// Дnderungen von W. Beckert
// Version 1.3, 25.09.2006
// neu mit Handbuchwerten
//ьberarbeitet Mehlin,Rainer 12.12.2006

[fltsim.0]
title=IL-14 INTERFLUG
sim=IL-14P
model=
panel=
sound=
texture=if
//texture=if_nonreflect
checklists=
atc_id=IFSAH
atc_airline=INTERFLUG
atc_flight_number=DM-SAH
ui_manufacturer=Iljuschin
ui_type=IL-14P
ui_variation=INTERFLUG
description=
atc_parking_types=Gate, Ramp
atc_parking_codes=
visual_damage=0
atc_heavy=0
prop_anim_ratio=0.5

[fltsim.1]
title=IL-14 DEUTSCHE LUFTHANSA
sim=IL-14P
model=
panel=
sound=
texture=dlh
//texture=dlh_nonreflect
checklists=
atc_id=IFSBV
atc_airline=DLH
atc_flight_number=DM-SBV
ui_manufacturer=Iljuschin
ui_type=IL-14P
ui_variation=DEUTSCHE LUFTHANSA
description=
atc_parking_types=Gate, Ramp
atc_parking_codes=
visual_damage=0
atc_heavy=0
prop_anim_ratio=0.5


[General]
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: 12200kg \nMaximum Weight: 17000kg \nMaximum Speed: 370 km/h \nCruising Speed: 320 km/h \nCeiling: 6700m \nRange: 1850km \nPayLoad: 26 seats or 2517 kg
atc_model=ILYUSHIN
atc_type=IL14

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3,  0.988, -51.666,  -0.950, fx_navred_max 
light.1=3,  -3.430, -51.666,  -0.950, fx_navred_max
light.2=3, 0.988,  51.666,  -0.950, fx_navgre_max 
light.3=3,  -3.430, 51.666,  -0.950, fx_navgre_max
light.4=2, -20.0, 0.0, -4.0, fx_beanconh
light.5=1, -40.0, 0.0, 27.0, fx_beanconh
light.10=2, -47.235,    0.000, 0.834, fx_navred_max  
light.11=2, -47.235,    0.000, 0.530, fx_navwhi_max  
light.6=3, 16.80,   2.70, 1.5, fx_vclight 
light.7=3, 16.80, -2.70, 1.5, fx_vclight 
light.8=3, 17.85,   2.70, 1.0, fx_vclight 
light.9=3, 17.85, -2.70, 1.0, fx_vclight 

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 27
max_generator_alternator_amps = 60

[forcefeedback]
gear_bump_nose_magnitude=3000		; 0 - 10000
gear_bump_nose_direction=18000		; 0 - 35999 degrees
gear_bump_nose_duration=250000		; in microseconds
gear_bump_left_magnitude=2700		; 0 - 10000
gear_bump_left_direction=35500		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=2700		; 0 - 10000
gear_bump_right_direction=00500		; 0 - 35999 degrees
gear_bump_right_duration=250000		; in microseconds
ground_bumps_magnitude1=1300		; 0 - 10000
ground_bumps_angle1=08900		; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200		; 0 - 10000
ground_bumps_angle2=09100		; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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=2500000			; in microseconds

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=  705.500000,  17.000000, 0.000000, 0.000000, 4xCrew a 80 kg
station_load.1=1102.500000,  10.000000, 0.000000, 0.000000, load max:500kg
station_load.2=2116.400000,    5.000000, 0.000000, 0.000000, 12xPax a 80 kg
station_load.3=2470.000000, -11.000000, 0.000000, 0.000000, 14xPax a 80 kg
station_load.4=1433.000000, -26.500000, 0.000000, 0.000000, load max:650kg

// Beladung fьr 1800km Reichweite
//station_load.0  = "175.0,   13.4,  -2.0,   0.0, Pilot"              //Weight, Lat, Lon, Vert Position
//station_load.1  = "175.0,   13.4,   2.0,   0.0, Kopilot"           
//station_load.2  = "340.0,   9.3,   0.0,   0.0, Flugbegleiter"
//station_load.3  = "680.0,   5.8,   0.0,   0.0, Passagierreihe 1"    
//station_load.4  = "680.0,   1.7,   0.0,   0.0, Passagierreihe 2"    
//station_load.5  = "680.0,  -2.7,   0.0,   0.0, Passagierreihe 3"    
//station_load.6  = "680.0,  -5.9,   0.0,   0.0, Passagierreihe 4"    
//station_load.7  = "680.0,  -8.2,   0.0,   0.0, Passagierreihe 5"    
//station_load.8  = "340.0,  -10.4,   0.0,   0.0, Passagierreihe 6"   
//station_load.9  = "340.0,  -13.4,   0.0,   0.0, Passagierreihe 7"    
//station_load.10 = "749.0,  10.8,   0.0,   0.0, Gepдck vorne"    
//station_load.11 = "258.0,  -22.3,   0.0,   0.0, Fracht hinten"   
//station_load.12 = "275.0,  0.0,   0.0,   0.0, Dienstlast" 
//station_load.13 = "331.0,  1.4,   0.0,   0.0, Schmierstoff"      
// Dry mass 33269 lb

empty_weight=27505.000
empty_weight_pitch_MOI=959699.030
empty_weight_roll_MOI=91179.100
empty_weight_yaw_MOI=291797.970
empty_weight_coupled_MOI=0.000
max_gross_weight=38631.000  // 17000 kg zivil  Version\ 40785.518504 lbs; 18500 kg miltary Version
CG_forward_limit=0.000
CG_aft_limit=0.000
// wet mass 38849 lb , 1371 lb overweight bei vollen Tanks. 228.5 Gal weniger befьllen.

[fuel]
// 930 USgal = 5580 lb
LeftMain=    -1.000, -15.000, 0.000, 465.000, 0.000
RightMain= -1.000,   15.000, 0.000, 465.000, 0.000
fuel_type=1.000
number_of_tank_selectors=1
electric_pump=1

[airplane_geometry]
wing_area=1076.000
wing_span=104.000
wing_root_chord=26.917
wing_dihedral=3.300
wing_incidence=2.000
wing_twist=0.000
oswald_efficiency_factor=0.950
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=1.000
wing_pos_apex_vert=-2.000
htail_area=194.000
htail_span=30.583
htail_pos_lon=-39.000
htail_pos_vert=1.000
htail_incidence=0.500
htail_sweep=0.000
vtail_area=135.600
vtail_span=13.000
vtail_sweep=33.000
vtail_pos_lon=-39.000
vtail_pos_vert=9.000
elevator_area=74.380
aileron_area=77.50
rudder_area=62.800
elevator_up_limit=30.000
elevator_down_limit=17.000
aileron_up_limit=25.000
aileron_down_limit=15.000
rudder_limit=25.000
elevator_trim_limit=8.000
spoiler_limit=59.989
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000


//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]
point.0=1.000, 13.200, 0.000, -11.780, 350.803, 0.000, 2.018, 40.000, 0.400, 1.550, 0.975, 10.000, 10.000, 0.000, 0.000, 0.000
point.1=1.000, -3.900, -14.460, -12.280, 600.803, 1.000, 3.018, 0.000, 1.000, 1.300, 0.823, 10.300, 10.300, 2.000, 0.000, 0.000
point.2=1.000, -3.900, 14.460, -12.280, 600.803, 2.000, 3.018, 0.000, 1.000, 1.300, 0.823, 10.310, 10.310, 3.000, 0.000, 0.000
point.3=2.000, -6.583, -55.917, 4.083, 5574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4=2.000, -6.583, 55.917, 4.083, 5574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5=2.000, -63.917, 0.000, 0.000, 5574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6=2.000, 46.917, 0.000, 0.000, 5574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=0.300
static_cg_height=11.300
gear_system_type=1 



[Flaps.0]
type=1
span-outboard=0.595
extending-time=30.000
system_type=1 
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=0.600
drag_scalar=0.500
pitch_scalar=0.200
flaps-position.0=0.000, 0.000
flaps-position.1=37.800, 0.000
flaps-position.2=100.000, 0.000

[Flaps.1]
type=1
span-outboard=0.595
extending-time=30.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=0.00
drag_scalar=0.00
pitch_scalar=0.00
flaps-position.0=0.000, 0.000
flaps-position.1=0.000, 0.000
flaps-position.2=100.000, 0.000

[flight_tuning]
cruise_lift_scalar=1.400
parasite_drag_scalar=1.300
induced_drag_scalar=2.500
elevator_effectiveness=1.500
aileron_effectiveness=1.300
rudder_effectiveness=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=0.20
aileron_trim_effectiveness=0.50
rudder_trim_effectiveness=1.000
p_factor_on_yaw          = 0.5
torque_on_roll           = 1.0
gyro_precession_on_yaw   = 1.0
gyro_precession_on_pitch = 1.0

[GeneralEngineData]
engine_type=0
Engine.0=3.55, -12.30, -0.10
Engine.1=3.55, 12.30, -0.10
fuel_flow_scalar=0.95      
min_throttle_limit=0.000000
master_ignition_switch=1        //Master Ignition Switch

[piston_engine]
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=2.000  
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.0
cylinder_displacement= 179.5  
compression_ratio= 6.9  
number_of_cylinders= 18
max_rated_rpm= 2600.000
max_rated_hp= 1894.000  
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.250
turbocharged= 1
max_design_mp= 49.0 // 1.7 ata
min_design_mp= 5.00    
critical_altitude= 24000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 1
auto_ignition= 1
power_scalar=1.000  

[propeller]
// Typ AB-50
propeller_type= 0
propeller_diameter= 12.46  
propeller_blades= 4
propeller_moi= 67.27 
beta_max= 46.00  
beta_min= 22.00  
min_gov_rpm= 1100.000  
prop_tc= 0.002     
gear_reduction_ratio= 1.740  
fixed_pitch_beta= 20.000
low_speed_theory_limit= 80.000  
prop_sync_available= 0
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 400.000
beta_feather= 94.000
power_absorbed_cf= 0.80
defeathering_accumulators_available= 0
prop_reverse_available= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
thrust_scalar=1.000
feathering_switches=1                         //Switches which invoke feathering

[Reference Speeds]
flaps_up_stall_speed=93.000
full_flaps_stall_speed=83.000
cruise_speed=210    // KTAS fьr AI, 180 KIAS auf 10000ft
max_indicated_speed=250.00 // KIAS oder 463 km/h
max_mach=0.56

[keyboard_response]
elevator=150.000, 250.000
aileron=150.000, 250.000
rudder=150.000, 250.000

[Views]
eyepoint=19.680, -1.20, 1.50


[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=200.000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=95.000 
pitch_takeoff_ga=8.000
use_no_default_bank=0
use_no_default_pitch=0
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2000.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=1920000.000000
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

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 1
Adf.1=1
Transponder.1=1
Marker.1=1

[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
startup=fx_engstrt_vega      

[direction_indicators]
direction_indicator.0=3,0

[brakes]
toe_brakes_scale=0.35 
parking_brake=1
differential_braking_scale =0.5 //Delta on the amount of brake when the rudder pedals deflected

[gear_warning_system]
gear_warning_available=1 
pct_throttle_limit=0.05
flap_limit_power=17.0
flap_limit_idle=0

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0