//////////////JUNKERS JU-W.33 BY LIONHEART CREATIONS LTD\\\\\\\\\\\\\\\\\\\
//////////////Copyright William Ortis, Lionheart Creations Ltd.\\\\\\\\\\\\\\\\\\\\

[fltsim.0]
title=Junkers Ju-W33L 177FP
sim=Junkers_JU_W34
model=Cargo
panel=
sound=
texture=177
kb_checklists=
kb_reference=
prop_anim_ratio=1.03 
atc_id=
ui_manufacturer=Junkers
ui_type=Junkers W.33L-5
ui_variation=СССР-177 Поплавковый
ui_typerole="Single Engine Prop"
ui_thumbnailfile=thumbnail2.jpg
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_parking_types=RAMP
description=

[General]
atc_type=Junkers
atc_model=W
editable=1
performance=

[weight_and_balance]

// ACM V2.5
max_gross_weight = 5730
empty_weight = 3200
reference_datum_position = 1, 0, 0
empty_weight_CG_position = -1.64, 0, 0
empty_weight_pitch_MOI = 34885.4
empty_weight_roll_MOI = 16264.7
empty_weight_yaw_MOI = 28402.6
empty_weight_coupled_MOI = 0
max_number_of_stations = 12

station_load.0 = "170.0,   -1.4,  -1.0,   0.0, Pilot"
station_load.1 = "170.0,   -1.4,   1.0,   0.0, Co-Pilot"
station_load.2 = "280.0,  -3,   0.0,   0.0, Passenger Row 1"
station_load.3 = "280.0,  -5,   0.0,   0.0, Passenger Row 2"
station_load.4 = "258.0,  -7,   0.0,   0.0, Passenger Row 3"
station_load.5 = "120.0,  -8,   0.0,   0.0, Rear Cargo"


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -1.05, -28.5, 0.75, fx_navred
light.1 = 3, -1.05, 28.5, 0.75, fx_navgre
light.2 = 3, -20.55, 0, 5.7, fx_navwhi
light.3 = 2, -0.3, 0, 2.05, fx_vclight
light.4 = 2, -4, 0, 2.7, fx_vclight
light.5 = 2, -8, 0, 2.3, fx_vclight


[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.67
min_throttle_limit = 0.0
engine.0 = 4.21, 0, 1, 

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup = fx_engstrt_vega
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 1
number_of_tank_selectors = 1
electric_pump = 0

LeftMain = -1, -5.9, 0, 70, 0
RightMain = -1, 5.9, 0, 70, 0


[contact_points]
static_pitch = 0.0
static_cg_height = 8.9
tailwheel_lock = 1
gear_system_type = 0
max_number_of_points = 12

point.0 = 1, 8.15,     -5.75,  -8.8, 1600, 0, 1.4, 30, 0.3, 2.5, 0.8, 4, 4, 0, 175, 175
point.1 = 1, 8.15,      5.75,  -8.8, 1600, 0, 1.4, 30, 0.3, 2.5, 0.8, 4, 4, 1, 175, 175
point.2 = 1, -4.4, -7.25, -8.9, 1600, 1, 1.5, 0, 0.4, 2.5, 0.8, 4, 4, 2, 175, 175
point.3 = 1, -4.4,       7.25,  -8.9, 1600, 2, 1.5, 0, 0.4, 2.5, 0.8, 4, 4, 3, 175, 175
point.4 = 4,  9.0,      -5.75,  -7.2, 1600, 0, 0, 0, 0.85, 2.5, 0.65, 0, 0, 0, 0, 0
point.5 = 4,  9.0,       5.75,  -7.2, 1600, 0, 0, 0, 0.85, 2.5, 0.65, 0, 0, 1, 0, 0
point.6 = 4, -11.35, -5.75,  -7.0, 1600, 0, 0, 0, 0.95, 2.5, 0.65, 0, 0, 2, 0, 0
point.7 = 4, -11.35,  5.75,  -7.0, 1600, 0, 0, 0, 0.95, 2.5, 0.65, 0, 0, 3, 0, 0
point.8 = 2, -1.6, -28.5, 0.7, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.9 = 2, -1.6, 28.5, 0.7, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.10 = 2, -22, 0, 1.1, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 6, 0, -0.5, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0


[keyboard_response]
elevator = 200, 1000
aileron = 200, 1000
rudder = 200, 1000


[forcefeedback]
ground_bumps_magnitude1 = 2600
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 3500000

[airplane_geometry]
wing_area = 447.05
wing_span = 56
wing_root_chord = 8.5
wing_dihedral = 7.0
wing_incidence = -1.5
wing_twist = 0.0
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 4.1
wing_pos_apex_lon = 1.50
wing_pos_apex_vert = -0.7up
htail_area = 114.0
htail_span = 18.3
htail_pos_lon = -17.7
htail_pos_vert = 2.4
htail_incidence = -1.6
htail_sweep = 0.0
vtail_area = 61.0
vtail_span = 3.4
vtail_sweep = 34.0
vtail_pos_lon = -17.5
vtail_pos_vert = 2.5
elevator_area = 23.4
aileron_area = 50.8
rudder_area = 20.7
elevator_up_limit = 30.0
elevator_down_limit = 20.0
aileron_up_limit = 18.0
aileron_down_limit = 12.0
rudder_limit = 30.0
elevator_trim_limit = 12.0
spoiler_limit = 0.1
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 25
max_generator_alternator_amps = 60
engine_generator_map = 1
electric_always_available = 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=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 

[Flaps.0]
type= 0

[piston_engine]
power_scalar=1.0                              //Piston power scalar
cylinder_displacement=233                    //Cubic inches per cylinder
compression_ratio=5.5                          //Compression ratio
number_of_cylinders=6                          //Number of cylinders
max_rated_rpm=1500                             //Max rated RPM
max_rated_hp=310                              //Max rated HP
fuel_metering_type=1                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=1                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3                  //Starter torque factor
turbocharged=0                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=0                               //Max design manifold pressure, (inHg)
min_design_mp=0                               //Min design manifold pressure, (inHg)
critical_altitude=9000                         //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                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=0.8       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.3                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.0                   //Scalar on idle RPM friction

[propeller]
thrust_scalar=1.0                             //Propeller thrust scalar
propeller_type=1                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=10.4                        //Propeller Diameter, (feet)
propeller_blades=2                             //Number of propeller blades
propeller_moi=9                            //Propeller moment of inertia
beta_max=18                                     //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=18                                     //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=0                                  //Miminum governed RPM
prop_tc=0.1                                    //Prop time-constant
gear_reduction_ratio=1.0                       //Propeller gear reduction ratio
fixed_pitch_beta=20                         //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80                      //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=0                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=0                          //Minimum RPM for prop feathering
beta_feather=0                                 //Feathering pitch angle (degrees)
power_absorbed_cf=0                            //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                       //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0                         //Minimum pitch angle in reverse, (degrees)
        //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

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.9  //Brake scalar
differential_braking_scale = 1.0        //Delta on the amount of brake when the rudder pedals deflected

[folding_wings]
wing_fold_system_type =  4
fold_rates =  0.12, 0.11

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

[hydraulic_system]
normal_pressure = 0.0    //PSI

[Views]
eyepoint=-1.331, -1.112, 2.771 

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

[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 = 2

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=2,0

[Reference Speeds]
flaps_up_stall_speed=42.5                  //Knots True (KTAS)
full_flaps_stall_speed=42.5                  //Knots True (KTAS)
cruise_speed=138.0                 //Knots True (KTAS)
max_indicated_speed     = 212                   //Red line (KIAS)

[autopilot]
autopilot_available=1 
flight_director_available=0 
pitch_takeoff_ga=0.0 
default_vertical_speed=700.000000 
autothrottle_available=0 
direction_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

[stall_warning]
type=0
[exits]
number_of_exits = 4
exit_rate.0 = 0.2                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second
exit_rate.2 = 0.4                               ;Percent per second
exit_rate.3 = 0.4                               ;Percent per second
