[fltsim.0]
title=Aero C-3a
sim=Aero_C3A
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=LB-05
ui_manufacturer=Aero
ui_type=C-3A
ui_variation=Czech Air Force
description= Multipurpose transport airplane Siebel Si 204D, first flight 1941,production continued in Czechoslovakia after 1945, up to the year 1950 was made 179 planes,they were used more than 10 years for civil and military tranport. LB-05 was made in 1946, it is the version \nC 3A, it was in military service, since 1957 in civil as OK-AIU till 1960.Since 2004 Aircraft Museum Kbely in Prague.\nAuthor: Jan Moravec, April 2005\nmoravec8@post.cz\n
[fltsim.1]
title=Aero/Siebel 204D
sim=Aero_C3A
model=
panel=
sound=
texture=ussr
kb_checklists=
kb_reference=
atc_id=06
ui_manufacturer=Aero
ui_type=C-3A
ui_variation=USSR
description= Multipurpose transport airplane Siebel Si 204D, first flight 1941,production continued in Czechoslovakia after 1945, up to the year 1950 was made 179 planes,they were used more than 10 years for civil and military tranport. LB-05 was made in 1946, it is the version \nC 3A, it was in military service, since 1957 in civil as OK-AIU till 1960.Since 2004 Aircraft Museum Kbely in Prague.\nAuthor: Jan Moravec, April 2005\nmoravec8@post.cz\n
[General]
atc_type=Aero/Siebel
atc_model=C 3A
editable=1
performance=DIMENSIONS:\nWing span: 21.28 m.\nLength: 12.01 m\nHeight: 3.93 m.\n\nWEIGHTS:\nEmpty equipped: 4150 kg\nMax. takeoff: 5400 kg\n\nPERFORMANCE:\nMax. speed: 380 km/h\nMax. cruising speed: 325 km/h\nApproach speed: 170 km/h\nStall speed (flaps and gear down): 120 km/h\nService ceiling: 7500 m\nRange: 1500 km with maximum fuel\n
[WEIGHT_AND_BALANCE]
max_gross_weight = 11906.000
empty_weight = 8665.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 1.800, 0.000, -2.000
max_number_of_stations =50
station_load.0 = 190, 3.94, -1.00, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, 3.94, 1.00, 0.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 170, 1.00, 0.00, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 170, 1.00, 0.00, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 170, -2.00, 0.00, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 170, -2.00, 0.00, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = 170, -4.00, 0.00, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = 170, -6.00, 0.00, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = 170, -6.00, 0.00, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = 120, -12.00, 0.00, 0.0 //Rear Cargo Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = 32, -23.00, 0.00, 0.0 //Ballast
;Moments of Inertia
empty_weight_pitch_MOI = 11500.000
empty_weight_roll_MOI = 10500.000
empty_weight_yaw_MOI = 22000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.500
parasite_drag_scalar =1.300
induced_drag_scalar =1.300
elevator_effectiveness =1.000
aileron_effectiveness =0.900
rudder_effectiveness =1.000
pitch_stability =1.400
roll_stability =1.100
yaw_stability =1.000
elevator_trim_effectiveness =0.750
aileron_trim_effectiveness =0.500
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 = 5.60, -7.600, -1.800
Engine.1 = 5.60, 7.600, -1.800
fuel_flow_scalar = 1.000
min_throttle_limit = 0.05 //Minimum percent throttle. Generally negative for turbine reverser
master_ignition_switch = 1 //Master Ignition Switch
[piston_engine]
power_scalar =0.954
cylinder_displacement= 108.110
compression_ratio= 6.300
number_of_cylinders= 12
max_rated_rpm= 2250.000
max_rated_hp= 590.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 1.300
turbocharged= 1
max_design_mp= 47.000
//min_design_mp= 9.000
min_design_mp= 1.000
critical_altitude= 8000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
//idle_rpm_friction_scalar=0.600
idle_rpm_friction_scalar=1.000
[propeller]
thrust_scalar =1.000
propeller_type= 0
propeller_diameter= 9.260
propeller_blades= 2
propeller_moi= 24.000
beta_max= 86.000
beta_min= 13.000
min_gov_rpm= 600.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 0
prop_reverse_available= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[contact_points]
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
//GEAR -1- -2- -3- -4- -5- -6- -7- -8- -9- -10- -11- -12--13--14- -15-
point.0 = 1, -21.137, 0.000, -2.650, 1600, 0, 0.62, 75, 0.52, 2.5, 1.0, 3.0, 3.0, 0, 0, 180
point.1 = 1, 3.000, -6.437, -5.900, 1600, 1, 1.34, 0, 0.60, 2.5, 1.0, 7.1, 7.3, 2, 166, 200
point.2 = 1, 3.000, 6.437, -5.900, 1600, 2, 1.34, 0, 0.60, 2.5, 1.0, 4.3, 4.1, 3, 166, 200
//SCRAPES
point.3= 2, -0.69, -23.79, 0.59, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4= 2, -0.69, 23.79, 0.59, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5= 2, -20.60, -7.58, 0.66, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6= 2, -20.60, 7.58, 0.66, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.7= 2, 11.02, 0.00, -0.23, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
static_pitch = 12.283
static_cg_height = 5.062
gear_system_type=0
tailwheel_lock = 1
[Views]
eyepoint = 5.9, -1.211, 3.9 //Longitudinal, Lateral, Vertical (feet)
[gear_warning_system]
gear_warning_available = 0 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.70 //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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, 5.00, 0.00, 3.25, fx_vclight,
light.1 = 4, 7.00, 1.50, 3.55, fx_vclight,
light.2 = 4, 7.00, -1.50, 3.55, fx_vclight,
light.3 = 4, 9.00, 0.00, 4.00, fx_vclight,
light.4 = 3, -1.00, -34.786, 2.95, fx_navredm ,
light.5 = 3, -1.00, 34.786, 2.95, fx_navgrem ,
[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, 0
Adf.1 = 1
Adf.2 = 1
Transponder.1 = 1
Marker.1 = 1
[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=1,0
direction_indicator.1=2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
attitude_indicator.1 = 2
[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_jenny
touchdown=fx_tchdwn_s, 1
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
//flap_motor = 0, 5 , 17.0
//gear_motor = 0, 5 , 17.0
//autopilot = 0, 5 , 17.0
//avionics_bus = 0, 5 , 17.0
//avionics = 1, 5 , 17.0
//pitot_heat = 0, 2 , 17.0
//additional_system = 0, 2 , 17.0
//marker_beacon = 1, 2 , 17.0
//gear_warning = 0, 2 , 17.0
//fuel_pump = 0, 5 , 17.0
//starter1 = 0, 20, 17.0
//starter2 = 0, 20, 17.0
//starter3 = 0, 20, 17.0
//starter4 = 0, 20, 17.0
//light_nav = 0, 5 , 17.0
//light_beacon = 0, 5 , 17.0
//light_landing = 0, 5 , 17.0
//light_taxi = 0, 5 , 17.0
//light_strobe = 0, 5 , 17.0
//light_panel = 0, 5 , 17.0
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 100
[fuel]
LeftMain = 0.0, -4.00, 0.0, 81.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 0.0, 4.00, 0.0, 81.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = 0.0, -10.00, 0.0, 64.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = 0.0, 10.00, 0.0, 64.0, 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
[airplane_geometry]
wing_area = 460.700
wing_span = 69.670
wing_root_chord = 11.083
wing_dihedral = 6.000
wing_incidence = 3.920
wing_twist = -3.530
oswald_efficiency_factor= 0.650
wing_winglets_flag = 0
wing_sweep = 13.220
wing_pos_apex_lon = 6.370
wing_pos_apex_vert = 0.000
htail_area = 87.330
htail_span = 14.970
htail_pos_lon = -16.730
htail_pos_vert = 2.460
htail_incidence = 0.000
htail_sweep = 13.810
vtail_area = 43.600
vtail_span = 5.420
vtail_sweep = 14.000
vtail_pos_lon = -16.560
vtail_pos_vert = 2.460
elevator_area = 34.930
aileron_area = 24.700
rudder_area = 21.800
elevator_up_limit = 30.000
elevator_down_limit = 20.000
aileron_up_limit = 30.000
aileron_down_limit = 15.000
rudder_limit = 18.000
elevator_trim_limit = 15.000
spoiler_limit = 0.000
spoilerons_available = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 67.500
full_flaps_stall_speed = 61.500
cruise_speed = 160.000
max_indicated_speed = 210 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
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
[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
[stall_warning]
type=2
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 7.000
system_type= 0
damaging-speed= 180.000
blowout-speed= 225.000
lift_scalar= 0.500
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 18.000, 0.000
flaps-position.2= 38.000, 0.000
[TailHook]
tailhook_length=3.0 ;(feet)
tailhook_position=0.0, 0.0, 3.5 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0
