[fltsim.0]
title=Junkers Ju-52 HAL
sim=Ju52_v60_Float
model=aqui
panel=
sound=
texture=
KB_checklists=Ju52_v60_check
kb_reference=Ju52_v60_ref
atc_id=N6362C
atc_id_color=0xffffffff
atc_airline=HAL
atc_flight_number=1155
ui_manufacturer=Junkers
ui_type="Ju-52/3m Wasser"
ui_variation=Heather Aviation Ltd.
visual_damage=1
description="The Junkers Ju52/3m has modern radio equipment, and is powered by 3 Ч BMW 132A-3 radials, rated at 660 hp each. The internal fuel capacity of 2.440 liters make a range radius of 1000 km possible at cruising speed at 4500 m." Repaint by Heather Sherman.




[General]
atc_type=Junkers
atc_model=JU52
editable=1
performance="Power:\t         3 x 660 hp BMW 132A \nWingspan:         29,25 m  ( 96 ft )\nLength:\t         18,90 m  ( 62 ft )\nHeight:\t         6,10 m\nWing Area:         110,50 m^2\nWeight Empty:    6'500 kg\nMTOW:\t          10,50 tonnes\nFuel capacity:    2'475 l\nFuel consumption: 450 l\/h\nTake off sp.:    ap. 120 km\/h \nCruise sp.:       ap. 190 km\/h\nTop speed:            260 km\/h\nRange:\t       ap. 1'000 km\s  ap. 5 h\nTake off run:    ap. 500 m\nLanding run:    ap. 350 m\nCeiling:\t       5'500 m (ap. 18'000 ft)\nInitial climb:     208 m (680 ft) p. min.\nFlap limit sp.: 10 deg....170 km\/h\n                         25 deg....160 km\/h\n                         40 deg....150 km\/\nAircrew            4\nPassengers    14\n\nVersion 6.0 FS2004\nDesigner: Pierino Primavesi"

[WEIGHT_AND_BALANCE]
max_gross_weight = 23100
empty_weight = 14617                            

reference_datum_position=0, 0, 0
empty_weight_CG_position=0, 0, 0  

max_number_of_stations=50

station_load.0  =  "170,   7.4,  -1.80, 0.0, Pilot"         
station_load.1  =  "170,   7.4,   1.80, 0.0, Copilot"        
station_load.2  =  "580,   6.0,    0.0, 0.0, Passengers 1. seats"        
station_load.3  =  "580,   3.6,    0.0, 0.0, Passengers 2. seats"         
station_load.4  =  "580,   0.6,    0.0, 0.0, Passengers 3. seats"         
station_load.5  =  "580,  -2.4,    0.0, 0.0, Passengers 4. seats"
station_load.6  =  "580,  -5.4,    0.0, 0.0, Passengers 5. seats"         
station_load.7  =  "580,  -8.4,    0.0, 0.0, Passengers 6. seats"     
station_load.8  =  "700, -12.3,    0.0, 0.0, Passengers 7. seats"         
;station_load.9  =  "990, -18.2,    0.0, 0.0, Freight" 

;Moments of Inertia
empty_weight_pitch_MOI   =  88758 
empty_weight_roll_MOI    =  70596 
empty_weight_yaw_MOI     =  158244 
empty_weight_coupled_MOI = 0

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 1.0
aileron_effectiveness  = 0.7 
rudder_effectiveness   = 0.3 
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0
p_factor_on_yaw          = 0.5
torque_on_roll           = 1.0
gyro_precession_on_yaw   = 1.0
gyro_precession_on_pitch = 1.0

[flaps.0]       //Trailing Edge Flaps
type = 1
span-outboard = 0.8
extending-time = 5
flaps-position.0 = -2.5
flaps-position.1 = 10
flaps-position.2 = 25
flaps-position.3 = 40
damaging-speed = 500
blowout-speed = 500
lift_scalar = 1.0                                       
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 3                                       

[GeneralEngineData]
engine_type=0
Engine.0=8.333333,-13.333333,1.250000
Engine.1=12.500000,0.000000,4.166667
Engine.2=8.333333,13.333333,1.250000
fuel_flow_scalar=1.0000
min_throttle_limit=0.000000
master_ignition_switch = 1 

[piston_engine]
power_scalar=1.0
cylinder_displacement=194.700000
compression_ratio=5.8
number_of_cylinders=9
max_rated_rpm=2200
max_rated_hp=660.000000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.15 
turbocharged=1
max_design_mp=23  
min_design_mp=5  
critical_altitude=5000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.0
idle_rpm_mechanical_efficiency_scalar=0.5 
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=0.5 

[propeller]
thrust_scalar = 1
propeller_type = 1 
propeller_diameter = 10.4
propeller_blades = 2
propeller_moi = 40.7
beta_max = 0 
beta_min = 0 
min_gov_rpm = 1200
prop_tc = 0.1
gear_reduction_ratio = 2.3  
fixed_pitch_beta = 19.5
low_speed_theory_limit = 50
prop_sync_available = 0
prop_deice_available = 0
prop_feathering_available = 0
prop_auto_feathering_available = 0
min_rpm_for_feather = 0
beta_feather = 0
power_absorbed_cf = 0
defeathering_accumulators_available = 0
prop_reverse_available = 0
minimum_on_ground_beta = 0
minimum_reverse_beta = 0
feathering_switches = 0

[contact_points]
//front hull right
point.0=4,15,-9.333,-8.533,1574.80,0,0.00,0,0.85,2.50,0.65,0,0,0,0,0
//front hull left
point.1=4,15,9.333,-8.533,1574.80,0,0.00,0,0.85,2.50,0.65,0,0,1,0,0

//left wing float 
//point.2=4,-3,8.833,-7.833,1574.80,0.00,0.0,0,0.95,2.50,0.65,0,0,2,0,0
//right wing float 
//point.3=4,-3,-8.833,-7.833,1574.80,0.00,0.0,0,0.95,2.50,0.65,0,0,3,0,0

//left wing rudder
point.2=4,-5,8.833,-7.833,1574.80,0.00,0.0,40,0.95,2.50,0.65,0,0,4,0,0
//right wing rudder 
point.3=4,-5,-8.833,-7.833,1574.80,0.00,0.0,40,0.95,2.50,0.65,0,0,3,0,0

point.4=2,-0.083333,-48.333333,4.583333,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.5=2,-0.083333,48.333333,4.583333,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.6=2,-38.333333,0.000000,2.500000,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.7=2,18.333333,0.000000,1.666667,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
point.8=2.000000,0,0.000000,-0.98,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
point.9=2.000000,0,0.000000,8.72,1574.803200,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000

static_pitch=2.346 //degrees (pitch when loaded on ground) 
static_cg_height=8.800 //(feet) altitude of CG when at rest (altitude when loaded on ground)
tailwheel_lock = 0

[gear_warning_system]
gear_warning_available = 0 
pct_throttle_limit =  0
flap_limit_idle    =  0
flap_limit_power   = 0

[brakes]
parking_brake=1
toe_brakes_scale=1
differential_braking_scale = 1.0 

[hydraulic_system]
normal_pressure=693.0556
electric_pumps=0
engine_map=1,1,1,0

[Views]
//eyepoint= 7.95, 1.66, 7.3	  // Copilot	
eyepoint= 7.95, -1.66, 7.3    // Pilot

[LIGHTS]
light.0=5, 5.39, -7.175, -0.68, fx_landing ,
light.1=5, 5.39,  7.175, -0.68, fx_landing ,
light.2=3, -2.56, -49.04, 3.94, fx_navredm ,
light.3=3, -2.56, 49.04, 3.94, fx_navgrem ,
light.4=1, -2.63, -49.04, 3.94, fx_strobe ,
light.5=1, -2.63, 49.04, 3.94, fx_strobe ,
light.6=1, -25.61, 0.00, 1.37, fx_beaconb ,
light.7=1, -38.71, 0.00, 15.07, fx_beaconh ,
light.8=4,  9.45, 0.00, 6.46, fx_vclight_ju ,
light.9=5, -0.246, -23.326, 0.9186, fx_taxi ,
light.10=5, -0.246, 23.326, 0.9186, fx_taxi ,
light.11=4,  1.6, 0, 3.5, fx_vclighth ,
light.12=4,  -1.5, 0, 5.00, fx_vclighth ,
light.13=4,  -4.5, 0, 5.00, fx_vclighth ,
light.14=4,  -7.5, 0, 5.00, fx_vclighth ,

[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 = 0
Marker.1      = 1

[keyboard_response]
elevator = 100, 170
aileron  = 180, 600
rudder   = 180, 600

[direction_indicators]
direction_indicator.0=1,0
direction_indicator.1=2,0

[attitude_indicators]
attitude_indicator.0 = 1 
attitude_indicator.1 = 2 

[turn_indicators]
turn_indicator.0=2,0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 24.5
max_generator_alternator_amps = 100

[fuel]
LeftMain=0.000000,-9.000000,0.000000,330.000000,0.000000
RightMain=0.000000,9.000000,0.000000,330.000000,0.000000
fuel_type=1
number_of_tank_selectors=3
electric_pump=0

[airplane_geometry]
wing_area = 1184
wing_span = 96
wing_root_chord = 12
wing_dihedral = 4
wing_incidence = 0.34
wing_twist = -1.0
oswald_efficiency_factor = 0.65
wing_winglets_flag = 0
wing_sweep  = 8.0
wing_pos_apex_lon = -2.5
wing_pos_apex_vert = 3.8

htail_area = 169 
tail_span = 32.8
htail_pos_lon = -35.9
htail_pos_vert = 6.5
htail_incidence = 3.33
htail_sweep = 0

vtail_area = 69.9 
vtail_span = 8.5
vtail_sweep = 35.2
vtail_pos_lon  = -39.4
vtail_pos_vert = 8.5

elevator_area = 97.8
aileron_area = 75.25 
rudder_area = 43
elevator_up_limit = 30
elevator_down_limit = 30
aileron_up_limit = 20.5
aileron_down_limit = 20.5
rudder_limit = 30
elevator_trim_limit = 3.2
spoiler_limit = 0
spoilerons_available = 0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
htail_span=0.000000

[Reference Speeds]
flaps_up_stall_speed=55                  
full_flaps_stall_speed=45                  
cruise_speed=100
max_indicated_speed=160.000000

[autopilot]
autopilot_available= 1
flight_director_available= 0
pitch_takeoff_ga=0.0
default_vertical_speed=0
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
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000

[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=1

[exits]
number_of_exits = 1
exit_rate.0 = 0.4  
                          
[SMOKESYSTEM]
smoke.0=3.576,6.266,-12.598, fx_smokeju
smoke.1=4.50,12.86,-3.28, fx_smokeju
smoke.2=3.576,6.266,12.598, fx_smokeju
smoke.3=4.50,12.86,3.28, fx_smokeju
             
[ground_reaction]
main_gear_static_compression=0.3		// (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=0.3            // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=0.7		// Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=0.7		// Center gear strut damping, 0 = undamped osciallations, 1 = critically damped

[EFFECTS]
wake=fx_wakeju
water=fx_sprayju
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1