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

[fltsim.0]
title=Junkers Ju-W33L Lufhansa
sim=Junkers_JU_W34
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
prop_anim_ratio=1.03 
atc_id=
ui_manufacturer=Junkers
ui_type=Junkers W.33L-5
ui_variation="Lufthansa"
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="Born from the successful F-13, Junkers creates the bigger and faster W-33.  Featuring room for 6 passengers, ample room for cargo, a durable, all metal skinned airframe, and a reliable powerplant, the W-33 quickly gains world recognition and soon can be found flying daily in remote regions of the world that before, were almost unreachable.  Cruising at 130 knots, the W33 is powered by the reliable Junkers L-5 straight six."

[General]
atc_type=Junkers
atc_model=W
editable=1
performance=Length: 10.5 m\nWing span: 17.75 m\nWeight: 1200 kg \/ 2100 kg\nPower: Junkers L-5 rated310 hp @ 1700 rpm\nDesigner: Alexander Belov\n

[weight_and_balance]

// ACM V2.5
max_gross_weight = 5947
empty_weight = 3520
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 = 15.75
static_cg_height = 5.2
tailwheel_lock = 1
gear_system_type = 0
max_number_of_points = 7

point.0 = 1, -19.8, 0,      -0.72, 1200, 0, 0.74, 40, 0.24, 2.5, 0.695, 0, 0, 0, 0, 0
point.1 = 1, -0.7, -4.98,  -6.10, 1600, 1, 1.53, 0, 0.504, 2.5, 0.686, 0, 0, 2, 0, 0
point.2 = 1, -0.7,  4.98,  -6.10, 1600, 2, 1.53, 0, 0.504, 2.5, 0.682, 0, 0, 3, 0, 0
point.3 = 2, -1.6, -28.5, 0.7, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.6, 28.5, 0.7, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -22, 0, 1.1, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 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