutely changed: the nasal part has been made narrower, has received well streamline form and the big area,and nasal plane DB-3 machine gun has been replaced by machine-gun installation. The state acceptance tests have successfully come to the end in June, 1939, and by the end of the same year the plane has been prepared for a batch production. The new variant Ilyushin DB-3F later was named as Il-4. Plane Il-4 Large-lot production proceeded till 1944. During this time 5256 cars have been constructed. Initial engine M-87 in 1942 has been replaced by more powerful motor M-88B with a two-level supercharger. The majority of the planes constructed in 1942, because of shortage of easy alloys had a wing with wooden longerons; in later serial cars metal again has been used. Except realisation of bombardments in deep back of the opponent, planes Il-4 which are a part of bombing cases of aircraft of distant action, were often applied in attacks to tactical targets in near back of the enemy, bearing the maximum bombing loading. Plane Il-4 was widely used by regiments of torpedo bombers on Baltiysk and Black the seas, and also on Northern fleet. Used in a role of a torpedo bomber plane Il-4 bore 940 kg of torpedoes 45-36-АН (for attack from small height) or torpedoes 45-36-AB (for attack from the big height).Under a back part of a fuselage there were fastenings for installation of external additional fuel tanks. In 1943 working out of plane Il-6, an advanced bomber with a tight cabin of crew for flights at the big height, with considerable direct a forward edge of the wing equipped with two diesel engines Charomsky АЧ-30Б by capacity of 1119 kw (1500 h.p. has begun.)."

[WEIGHT_AND_BALANCE]
empty_weight = 14599

reference_datum_position = 0, 0, 0
empty_weight_CG_position  = -0.02, 0, 0

max_number_of_stations = 10
station_load.0 = 200, 3.6, 0, 1.5, // Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 200, 9.2, 0, -1.5, // bombadier
station_load.2 = 200, -11.9, 0, 0, // rear gunner
station_load.3 = 0, 0, 0, 0, //
station_load.4 = 0, 0, 0, 0, //
station_load.5 = 0, 0, 0, 0, //
station_load.6 = 0, 0, 0, 0, //
station_load.7 = 0, 0, 0, 0, //
station_load.8 = 0, 0, 0, 0, //
station_load.9 = 0, 0, 0, 0, //

empty_weight_pitch_MOI = 28424
empty_weight_roll_MOI = 42555
empty_weight_yaw_MOI = 70030
empty_weight_coupled_MOI=0.000000
max_gross_weight=22798.500000

[flight_tuning]
cruise_lift_scalar = 1
parasite_drag_scalar = 1
induced_drag_scalar = 1
elevator_effectiveness = 1
aileron_effectiveness = 1
rudder_effectiveness = 1
pitch_stability = 1
roll_stability = 1
yaw_stability = 1
elevator_trim_effectiveness = 1
aileron_trim_effectiveness = 1
rudder_trim_effectiveness = 1

[piston_engine]
power_scalar = 1
cylinder_displacement = 91.6666666666667
compression_ratio = 6
number_of_cylinders = 18
max_rated_rpm = 2650
max_rated_hp = 1000
fuel_metering_type = 2
cooling_type = 1
normalized_starter_torque = 0.035
turbocharged = 1
max_design_mp = 50
min_design_mp = 9
critical_altitude = 26000
emergency_boost_type = 3
emergency_boost_mp_offset = 0
emergency_boost_gain_offset = 0
fuel_air_auto_mixture = 0
auto_ignition = 0
max_rpm_mechanical_efficiency_scalar = 1
idle_rpm_mechanical_efficiency_scalar = 1
max_rpm_friction_scalar = 1
idle_rpm_friction_scalar = 1

[propeller]
thrust_scalar = 1
propeller_type = 0
propeller_diameter = 10.3
propeller_blades = 3
propeller_moi = 24.9
beta_max = 65
beta_min = 15
min_gov_rpm = 397.5
prop_tc = 0.01
gear_reduction_ratio = 2.38
fixed_pitch_beta = 30
low_speed_theory_limit = 80
prop_sync_available = 1
prop_deice_available = 1
prop_feathering_available = 1
prop_auto_feathering_available = 1
min_rpm_for_feather = 700
beta_feather = 88.5
power_absorbed_cf = 0.9
defeathering_accumulators_available = 0
prop_reverse_available = 0
minimum_on_ground_beta = 1
minimum_reverse_beta = -14
rotation = -1, -1

[folding_wings]
wing_fold_system_type =  4
fold_rates =  0.12, 0.11

[TailHook]
tailhook_length = 4
tailhook_position = -15, 0, -1
cable_force_adjust = 1

[contact_points]
max_number_of_points = 7
point.0 = 1, -32, 0, -4.25, 1600, 0, 0.9, 75, 0.6, 2.5, 0.8, 6, 6, 0, 104, 116
point.1 = 1, 1.74, -10, -9.9, 2200, 1, 2, 0, 0.9, 2.5, 0.8, 7.5, 8.5, 2, 104, 116
point.2 = 1, 1.74, 10, -9.9, 2200, 2, 2, 0, 0.9, 2.5, 0.8, 8, 7, 3, 104, 116
point.3 = 2, 0, -41, 2.3, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5
point.4 = 2, 0, 41, 2.3, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6
point.5 = 2, -42, 0, -1, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 9
point.6 = 2, 17.16, 0, -2.83, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 4

static_pitch= 9.44
static_cg_height= 9.567
gear_system_type=0


[Views]
eyepoint= 3, 0.1, 2.4

[flaps.0]       //Trailing Edge Flaps
type = 1
span-outboard = 0.5
extending-time = 5
flaps-position.0 = 0
flaps-position.1 = 11, 134
flaps-position.2 = 22, 128
flaps-position.3 = 33, 122
flaps-position.4 = 45, 117
damaging-speed = 134
blowout-speed = 145

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 160
electric_always_available = 1

flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
starter3 = 0, 20, 17
starter4 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
prop_sync = 0, 15, 17
auto_feather = 0, 15, 17
auto_brakes = 0, 15, 17
standby_vacuum = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17

[LIGHTS]
panel = 0, 0.35, -0.8, fx_vclight

[LSO]
LSOAdjustSpeed = 1.2

[exits]
number_of_exits = 1
exit_rate.0 = 0.4

[forcefeedback]
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
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
[General]
performance=* Weight: 15199 lbs    Max 22383 lbs\n* Power: 1000 hp MIL  1000 hp WEP\n* 5.5g Corner speed: 172 mph\n* Max speed @ SL: 278 mph\n* Max speed: 330 mph @ 26000 ft\n* Climb rate: 2051 ft\/min @ 143 mph\nFlight Model By: Cbielat\nSB-2-100\n5\/22\/04 02:52 PM\nFlight Model Workbook V2.82.99
[fuel]
LeftMain=0.000000,-13.400000,0.000000,400.000000,0.000000
RightMain=0.000000,13.400000,0.000000,400.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=718.000000
wing_span=70.333333
wing_root_chord=10.250000
wing_dihedral=1.395264
wing_incidence=0.000000
wing_twist=0.000000
oswald_efficiency_factor=0.885332
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=112.000000
htail_span=23.250000
htail_pos_lon=-27.000000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=40.000000
vtail_span=7.211103
vtail_sweep=0.000000
vtail_pos_lon=-27.583333
vtail_pos_vert=10.666667
elevator_area=65.000000
aileron_area=44.500000
rudder_area=30.000000
elevator_up_limit=30.000000
elevator_down_limit=20.000000
aileron_up_limit=15.000000
aileron_down_limit=15.000000
rudder_limit=30.000000
elevator_trim_limit=18.000000
spoiler_limit=90.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
[brakes]
toe_brakes_scale=0.640889
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=33.750000
flap_limit_idle=16.875000
[GeneralEngineData]
engine_type=0
Engine.0=6.916667,-8.166667,-2.000000
Engine.1=6.916667,8.083333,-2.000000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000
[Reference Speeds]
flaps_up_stall_speed=85.000000
full_flaps_stall_speed=68.000000
cruise_speed=245.166950
max_indicated_speed=334.398438
[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
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
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=6.930556
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=1,0